- The instructions above tune the vehicle in [Altitude mode](../flight_modes_mc/altitude.md).
- You can instead takeoff in [Takeoff mode](../flight_modes_mc/takeoff.md) and tune in [Position mode](../flight_modes_mc/position.md) if the vehicle is is _known_ to be stable in these modes.
+ You can instead takeoff in [Takeoff mode](../flight_modes_mc/takeoff.md) and tune in [Position mode](../flight_modes_mc/position.md) if the vehicle is _known_ to be stable in these modes.
@@ -243,7 +243,7 @@ To map a switch:
2. Set [RC_MAP_AUX1](../advanced_config/parameter_reference.md#RC_MAP_AUX1) to match the RC channel for your switch (you can use any of `RC_MAP_AUX1` to `RC_MAP_AUX6`).
3. Set [FW_AT_MAN_AUX](../advanced_config/parameter_reference.md#FW_AT_MAN_AUX) to the selected channel (i.e. `1: Aux 1` if you mapped `RC_MAP_AUX1`).
-The auto tuner will be disabled when the switch is below `0.5` (on the manual control setpoint range of of `[-1, 1]`) and enabled when the switch channel is above `0.5`.
+The auto tuner will be disabled when the switch is below `0.5` (on the manual control setpoint range of `[-1, 1]`) and enabled when the switch channel is above `0.5`.
If using an RC AUX switch to enable autotuning, make sure to [select the tuning axes](#select-tuning-axis) before flight.
diff --git a/docs/ko/config/joystick.md b/docs/ko/config/joystick.md
index 3ac6d2699f..9c2dfb3327 100644
--- a/docs/ko/config/joystick.md
+++ b/docs/ko/config/joystick.md
@@ -23,8 +23,7 @@ Information about how to set up a joystick is covered in: [QGroundControl > Joys
요약
- Open _QGroundControl_
-- Set the parameter [COM_RC_IN_MODE=1](../advanced_config/parameter_reference.md#COM_RC_IN_MODE) - `Joystick`
- - See [Parameters](https://docs.qgroundcontrol.com/master/en/qgc-user-guide/setup_view/parameters.html) for information about setting parameters
- - Setting the parameter to `2` or `3` also enables Joystick under some circumstances.
+- [Enable a `COM_RC_IN_MODE` mode that allows Joystick](../config/manual_control.md#px4-configuration).
+ The default `RC or MAVLink keep first` should work if you plan to only have a Joystick connected.
- 조이스틱을 연결합니다.
- Configure the connected joystick in: **Vehicle Setup > Joystick**.
diff --git a/docs/ko/config/manual_control.md b/docs/ko/config/manual_control.md
new file mode 100644
index 0000000000..312436ab97
--- /dev/null
+++ b/docs/ko/config/manual_control.md
@@ -0,0 +1,58 @@
+# Manual Control
+
+Pilots can control a vehicle manually using either a [Radio Control (RC) System](../getting_started/rc_transmitter_receiver.md) or a [Joystick/Gamepad](../config/joystick.md) controller connected via QGroundControl.
+PX4 also supports using RC and/or multiple Joysticks, with fallback from one type to the other.
+
+ 
+
+## 개요
+
+_Joystick_ setups use QGroundControl to encode the control information from a "standard" computer gaming joystick into [MAVLink messages](https://mavlink.io/en/services/manual_control.html) that are sent to the vehicle over the (shared) telemetry radio channel.
+They are often used in integrated GCS/manual control systems because it is cheaper and easier to integrate a joystick than a separate radio system.
+
+Joysticks are suitable for most applications provided your telemetry channel has a high enough bandwidth/low latency.
+They are perfect for flying the PX4 simulator, because you can plug them directly into your ground control computer and start flying.
+
+_RC systems_ use a dedicated ground-based radio transmitter and vehicle-based receiver for sending control information.
+They offer lower latency than Joysticks, and are very highly recommended when first tuning/testing a new frame design, when flying racers/acrobatically, and in other cases where low latency is important.
+They can also be useful as a robust backup link for safety.
+Note RC systems usually require significantly more configuration and calibration, much of which may be brand or model-specific.
+
+:::info
+PX4 does not _require_ a manual control system for autonomous flight modes.
+:::
+
+## PX4 설정
+
+:::tip
+This section explains how to configure PX4 to use and prioritise various manual control sources (other configuration is covered in the guides for each type of manual control).
+:::
+
+If you only have one manual control system, either RC or Joystick, then by default no manual control selection is required.
+In this case PX4 locks to the first valid manual control source it detects and uses that source until the vehicle is rebooted.
+
+If you have multiple control sources, such as an RC system and/or one or more Joysticks, then you can use the [COM_RC_IN_MODE](../advanced_config/parameter_reference.md#COM_RC_IN_MODE) parameter to determine which source is active, specifying selection priorities and fallback behavior ([parameters can be set](../advanced_config/parameters.md#finding-a-parameter) using QGC):
+
+- `0`: RC only.
+- `1`: MAVLink only.
+- `2`: RC or MAVLink with fallback (switches if current source becomes invalid).
+- `3`: RC or MAVLink keep first (locks to the first valid source until reboot).
+- `4`: Disable manual control (ignores all sources).
+- `5`: RC priority, then MAVLink (lower instance before higher) — `RC > MAVLink 1 > MAVLink 2`
+- `6`: MAVLink priority (lower instance before higher), then RC — `MAVLink 1 > MAVLink 2 > RC`
+- `7`: RC priority, then MAVLink (higher instance before lower) — `RC > MAVLink 2 > MAVLink 1`
+- `8`: MAVLink priority (higher instance before lower), then RC — `MAVLink 2 > MAVLink 1 > RC`
+
+The [MAVLink instance](../peripherals/mavlink_peripherals.md#mavlink-instances) refers to an instance assigned to a serial port, such as [MAV_0_CONFIG](../advanced_config/parameter_reference.md#MAV_0_CONFIG).
+
+참고:
+
+- RC checks are run for any option that uses RC (so not for `MAVLink only` or `Disable manual control`).
+- When using priority sources, sources are evaluated as soon as they become valid and may trigger an immediate switch (if higher priority than the currently active source).
+- A [Manual Control Loss Failsafe](../config/safety.md#manual-control-loss-failsafe) is triggered when none of the manual control inputs allowed by the `COM_RC_IN_MODE` mode are available for a time that is greater than the RC Loss Timeout.
+ As long as there is a fallback input source available, the failsafe is not triggered.
+
+## See Also
+
+- [Radio Control (RC)](../getting_started/rc_transmitter_receiver.md)
+- [Joysticks](../config/joystick.md)
diff --git a/docs/ko/config/radio.md b/docs/ko/config/radio.md
index 1ca698c54a..23cbbb80d6 100644
--- a/docs/ko/config/radio.md
+++ b/docs/ko/config/radio.md
@@ -1,10 +1,12 @@
# Radio Control (RC) Setup
-The _Radio Setup_ screen is used to configure the mapping of your RC controller's main attitude control sticks (roll, pitch, yaw, throttle) to channels, and to calibrate the minimum, maximum, trim and reverse settings for all other transmitter controls/RC channels.
+The _Radio Setup_ screen is used to configure the mapping of your [RC controller's](../getting_started/rc_transmitter_receiver.md) main attitude control sticks (roll, pitch, yaw, throttle) to channels, and to calibrate the minimum, maximum, trim and reverse settings for all other transmitter controls/RC channels.
:::info
-A [Joystick](../config/joystick.md) can be used instead of RC for manual control.
-The [COM_RC_IN_MODE](../advanced_config/parameter_reference.md#COM_RC_IN_MODE) parameter [can be set](../advanced_config/parameters.md) to define what kind of manual controller(s) are enabled.
+A [Joystick](../config/joystick.md) can also be used for [Manual Control](../config/manual_control.md).
+
+By default PX4 will latch the first valid controller it discovers and use it until the vehicle reboots.
+If you have multiple controllers and you want to define their priority see [Manual Control > PX4 Configuration](../config/manual_control.md#px4-configuration).
:::
## 수신기 바인딩
diff --git a/docs/ko/config/safety.md b/docs/ko/config/safety.md
index afa785d204..e70f6454c2 100644
--- a/docs/ko/config/safety.md
+++ b/docs/ko/config/safety.md
@@ -111,19 +111,17 @@ There are several other "battery related" failsafe mechanisms that may be config
## Manual Control Loss Failsafe
-The manual control loss failsafe may be triggered if the connection to the [RC transmitter](../getting_started/rc_transmitter_receiver.md) or [joystick](../config/joystick.md) is lost, and there is no fallback.
-If using an [RC transmitter](../getting_started/rc_transmitter_receiver.md) this is triggered if the RC [transmitter link is lost](../getting_started/rc_transmitter_receiver.md#set-signal-loss-behaviour).
-If using [joysticks](../config/joystick.md) connected over a MAVLink data link, this is triggered if the joysticks are disconnected or the data link is lost.
-
-:::info
-PX4 and the receiver may also need to be configured in order to _detect RC loss_: [Radio Setup > RC Loss Detection](../config/radio.md#rc-loss-detection).
-:::
+A [Manual Control Loss Failsafe](../config/safety.md#manual-control-loss-failsafe) is triggered after a [manual control loss timeout](#COM_RC_LOSS_T) in which none of the configured [Manual Controllers](../config/manual_control.md) are available.
The QGCroundControl Safety UI allows you to set the [failsafe action](#failsafe-actions) and [manual control loss timeout](#COM_RC_LOSS_T).
Users that want to disable this failsafe in specific modes can do so using the parameter [COM_RCL_EXCEPT](#COM_RCL_EXCEPT).
+:::info
+PX4 and the receiver may also need to be configured in order to _detect RC loss_: [Radio Setup > RC Loss Detection](../config/radio.md#rc-loss-detection).
+:::
+
Additional (and underlying) parameter settings are shown below.
| 매개변수 | 설정 | 설명 |
@@ -181,17 +179,22 @@ Due to the inherent danger of this, this function is disabled using [CBRK_FLIGHT
| Preemptive geofence triggering | [GF_PREDICT](../advanced_config/parameter_reference.md#GF_PREDICT) | (Experimental) Trigger geofence if current motion of the vehicle is predicted to trigger the breach (rather than late triggering after the breach). |
| Circuit breaker for flight termination | [CBRK_FLIGHTTERM](../advanced_config/parameter_reference.md#CBRK_FLIGHTTERM) | 비행 종료 작업을 활성화/비활성화합니다 (기본적으로 비활성화 됨). |
-## Position (GNSS) Loss Failsafe
+## Position Estimation Failsafes
+
+This section describes failsafes related to the quality of the vehicle's position estimate.
+
+### Position Loss Failsafe
The _Position Loss Failsafe_ is triggered if the quality of the PX4 position estimate falls below acceptable levels (this might be caused by GPS loss) while in a mode that requires an acceptable position estimate.
-The sections below cover first the trigger and then the failsafe action taken by the controller.
### Position Loss Failsafe Trigger
-There are basically two mechanisms in PX4 to trigger position failsafes:
+The position loss failsafe triggers if the position estimate becomes _invalid_. There are two mechanisms in PX4 to invalidate the position estimate:
-- A timeout since the last sensor data was fused that provides direct speed or horizontal position measurements. Sensors that fall into that category are: GNSS, optical flow, airspeed, VIO, auxiliary global position.
-- The estimated horizontal position accuracy exceeds a certain threshold. This check is only done on hovering systems (rotary wing vehicles or VTOLs in hover phase).
+- A timeout since the last sensor data was fused that provides direct speed or horizontal position measurements.
+ - Sensors that fall into that category are: GNSS, optical flow, airspeed, VIO, auxiliary global position.
+- The estimated horizontal position inaccuracy exceeds the threshold [COM_POS_LOW_EPH](../advanced_config/parameter_reference.md#COM_POS_LOW_EPH)
+ - This check is only done on hovering systems (rotary-wing vehicles or VTOLs in hover phase). For fixed-wing vehicles, refer to the [Position Accuracy Low](#position-accuracy-low-failsafe) section.
The relevant parameters shown below.
@@ -207,14 +210,24 @@ Multicopters will switch to [Altitude mode](../flight_modes_mc/altitude.md) if a
Fixed-wing planes, and VTOLs not configured to land in hover ([NAV_FORCE_VT](../advanced_config/parameter_reference.md#NAV_FORCE_VT)), have a parameter ([FW_GPSF_LT](../advanced_config/parameter_reference.md#FW_GPSF_LT)) that defines how long they will loiter (circle with a constant roll angle ([FW_GPSF_R](../advanced_config/parameter_reference.md#FW_GPSF_R)) at the current altitude) after losing position before attempting to land.
If VTOLs have are configured to switch to hover for landing ([NAV_FORCE_VT](../advanced_config/parameter_reference.md#NAV_FORCE_VT)) then they will first transition and then descend.
-The relevant parameters for all vehicles shown below.
+The relevant parameters are:
-Parameters that only affect Fixed-wing vehicles:
+| 매개변수 | 설명 |
+| ----------------------------------------------------------------------------------------------------------------------------------------- | --------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- |
+| [FW_GPSF_LT](../advanced_config/parameter_reference.md#FW_GPSF_LT) | Fixed-wing only: Loiter time (waiting at current altitude for position estimation recovery before starting to descend). 비활성화 하려면 0으로 설정하십시오. |
+| [FW_GPSF_R](../advanced_config/parameter_reference.md#FW_GPSF_R) | 선회 비행시 고정 롤/뱅크 각도. |
+| [NAV_FORCE_VT](../advanced_config/parameter_reference.md#NAV_FORCE_VT) | If true, force VTOL takeoff and landing, even in `Descend` failsafe. |
-| 매개변수 | 설명 |
-| ----------------------------------------------------------------------------------------------------------------------------------- | -------------------------------------------------------------------------------------------------------------------------------------------------------------- |
-| [FW_GPSF_LT](../advanced_config/parameter_reference.md#FW_GPSF_LT) | Loiter time (waiting for GPS recovery before it goes into land or flight termination). 비활성화 하려면 0으로 설정하십시오. |
-| [FW_GPSF_R](../advanced_config/parameter_reference.md#FW_GPSF_R) | 선회 비행시 고정 롤/뱅크 각도. |
+### Position Accuracy Low Failsafe
+
+In Fixed-wing, the position estimate is never strictly invalidated as long as we have a horizontal aiding source, such as an airspeed sensor. In that case, a separate failsafe can be configured that triggers if the position estimate inacuraccy exceeds the threshold [COM_POS_LOW_EPH](../advanced_config/parameter_reference.md#COM_POS_LOW_EPH). The failsafe action is taken if the vehicle is in mission or hold mode, otherwise it is only a warning. The relevant parameters are:
+
+| 매개변수 | 설명 |
+| ----------------------------------------------------------------------------------------------------------------------------------------------------------------------- | -------------------------------------------------------------------------------------------------------------------------------------------------- |
+| [COM_POS_LOW_EPH](../advanced_config/parameter_reference.md#COM_POS_LOW_EPH) | Position inaccuracy threshold above which COM_POS_LOW_ACT is taken. |
+| [COM_POS_LOW_ACT](../advanced_config/parameter_reference.md#COM_POS_LOW_ACT) | Failsafe action taken when position inaccuracy is above configured threshold. |
+
+Note that if there is no horizontal aiding source anymore, the position estimate is invalidated after `EKF2_NOAID_TOUT`, and the standard position loss failsafe applies.
## 오프 보드 안전 장치
@@ -261,7 +274,7 @@ The parameters that control when the quad-chute will trigger are listed in the t
## High Wind Failsafe
-The high wind failsafe can trigger a warning and/or other mode change when the wind speed exceeds the warning and maximum wind-speed threshhold values.
+The high wind failsafe can trigger a warning and/or other mode change when the wind speed exceeds the warning and maximum wind-speed threshold values.
The relevant parameters are listed in the table below.
| 매개변수 | 설명 |
@@ -315,8 +328,8 @@ The failure detector can be configured to detect a motor failure while armed (an
| ----------------------------------------------------------------------------------------------------------------------------------------------------------------------- | --------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- |
| [FD_ACT_EN](../advanced_config/parameter_reference.md#FD_ACT_EN) | Enable/disable the motor failure trigger completely. |
| [FD_ACT_MOT_THR](../advanced_config/parameter_reference.md#FD_ACT_MOT_THR) | Minimum normalized [0,1] motor command below which motor under current is ignored. |
-| [FD_ACT_MOT_C2T](../advanced_config/parameter_reference.md#FD_ACT_MOT_C2T) | Scale between normalized [0,1] motor command and expected minimally reported currrent when the rotor is healthy. |
-| [FD_ACT_MOT_TOUT](../advanced_config/parameter_reference.md#FD_ACT_MOT_TOUT) | Time in miliseconds for which the under current detection condition needs to stay true. |
+| [FD_ACT_MOT_C2T](../advanced_config/parameter_reference.md#FD_ACT_MOT_C2T) | Scale between normalized [0,1] motor command and expected minimally reported current when the rotor is healthy. |
+| [FD_ACT_MOT_TOUT](../advanced_config/parameter_reference.md#FD_ACT_MOT_TOUT) | Time in milliseconds for which the under current detection condition needs to stay true. |
| [CA_FAILURE_MODE](../advanced_config/parameter_reference.md#CA_FAILURE_MODE) | Configure to not only warn about a motor failure but remove the first motor that detects a failure from the allocation effectiveness which turns off the motor and tries to operate the vehicle without it until disarming the next time. |
### 외부 자동 작동 시스템 (ATS)
diff --git a/docs/ko/config_mc/pid_tuning_guide_multicopter_basic.md b/docs/ko/config_mc/pid_tuning_guide_multicopter_basic.md
index c17c455ddd..b6569ea0c4 100644
--- a/docs/ko/config_mc/pid_tuning_guide_multicopter_basic.md
+++ b/docs/ko/config_mc/pid_tuning_guide_multicopter_basic.md
@@ -13,7 +13,7 @@ For example, different ESCs or motors change the optimal tuning gains.
## 소개
-PX4 uses **P**roportional, **I**ntegral, **D**erivative (PID) controllers (these are the most widespread control technique).
+PX4 uses **P**roportional, **I**integral, **D**erivative (PID) controllers (these are the most widespread control technique).
The _QGroundControl_ **PID Tuning** setup provides real-time plots of the vehicle setpoint and response curves.
The goal of tuning is to set the P/I/D values such that the _Response_ curve matches the _Setpoint_ curve as closely as possible (i.e. a fast response without overshoots).
diff --git a/docs/ko/config_rover/attitude_tuning.md b/docs/ko/config_rover/attitude_tuning.md
index b2efc4d5c7..cf176e587f 100644
--- a/docs/ko/config_rover/attitude_tuning.md
+++ b/docs/ko/config_rover/attitude_tuning.md
@@ -16,7 +16,7 @@ Configure the following [parameters](../advanced_config/parameters.md) in QGroun
Put the rover into stabilized mode and move the left stick of your controller up to drive forwards.
Disarm the rover and from the flight log plot the `measured_yaw` and the `adjusted_yaw_setpoint` from the [RoverAttitudeStatus](../msg_docs/RoverAttitudeStatus.md) message over each other.
Increase/Decrease the parameter until you are satisfied with the setpoint tracking.
- If you observe a steady state error in the yaw setpoint increase the the integrator of the rate controller: [RO_YAW_RATE_I](../advanced_config/parameter_reference.md#RO_YAW_RATE_I) .
+ If you observe a steady state error in the yaw setpoint increase the integrator of the rate controller: [RO_YAW_RATE_I](../advanced_config/parameter_reference.md#RO_YAW_RATE_I) .
:::
@@ -30,7 +30,7 @@ The attitude controller uses the following structure:
-The rate and attitude controllers are cascaded, therefor we only require one integrator in the structure to eliminate steady state errors.
+The rate and attitude controllers are cascaded, therefore we only require one integrator in the structure to eliminate steady state errors.
We placed the integrator in the rate controller since it can run without the attitude controller but not the other way around.
## Parameter Overview
diff --git a/docs/ko/config_rover/basic_setup.md b/docs/ko/config_rover/basic_setup.md
index 53b9e2ddb1..f9bcc3a665 100644
--- a/docs/ko/config_rover/basic_setup.md
+++ b/docs/ko/config_rover/basic_setup.md
@@ -138,7 +138,7 @@ In [Manual mode](../flight_modes_rover/manual.md#manual-mode) we can additionall
- Differential Rover: $r=$ [RD_YAW_STK_GAIN](#RD_YAW_STK_GAIN), which enables adjusting the slope of the input mapping. This leads to a normalized steering input $\hat{\delta} = \delta \cdot r \in$ [-[RD_YAW_STK_GAIN](#RD_YAW_STK_GAIN), [RD_YAW_STK_GAIN](#RD_YAW_STK_GAIN)].
- Mecanum Rover: $r=$ [RM_YAW_STK_GAIN](#RM_YAW_STK_GAIN), which enables adjusting the slope of the input mapping. This leads to a normalized steering input $\hat{\delta} = \delta \cdot r \in$ [-[RM_YAW_STK_GAIN](#RM_YAW_STK_GAIN), [RM_YAW_STK_GAIN](#RM_YAW_STK_GAIN)].
-This scaling is useful to limit the normalized steering setpoint, if it is too aggresive for your rover in manual mode.
+This scaling is useful to limit the normalized steering setpoint, if it is too aggressive for your rover in manual mode.
You can experiment with the relationships graphically using the [PX4 SuperExpo Rover calculator](https://www.desmos.com/calculator/gwm8lrlanx).
diff --git a/docs/ko/config_rover/index.md b/docs/ko/config_rover/index.md
index aff8b6389a..960fedc2f4 100644
--- a/docs/ko/config_rover/index.md
+++ b/docs/ko/config_rover/index.md
@@ -39,7 +39,7 @@ make px4_fmu-v6x_rover
Note that configuration targets are constructed with the format "VENDOR_MODEL_VARIANT".
-The built firmware can be installed as custom firmware, as shown above in in [Flashing the Rover Build](#flashing-the-rover-build).
+The built firmware can be installed as custom firmware, as shown above in [Flashing the Rover Build](#flashing-the-rover-build).
:::info
You can also enable the modules in default builds by adding these lines to your [board configuration](../hardware/porting_guide_config.md) (e.g. for fmu-v6x you might add them to [`main/boards/px4/fmu-v6x/default.px4board`](https://github.com/PX4/PX4-Autopilot/blob/main/boards/px4/fmu-v6x/default.px4board)):
diff --git a/docs/ko/config_rover/rate_tuning.md b/docs/ko/config_rover/rate_tuning.md
index 47ee11cbf9..2b317b4631 100644
--- a/docs/ko/config_rover/rate_tuning.md
+++ b/docs/ko/config_rover/rate_tuning.md
@@ -11,7 +11,7 @@ Configure the following [parameters](../advanced_config/parameters.md) in QGroun
1. [RO_YAW_RATE_LIM](#RO_YAW_RATE_LIM): Maximum yaw rate you want to allow for your rover.
:::tip
- Limiting the yaw rate is necessary if the rover is prone rolling over, loosing traction at high speeds or if passenger comfort is important.
+ Limiting the yaw rate is necessary if the rover is prone rolling over, losing traction at high speeds or if passenger comfort is important.
Small rovers especially can be prone to rolling over when steering aggressively at high speeds.
If this is the case:
diff --git a/docs/ko/config_rover/velocity_tuning.md b/docs/ko/config_rover/velocity_tuning.md
index 8e7f44f954..6b91165ed2 100644
--- a/docs/ko/config_rover/velocity_tuning.md
+++ b/docs/ko/config_rover/velocity_tuning.md
@@ -60,7 +60,7 @@ To tune the velocity controller configure the following [parameters](../advanced
## Manual Position Mode Parameters
-These steps are only necessary if you are tuning/want to unlock the manual [Position mode](../flight_modes_rover/manual.md#position-mode). Othwerwise, you can continue with [position tuning](position_tuning.md) where these same parameters will also be configured.
+These steps are only necessary if you are tuning/want to unlock the manual [Position mode](../flight_modes_rover/manual.md#position-mode). Otherwise, you can continue with [position tuning](position_tuning.md) where these same parameters will also be configured.
1. [PP_LOOKAHD_GAIN](#PP_LOOKAHD_GAIN): When driving in a straight line (right stick centered) position mode leverages the same path following algorithm used in [auto modes](../flight_modes_rover/auto.md) called [pure pursuit](position_tuning.md#pure-pursuit-guidance-logic-info-only) to achieve the best possible straight line driving behaviour.
This parameter determines how aggressive the controller will steer towards the path.
@@ -109,7 +109,7 @@ The speed controller uses the following structure:
The feed forward mapping is done by interpolating the speed setpoint from [-[RO_MAX_THR_SPEED](../advanced_config/parameter_reference.md#RO_MAX_THR_SPEED), [RO_MAX_THR_SPEED](../advanced_config/parameter_reference.md#RO_MAX_THR_SPEED)] to [-1, 1].
-For ackermann and differential rovers the bearing is aligned with the vehicle yaw. Therefor the bearing is simply sent as a yaw setpoint to the [yaw controller](attitude_tuning.md#attitude-controller-structure-info-only) and the speed setpoint is always defined in body x direction.
+For ackermann and differential rovers the bearing is aligned with the vehicle yaw. Therefore the bearing is simply sent as a yaw setpoint to the [yaw controller](attitude_tuning.md#attitude-controller-structure-info-only) and the speed setpoint is always defined in body x direction.
For mecanum vehicles, the bearing and yaw are decoupled. The direction is controlled by splitting the velocity vector into one speed component in body x direction and one in body y direction.
Both these setpoint are then sent to their own closed loop speed controllers.
diff --git a/docs/ko/config_vtol/vtol_ice_shedding.md b/docs/ko/config_vtol/vtol_ice_shedding.md
index ae719602af..76b084333b 100644
--- a/docs/ko/config_vtol/vtol_ice_shedding.md
+++ b/docs/ko/config_vtol/vtol_ice_shedding.md
@@ -6,7 +6,7 @@ Ice shedding is a feature that periodically spins unused motors in fixed-wing
flight, to break off any ice that is starting to build up in the motors while it
is still feasible to do so.
-It is configured by the paramter `CA_ICE_PERIOD`. When it is 0, the feature is
+It is configured by the parameter `CA_ICE_PERIOD`. When it is 0, the feature is
disabled, when it is above 0, it sets the duration of the ice shedding cycle in
seconds. In each cycle, the rotors are spun for two seconds at a motor output of
0.01.
diff --git a/docs/ko/config_vtol/vtol_quad_configuration.md b/docs/ko/config_vtol/vtol_quad_configuration.md
index d442eda0b6..88af569268 100644
--- a/docs/ko/config_vtol/vtol_quad_configuration.md
+++ b/docs/ko/config_vtol/vtol_quad_configuration.md
@@ -95,7 +95,7 @@ It should be set to a value which ensures that the vehicle reaches a high enough
[VT_TRANS_TIMEOUT](../advanced_config/parameter_reference.md#VT_TRANS_TIMEOUT)
This specifies the upper limit for the duration of the front transition. If the vehicle has not reached the transition airspeed after this time, then the transition will be aborted and a [Quadchute](../config/safety.md#quad-chute-failsafe) event will be triggered.
-:::note
+::: info
Additionally, if an airspeed sensor is present, the transition will also be aborted if the airspeed has not reached [VT_ARSP_BLEND](../advanced_config/parameter_reference.md#VT_ARSP_BLEND) after the openloop transition time [VT_F_TR_OL_TM](../advanced_config/parameter_reference.md#VT_F_TR_OL_TM) has elapsed. This checks is used to avoid a scenario where the vehicle gains excessive speed when the airspeed sensor is faulty.
:::
diff --git a/docs/ko/contribute/dev_call.md b/docs/ko/contribute/dev_call.md
index ff5ed0e045..b980479813 100644
--- a/docs/ko/contribute/dev_call.md
+++ b/docs/ko/contribute/dev_call.md
@@ -7,7 +7,7 @@ const { site } = useData();
@@ -36,4 +36,4 @@ Please add your topics for discussion to the agenda before the meeting begins, b
## 일정
- TIME: Wednesday 17h00 CET ([subscribe to calendar](https://dronecode.org/calendar/))
-- **Join the call**: [https://discord.gg/BDYmr6FA6Q](https://discord.gg/BDYmr6FA6Q)
+- **Join the call**: [https://discord.com/invite/BDYmr6FA6Q](https://discord.com/invite/BDYmr6FA6Q)
diff --git a/docs/ko/contribute/docs.md b/docs/ko/contribute/docs.md
index f0713b2edf..21d05cfbfb 100644
--- a/docs/ko/contribute/docs.md
+++ b/docs/ko/contribute/docs.md
@@ -56,7 +56,7 @@ If you already have a clone of the [PX4-Autopilot](https://github.com/PX4/PX4-Au
라이브러리 소스를 로컬 컴퓨터로 가져오려면 git 명령어를 사용하여야 합니다.
아래 지침은 git을 가져와 로컬 컴퓨터에서 사용하는 방법을 설명합니다.
-1. Download git for your computer from [https://git-scm.com/downloads](https://git-scm.com/downloads)
+1. Download git for your computer from [https://git-scm.com/downloads/](https://git-scm.com/downloads/)
2. [Sign up](https://github.com/signup) for Github if you haven't already
@@ -84,10 +84,10 @@ If you already have a clone of the [PX4-Autopilot](https://github.com/PX4/PX4-Au
6. Add a _remote_ called "upstream" to point to the "official" PX4 version of the library:
```sh
- git remote add upstream https://github.com/PX4/PX4-Autopilot.git
+ git remote add upstream https://github.com/PX4/PX4-Autopilot
```
- :::tip
+ ::: tip
A "remote" is a handle to a particular repository.
The remote named _origin_ is created by default when you clone the repository, and points to _your fork_ of the guide.
Above you create a new remote _upstream_ that points to the PX4 project version of the documents.
@@ -167,7 +167,9 @@ Within the repository you created above:
yarn install
```
-4. Preview and serve the library:
+4. (Optional) [Build the docs for PX4 metadata](#building-px4-docs-metadata) if your source contains changes to parameter or module docs that you want to check.
+
+5. Preview and serve the library:
```sh
yarn docs:dev
@@ -177,7 +179,7 @@ Within the repository you created above:
This will be something like: `http://localhost:5173/px4_user_guide/`.
- Stop serving using **CTRL+C** in the terminal prompt.
-5. Open previewed pages in your local editor:
+6. Open previewed pages in your local editor:
First specify a local text editor file using the `EDITOR` environment variable, before calling `yarn start` to preview the library.
For example, you can enable VSCode as your default editor by entering:
@@ -196,7 +198,7 @@ Within the repository you created above:
The **Open in your editor** link at the bottom of each page will then open the current page in the editor (this replaces the _Open in GitHub_ link).
-6. 다음을 사용하여 라이브러리를 빌드합니다.
+7. 다음을 사용하여 라이브러리를 빌드합니다.
```sh
# Ubuntu
@@ -211,6 +213,32 @@ Use `yarn start` to preview changes _as you make them_ (documents are updated an
Before submitting a PR you should also build it using `yarn docs:build`, as this can highlight issues that are not visible when using `yarn start`.
:::
+#### Building PX4 docs metadata
+
+PX4 Metadata is not automatically updated in the local docs tree when you make changes to source.
+This can result in broken links showing up during testing if you link to new parameters, modules, airframes, or other content that is generated from source.
+
+You can generate the metadata and copy it into the tree on _Ubuntu_ (only) using the convenient yarn command:
+
+```sh
+# Ubuntu
+yarn build_docs_metadata_ubuntu
+```
+
+:::info
+The generated metadata docs should not be included in PRs as they will complicate reveiwing (metadata is automatically generated when a PR merges in main).
+It is not a problem if you do add such metadata, as it will be swamped on merge.
+:::
+
+#### Check for broken links
+
+You can use the following command to check for broken links in the whole document:
+
+```sh
+# Ubuntu
+yarn linkcheck
+```
+
### 소스 코드 구조
The guide uses the [Vitepress](https://vitepress.dev/) toolchain.
diff --git a/docs/ko/contribute/git_examples.md b/docs/ko/contribute/git_examples.md
index 96773607f6..0b89d1bfcd 100644
--- a/docs/ko/contribute/git_examples.md
+++ b/docs/ko/contribute/git_examples.md
@@ -22,7 +22,7 @@ PX4 기능 추가 절차는 다음과 같습니다. 다음 예제를 따라 PX4
```sh
cd PX4-Autopilot
git submodule update --init --recursive
- git remote add upstream https://github.com/PX4/PX4-Autopilot.git
+ git remote add upstream https://github.com/PX4/PX4-Autopilot
```
- You should have now two remote repositories: One repository is called `upstream` that points to PX4/PX4-Autopilot, and one repository `origin` that points to your forked copy of the PX4 repository.
@@ -49,7 +49,7 @@ PX4 기능 추가 절차는 다음과 같습니다. 다음 예제를 따라 PX4
git add
```
- If you prefer having a GUI to add your files see [Gitk](https://git-scm.com/book/en/v2/Git-in-Other-Environments-Graphical-Interfaces) or [`git add -p`](https://nuclearsquid.com/writings/git-add/).
+ If you prefer having a GUI to add your files see [Gitk](https://git-scm.com/book/en/v2/Appendix-A:-Git-in-Other-Environments-Graphical-Interfaces) or [`git add -p`](https://nuclearsquid.com/writings/git-add/).
- 변경 사항을 설명하는 메시지와 함께 추가된 파일을 커밋합니다.
@@ -59,7 +59,7 @@ PX4 기능 추가 절차는 다음과 같습니다. 다음 예제를 따라 PX4
For a good commit message, please refer to the [Source Code Management](../contribute/code.md#commits-and-commit-messages) section.
-- Some time might have passed and the [upstream main](https://github.com/PX4/PX4-Autopilot.git) has changed.
+- Some time might have passed and the [upstream main](https://github.com/PX4/PX4-Autopilot) has changed.
PX4 prefers a linear commit history and uses [git rebase](https://git-scm.com/book/en/v2/Git-Branching-Rebasing).
To include the newest changes from upstream in your local branch, switch to your main branch
@@ -139,7 +139,7 @@ To get the source code for a _specific older release_ (tag):
1. Clone the PX4-Autopilot repo and navigate into _PX4-Autopilot_ directory:
```sh
- git clone https://github.com/PX4/PX4-Autopilot.git
+ git clone https://github.com/PX4/PX4-Autopilot
cd PX4-Autopilot
```
@@ -179,7 +179,7 @@ To get a release branch:
- Clone the PX4-Autopilot repo and navigate into _PX4-Autopilot_ directory:
```sh
- git clone https://github.com/PX4/PX4-Autopilot.git
+ git clone https://github.com/PX4/PX4-Autopilot
cd PX4-Autopilot
```
diff --git a/docs/ko/contribute/index.md b/docs/ko/contribute/index.md
index adf08e6a79..38a3124e14 100644
--- a/docs/ko/contribute/index.md
+++ b/docs/ko/contribute/index.md
@@ -7,7 +7,7 @@ const { site } = useData();
diff --git a/docs/ko/contribute/support.md b/docs/ko/contribute/support.md
index ae7d5b0203..cc286cb3d5 100644
--- a/docs/ko/contribute/support.md
+++ b/docs/ko/contribute/support.md
@@ -7,7 +7,7 @@ const { site } = useData();
@@ -18,7 +18,7 @@ const { site } = useData();
The core development team and community are active on the following channels:
- [PX4 Discuss Forum](https://discuss.px4.io/) - Post here first!
-- [PX4 Discord](https://discord.gg/dronecode) - Post here if you don't get a response in discuss within a few days (include a link to your forum topic).
+- [PX4 Discord](https://discord.com/invite/dronecode) - Post here if you don't get a response in discuss within a few days (include a link to your forum topic).
:::tip
The Discuss Forum is much preferred because it is indexed by search engines and serves as a common knowledge base.
diff --git a/docs/ko/debug/asset_tracking.md b/docs/ko/debug/asset_tracking.md
index 31461d4a29..bd6a79d128 100644
--- a/docs/ko/debug/asset_tracking.md
+++ b/docs/ko/debug/asset_tracking.md
@@ -1,6 +1,6 @@
# Asset Tracking
-/Tools/jlink-nuttx.so`, as shown in the image below.
diff --git a/docs/ko/debug/plotting_realtime_uorb_data.md b/docs/ko/debug/plotting_realtime_uorb_data.md
index bb11f5c109..17334f8fa8 100644
--- a/docs/ko/debug/plotting_realtime_uorb_data.md
+++ b/docs/ko/debug/plotting_realtime_uorb_data.md
@@ -72,7 +72,7 @@ cd ~/PX4-Autopilot
make px4_sitl gz_x500
```
-Open another terminal and start the `MicroXRCEAgent` to connect to the the simulator:
+Open another terminal and start the `MicroXRCEAgent` to connect to the simulator:
```sh
MicroXRCEAgent udp4 -p 8888; exec bash
diff --git a/docs/ko/debug/probe_mculink.md b/docs/ko/debug/probe_mculink.md
index d61135b956..1e03cca665 100644
--- a/docs/ko/debug/probe_mculink.md
+++ b/docs/ko/debug/probe_mculink.md
@@ -1,6 +1,6 @@
# MCU-Link Debug Probe
-The [MCU-Link Debug Probe](https://www.nxp.com/design/design-center/software/development-software/mcuxpresso-software-and-tools-/mcu-link-debug-probe:MCU-LINK) is a cheap, fast and highly capable debug probe that can serve as a stand-alone debug and console communicator whn working with Pixhawk boards.
+The [MCU-Link Debug Probe](https://www.nxp.com/design/design-center/software/development-software/mcuxpresso-software-and-tools-/mcu-link-debug-probe:MCU-LINK) is a cheap, fast and highly capable debug probe that can serve as a stand-alone debug and console communicator when working with Pixhawk boards.
주요 기능:
diff --git a/docs/ko/debug/simulation_debugging.md b/docs/ko/debug/simulation_debugging.md
index d73c942298..fa0945db8b 100644
--- a/docs/ko/debug/simulation_debugging.md
+++ b/docs/ko/debug/simulation_debugging.md
@@ -106,7 +106,7 @@ You can also start your simulation, and _then_ attach `gdb`:
```
As the script runs, note the **SITL COMMAND:** output text located right above the large "PX4" text.
- It will list the location of your px4 bin file for later use.
+ It will list the location of your PX4 bin file for later use.
```sh
SITL COMMAND: "" ""/etc
diff --git a/docs/ko/debug/swd_debug.md b/docs/ko/debug/swd_debug.md
index b8730cea52..52d2de4261 100644
--- a/docs/ko/debug/swd_debug.md
+++ b/docs/ko/debug/swd_debug.md
@@ -1,6 +1,6 @@
# SWD Debug Port
-PX4 runs on ARM Cortex-M microcontrollers, which contain dedicated hardware for interactive debugging via the [_Serial Wire Debug (SWD)_][swd] interface and non-invasive profiling and high-bandwidth tracing via the [_Serial Wire Ouput (SWO)_][itm] and [_TRACE_ pins][etm].
+PX4 runs on ARM Cortex-M microcontrollers, which contain dedicated hardware for interactive debugging via the [_Serial Wire Debug (SWD)_][swd] interface and non-invasive profiling and high-bandwidth tracing via the [_Serial Wire Output (SWO)_][itm] and [_TRACE_ pins][etm].
The SWD debug interface allows direct, low-level, hardware access to the microcontroller's processor and peripherals, so it does not depend on any software on the device.
Therefore it can be used to debug bootloaders and operating systems such as NuttX.
@@ -27,9 +27,7 @@ The SWO pin can emit low-overhead, real-time profiling data with nanosecond time
The TRACE pins require specialized debug probes to deal with the high bandwidth and subsequent datastream decoding.
They are usually not accessible and are typically only used to debug very specific timing issues.
-
-
-## 자동비행장치 디버그 포트
+## Autopilot Debug Ports {#debug-ports}
Flight controllers commonly provide a single debug port that exposes both the [SWD Interface](#debug-signals) and [System Console](system_console).
@@ -40,23 +38,35 @@ The debug port location and pinouts for a subset of autopilots are linked below:
-| 오토파일럿 | 디버그 포트 |
-| :----------------------------------------------------------------------------------------------------- | :---------------------------------------------------------------------------------------------------------------------------------------------------------------- |
-| Holybro Pixhawk 6X-RT (FMUv6X-RT) | [Pixhawk Debug Full](#pixhawk-debug-full) |
-| Holybro Pixhawk 6X (FMUv6x) | [Pixhawk Debug Full](#pixhawk-debug-full) |
-| Holybro Pixhawk 5X (FMUv5x) | [Pixhawk Debug Full](#pixhawk-debug-full) |
-| [Holybro Durandal](../flight_controller/durandal.md#debug-port) | [Pixhawk Debug Mini](#pixhawk-debug-mini) |
-| [Holybro Kakute F7](../flight_controller/kakutef7.md#debug-port) | Solder pads |
-| [Holybro Pixhawk 4 Mini](../flight_controller/pixhawk4_mini.md#debug-port) (FMUv5) | [Pixhawk Debug Mini](#pixhawk-debug-mini) |
-| [Holybro Pixhawk 4](../flight_controller/pixhawk4.md#debug_port) (FMUv5) | [Pixhawk Debug Mini](#pixhawk-debug-mini) |
-| [Drotek Pixhawk 3 Pro](../flight_controller/pixhawk3_pro.md#debug-port) (FMU-v4pro) | [Pixhawk Debug Mini](#pixhawk-debug-mini) |
-| [CUAV V5+](../flight_controller/cuav_v5_plus.md#debug-port) | 6-pin JST GH
Digikey: [BM06B-GHS-TBT(LF)(SN)(N)][bm06b-ghs-tbt(lf)(sn)(n)] (vertical mount), [SM06B-GHS-TBT(LF)(SN)(N)][sm06b-ghs-tbt(lf)(sn)(n)] (side mount) | -| [CUAV V5nano](../flight_controller/cuav_v5_nano.md#debug_port) | 6-pin JST GH
Digikey: [BM06B-GHS-TBT(LF)(SN)(N)][bm06b-ghs-tbt(lf)(sn)(n)] (vertical mount), [SM06B-GHS-TBT(LF)(SN)(N)][sm06b-ghs-tbt(lf)(sn)(n)] (side mount) | -| [3DR Pixhawk](../flight_controller/pixhawk.md#swd-port) | ARM 10-pin JTAG Connector (also used for FMUv2 boards including: _mRo Pixhawk_, _HobbyKing HKPilot32_). | +| 오토파일럿 | 디버그 포트 | +| :------------------------------------------------------------------------------------------------------ | :----------------------------------------------------------------------- | +| [Holybro Pixhawk 6X-RT](../flight_controller/pixhawk6x-rt.md#debug_port) (FMUv6X-RT) | [Pixhawk Debug Full](#pixhawk-debug-full) | +| [Holybro Pixhawk 6X](../flight_controller/pixhawk6x.md#debug_port) (FMUv6x) | [Pixhawk Debug Full](#pixhawk-debug-full) | +| [Holybro Pixhawk 5X](../flight_controller/pixhawk5x.md#debug_port) (FMUv5x) | [Pixhawk Debug Full](#pixhawk-debug-full) | +| [Holybro Durandal](../flight_controller/durandal.md#debug-port) | [Pixhawk Debug Mini](#pixhawk-debug-mini) | +| [Holybro Pixhawk 4](../flight_controller/pixhawk4.md#debug_port) (FMUv5) | [Pixhawk Debug Mini](#pixhawk-debug-mini) | +| [Holybro Pixhawk 6X Pro](../flight_controller/pixhawk6x_pro.md#debug-port) | [Pixhawk Debug Full](#pixhawk-debug-full) | +| [Holybro Pixhawk 6C](../flight_controller/pixhawk6c.md#debug_port) | [Pixhawk Debug Full](#pixhawk-debug-full) | +| [Holybro Pixhawk 6C Mini](../flight_controller/pixhawk6c_mini.md#debug_port) | [Pixhawk Debug Mini](#pixhawk-debug-mini) | +| [Holybro Pix32 v6](../flight_controller/holybro_pix32_v6.md#debug_port) | [Pixhawk Debug Full](#pixhawk-debug-full) | +| [Holybro Pix32 v5](../flight_controller/holybro_pix32_v5.md#debug-port) | [Pixhawk Debug Mini](#pixhawk-debug-mini) | +| [Holybro Kakute H7](../flight_controller/kakuteh7.md#debug-port) | SWD pads and system console | +| [Holybro Kakute H7 mini](../flight_controller/kakuteh7mini.md#debug-port) | SWD pads and system console | +| [Holybro Kakute H7 V2](../flight_controller/kakuteh7v2.md#debug-port) | SWD pads and system console | +| [CUAV V5+](../flight_controller/cuav_v5_plus.md#debug-port) | Custom port but comes with adaptor cable | +| [CUAV V5nano](../flight_controller/cuav_v5_nano.md#debug_port) | Custom port but comes with adaptor cable | +| [CUAV Pixhawk V6X](../flight_controller/cuav_pixhawk_v6x.md#debug_port) | [Pixhawk Debug Full](#pixhawk-debug-full) | +| [CUAV X25-SUPER](../flight_controller/cuav_x25-super.md#debug_port) | [Pixhawk Debug Mini] | +| [CUAV X25-EVO](../flight_controller/cuav_x25-evo.md#debug_port) | [Pixhawk Debug Mini] | +| [CUAV Nora](../flight_controller/cuav_nora.md#debug-port) | Custom port but comes with adaptor cable. | +| [ARK Pixhawk Autopilot Bus Carrier](../flight_controller/ark_pab.md#debug-port) | [Pixhawk Debug Full](#pixhawk-debug-full) | +| [NXP MR-VMU-RT1176](../flight_controller/nxp_mr_vmu_rt1176.md#debug_port) | [Pixhawk Debug Full](#pixhawk-debug-full) | +| [mRo Pixracer](../flight_controller/pixracer.md#debug-port) | [Pixhawk Debug Mini](#pixhawk-debug-mini) | +| [S-Vehicle E2](../flight_controller/svehicle_e2.md#debug-port) | [Pixhawk Debug Mini] | +| [AP-H743-R1](../flight_controller/x-mav_ap-h743r1.md#debug-port) | 4-pin JST GH (SWD only) | +| [mRo Control Zero F7](../flight_controller/mro_control_zero_f7.md#debug_port) | | - - -## Pixhawk Connector Standard Debug Ports +## Pixhawk Connector Standard Debug Ports {#pixhawk-standard-debug-ports} The Pixhawk project has defines a standard pinout and connector type for different Pixhawk FMU releases: @@ -64,16 +74,16 @@ The Pixhawk project has defines a standard pinout and connector type for differe Check your [specific board](#port-information) to confirm the port used. ::: -| FMU 버전 | Pixhawk Version | 디버그 포트 | -| :-------- | :-------------------------------------------------------------- | :---------------------------------------- | -| FMUv2 | [Pixhawk / Pixhawk 1](../flight_controller/pixhawk.md#swd-port) | 10핀 ARM 디버그 | -| FMUv3 | Pixhawk 2 | 6핀 SUR 디버그 | -| FMUv4 | Pixhawk 3 | [Pixhawk Debug Mini](#pixhawk-debug-mini) | -| FMUv5 | Pixhawk 4 FMUv5 | [Pixhawk Debug Mini](#pixhawk-debug-mini) | -| FMUv5X | Pixhawk 5X | [Pixhawk Debug Full](#pixhawk-debug-full) | -| FMUv6 | Pixhawk 6 | [Pixhawk Debug Full](#pixhawk-debug-full) | -| FMUv6X | Pixhawk 6X | [Pixhawk Debug Full](#pixhawk-debug-full) | -| FMUv6X-RT | Pixhawk 6X-RT | [Pixhawk Debug Full](#pixhawk-debug-full) | +| FMU 버전 | Pixhawk Version | 디버그 포트 | +| :-------- | :------------------ | :---------------------------------------- | +| FMUv2 | Pixhawk / Pixhawk 1 | 10핀 ARM 디버그 | +| FMUv3 | Pixhawk 2 | 6핀 SUR 디버그 | +| FMUv4 | Pixhawk 3 | [Pixhawk Debug Mini](#pixhawk-debug-mini) | +| FMUv5 | Pixhawk 4 FMUv5 | [Pixhawk Debug Mini](#pixhawk-debug-mini) | +| FMUv5X | Pixhawk 5X | [Pixhawk Debug Full](#pixhawk-debug-full) | +| FMUv6 | Pixhawk 6 | [Pixhawk Debug Full](#pixhawk-debug-full) | +| FMUv6X | Pixhawk 6X | [Pixhawk Debug Full](#pixhawk-debug-full) | +| FMUv6X-RT | Pixhawk 6X-RT | [Pixhawk Debug Full](#pixhawk-debug-full) | :::info There FMU and Pixhawk versions are (only) consistent after FMUv5X. @@ -142,9 +152,7 @@ You can connect to the debug port using a [cable like this one](https://www.digi  - - -## Debug Probes for PX4 Hardware +## Debug Probes for PX4 Hardware {#debug-probes} Flight controllers commonly provide a [single debug port](#autopilot-debug-ports) that exposes both the [SWD Interface](#debug-signals) and [System Console](system_console). @@ -217,5 +225,3 @@ This reduces the risk or poor wiring contributing to debugging problems, and has [swd]: https://developer.arm.com/documentation/ihi0031/a/The-Serial-Wire-Debug-Port--SW-DP- [itm]: https://developer.arm.com/documentation/ddi0403/d/Appendices/Debug-ITM-and-DWT-Packet-Protocol?lang=en [etm]: https://developer.arm.com/documentation/ihi0064/latest/ -[bm06b-ghs-tbt(lf)(sn)(n)]: https://www.digikey.com/en/products/detail/jst-sales-america-inc/BM06B-GHS-TBT/807804 -[sm06b-ghs-tbt(lf)(sn)(n)]: https://www.digikey.com/en/products/detail/jst-sales-america-inc/SM06B-GHS-TB/807790 diff --git a/docs/ko/dev_airframes/adding_a_new_frame.md b/docs/ko/dev_airframes/adding_a_new_frame.md index 59aece9838..5f5133b9b7 100644 --- a/docs/ko/dev_airframes/adding_a_new_frame.md +++ b/docs/ko/dev_airframes/adding_a_new_frame.md @@ -124,118 +124,79 @@ param set-default CA_ROTOR3_PY 0.15 param set-default CA_ROTOR3_KM -0.05 ``` -### Example - Babyshark VTOL Complete Vehicle +### Example - HolyBro QAV250 Complete Vehicle -A more complicated configuration file for a complete vehicle is provided below. -This is the configuration for the Baby Shark [Standard VTOL](../frames_vtol/standardvtol.md) ([original file here](https://github.com/PX4/PX4-Autopilot/blob/main/ROMFS/px4fmu_common/init.d/airframes/13014_vtol_babyshark)). +A more complete configuration file for a real vehicle is provided below. +This is the configuration for the [HolyBro QAV250](../frames_multicopter/holybro_qav250_pixhawk4_mini.md) quadrotor ([original file here](https://github.com/PX4/PX4-Autopilot/blob/main/ROMFS/px4fmu_common/init.d/airframes/4052_holybro_qav250)). -The shebang and documentation sections are similar to those for the generic frame, but here we also document what `outputs` are mapped to each motor and actuator. -Note that these outputs are documentation only; the actual mapping is done using parameters. +The shebang and documentation sections are similar to those for the generic frame. +Here we also add a `@url` link to the vehicle documentation, a `@maintainer`, and additional board exclusions. ```sh #!/bin/sh # -# @name BabyShark VTOL +# @name HolyBro QAV250 # -# @type Standard VTOL -# @class VTOL +# @url https://docs.px4.io/main/en/frames_multicopter/holybro_qav250_pixhawk4_mini # -# @maintainer Silvan Fuhrer
+# @type Quadrotor x
+# @class Copter
#
-# @output Motor1 motor 1
-# @output Motor2 motor 2
-# @output Motor3 motor 3
-# @output Motor4 motor 4
-# @output Motor5 Pusher motor
-# @output Servo1 Ailerons
-# @output Servo2 A-tail left
-# @output Servo3 A-tail right
+# @maintainer Beat Kueng
#
# @board px4_fmu-v2 exclude
# @board bitcraze_crazyflie exclude
-# @board holybro_kakutef7 exclude
+# @board px4_fmu-v6x exclude
+# @board ark_fmu-v6x exclude
#
```
-As for the generic frame, we then include the generic VTOL defaults.
+Next, we source the multicopter defaults.
```sh
-. ${R}etc/init.d/rc.vtol_defaults
+. ${R}etc/init.d/rc.mc_defaults
```
Then we define configuration parameters and [tuning gains](#tuning-gains):
```sh
-param set-default MAV_TYPE 22
+# The set does not include a battery, but most people will probably use 4S
+param set-default BAT1_N_CELLS 4
-param set-default BAT1_N_CELLS 6
+param set-default IMU_GYRO_CUTOFF 120
+param set-default IMU_DGYRO_CUTOFF 45
-param set-default FW_AIRSPD_MAX 30
-param set-default FW_AIRSPD_MIN 19
-param set-default FW_AIRSPD_TRIM 23
-param set-default FW_PN_R_SLEW_MAX 40
-param set-default FW_PSP_OFF 3
-param set-default FW_P_LIM_MAX 18
-param set-default FW_P_LIM_MIN -25
-param set-default FW_RLL_TO_YAW_FF 0.1
-param set-default FW_RR_P 0.08
-param set-default FW_R_LIM 45
-param set-default FW_R_RMAX 50
-param set-default FW_THR_TRIM 0.65
-param set-default FW_THR_MIN 0.3
-param set-default FW_THR_SLEW_MAX 0.6
-param set-default FW_T_HRATE_FF 0
-param set-default FW_T_SINK_MAX 15
-param set-default FW_T_SINK_MIN 3
-param set-default FW_YR_P 0.15
-
-param set-default IMU_DGYRO_CUTOFF 15
-param set-default MC_PITCHRATE_MAX 60
-param set-default MC_ROLLRATE_MAX 60
-param set-default MC_YAWRATE_I 0.15
-param set-default MC_YAWRATE_MAX 40
-param set-default MC_YAWRATE_P 0.3
-
-param set-default MPC_ACC_DOWN_MAX 2
-param set-default MPC_ACC_HOR_MAX 2
-param set-default MPC_ACC_UP_MAX 3
param set-default MC_AIRMODE 1
-param set-default MPC_JERK_AUTO 4
-param set-default MPC_LAND_SPEED 1
-param set-default MPC_MAN_TILT_MAX 25
-param set-default MPC_MAN_Y_MAX 40
-param set-default COM_SPOOLUP_TIME 1.5
-param set-default MPC_THR_HOVER 0.45
-param set-default MPC_TILTMAX_AIR 25
-param set-default MPC_TKO_RAMP_T 1.8
-param set-default MPC_TKO_SPEED 1
-param set-default MPC_VEL_MANUAL 3
-param set-default MPC_XY_CRUISE 3
-param set-default MPC_XY_VEL_MAX 3.5
-param set-default MPC_YAWRAUTO_MAX 40
-param set-default MPC_Z_VEL_MAX_UP 2
+param set-default MC_PITCHRATE_D 0.0012
+param set-default MC_PITCHRATE_I 0.35
+param set-default MC_PITCHRATE_MAX 1200
+param set-default MC_PITCHRATE_P 0.082
+param set-default MC_PITCH_P 8
+param set-default MC_ROLLRATE_D 0.0012
+param set-default MC_ROLLRATE_I 0.3
+param set-default MC_ROLLRATE_MAX 1200
+param set-default MC_ROLLRATE_P 0.076
+param set-default MC_ROLL_P 8
+param set-default MC_YAWRATE_I 0.3
+param set-default MC_YAWRATE_MAX 600
+param set-default MC_YAWRATE_P 0.25
+param set-default MC_YAW_P 4
-param set-default NAV_ACC_RAD 3
+param set-default MPC_MANTHR_MIN 0
+param set-default MPC_MAN_TILT_MAX 60
+param set-default MPC_THR_CURVE 1
+param set-default MPC_THR_HOVER 0.25
+param set-default MPC_THR_MIN 0.05
+param set-default MPC_Z_VEL_I_ACC 1.7
-param set-default SENS_BOARD_ROT 4
-
-param set-default VT_ARSP_BLEND 10
-param set-default VT_ARSP_TRANS 21
-param set-default VT_B_DEC_MSS 1.5
-param set-default VT_B_TRANS_DUR 12
-param set-default VT_ELEV_MC_LOCK 0
-param set-default VT_FWD_THRUST_SC 1.2
-param set-default VT_F_TR_OL_TM 8
-param set-default VT_PSHER_SLEW 0.5
-param set-default VT_TRANS_MIN_TM 4
-param set-default VT_TYPE 2
+param set-default THR_MDL_FAC 0.3
```
-Last of all, the file defines the control allocation parameters for the geometry and the parameters that set which outputs map to different motors and servos.
+Last of all, the file defines the control allocation parameters for the geometry and the parameters that set which outputs map to different motors.
```sh
-param set-default CA_AIRFRAME 2
-param set-default CA_ROTOR_COUNT 5
+# Square quadrotor X PX4 numbering
+param set-default CA_ROTOR_COUNT 4
param set-default CA_ROTOR0_PX 1
param set-default CA_ROTOR0_PY 1
param set-default CA_ROTOR1_PX -1
@@ -246,34 +207,11 @@ param set-default CA_ROTOR2_KM -0.05
param set-default CA_ROTOR3_PX -1
param set-default CA_ROTOR3_PY 1
param set-default CA_ROTOR3_KM -0.05
-param set-default CA_ROTOR4_AX 1.0
-param set-default CA_ROTOR4_AZ 0.0
-param set-default CA_SV_CS_COUNT 3
-param set-default CA_SV_CS0_TYPE 15
-param set-default CA_SV_CS0_TRQ_R 1.0
-param set-default CA_SV_CS1_TRQ_P 0.5000
-param set-default CA_SV_CS1_TRQ_R 0.0000
-param set-default CA_SV_CS1_TRQ_Y -0.5000
-param set-default CA_SV_CS1_TYPE 13
-param set-default CA_SV_CS2_TRQ_P 0.5000
-param set-default CA_SV_CS2_TRQ_Y 0.5000
-param set-default CA_SV_CS2_TYPE 14
-
-param set-default PWM_MAIN_FUNC1 201
-param set-default PWM_MAIN_FUNC2 202
-param set-default PWM_MAIN_FUNC3 105
-param set-default PWM_MAIN_FUNC4 203
-param set-default PWM_MAIN_FUNC5 101
-param set-default PWM_MAIN_FUNC6 102
-param set-default PWM_MAIN_FUNC7 103
-param set-default PWM_MAIN_FUNC8 104
-
-param set-default PWM_MAIN_TIM0 50
-param set-default PWM_MAIN_DIS1 1500
-param set-default PWM_MAIN_DIS2 1500
-param set-default PWM_MAIN_DIS3 1000
-param set-default PWM_MAIN_DIS4 1500
+param set-default PWM_MAIN_FUNC1 101
+param set-default PWM_MAIN_FUNC2 102
+param set-default PWM_MAIN_FUNC3 103
+param set-default PWM_MAIN_FUNC4 104
```
## 새 기체 그룹 추가
diff --git a/docs/ko/dev_log/log_encryption.md b/docs/ko/dev_log/log_encryption.md
index e8a9a04267..663de12daf 100644
--- a/docs/ko/dev_log/log_encryption.md
+++ b/docs/ko/dev_log/log_encryption.md
@@ -15,7 +15,7 @@ To use it you will need to build firmware with this feature enabled and then upl
Log encryption was has been improved in PX4 v1.16 to generate a single encrypted log file that contains both encrypted log data, and an encrypted symmetric key that you can use to decrypt it (provided you can decrypt the symmetric key).
In earlier versions the encrypted symmetric key was stored in a separate file.
-For more information see the [Log Encryption (PX4 v1.15)](https://docs.px4.io/v1.15/en/dev_log/log_encryption.html).
+For more information see the [Log Encryption (PX4 v1.15)](https://docs.px4.io/v1.15/en/dev_log/log_encryption).
:::
## How ULog Encryption Works
@@ -142,7 +142,7 @@ Note that the value is generated fresh for each log, and any value specified in
You can use choose different locations for your keys as long as they aren't used by anything else.
:::
-The key in `CONFIG_PUBLIC_KEY1` is the public key used to wrap the symmetric key in the the beginning of `.ulge` file (by default: see [SDLOG_EXCH_KEY](../advanced_config/parameter_reference.md#SDLOG_EXCH_KEY)).
+The key in `CONFIG_PUBLIC_KEY1` is the public key used to wrap the symmetric key in the beginning of `.ulge` file (by default: see [SDLOG_EXCH_KEY](../advanced_config/parameter_reference.md#SDLOG_EXCH_KEY)).
You can use the `rsa2048.pub` key for testing, or replace it with the path to your own public key in the file (see [Generate RSA Public & Private Keys](#generate-rsa-public-private-keys)).
Build the firmware like this:
diff --git a/docs/ko/dev_setup/dev_env_mac.md b/docs/ko/dev_setup/dev_env_mac.md
index 63e8e3ca38..b42a457690 100644
--- a/docs/ko/dev_setup/dev_env_mac.md
+++ b/docs/ko/dev_setup/dev_env_mac.md
@@ -1,116 +1,122 @@
# macOS Development Environment
-아래에서 macOS용 PX4 개발 환경 설정 방법을 설명합니다.
+The following instructions set up a PX4 development environment on macOS.
PX4 빌드에 사용되어 집니다.
- Pixhawk와 기타 NuttX 기반 하드웨어
-- [Gazebo Classic Simulation](../sim_gazebo_classic/index.md)
+- [Gazebo Simulation](../sim_gazebo_gz/index.md) (Gazebo Harmonic)
+
+It works on both Intel and Apple Silicon Macs.
:::tip
This setup is supported by the PX4 dev team.
-To build other targets you will need to use a [different OS](../dev_setup/dev_env.md#supported-targets) (or an [unsupported development environment](../advanced/community_supported_dev_env.md)).
+To build for [other targets](../dev_setup/dev_env.md#supported-targets) you will need to use a [different OS](../dev_setup/dev_env.md#supported-targets) or an [unsupported development environment](../advanced/community_supported_dev_env.md).
:::
-## 영상 가이드
+## Development Environment Setup
-
```
@@ -116,7 +116,7 @@ echo "PermitRootLogin yes" >> /etc/ssh/sshd_config && systemctl restart sshd
The ARM Cross Compiler for _BeagleBone Blue_ can be found at [Linaro Toolchain Binaries site](https://www.linaro.org/downloads/#gnu_and_llvm).
- :::tip
+ ::: tip
GCC in the toolchain should be compatible with kernel in _BeagleBone Blue_.
General rule of thumb is to choose a toolchain where version of GCC is not higher than version of GCC which comes with the OS image on _BeagleBone Blue_.
@@ -131,7 +131,7 @@ echo "PermitRootLogin yes" >> /etc/ssh/sshd_config && systemctl restart sshd
tar -xf gcc-linaro-13.0.0-2022.06-x86_64_arm-linux-gnueabihf.tar.xz
```
- :::tip
+ ::: tip
The GCC version of the toolchain should be compatible with kernel in _BeagleBone Blue_.
:::
@@ -151,7 +151,7 @@ echo "PermitRootLogin yes" >> /etc/ssh/sshd_config && systemctl restart sshd
3. Setup other dependencies by downloading the PX4 source code and then running the setup scripts:
- ````
+ ````sh
git clone https://github.com/PX4/PX4-Autopilot.git --recursive
ols
```
@@ -170,7 +170,7 @@ echo "PermitRootLogin yes" >> /etc/ssh/sshd_config && systemctl restart sshd
Compile and Upload
-```
+```sh
make beaglebone_blue_default upload
```
@@ -189,9 +189,7 @@ sudo ./bin/px4 -s px4.config
Currently _librobotcontrol_ requires root access.
:::
-
-
-## 네이티브 빌드(선택 사항)
+## Native Builds (optional) {#native_builds}
You can also natively build PX4 builds directly on the BeagleBone Blue.
@@ -216,7 +214,7 @@ Run the following commands on the BeagleBone Blue (i.e. via SSH):
## Changes in config
-All changes can be made in de px4.config file directly on beaglebone.
+All changes can be made in the px4.config file directly on beaglebone.
For example, you can change the WIFI to wlan.
:::info
@@ -295,8 +293,6 @@ For a quadcopter with GPS and an SBUS receiver, here are typical connections:
1. 비글본 블루에서 모터 1, 2, 3 및 4의 ESC를 서보 출력의 채널 1, 2, 3 및 4에 연결합니다.
비글본 블루에서 ESC 커넥터에 전원 출력이 포함되어 있는 경우 핀, 제거 및 서보 채널의 전원 출력 핀에 연결하지 마십시오.
-
2. Connect the above mentioned converted SBUS signal to the dsm2 port if you have the matching connector for dsm2, otherwise connect it to any other available UART port and change the corresponding port in **/home/debian/px4/px4.config** accordingly.
-
3. GPS 모듈의 신호를 비글본 블루의 GPS 포트에 연결합니다
BeagleBone Blue에있는 GPS 포트의 신호 핀은 3.3V만 허용하므로 이에 적합한 GPS 모듈을 선택하십시오.
diff --git a/docs/ko/flight_controller/cuav_nora.md b/docs/ko/flight_controller/cuav_nora.md
index 1729b7e98e..ee99bfce15 100644
--- a/docs/ko/flight_controller/cuav_nora.md
+++ b/docs/ko/flight_controller/cuav_nora.md
@@ -5,7 +5,7 @@ PX4 does not manufacture this (or any) autopilot.
Contact the [manufacturer](https://www.cuav.net) for hardware support or compliance issues.
:::
-The [Nora](https://doc.cuav.net/flight-controller/x7/en/nora.html)® flight controller is a high-performance autopilot.
+The [Nora](https://doc.cuav.net/controller/x7/en/nora-plus.html)® flight controller is a high-performance autopilot.
산업용 드론과 대형 대형 드론에 적합합니다.
주로 상용 제조업체에 공급됩니다.
@@ -31,7 +31,7 @@ This flight controller is [manufacturer supported](../flight_controller/autopilo
- 고성능 프로세서
:::tip
-The manufacturer [CUAV Docs](https://doc.cuav.net/flight-controller/x7/en/nora.html) are the canonical reference for Nora.
+The manufacturer [CUAV Docs](https://doc.cuav.net/controller/x7/en/nora-plus.html) are the canonical reference for Nora.
가장 정확한 최신 정보를 포함하고 있습니다.
:::
@@ -76,14 +76,14 @@ When it runs PX4 firmware, only 8 PWM outputs work.
나머지 6 개의 PWM 포트는 여전히 조정중입니다(따라서 작성시 VOLT와 호환되지 않음).
:::
-## 구매처
+## Where to Buy {#store}
- [CUAV Store](https://store.cuav.net)<\br>
- [CUAV Aliexpress](https://www.aliexpress.com/item/4001042501927.html?gps-id=8041884&scm=1007.14677.110221.0&scm_id=1007.14677.110221.0&scm-url=1007.14677.110221.0&pvid=3dc0a3ba-fa82-43d2-b0b3-6280e4329cef&spm=a2g0o.store_home.promoteRecommendProducts_7913969.58)
## 배선
-[CUAV nora Wiring Quickstart](https://doc.cuav.net/flight-controller/x7/en/quick-start/quick-start-nora.html)
+[CUAV nora Wiring Quickstart](https://doc.cuav.net/controller/x7/en/quick-start/quick-start-nora.html)
## 크기와 핀배열
@@ -120,7 +120,7 @@ It is pre-built and automatically installed by _QGroundControl_ when appropriate
To [build PX4](../dev_setup/building_px4.md) for this target:
-```
+```sh
make cuav_nora_default
```
@@ -171,6 +171,6 @@ The complete set of supported configurations can be seen in the [Airframes Refer
## 추가 정보
-- [Quick start](https://doc.cuav.net/flight-controller/x7/en/quick-start/quick-start-nora.html)
+- [Quick start](https://doc.cuav.net/controller/x7/en/quick-start/quick-start-nora.html)
- [CUAV docs](https://doc.cuav.net/)
- [nora schematic](https://github.com/cuav/hardware/tree/master/X7_Autopilot)
diff --git a/docs/ko/flight_controller/cuav_pixhawk_v6x.md b/docs/ko/flight_controller/cuav_pixhawk_v6x.md
index b253c1a36d..1dcf6982f0 100644
--- a/docs/ko/flight_controller/cuav_pixhawk_v6x.md
+++ b/docs/ko/flight_controller/cuav_pixhawk_v6x.md
@@ -61,7 +61,7 @@ The Pixhawk® V6X is ideal for corporate research labs, academic research and co
- 16- PWM servo outputs
- 1 Dedicated R/C input for Spektrum / DSM and S.Bus with analog / PWM RSSI input
- 3 TELEM Ports（with full flow control）
-- 1 UART4(Seial and I2C)
+- 1 UART4(Serial and I2C)
- 2 GPS ports
- 1 full GPS plus Safety Switch Port(GPS1)
- 1 basic GPS port(with I2C,GPS2)
@@ -104,7 +104,7 @@ The Pixhawk® V6X is ideal for corporate research labs, academic research and co
-## 구매처
+## Where to Buy {#store}
Order from [CUAV](https://store.cuav.net/).
@@ -173,13 +173,11 @@ It is pre-built and automatically installed by _QGroundControl_ when appropriate
To [build PX4](../dev_setup/building_px4.md) for this target:
-```
+```sh
make px4_fmu-v6x_default
```
-
-
-## 디버그 포트
+## Debug Port {#debug_port}
The [PX4 System Console](../debug/system_console.md) and [SWD interface](../debug/swd_debug.md) run on the **FMU Debug** port.
diff --git a/docs/ko/flight_controller/cuav_v5.md b/docs/ko/flight_controller/cuav_v5.md
index 45867dd428..ed3719fbc0 100644
--- a/docs/ko/flight_controller/cuav_v5.md
+++ b/docs/ko/flight_controller/cuav_v5.md
@@ -1,149 +1,7 @@
-# CUAV v5 (단종)
+
@@ -93,7 +93,7 @@ This flight controller is perfect for people that is looking for a affordable an
- 기타 특성:
- Operating & storage temperature: -40 ~ 85°c
-## 구매처
+## Where to Buy {#store}
Order from [Holybro](https://holybro.com/products/pix32-v6).
@@ -156,13 +156,11 @@ It is pre-built and automatically installed by _QGroundControl_ when appropriate
To [build PX4](../dev_setup/building_px4.md) for this target:
-```
+```sh
make px4_fmu-v6c_default
```
-
-
-## 디버그 포트
+## Debug Port {#debug_port}
The [PX4 System Console](../debug/system_console.md) and [SWD interface](../debug/swd_debug.md) run on the **FMU Debug** port.
diff --git a/docs/ko/flight_controller/kakutef7.md b/docs/ko/flight_controller/kakutef7.md
index 09871f8b6b..72e2f77c50 100644
--- a/docs/ko/flight_controller/kakutef7.md
+++ b/docs/ko/flight_controller/kakutef7.md
@@ -1,142 +1,7 @@
+
diff --git a/docs/ko/frames_multicopter/kits.md b/docs/ko/frames_multicopter/kits.md
index c28d84a72f..1f2263854a 100644
--- a/docs/ko/frames_multicopter/kits.md
+++ b/docs/ko/frames_multicopter/kits.md
@@ -18,6 +18,7 @@ Kits generally do not include:
The following kits are currently available:
+- [Holybro X650 PX4 Development Kit](https://holybro.com/collections/x650-kits) (Pixhawk 6C/6X) ([Frame assembly guide](https://docs.holybro.com/drone-development-kit/x650-development-kit/download))
- [Holybro X500 v2 PX4 Development Kit](https://holybro.com/collections/x500-kits) (Pixhawk 6c) ([Build instructions](../frames_multicopter/holybro_x500v2_pixhawk6c.md))
- [Holybro S500 Kit v2](https://holybro.com/collections/s500/products/s500-v2-development-kit) (Pixhawk 6c)
- [Holybro QAV250 Kit](https://holybro.com/products/qav250-kit) (Pixhawk 6c)
@@ -27,7 +28,7 @@ The following kits are currently available:
## Build Guides
The build guides below show how to assemble a number of kits.
-Many kits vary only a little between revisions (for example, the new kit might simply upgrade the flight controller used, and is otherwise identical), so these are likely to be be useful for building the kits in the section above.
+Many kits vary only a little between revisions (for example, the new kit might simply upgrade the flight controller used, and is otherwise identical), so these are likely to be useful for building the kits in the section above.
- [Holybro X500 v2 (Pixhawk 6C)](../frames_multicopter/holybro_x500v2_pixhawk6c.md)
- [Holybro X500 v2 (Pixhawk 5X)](../frames_multicopter/holybro_x500V2_pixhawk5x.md) — Discontinued (v2 kit uses Pixhawk 6c)
diff --git a/docs/ko/frames_multicopter/omnicopter.md b/docs/ko/frames_multicopter/omnicopter.md
index 1c9267c486..bf895481e3 100644
--- a/docs/ko/frames_multicopter/omnicopter.md
+++ b/docs/ko/frames_multicopter/omnicopter.md
@@ -19,8 +19,8 @@ This build follows the original design from [Brescianini, Dario, and Raffaello D
You can select your own flight controller of choice, it just needs to support 8 DShot outputs.
:::
- - GPS: [ZED-F9P](https://gnss.store/zed-f9p-gnss-modules/105-elt0092.html)
- - [GPS helix antenna](https://gnss.store/gnss-rtk-multiband-antennas/28-elt0014.html)
+ - GPS: [ZED-F9P](https://gnss.store/products/elt0092)
+ - [GPS helix antenna](https://gnss.store/products/elt0014)
::: info
Any other GPS may work as well, however a helix antenna is expected to perform better for inverted flights.
@@ -34,8 +34,8 @@ This build follows the original design from [Brescianini, Dario, and Raffaello D
- Battery: we used a 6S 3300mAh LiPo. Make sure to check the dimensions so it fits the frame.
- Battery strap
- Frame:
- - Carbon square tube R 8mm X 7mm X 1000mm, e.g. [here on shop.swiss-composite.ch](https://shop.swiss-composite.ch/pi.php/Halbfabrikate/Rohre/Vierkant-Rohre/CFK-Vierkantrohr-8x8-7x7mm.html)
- - Carbon Rods R 3mm X 2mm X 1000mm, e.g. [here on shop.swiss-composite.ch](https://shop.swiss-composite.ch/pi.php/Halbfabrikate/Rohre/CFK-Rohre-pultrudiert-pullwinding/Carbon-Microtubes-100cm-x-20-3mm.html)
+ - Carbon square tube R 8mm X 7mm X 1000mm, e.g. [here on shop.swiss-composite.ch](https://www.shop.swiss-composite.ch/de/produkt/cfk-vierkantrohr-8x8-7x7mm)
+ - Carbon Rods R 3mm X 2mm X 1000mm, e.g. [here on shop.swiss-composite.ch](https://www.shop.swiss-composite.ch/de/produkt/carbon-microtubes-100cm-x-20-3mm)
- Required lengths:
- square tube: 8 pieces with length of 248mm
- rods: 12x328mm, 6x465mm
diff --git a/docs/ko/frames_plane/reptile_dragon_2.md b/docs/ko/frames_plane/reptile_dragon_2.md
index cf761afce0..f8751129d0 100644
--- a/docs/ko/frames_plane/reptile_dragon_2.md
+++ b/docs/ko/frames_plane/reptile_dragon_2.md
@@ -56,7 +56,7 @@ Key build features
- MS4525DO differential pressure module and pitot tube
-- [Caddx Vista FPV air unit](https://caddxfpv.com/collections/vista-kit)
+- [Caddx Vista FPV air unit](https://www.caddxfpv.com/collections/vista-kit)
- [Emax ES08MA ii](https://emaxmodel.com/products/emax-es08ma-ii-12g-mini-metal-gear-analog-servo-for-rc-model-robot-pwm-servo)
@@ -66,7 +66,7 @@ Key build features
- [5V BEC](https://www.readymaderc.com/products/details/rmrc-3a-power-regulator-5-to-6-volt-ubec)
-- [6s2p 18650 LiIon flight battery](https://www.upgradeenergytech.com/product-page/6s-22-2v-5600mah-30c-dark-lithium-liion-drone-battery) (select XT60 connector)
+- [6s2p 18650 LiIon flight battery](https://www.upgradeenergytech.com/products/red-6s1p-5000mah-molicel-p50b) (select XT60 connector)
- [Custom designed 3D printed parts](https://github.com/PX4/PX4-Autopilot/raw/main/docs/assets/airframes/fw/reptile_dragon_2/rd2_3d_printed_parts.zip)
- ARK6X carrier mount
@@ -97,7 +97,7 @@ The airplane needs some assembly out of the box.
Servos, wings, and the tail will need to be installed.
:::info
-For this portion of assembly, the instructions included with the kit should be sufficent, but some helpful tips are listed below.
+For this portion of assembly, the instructions included with the kit should be sufficient, but some helpful tips are listed below.
:::
### Gluing Foam
@@ -225,7 +225,7 @@ An alternative carrier board is the Holybro Pixhawk 5X carrier.
The carrier comes installed in a plastic case.
While the case does look nice, it is extra weight, so the carrier was removed from the case.
-Once removed from the case, the ARK6X was installed, and a protective cover fitted ontop.
+Once removed from the case, the ARK6X was installed, and a protective cover fitted on top.
@@ -353,7 +353,7 @@ For more information see [TBS Crossfire (CRSF) Telemetry](../telemetry/crsf_tele
### `msp_osd` Module
-The `msp_osd` module steams MSP telemetry to a selected serial port.
+The `msp_osd` module streams MSP telemetry to a selected serial port.
The Caddx Vista Air Unit supports listening to MSP telemetry and will show the received telemetry values in its OSD (on screen display).
1. In the PX4 board config tool, navigate to the `drivers` submenu, then scroll down to highlight `OSD`.
diff --git a/docs/ko/frames_plane/turbo_timber_evolution.md b/docs/ko/frames_plane/turbo_timber_evolution.md
index bf5b5988a0..31bdc80f00 100644
--- a/docs/ko/frames_plane/turbo_timber_evolution.md
+++ b/docs/ko/frames_plane/turbo_timber_evolution.md
@@ -50,7 +50,7 @@ Key Build Features:
- MS4525DO differential pressure module and pitot tube
-- [Caddx Vista FPV air unit](https://caddxfpv.com/collections/vista-kit)
+- [Caddx Vista FPV air unit](https://www.caddxfpv.com/collections/vista-kit)
- [DJI FPV Goggles](https://www.dji.com/fpv)
@@ -74,7 +74,7 @@ Servos and linkages have already been installed, and the only real remaining wor
For this portion of the assembly, simply follow the manual.
:::info
-[Some reports](https://www.rcgroups.com/forums/showthread.php?3904021-NEW-E-flite-Turbo-Timber-Evolution-1-5m-%C2%96-Smartest-Most-Capable-Durable-Timber-Yet/page50) have indicated that the stock ESC bundled with the airplane has an issue with overheating.
+[Some reports](https://www.rcgroups.com/forums/showthread.php?3904021-NEW-E-flite-Turbo-Timber-Evolution-1-5m/page50) have indicated that the stock ESC bundled with the airplane has an issue with overheating.
As this build will be especially heavy, and therefore likely demand higher average power from the ESC, the stock 60A ESC was replaced with an 80A Turnigy PLUSH-32 during testing.
The stock motor was also replaced with a [higher power motor](https://hobbyking.com/en_us/turnigy-aerodrive-sk3-3548-840kv-brushless-outrunner-motor.html).
@@ -90,7 +90,7 @@ A long M3 nylon screw and a washer on the underside, followed by a washer and st
-
+
## Pitot Pod
@@ -150,7 +150,7 @@ Power for the servo and lighting will be provided by the "BEC" power supply in t
The TTE is very flexible when it comes to battery options.
I use both a 3.6Ah 4S Turnigy pack as well as a Upgrade Energy 4s2p liion pack.
-While the 3.6Ah LiPo is inexpensive, nearly twice the flight time (24 minutes vs 12 minutes) can be acheived with the Upgrade Energy Liion pack.
+While the 3.6Ah LiPo is inexpensive, nearly twice the flight time (24 minutes vs 12 minutes) can be achieved with the Upgrade Energy Liion pack.
@@ -177,10 +177,10 @@ Similarly, a JST PH to std spaced headers adapter was made, and it was also left
#### 무선 수신기
-A custom cable was made to connect the ExpressLRS RX ([RC Reciever](../getting_started/rc_transmitter_receiver.md)) to the Pixhawk 4 Mini.
+A custom cable was made to connect the ExpressLRS RX ([RC Receiver](../getting_started/rc_transmitter_receiver.md)) to the Pixhawk 4 Mini.
Because the Pixhawk 4 Mini has limited uarts, the RX was connected to RC input which does not have a TX pin.
-This means that the RX will only send control data to the FCU but telemtry cannot be sent to the RX from the FCU.
+This means that the RX will only send control data to the FCU but telemetry cannot be sent to the RX from the FCU.
Heatshrink was used to secure the dupont connector of the cable such that it cannot back out off the headers of the ExpressLRS RX.
#### FPV Pod & Airspeed Cable
@@ -189,7 +189,7 @@ Another custom cable was made to connect the Caddx Vista FPV transmitter to the
A Molex microfit was added close to the Vista so that it could be easily disconnected without needing to gain access to the Pixhawk.
As the name implies, the `UART/I2C B` port provides both a UART and I2C interface.
This port is split with the custom cable and one side provides power and data to the I2C airspeed sensor, while the other side provides power and UART TX/RX to the Caddx Vista.
-From the UART/I2C B port, 5V, GND, and I2C SCL/SDA, are connected to the I2C airspeed sensor, while just serial RX and TX are connected to the Caddx Vista (Ground is provided the seperate battery power/gnd leads for the Vista)
+From the UART/I2C B port, 5V, GND, and I2C SCL/SDA, are connected to the I2C airspeed sensor, while just serial RX and TX are connected to the Caddx Vista (Ground is provided the separate battery power/gnd leads for the Vista)
The [msp_osd](../modules/modules_driver.md#msp-osd) module is used to stream telemetry to the Caddx Vista which can be seen on the DJI Goggles with the "custom OSD" feature enabled.
@@ -204,7 +204,7 @@ Heatshrink was used to electrically insulate the bare board and the radio was in
Overall, this build was a success.
-Even with the added weight of the Pixhawk 4 Mini installation, the airplane balances well and has plenty of power to retain its original STOL characterisitics.
+Even with the added weight of the Pixhawk 4 Mini installation, the airplane balances well and has plenty of power to retain its original STOL characteristics.
PX4 is easily capable of stabilizing the airplane and fine tuning of the rate loops were accomplished using [fixed-wing autotuning](../config/autotune_fw.md).
The results of tuning can be found in the [parameter file linked below](#parameter-file).
diff --git a/docs/ko/frames_plane/wing_wing_z84.md b/docs/ko/frames_plane/wing_wing_z84.md
index f76275ae14..298dfdaf07 100644
--- a/docs/ko/frames_plane/wing_wing_z84.md
+++ b/docs/ko/frames_plane/wing_wing_z84.md
@@ -33,7 +33,7 @@ Any small (>=12A) ESC will do:
- FrSky D4R-II 수신기 또는 동급 (설명서에 따라 PPM 합계 출력으로 점퍼됨)
- [Mini telemetry set](../flight_controller/pixfalcon.md#availability) for Holybro pix32
- [Digital airspeed sensor](../flight_controller/pixfalcon.md#availability) for Holybro pix32 / Pixfalcon
-- 1800 mAh 2S LiPo Battery - e.g. [Team Orion 1800mAh 7.4V 50C 2S1P](https://teamorion.com/en/batteries-en/lipo/soft-case/team-orion-lipo-1800-2s-7-4v-50c-xt60-en/)
+- 1800 mAh 2S LiPo Battery - e.g. Team Orion 1800mAh 7.4V 50C 2S1P with XT 60 plug.
### 권장 예비 부품
diff --git a/docs/ko/frames_sub/bluerov2.md b/docs/ko/frames_sub/bluerov2.md
index 49c4870366..ae43036907 100644
--- a/docs/ko/frames_sub/bluerov2.md
+++ b/docs/ko/frames_sub/bluerov2.md
@@ -2,21 +2,25 @@
@@ -29,6 +33,15 @@ The vehicle will then match the configuration documented in the [Airframe Refere
- **MAIN7:** motor 7 CCW, stern starboard vertical, propeller CW
- **MAIN8:** motor 8 CCW, stern port vertical, propeller CCW
+## Manual Modes
+
+| Mode | 설명 |
+| -------- | ---------------------------------------------------------------------------------------------------------------------------------------------------- |
+| Manual | Direct manual control of yaw and thrust. |
+| Acro | Manual control of yaw/thrust, but keeps roll/pitch zero |
+| Altitude | Manual control of x/y thrust and yaw. Control of height with PID, manually controlled by user. Keeps roll/pitch zero |
+| Position | Controls x/y/z and yaw. Manually controlled by user. Keeps roll/pitch zero |
+
## 기체 설정
BlueROV2 does not come with PX4 installed.
diff --git a/docs/ko/frames_vtol/tailsitter.md b/docs/ko/frames_vtol/tailsitter.md
index 2bb1d4c4d5..8ce9063e61 100644
--- a/docs/ko/frames_vtol/tailsitter.md
+++ b/docs/ko/frames_vtol/tailsitter.md
@@ -91,7 +91,7 @@ This section contains videos that are specific to Tailsitter VTOL (videos that a
+
+## 개요
+
+_Joystick_ setups use QGroundControl to encode the control information from a "standard" computer gaming joystick into [MAVLink messages](https://mavlink.io/en/services/manual_control.html) that are sent to the vehicle over the (shared) telemetry radio channel.
+They are often used in integrated GCS/manual control systems because it is cheaper and easier to integrate a joystick than a separate radio system.
+
+Joysticks are suitable for most applications provided your telemetry channel has a high enough bandwidth/low latency.
+They are perfect for flying the PX4 simulator, because you can plug them directly into your ground control computer and start flying.
+
+_RC systems_ use a dedicated ground-based radio transmitter and vehicle-based receiver for sending control information.
+They offer lower latency than Joysticks, and are very highly recommended when first tuning/testing a new frame design, when flying racers/acrobatically, and in other cases where low latency is important.
+They can also be useful as a robust backup link for safety.
+Note RC systems usually require significantly more configuration and calibration, much of which may be brand or model-specific.
+
+:::info
+PX4 does not _require_ a manual control system for autonomous flight modes.
+:::
+
+## PX4 설정
+
+:::tip
+This section explains how to configure PX4 to use and prioritise various manual control sources (other configuration is covered in the guides for each type of manual control).
+:::
+
+If you only have one manual control system, either RC or Joystick, then by default no manual control selection is required.
+In this case PX4 locks to the first valid manual control source it detects and uses that source until the vehicle is rebooted.
+
+If you have multiple control sources, such as an RC system and/or one or more Joysticks, then you can use the [COM_RC_IN_MODE](../advanced_config/parameter_reference.md#COM_RC_IN_MODE) parameter to determine which source is active, specifying selection priorities and fallback behavior ([parameters can be set](../advanced_config/parameters.md#finding-a-parameter) using QGC):
+
+- `0`: RC only.
+- `1`: MAVLink only.
+- `2`: RC or MAVLink with fallback (switches if current source becomes invalid).
+- `3`: RC or MAVLink keep first (locks to the first valid source until reboot).
+- `4`: Disable manual control (ignores all sources).
+- `5`: RC priority, then MAVLink (lower instance before higher) — `RC > MAVLink 1 > MAVLink 2`
+- `6`: MAVLink priority (lower instance before higher), then RC — `MAVLink 1 > MAVLink 2 > RC`
+- `7`: RC priority, then MAVLink (higher instance before lower) — `RC > MAVLink 2 > MAVLink 1`
+- `8`: MAVLink priority (higher instance before lower), then RC — `MAVLink 2 > MAVLink 1 > RC`
+
+The [MAVLink instance](../peripherals/mavlink_peripherals.md#mavlink-instances) refers to an instance assigned to a serial port, such as [MAV_0_CONFIG](../advanced_config/parameter_reference.md#MAV_0_CONFIG).
+
+참고:
+
+- RC checks are run for any option that uses RC (so not for `MAVLink only` or `Disable manual control`).
+- When using priority sources, sources are evaluated as soon as they become valid and may trigger an immediate switch (if higher priority than the currently active source).
+- A [Manual Control Loss Failsafe](../config/safety.md#manual-control-loss-failsafe) is triggered when none of the manual control inputs allowed by the `COM_RC_IN_MODE` mode are available for a time that is greater than the RC Loss Timeout.
+ As long as there is a fallback input source available, the failsafe is not triggered.
+
+## See Also
+
+- [Radio Control (RC)](../getting_started/rc_transmitter_receiver.md)
+- [Joysticks](../config/joystick.md)
diff --git a/docs/ko/config/radio.md b/docs/ko/config/radio.md
index 1ca698c54a..23cbbb80d6 100644
--- a/docs/ko/config/radio.md
+++ b/docs/ko/config/radio.md
@@ -1,10 +1,12 @@
# Radio Control (RC) Setup
-The _Radio Setup_ screen is used to configure the mapping of your RC controller's main attitude control sticks (roll, pitch, yaw, throttle) to channels, and to calibrate the minimum, maximum, trim and reverse settings for all other transmitter controls/RC channels.
+The _Radio Setup_ screen is used to configure the mapping of your [RC controller's](../getting_started/rc_transmitter_receiver.md) main attitude control sticks (roll, pitch, yaw, throttle) to channels, and to calibrate the minimum, maximum, trim and reverse settings for all other transmitter controls/RC channels.
:::info
-A [Joystick](../config/joystick.md) can be used instead of RC for manual control.
-The [COM_RC_IN_MODE](../advanced_config/parameter_reference.md#COM_RC_IN_MODE) parameter [can be set](../advanced_config/parameters.md) to define what kind of manual controller(s) are enabled.
+A [Joystick](../config/joystick.md) can also be used for [Manual Control](../config/manual_control.md).
+
+By default PX4 will latch the first valid controller it discovers and use it until the vehicle reboots.
+If you have multiple controllers and you want to define their priority see [Manual Control > PX4 Configuration](../config/manual_control.md#px4-configuration).
:::
## 수신기 바인딩
diff --git a/docs/ko/config/safety.md b/docs/ko/config/safety.md
index afa785d204..e70f6454c2 100644
--- a/docs/ko/config/safety.md
+++ b/docs/ko/config/safety.md
@@ -111,19 +111,17 @@ There are several other "battery related" failsafe mechanisms that may be config
## Manual Control Loss Failsafe
-The manual control loss failsafe may be triggered if the connection to the [RC transmitter](../getting_started/rc_transmitter_receiver.md) or [joystick](../config/joystick.md) is lost, and there is no fallback.
-If using an [RC transmitter](../getting_started/rc_transmitter_receiver.md) this is triggered if the RC [transmitter link is lost](../getting_started/rc_transmitter_receiver.md#set-signal-loss-behaviour).
-If using [joysticks](../config/joystick.md) connected over a MAVLink data link, this is triggered if the joysticks are disconnected or the data link is lost.
-
-:::info
-PX4 and the receiver may also need to be configured in order to _detect RC loss_: [Radio Setup > RC Loss Detection](../config/radio.md#rc-loss-detection).
-:::
+A [Manual Control Loss Failsafe](../config/safety.md#manual-control-loss-failsafe) is triggered after a [manual control loss timeout](#COM_RC_LOSS_T) in which none of the configured [Manual Controllers](../config/manual_control.md) are available.
The QGCroundControl Safety UI allows you to set the [failsafe action](#failsafe-actions) and [manual control loss timeout](#COM_RC_LOSS_T).
Users that want to disable this failsafe in specific modes can do so using the parameter [COM_RCL_EXCEPT](#COM_RCL_EXCEPT).
+:::info
+PX4 and the receiver may also need to be configured in order to _detect RC loss_: [Radio Setup > RC Loss Detection](../config/radio.md#rc-loss-detection).
+:::
+
Additional (and underlying) parameter settings are shown below.
| 매개변수 | 설정 | 설명 |
@@ -181,17 +179,22 @@ Due to the inherent danger of this, this function is disabled using [CBRK_FLIGHT
| Preemptive geofence triggering | [GF_PREDICT](../advanced_config/parameter_reference.md#GF_PREDICT) | (Experimental) Trigger geofence if current motion of the vehicle is predicted to trigger the breach (rather than late triggering after the breach). |
| Circuit breaker for flight termination | [CBRK_FLIGHTTERM](../advanced_config/parameter_reference.md#CBRK_FLIGHTTERM) | 비행 종료 작업을 활성화/비활성화합니다 (기본적으로 비활성화 됨). |
-## Position (GNSS) Loss Failsafe
+## Position Estimation Failsafes
+
+This section describes failsafes related to the quality of the vehicle's position estimate.
+
+### Position Loss Failsafe
The _Position Loss Failsafe_ is triggered if the quality of the PX4 position estimate falls below acceptable levels (this might be caused by GPS loss) while in a mode that requires an acceptable position estimate.
-The sections below cover first the trigger and then the failsafe action taken by the controller.
### Position Loss Failsafe Trigger
-There are basically two mechanisms in PX4 to trigger position failsafes:
+The position loss failsafe triggers if the position estimate becomes _invalid_. There are two mechanisms in PX4 to invalidate the position estimate:
-- A timeout since the last sensor data was fused that provides direct speed or horizontal position measurements. Sensors that fall into that category are: GNSS, optical flow, airspeed, VIO, auxiliary global position.
-- The estimated horizontal position accuracy exceeds a certain threshold. This check is only done on hovering systems (rotary wing vehicles or VTOLs in hover phase).
+- A timeout since the last sensor data was fused that provides direct speed or horizontal position measurements.
+ - Sensors that fall into that category are: GNSS, optical flow, airspeed, VIO, auxiliary global position.
+- The estimated horizontal position inaccuracy exceeds the threshold [COM_POS_LOW_EPH](../advanced_config/parameter_reference.md#COM_POS_LOW_EPH)
+ - This check is only done on hovering systems (rotary-wing vehicles or VTOLs in hover phase). For fixed-wing vehicles, refer to the [Position Accuracy Low](#position-accuracy-low-failsafe) section.
The relevant parameters shown below.
@@ -207,14 +210,24 @@ Multicopters will switch to [Altitude mode](../flight_modes_mc/altitude.md) if a
Fixed-wing planes, and VTOLs not configured to land in hover ([NAV_FORCE_VT](../advanced_config/parameter_reference.md#NAV_FORCE_VT)), have a parameter ([FW_GPSF_LT](../advanced_config/parameter_reference.md#FW_GPSF_LT)) that defines how long they will loiter (circle with a constant roll angle ([FW_GPSF_R](../advanced_config/parameter_reference.md#FW_GPSF_R)) at the current altitude) after losing position before attempting to land.
If VTOLs have are configured to switch to hover for landing ([NAV_FORCE_VT](../advanced_config/parameter_reference.md#NAV_FORCE_VT)) then they will first transition and then descend.
-The relevant parameters for all vehicles shown below.
+The relevant parameters are:
-Parameters that only affect Fixed-wing vehicles:
+| 매개변수 | 설명 |
+| ----------------------------------------------------------------------------------------------------------------------------------------- | --------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- |
+| [FW_GPSF_LT](../advanced_config/parameter_reference.md#FW_GPSF_LT) | Fixed-wing only: Loiter time (waiting at current altitude for position estimation recovery before starting to descend). 비활성화 하려면 0으로 설정하십시오. |
+| [FW_GPSF_R](../advanced_config/parameter_reference.md#FW_GPSF_R) | 선회 비행시 고정 롤/뱅크 각도. |
+| [NAV_FORCE_VT](../advanced_config/parameter_reference.md#NAV_FORCE_VT) | If true, force VTOL takeoff and landing, even in `Descend` failsafe. |
-| 매개변수 | 설명 |
-| ----------------------------------------------------------------------------------------------------------------------------------- | -------------------------------------------------------------------------------------------------------------------------------------------------------------- |
-| [FW_GPSF_LT](../advanced_config/parameter_reference.md#FW_GPSF_LT) | Loiter time (waiting for GPS recovery before it goes into land or flight termination). 비활성화 하려면 0으로 설정하십시오. |
-| [FW_GPSF_R](../advanced_config/parameter_reference.md#FW_GPSF_R) | 선회 비행시 고정 롤/뱅크 각도. |
+### Position Accuracy Low Failsafe
+
+In Fixed-wing, the position estimate is never strictly invalidated as long as we have a horizontal aiding source, such as an airspeed sensor. In that case, a separate failsafe can be configured that triggers if the position estimate inacuraccy exceeds the threshold [COM_POS_LOW_EPH](../advanced_config/parameter_reference.md#COM_POS_LOW_EPH). The failsafe action is taken if the vehicle is in mission or hold mode, otherwise it is only a warning. The relevant parameters are:
+
+| 매개변수 | 설명 |
+| ----------------------------------------------------------------------------------------------------------------------------------------------------------------------- | -------------------------------------------------------------------------------------------------------------------------------------------------- |
+| [COM_POS_LOW_EPH](../advanced_config/parameter_reference.md#COM_POS_LOW_EPH) | Position inaccuracy threshold above which COM_POS_LOW_ACT is taken. |
+| [COM_POS_LOW_ACT](../advanced_config/parameter_reference.md#COM_POS_LOW_ACT) | Failsafe action taken when position inaccuracy is above configured threshold. |
+
+Note that if there is no horizontal aiding source anymore, the position estimate is invalidated after `EKF2_NOAID_TOUT`, and the standard position loss failsafe applies.
## 오프 보드 안전 장치
@@ -261,7 +274,7 @@ The parameters that control when the quad-chute will trigger are listed in the t
## High Wind Failsafe
-The high wind failsafe can trigger a warning and/or other mode change when the wind speed exceeds the warning and maximum wind-speed threshhold values.
+The high wind failsafe can trigger a warning and/or other mode change when the wind speed exceeds the warning and maximum wind-speed threshold values.
The relevant parameters are listed in the table below.
| 매개변수 | 설명 |
@@ -315,8 +328,8 @@ The failure detector can be configured to detect a motor failure while armed (an
| ----------------------------------------------------------------------------------------------------------------------------------------------------------------------- | --------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- |
| [FD_ACT_EN](../advanced_config/parameter_reference.md#FD_ACT_EN) | Enable/disable the motor failure trigger completely. |
| [FD_ACT_MOT_THR](../advanced_config/parameter_reference.md#FD_ACT_MOT_THR) | Minimum normalized [0,1] motor command below which motor under current is ignored. |
-| [FD_ACT_MOT_C2T](../advanced_config/parameter_reference.md#FD_ACT_MOT_C2T) | Scale between normalized [0,1] motor command and expected minimally reported currrent when the rotor is healthy. |
-| [FD_ACT_MOT_TOUT](../advanced_config/parameter_reference.md#FD_ACT_MOT_TOUT) | Time in miliseconds for which the under current detection condition needs to stay true. |
+| [FD_ACT_MOT_C2T](../advanced_config/parameter_reference.md#FD_ACT_MOT_C2T) | Scale between normalized [0,1] motor command and expected minimally reported current when the rotor is healthy. |
+| [FD_ACT_MOT_TOUT](../advanced_config/parameter_reference.md#FD_ACT_MOT_TOUT) | Time in milliseconds for which the under current detection condition needs to stay true. |
| [CA_FAILURE_MODE](../advanced_config/parameter_reference.md#CA_FAILURE_MODE) | Configure to not only warn about a motor failure but remove the first motor that detects a failure from the allocation effectiveness which turns off the motor and tries to operate the vehicle without it until disarming the next time. |
### 외부 자동 작동 시스템 (ATS)
diff --git a/docs/ko/config_mc/pid_tuning_guide_multicopter_basic.md b/docs/ko/config_mc/pid_tuning_guide_multicopter_basic.md
index c17c455ddd..b6569ea0c4 100644
--- a/docs/ko/config_mc/pid_tuning_guide_multicopter_basic.md
+++ b/docs/ko/config_mc/pid_tuning_guide_multicopter_basic.md
@@ -13,7 +13,7 @@ For example, different ESCs or motors change the optimal tuning gains.
## 소개
-PX4 uses **P**roportional, **I**ntegral, **D**erivative (PID) controllers (these are the most widespread control technique).
+PX4 uses **P**roportional, **I**integral, **D**erivative (PID) controllers (these are the most widespread control technique).
The _QGroundControl_ **PID Tuning** setup provides real-time plots of the vehicle setpoint and response curves.
The goal of tuning is to set the P/I/D values such that the _Response_ curve matches the _Setpoint_ curve as closely as possible (i.e. a fast response without overshoots).
diff --git a/docs/ko/config_rover/attitude_tuning.md b/docs/ko/config_rover/attitude_tuning.md
index b2efc4d5c7..cf176e587f 100644
--- a/docs/ko/config_rover/attitude_tuning.md
+++ b/docs/ko/config_rover/attitude_tuning.md
@@ -16,7 +16,7 @@ Configure the following [parameters](../advanced_config/parameters.md) in QGroun
Put the rover into stabilized mode and move the left stick of your controller up to drive forwards.
Disarm the rover and from the flight log plot the `measured_yaw` and the `adjusted_yaw_setpoint` from the [RoverAttitudeStatus](../msg_docs/RoverAttitudeStatus.md) message over each other.
Increase/Decrease the parameter until you are satisfied with the setpoint tracking.
- If you observe a steady state error in the yaw setpoint increase the the integrator of the rate controller: [RO_YAW_RATE_I](../advanced_config/parameter_reference.md#RO_YAW_RATE_I) .
+ If you observe a steady state error in the yaw setpoint increase the integrator of the rate controller: [RO_YAW_RATE_I](../advanced_config/parameter_reference.md#RO_YAW_RATE_I) .
:::
@@ -30,7 +30,7 @@ The attitude controller uses the following structure:
-The rate and attitude controllers are cascaded, therefor we only require one integrator in the structure to eliminate steady state errors.
+The rate and attitude controllers are cascaded, therefore we only require one integrator in the structure to eliminate steady state errors.
We placed the integrator in the rate controller since it can run without the attitude controller but not the other way around.
## Parameter Overview
diff --git a/docs/ko/config_rover/basic_setup.md b/docs/ko/config_rover/basic_setup.md
index 53b9e2ddb1..f9bcc3a665 100644
--- a/docs/ko/config_rover/basic_setup.md
+++ b/docs/ko/config_rover/basic_setup.md
@@ -138,7 +138,7 @@ In [Manual mode](../flight_modes_rover/manual.md#manual-mode) we can additionall
- Differential Rover: $r=$ [RD_YAW_STK_GAIN](#RD_YAW_STK_GAIN), which enables adjusting the slope of the input mapping. This leads to a normalized steering input $\hat{\delta} = \delta \cdot r \in$ [-[RD_YAW_STK_GAIN](#RD_YAW_STK_GAIN), [RD_YAW_STK_GAIN](#RD_YAW_STK_GAIN)].
- Mecanum Rover: $r=$ [RM_YAW_STK_GAIN](#RM_YAW_STK_GAIN), which enables adjusting the slope of the input mapping. This leads to a normalized steering input $\hat{\delta} = \delta \cdot r \in$ [-[RM_YAW_STK_GAIN](#RM_YAW_STK_GAIN), [RM_YAW_STK_GAIN](#RM_YAW_STK_GAIN)].
-This scaling is useful to limit the normalized steering setpoint, if it is too aggresive for your rover in manual mode.
+This scaling is useful to limit the normalized steering setpoint, if it is too aggressive for your rover in manual mode.
You can experiment with the relationships graphically using the [PX4 SuperExpo Rover calculator](https://www.desmos.com/calculator/gwm8lrlanx).
diff --git a/docs/ko/config_rover/index.md b/docs/ko/config_rover/index.md
index aff8b6389a..960fedc2f4 100644
--- a/docs/ko/config_rover/index.md
+++ b/docs/ko/config_rover/index.md
@@ -39,7 +39,7 @@ make px4_fmu-v6x_rover
Note that configuration targets are constructed with the format "VENDOR_MODEL_VARIANT".
-The built firmware can be installed as custom firmware, as shown above in in [Flashing the Rover Build](#flashing-the-rover-build).
+The built firmware can be installed as custom firmware, as shown above in [Flashing the Rover Build](#flashing-the-rover-build).
:::info
You can also enable the modules in default builds by adding these lines to your [board configuration](../hardware/porting_guide_config.md) (e.g. for fmu-v6x you might add them to [`main/boards/px4/fmu-v6x/default.px4board`](https://github.com/PX4/PX4-Autopilot/blob/main/boards/px4/fmu-v6x/default.px4board)):
diff --git a/docs/ko/config_rover/rate_tuning.md b/docs/ko/config_rover/rate_tuning.md
index 47ee11cbf9..2b317b4631 100644
--- a/docs/ko/config_rover/rate_tuning.md
+++ b/docs/ko/config_rover/rate_tuning.md
@@ -11,7 +11,7 @@ Configure the following [parameters](../advanced_config/parameters.md) in QGroun
1. [RO_YAW_RATE_LIM](#RO_YAW_RATE_LIM): Maximum yaw rate you want to allow for your rover.
:::tip
- Limiting the yaw rate is necessary if the rover is prone rolling over, loosing traction at high speeds or if passenger comfort is important.
+ Limiting the yaw rate is necessary if the rover is prone rolling over, losing traction at high speeds or if passenger comfort is important.
Small rovers especially can be prone to rolling over when steering aggressively at high speeds.
If this is the case:
diff --git a/docs/ko/config_rover/velocity_tuning.md b/docs/ko/config_rover/velocity_tuning.md
index 8e7f44f954..6b91165ed2 100644
--- a/docs/ko/config_rover/velocity_tuning.md
+++ b/docs/ko/config_rover/velocity_tuning.md
@@ -60,7 +60,7 @@ To tune the velocity controller configure the following [parameters](../advanced
## Manual Position Mode Parameters
-These steps are only necessary if you are tuning/want to unlock the manual [Position mode](../flight_modes_rover/manual.md#position-mode). Othwerwise, you can continue with [position tuning](position_tuning.md) where these same parameters will also be configured.
+These steps are only necessary if you are tuning/want to unlock the manual [Position mode](../flight_modes_rover/manual.md#position-mode). Otherwise, you can continue with [position tuning](position_tuning.md) where these same parameters will also be configured.
1. [PP_LOOKAHD_GAIN](#PP_LOOKAHD_GAIN): When driving in a straight line (right stick centered) position mode leverages the same path following algorithm used in [auto modes](../flight_modes_rover/auto.md) called [pure pursuit](position_tuning.md#pure-pursuit-guidance-logic-info-only) to achieve the best possible straight line driving behaviour.
This parameter determines how aggressive the controller will steer towards the path.
@@ -109,7 +109,7 @@ The speed controller uses the following structure:
The feed forward mapping is done by interpolating the speed setpoint from [-[RO_MAX_THR_SPEED](../advanced_config/parameter_reference.md#RO_MAX_THR_SPEED), [RO_MAX_THR_SPEED](../advanced_config/parameter_reference.md#RO_MAX_THR_SPEED)] to [-1, 1].
-For ackermann and differential rovers the bearing is aligned with the vehicle yaw. Therefor the bearing is simply sent as a yaw setpoint to the [yaw controller](attitude_tuning.md#attitude-controller-structure-info-only) and the speed setpoint is always defined in body x direction.
+For ackermann and differential rovers the bearing is aligned with the vehicle yaw. Therefore the bearing is simply sent as a yaw setpoint to the [yaw controller](attitude_tuning.md#attitude-controller-structure-info-only) and the speed setpoint is always defined in body x direction.
For mecanum vehicles, the bearing and yaw are decoupled. The direction is controlled by splitting the velocity vector into one speed component in body x direction and one in body y direction.
Both these setpoint are then sent to their own closed loop speed controllers.
diff --git a/docs/ko/config_vtol/vtol_ice_shedding.md b/docs/ko/config_vtol/vtol_ice_shedding.md
index ae719602af..76b084333b 100644
--- a/docs/ko/config_vtol/vtol_ice_shedding.md
+++ b/docs/ko/config_vtol/vtol_ice_shedding.md
@@ -6,7 +6,7 @@ Ice shedding is a feature that periodically spins unused motors in fixed-wing
flight, to break off any ice that is starting to build up in the motors while it
is still feasible to do so.
-It is configured by the paramter `CA_ICE_PERIOD`. When it is 0, the feature is
+It is configured by the parameter `CA_ICE_PERIOD`. When it is 0, the feature is
disabled, when it is above 0, it sets the duration of the ice shedding cycle in
seconds. In each cycle, the rotors are spun for two seconds at a motor output of
0.01.
diff --git a/docs/ko/config_vtol/vtol_quad_configuration.md b/docs/ko/config_vtol/vtol_quad_configuration.md
index d442eda0b6..88af569268 100644
--- a/docs/ko/config_vtol/vtol_quad_configuration.md
+++ b/docs/ko/config_vtol/vtol_quad_configuration.md
@@ -95,7 +95,7 @@ It should be set to a value which ensures that the vehicle reaches a high enough
[VT_TRANS_TIMEOUT](../advanced_config/parameter_reference.md#VT_TRANS_TIMEOUT)
This specifies the upper limit for the duration of the front transition. If the vehicle has not reached the transition airspeed after this time, then the transition will be aborted and a [Quadchute](../config/safety.md#quad-chute-failsafe) event will be triggered.
-:::note
+::: info
Additionally, if an airspeed sensor is present, the transition will also be aborted if the airspeed has not reached [VT_ARSP_BLEND](../advanced_config/parameter_reference.md#VT_ARSP_BLEND) after the openloop transition time [VT_F_TR_OL_TM](../advanced_config/parameter_reference.md#VT_F_TR_OL_TM) has elapsed. This checks is used to avoid a scenario where the vehicle gains excessive speed when the airspeed sensor is faulty.
:::
diff --git a/docs/ko/contribute/dev_call.md b/docs/ko/contribute/dev_call.md
index ff5ed0e045..b980479813 100644
--- a/docs/ko/contribute/dev_call.md
+++ b/docs/ko/contribute/dev_call.md
@@ -7,7 +7,7 @@ const { site } = useData();
-
This page may be out out of date. See the latest version.
+This page may be out of date. See the latest version.
-
This page may be out out of date. See the latest version.
+This page may be out of date. See the latest version.
-
This page may be out out of date. See the latest version.
+This page may be out of date. See the latest version.
Digikey: [BM06B-GHS-TBT(LF)(SN)(N)][bm06b-ghs-tbt(lf)(sn)(n)] (vertical mount), [SM06B-GHS-TBT(LF)(SN)(N)][sm06b-ghs-tbt(lf)(sn)(n)] (side mount) | -| [CUAV V5nano](../flight_controller/cuav_v5_nano.md#debug_port) | 6-pin JST GH
Digikey: [BM06B-GHS-TBT(LF)(SN)(N)][bm06b-ghs-tbt(lf)(sn)(n)] (vertical mount), [SM06B-GHS-TBT(LF)(SN)(N)][sm06b-ghs-tbt(lf)(sn)(n)] (side mount) | -| [3DR Pixhawk](../flight_controller/pixhawk.md#swd-port) | ARM 10-pin JTAG Connector (also used for FMUv2 boards including: _mRo Pixhawk_, _HobbyKing HKPilot32_). | +| 오토파일럿 | 디버그 포트 | +| :------------------------------------------------------------------------------------------------------ | :----------------------------------------------------------------------- | +| [Holybro Pixhawk 6X-RT](../flight_controller/pixhawk6x-rt.md#debug_port) (FMUv6X-RT) | [Pixhawk Debug Full](#pixhawk-debug-full) | +| [Holybro Pixhawk 6X](../flight_controller/pixhawk6x.md#debug_port) (FMUv6x) | [Pixhawk Debug Full](#pixhawk-debug-full) | +| [Holybro Pixhawk 5X](../flight_controller/pixhawk5x.md#debug_port) (FMUv5x) | [Pixhawk Debug Full](#pixhawk-debug-full) | +| [Holybro Durandal](../flight_controller/durandal.md#debug-port) | [Pixhawk Debug Mini](#pixhawk-debug-mini) | +| [Holybro Pixhawk 4](../flight_controller/pixhawk4.md#debug_port) (FMUv5) | [Pixhawk Debug Mini](#pixhawk-debug-mini) | +| [Holybro Pixhawk 6X Pro](../flight_controller/pixhawk6x_pro.md#debug-port) | [Pixhawk Debug Full](#pixhawk-debug-full) | +| [Holybro Pixhawk 6C](../flight_controller/pixhawk6c.md#debug_port) | [Pixhawk Debug Full](#pixhawk-debug-full) | +| [Holybro Pixhawk 6C Mini](../flight_controller/pixhawk6c_mini.md#debug_port) | [Pixhawk Debug Mini](#pixhawk-debug-mini) | +| [Holybro Pix32 v6](../flight_controller/holybro_pix32_v6.md#debug_port) | [Pixhawk Debug Full](#pixhawk-debug-full) | +| [Holybro Pix32 v5](../flight_controller/holybro_pix32_v5.md#debug-port) | [Pixhawk Debug Mini](#pixhawk-debug-mini) | +| [Holybro Kakute H7](../flight_controller/kakuteh7.md#debug-port) | SWD pads and system console | +| [Holybro Kakute H7 mini](../flight_controller/kakuteh7mini.md#debug-port) | SWD pads and system console | +| [Holybro Kakute H7 V2](../flight_controller/kakuteh7v2.md#debug-port) | SWD pads and system console | +| [CUAV V5+](../flight_controller/cuav_v5_plus.md#debug-port) | Custom port but comes with adaptor cable | +| [CUAV V5nano](../flight_controller/cuav_v5_nano.md#debug_port) | Custom port but comes with adaptor cable | +| [CUAV Pixhawk V6X](../flight_controller/cuav_pixhawk_v6x.md#debug_port) | [Pixhawk Debug Full](#pixhawk-debug-full) | +| [CUAV X25-SUPER](../flight_controller/cuav_x25-super.md#debug_port) | [Pixhawk Debug Mini] | +| [CUAV X25-EVO](../flight_controller/cuav_x25-evo.md#debug_port) | [Pixhawk Debug Mini] | +| [CUAV Nora](../flight_controller/cuav_nora.md#debug-port) | Custom port but comes with adaptor cable. | +| [ARK Pixhawk Autopilot Bus Carrier](../flight_controller/ark_pab.md#debug-port) | [Pixhawk Debug Full](#pixhawk-debug-full) | +| [NXP MR-VMU-RT1176](../flight_controller/nxp_mr_vmu_rt1176.md#debug_port) | [Pixhawk Debug Full](#pixhawk-debug-full) | +| [mRo Pixracer](../flight_controller/pixracer.md#debug-port) | [Pixhawk Debug Mini](#pixhawk-debug-mini) | +| [S-Vehicle E2](../flight_controller/svehicle_e2.md#debug-port) | [Pixhawk Debug Mini] | +| [AP-H743-R1](../flight_controller/x-mav_ap-h743r1.md#debug-port) | 4-pin JST GH (SWD only) | +| [mRo Control Zero F7](../flight_controller/mro_control_zero_f7.md#debug_port) | | - - -## Pixhawk Connector Standard Debug Ports +## Pixhawk Connector Standard Debug Ports {#pixhawk-standard-debug-ports} The Pixhawk project has defines a standard pinout and connector type for different Pixhawk FMU releases: @@ -64,16 +74,16 @@ The Pixhawk project has defines a standard pinout and connector type for differe Check your [specific board](#port-information) to confirm the port used. ::: -| FMU 버전 | Pixhawk Version | 디버그 포트 | -| :-------- | :-------------------------------------------------------------- | :---------------------------------------- | -| FMUv2 | [Pixhawk / Pixhawk 1](../flight_controller/pixhawk.md#swd-port) | 10핀 ARM 디버그 | -| FMUv3 | Pixhawk 2 | 6핀 SUR 디버그 | -| FMUv4 | Pixhawk 3 | [Pixhawk Debug Mini](#pixhawk-debug-mini) | -| FMUv5 | Pixhawk 4 FMUv5 | [Pixhawk Debug Mini](#pixhawk-debug-mini) | -| FMUv5X | Pixhawk 5X | [Pixhawk Debug Full](#pixhawk-debug-full) | -| FMUv6 | Pixhawk 6 | [Pixhawk Debug Full](#pixhawk-debug-full) | -| FMUv6X | Pixhawk 6X | [Pixhawk Debug Full](#pixhawk-debug-full) | -| FMUv6X-RT | Pixhawk 6X-RT | [Pixhawk Debug Full](#pixhawk-debug-full) | +| FMU 버전 | Pixhawk Version | 디버그 포트 | +| :-------- | :------------------ | :---------------------------------------- | +| FMUv2 | Pixhawk / Pixhawk 1 | 10핀 ARM 디버그 | +| FMUv3 | Pixhawk 2 | 6핀 SUR 디버그 | +| FMUv4 | Pixhawk 3 | [Pixhawk Debug Mini](#pixhawk-debug-mini) | +| FMUv5 | Pixhawk 4 FMUv5 | [Pixhawk Debug Mini](#pixhawk-debug-mini) | +| FMUv5X | Pixhawk 5X | [Pixhawk Debug Full](#pixhawk-debug-full) | +| FMUv6 | Pixhawk 6 | [Pixhawk Debug Full](#pixhawk-debug-full) | +| FMUv6X | Pixhawk 6X | [Pixhawk Debug Full](#pixhawk-debug-full) | +| FMUv6X-RT | Pixhawk 6X-RT | [Pixhawk Debug Full](#pixhawk-debug-full) | :::info There FMU and Pixhawk versions are (only) consistent after FMUv5X. @@ -142,9 +152,7 @@ You can connect to the debug port using a [cable like this one](https://www.digi  - - -## Debug Probes for PX4 Hardware +## Debug Probes for PX4 Hardware {#debug-probes} Flight controllers commonly provide a [single debug port](#autopilot-debug-ports) that exposes both the [SWD Interface](#debug-signals) and [System Console](system_console). @@ -217,5 +225,3 @@ This reduces the risk or poor wiring contributing to debugging problems, and has [swd]: https://developer.arm.com/documentation/ihi0031/a/The-Serial-Wire-Debug-Port--SW-DP- [itm]: https://developer.arm.com/documentation/ddi0403/d/Appendices/Debug-ITM-and-DWT-Packet-Protocol?lang=en [etm]: https://developer.arm.com/documentation/ihi0064/latest/ -[bm06b-ghs-tbt(lf)(sn)(n)]: https://www.digikey.com/en/products/detail/jst-sales-america-inc/BM06B-GHS-TBT/807804 -[sm06b-ghs-tbt(lf)(sn)(n)]: https://www.digikey.com/en/products/detail/jst-sales-america-inc/SM06B-GHS-TB/807790 diff --git a/docs/ko/dev_airframes/adding_a_new_frame.md b/docs/ko/dev_airframes/adding_a_new_frame.md index 59aece9838..5f5133b9b7 100644 --- a/docs/ko/dev_airframes/adding_a_new_frame.md +++ b/docs/ko/dev_airframes/adding_a_new_frame.md @@ -124,118 +124,79 @@ param set-default CA_ROTOR3_PY 0.15 param set-default CA_ROTOR3_KM -0.05 ``` -### Example - Babyshark VTOL Complete Vehicle +### Example - HolyBro QAV250 Complete Vehicle -A more complicated configuration file for a complete vehicle is provided below. -This is the configuration for the Baby Shark [Standard VTOL](../frames_vtol/standardvtol.md) ([original file here](https://github.com/PX4/PX4-Autopilot/blob/main/ROMFS/px4fmu_common/init.d/airframes/13014_vtol_babyshark)). +A more complete configuration file for a real vehicle is provided below. +This is the configuration for the [HolyBro QAV250](../frames_multicopter/holybro_qav250_pixhawk4_mini.md) quadrotor ([original file here](https://github.com/PX4/PX4-Autopilot/blob/main/ROMFS/px4fmu_common/init.d/airframes/4052_holybro_qav250)). -The shebang and documentation sections are similar to those for the generic frame, but here we also document what `outputs` are mapped to each motor and actuator. -Note that these outputs are documentation only; the actual mapping is done using parameters. +The shebang and documentation sections are similar to those for the generic frame. +Here we also add a `@url` link to the vehicle documentation, a `@maintainer`, and additional board exclusions. ```sh #!/bin/sh # -# @name BabyShark VTOL +# @name HolyBro QAV250 # -# @type Standard VTOL -# @class VTOL +# @url https://docs.px4.io/main/en/frames_multicopter/holybro_qav250_pixhawk4_mini # -# @maintainer Silvan Fuhrer
@@ -93,7 +93,7 @@ This flight controller is perfect for people that is looking for a affordable an
- 기타 특성:
- Operating & storage temperature: -40 ~ 85°c
-## 구매처
+## Where to Buy {#store}
Order from [Holybro](https://holybro.com/products/pix32-v6).
@@ -156,13 +156,11 @@ It is pre-built and automatically installed by _QGroundControl_ when appropriate
To [build PX4](../dev_setup/building_px4.md) for this target:
-```
+```sh
make px4_fmu-v6c_default
```
-
-
-## 디버그 포트
+## Debug Port {#debug_port}
The [PX4 System Console](../debug/system_console.md) and [SWD interface](../debug/swd_debug.md) run on the **FMU Debug** port.
diff --git a/docs/ko/flight_controller/kakutef7.md b/docs/ko/flight_controller/kakutef7.md
index 09871f8b6b..72e2f77c50 100644
--- a/docs/ko/flight_controller/kakutef7.md
+++ b/docs/ko/flight_controller/kakutef7.md
@@ -1,142 +1,7 @@
+ROTATION_NONE 권장 방향을 나타냅니다.
-
-## 구매처
-
-- No longer available
-
-## 빠른 시작
-
-### 방향
-
-The diagram below shows the recommended orientation, which corresponds to `ROTATION_NONE` starting with PX4 v1.11.
-
-
-
-### 커넥터
-
-Detailed information about the pinouts can be found [here](https://docs.modalai.com/flight-core-datasheet-connectors).
-
-
-
-| 커넥터 | 요약 |
-| --- | --------------------------------------------------------- |
-| J1 | VOXL 통신 인터페이스 커넥터 (TELEM2) |
-| J2 | 프로그래밍 및 디버그 커넥터 |
-| J3 | USB 커넥터 |
-| J4 | UART2, UART ESC (TELEM3) |
-| J5 | 텔레메트리 커넥터 (TELEM1) |
-| J6 | VOXL - 전원 관리 입력/확장 |
-| J7 | 8 채널 PWM 출력 커넥터 |
-| J8 | CAN 버스 커넥터 |
-| J9 | PPM RC 입력 |
-| J10 | External GPS & Magnetometer Connector |
-| J12 | RC 입력, Spektrum/SBus/UART 커넥터 |
-| J13 | I2C 디스플레이(예비 센서 커넥터)/안전 버튼 입력 |
-
-
-
-### 사용자 가이드
-
-The full user guide is available [here](https://docs.modalai.com/flight-core-manual/).
-
-### 빌드 방법
-
-To [build PX4](../dev_setup/building_px4.md) for this target:
-
-```
-make modalai_fc-v1
-```
-
-## 시리얼 포트 매핑
-
-| UART | 장치 | 포트 |
-| ------ | ---------- | ------------------------------------------ |
-| USART1 | /dev/ttyS0 | GPS1 (J10) |
-| USART2 | /dev/ttyS1 | TELEM3 (J4) |
-| USART3 | /dev/ttyS2 | 디버깅 콘솔(J2) |
-| UART4 | /dev/ttyS3 | 확장 UART (J6) |
-| UART5 | /dev/ttyS4 | TELEM2, 기본 VOXL 통신 (J1) |
-| USART6 | /dev/ttyS5 | RC (J12) |
-| UART7 | /dev/ttyS6 | TELEM1 (J5) |
-| UART8 | /dev/ttyS7 | 해당없음 |
-
-
-
-## 지원
-
-Please visit the [ModalAI Forum](https://forum.modalai.com/category/10/flight-core) for more information.
+DOC REMOVED: 202603
+-->
diff --git a/docs/ko/flight_controller/modalai_voxl_2.md b/docs/ko/flight_controller/modalai_voxl_2.md
index 51a37f1928..2915d8f092 100644
--- a/docs/ko/flight_controller/modalai_voxl_2.md
+++ b/docs/ko/flight_controller/modalai_voxl_2.md
@@ -5,7 +5,7 @@ PX4 does not manufacture this (or any) autopilot.
Contact the [manufacturer](https://forum.modalai.com/) for hardware support or compliance issues.
:::
-The ModalAI [VOXL 2](https://modalai.com/voxl-2) ([Datasheet](https://docs.modalai.com/voxl2-datasheets/)) is ModalAI’s next-gen autonomous computing platform built around the Qualcomm QRB5165 processor. VOXL 2 boasts 8 cores, integrated PX4, seven camera concurrency, advanced onboard AI up to 15+ TOPS, and 5G connectivity. At 16 grams, VOXL 2 is the future of fully autonomous and connected drones!
+The ModalAI [VOXL 2](https://www.modalai.com/products/voxl-2) ([Datasheet](https://docs.modalai.com/voxl2-datasheets/)) is ModalAI's next-gen autonomous computing platform built around the Qualcomm QRB5165 processor. VOXL 2 boasts 8 cores, integrated PX4, seven camera concurrency, advanced onboard AI up to 15+ TOPS, and 5G connectivity. At 16 grams, VOXL 2 is the future of fully autonomous and connected drones!
@@ -62,7 +62,7 @@ ModalAI is actively maintaining a [branched PX4 version](https://github.com/moda
As VOXL 2 runs Ubuntu, the production releases of PX4 for VOXL 2 are distributed through [apt package management](https://docs.modalai.com/configure-pkg-manager/) and the [VOXL SDK](https://docs.modalai.com/voxl-sdk/).
-More information about the firmware can be found [here](https://docs.modalai.com/voxl2-px4-developer-guide/).
+More information about the firmware can be found [here](https://docs.modalai.com/voxl-px4/).
### main branch
@@ -70,7 +70,7 @@ PX4 mainline supports VOXL 2 (board documentation [here](https://github.com/PX4/
## QGroundControl 지원
-아래 다이어그램은 PX4 v1.11(및 ModalAI가 유지하는 PX4 v1.10 브랜치)부터 ROTATION_NONE 권장 방향을 나타냅니다.
+This board is supported in QGroundControl 4.0 and later.
## 구매처
@@ -78,17 +78,16 @@ PX4 mainline supports VOXL 2 (board documentation [here](https://github.com/PX4/
- [Starling 2 MAX](https://www.modalai.com/products/starling-2-max)
- [Sentinel Development Drone powered by VOXL 2](https://www.modalai.com/pages/sentinel)
- [Demo Video](https://www.youtube.com/watch?v=hMhQgWPLGXo)
-- [VOXL 2 Flight Deck, ready to mount, tune and fly](https://www.modalai.com/collections/ready-to-mount/products/voxl-2-flight-deck)
- [VOXL 2 Development Kits](https://www.modalai.com/products/voxl-2)
- [Demo Video](https://www.youtube.com/watch?v=aVHBWbwp488)
## 빠른 시작
-Quickstarts from the vendor are located [here](https://docs.modalai.com/voxl2-quickstarts/).
+Quickstarts from the vendor are located [here](https://docs.modalai.com/voxl-2-hardware-quickstart/).
### VOXL SDK
-VOXL SDK (Software Development Kit) consists of the open source [voxl-px4](https://docs.modalai.com/voxl-px4/), [core libraries](https://docs.modalai.com/core-libs/), [services](https://docs.modalai.com/mpa-services/), [tools](https://docs.modalai.com/inspect-tools/), [utilities](https://docs.modalai.com/sdk-utilities/), and [build environments](https://docs.modalai.com/build-environments/) that ModalAI provide to accelerate the use and development of VOXL compute boards and accessories.
+VOXL SDK (Software Development Kit) consists of the open source [voxl-px4](https://docs.modalai.com/voxl-px4/), [core libraries](https://docs.modalai.com/core-libs/), [services](https://docs.modalai.com/mpa-services/), [tools](https://docs.modalai.com/inspect-tools/), and [build environments](https://docs.modalai.com/build-environments/) that ModalAI provide to accelerate the use and development of VOXL compute boards and accessories.
VOXL SDK runs on VOXL, VOXL 2 and RB5 Flight!
@@ -123,11 +122,11 @@ The PX4 user guide for VOXL 2 is available [here](https://docs.modalai.com/voxl-
### Developer Guide
-The PX4 developer guide for VOXL 2 is available [here](https://docs.modalai.com/voxl-px4-developer-guide/).
+The PX4 developer guide for VOXL 2 is available [here](https://docs.modalai.com/voxl-px4/).
### 빌드 방법
-See the [VOXL PX4 Build Guide](https://docs.modalai.com/voxl2-px4-build-guide/) on how to build.
+See the [VOXL PX4 Build Guide](https://docs.modalai.com/voxl-px4-dev-build-guide/) on how to build.
## 지원
diff --git a/docs/ko/flight_controller/modalai_voxl_flight.md b/docs/ko/flight_controller/modalai_voxl_flight.md
index 848dd9fd19..7f5ee9210d 100644
--- a/docs/ko/flight_controller/modalai_voxl_flight.md
+++ b/docs/ko/flight_controller/modalai_voxl_flight.md
@@ -1,202 +1,7 @@
-# ModalAI VOXL Flight
+ROTATION_NONE 권장 방향을 나타냅니다.
-
-## 구매처
-
-No longer available.
-
-## 빠른 시작
-
-A quickstart from the vendor is located [here](https://docs.modalai.com/voxl-flight-quickstart/).
-
-### voxl-vision-px4
-
-The VOXL Flight runs [voxl-vision-px4](https://gitlab.com/voxl-public/modal-pipe-architecture/voxl-vision-px4) on the companion computer portion of the hardware serving as a sort of MAVLink proxy.
-For details, the source code is available [here](https://gitlab.com/voxl-public/modal-pipe-architecture/voxl-vision-px4)
-
-### 커넥터
-
-Detailed information about the pinouts can be found [here](https://docs.modalai.com/voxl-flight-datasheet-connectors/).
-
-#### 상단
-
-
-
-_Note: 1000 Series connectors accessible from the STM32/PX4_
-
-| 커넥터 | 요약 | 사용처 |
-| ----- | ------------------------------------------------------------------- | ---------------------------------------------------- |
-| J2 | 4k 이미지 센서 (CSI0) 고용 | Snapdragon - Linux |
-| J3 | 스테레오 이미지 센서 (CSI1) | Snapdragon - Linux |
-| J6 | 냉각 팬 커넥터 | Snapdragon - Linux |
-| J7 | BLSP6 (GPIO) and BLSP9 (UART) | Snapdragon - Linux |
-| J13 | 확장 B2B | Snapdragon - Linux |
-| J14 | 통합 GNSS 안테나 연결 | Snapdragon - Linux |
-| J1001 | 프로그래밍 및 디버그/UART3 | STM32 - PX4 |
-| J1002 | UART ESC, UART2/TELEM3 | STM32 - PX4 |
-| J1003 | PPM RC 입력 | STM32 - PX4 |
-| J1004 | RC 입력, Spektrum/SBus/UART6 | STM32 - PX4 |
-| J1006 | USB 2.0 커넥터(PX4/QGroundControl) | STM32 - PX4 |
-| J1007 | 8 채널 PWM/DShot 출력 | STM32 - PX4 |
-| J1008 | CAN 버스 | STM32 - PX4 |
-| J1009 | I2C3, UART4 | STM32 - PX4 |
-| J1010 | 텔레메트리 (TELEM1) | STM32 - PX4 |
-| J1011 | I2C2, 안전 버튼 입력 | STM32 - PX4 |
-| J1012 | External GPS & Mag, UART1, I2C1 | STM32 - PX4 |
-| J1013 | 전원 입력, I2C3 | STM32 - PX4 (powers whole system) |
-
-#### 하단
-
-
-
-_Note: 1000 Series connectors accessible from the STM32/PX4_
-
-| 커넥터 | 요약 | 사용처 |
-| ------------ | -------------------------------------- | --------------------------- |
-| J4 | 추적/광류 이미지 센서 (CSI2) | Snapdragon - Linux |
-| J8 | USB 3.0 OTG | Snapdragon - Linux, **adb** |
-| J10 | BLSP7 UART 및 I2C 오프보드 | Snapdragon - Linux |
-| J11 | BLSP12 UART 및 I2C 오프보드 | Snapdragon - Linux |
-| VOXL microSD | | Snapdragon - Linux |
-| PX4 microSD | 32Gb Max | STM32 - PX4 |
-| Wi-Fi 안테나 | 포함됨. | Snapdragon - Linux |
-
-### 사용자 가이드
-
-The full user guide is available [here](https://docs.modalai.com/voxl-flight-quickstart).
-
-### 빌드 방법
-
-To [build PX4](../dev_setup/building_px4.md) for this target:
-
-```
-make modalai_fc-v1
-```
-
-## 시리얼 포트 매핑
-
-_Note: mappings shown are for the PX4 controlled interfaces only_
-
-| UART | 장치 | 포트 |
-| ------ | ---------- | --------------------------------- |
-| USART1 | /dev/ttyS0 | GPS1 (J1012) |
-| USART2 | /dev/ttyS1 | TELEM3 (J1002) |
-| USART3 | /dev/ttyS2 | 디버그 콘솔(J1001) |
-| UART4 | /dev/ttyS3 | 확장 UART (J6) |
-| UART5 | /dev/ttyS4 | PX4와 보조 컴퓨터간의 UART |
-| USART6 | /dev/ttyS5 | RC (J1004) |
-| UART7 | /dev/ttyS6 | TELEM1 (J1010) |
-| UART8 | /dev/ttyS7 | 해당없음 |
-
-
-
-## 지원
-
-Please visit the [ModalAI Forum](https://forum.modalai.com/category/8/voxl-flight) for more information.
+DOC REMOVED: 202603
+-->
diff --git a/docs/ko/flight_controller/mro_control_zero_f7.md b/docs/ko/flight_controller/mro_control_zero_f7.md
index 384d719929..c0d537ac5e 100644
--- a/docs/ko/flight_controller/mro_control_zero_f7.md
+++ b/docs/ko/flight_controller/mro_control_zero_f7.md
@@ -30,7 +30,7 @@ This flight controller is [manufacturer supported](../flight_controller/autopilo
- [Bosch BMI088](https://www.bosch-sensortec.com/products/motion-sensors/imus/bmi088/) 3-axis accelerometer/gyroscope (internally vibration dampened)
- [Invensense ICM-20602](https://invensense.tdk.com/products/motion-tracking/6-axis/icm-20602/) 3-axis accelerometer/gyroscope
- [Invensense ICM-20948](https://invensense.tdk.com/products/motion-tracking/9-axis/icm-20948/) 3-axis accelerometer/gyroscope/magnetometer
- - [Infineon DPS310 barometer](https://www.infineon.com/assets/row/public/documents/24/49/infineon-dps310-datasheet-en.pdf) - [Discontinued](https://www.infineon.com/part/DPS310) (So smooth and NO more light sensitivity)
+ - Infineon DPS310 barometer - [Discontinued](https://www.infineon.com/products/sensor/pressure-sensors/pressure-sensors-for-iot) (So smooth and NO more light sensitivity)
- 인터페이스:
- 6x UART(총 직렬 포트), 3x(HW 흐름 제어 포함), 1x FRSky Telemetry(D 또는 X 유형), 1x 콘솔 및 1x GPS + I2C
@@ -56,7 +56,7 @@ This flight controller is [manufacturer supported](../flight_controller/autopilo
- 전원시스템
- 초저잡음 LDO 전압 조정기 3개
-## 구매처
+## Where to Buy {#store}
- [mRo Control Zero](https://store.mrobotics.io/mRo-Control-Zero-F7-p/mro-ctrl-zero-f7.htm)
@@ -69,22 +69,22 @@ It is pre-built and automatically installed by _QGroundControl_ when appropriate
To [build PX4](../dev_setup/building_px4.md) for this target:
-```
+```sh
make mro_ctrl-zero-f7
```
-## 디버그 포트
+## Debug Ports {#debug_port}
### 콘솔 포트
The [PX4 System Console](../debug/system_console.md) runs on `USART7` using the pins listed below.
This is a standard serial pinout, designed to connect to a [3.3V FTDI](https://www.digikey.com/en/products/detail/TTL-232R-3V3/768-1015-ND/1836393) cable (5V tolerant).
-\| mRo control zero f7 | | FTDI |
-\| ------------------- | ----------- | ---- | ---------------- |
-\| 17 | USART7 Tx | 5 | FTDI RX (yellow) |
-\| 19 | USART7 Rx | 4 | FTDI TX (orange) |
-\| 6 | USART21 GND | 1 | FTDI GND (black) |
+| mRo control zero f7 | | FTDI | |
+| ------------------- | ----------- | ---- | ------------------------------- |
+| 17 | USART7 Tx | 5 | FTDI RX (황) |
+| 19 | USART7 Rx | 4 | FTDI TX (적황) |
+| 6 | USART21 GND | 1 | FTDI GND (흑) |
### SWD 포트
diff --git a/docs/ko/flight_controller/mro_pixhawk.md b/docs/ko/flight_controller/mro_pixhawk.md
index ecfc33c9d2..9f46b7694e 100644
--- a/docs/ko/flight_controller/mro_pixhawk.md
+++ b/docs/ko/flight_controller/mro_pixhawk.md
@@ -72,7 +72,7 @@ It is pre-built and automatically installed by _QGroundControl_ when appropriate
To [build PX4](../dev_setup/building_px4.md) for this target:
-```
+```sh
make px4_fmu-v3_default
```
diff --git a/docs/ko/flight_controller/mro_x2.1.md b/docs/ko/flight_controller/mro_x2.1.md
index aa601aebe5..1be40508d7 100644
--- a/docs/ko/flight_controller/mro_x2.1.md
+++ b/docs/ko/flight_controller/mro_x2.1.md
@@ -1,121 +1,10 @@
+
diff --git a/docs/ko/frames_multicopter/kits.md b/docs/ko/frames_multicopter/kits.md
index c28d84a72f..1f2263854a 100644
--- a/docs/ko/frames_multicopter/kits.md
+++ b/docs/ko/frames_multicopter/kits.md
@@ -18,6 +18,7 @@ Kits generally do not include:
The following kits are currently available:
+- [Holybro X650 PX4 Development Kit](https://holybro.com/collections/x650-kits) (Pixhawk 6C/6X) ([Frame assembly guide](https://docs.holybro.com/drone-development-kit/x650-development-kit/download))
- [Holybro X500 v2 PX4 Development Kit](https://holybro.com/collections/x500-kits) (Pixhawk 6c) ([Build instructions](../frames_multicopter/holybro_x500v2_pixhawk6c.md))
- [Holybro S500 Kit v2](https://holybro.com/collections/s500/products/s500-v2-development-kit) (Pixhawk 6c)
- [Holybro QAV250 Kit](https://holybro.com/products/qav250-kit) (Pixhawk 6c)
@@ -27,7 +28,7 @@ The following kits are currently available:
## Build Guides
The build guides below show how to assemble a number of kits.
-Many kits vary only a little between revisions (for example, the new kit might simply upgrade the flight controller used, and is otherwise identical), so these are likely to be be useful for building the kits in the section above.
+Many kits vary only a little between revisions (for example, the new kit might simply upgrade the flight controller used, and is otherwise identical), so these are likely to be useful for building the kits in the section above.
- [Holybro X500 v2 (Pixhawk 6C)](../frames_multicopter/holybro_x500v2_pixhawk6c.md)
- [Holybro X500 v2 (Pixhawk 5X)](../frames_multicopter/holybro_x500V2_pixhawk5x.md) — Discontinued (v2 kit uses Pixhawk 6c)
diff --git a/docs/ko/frames_multicopter/omnicopter.md b/docs/ko/frames_multicopter/omnicopter.md
index 1c9267c486..bf895481e3 100644
--- a/docs/ko/frames_multicopter/omnicopter.md
+++ b/docs/ko/frames_multicopter/omnicopter.md
@@ -19,8 +19,8 @@ This build follows the original design from [Brescianini, Dario, and Raffaello D
You can select your own flight controller of choice, it just needs to support 8 DShot outputs.
:::
- - GPS: [ZED-F9P](https://gnss.store/zed-f9p-gnss-modules/105-elt0092.html)
- - [GPS helix antenna](https://gnss.store/gnss-rtk-multiband-antennas/28-elt0014.html)
+ - GPS: [ZED-F9P](https://gnss.store/products/elt0092)
+ - [GPS helix antenna](https://gnss.store/products/elt0014)
::: info
Any other GPS may work as well, however a helix antenna is expected to perform better for inverted flights.
@@ -34,8 +34,8 @@ This build follows the original design from [Brescianini, Dario, and Raffaello D
- Battery: we used a 6S 3300mAh LiPo. Make sure to check the dimensions so it fits the frame.
- Battery strap
- Frame:
- - Carbon square tube R 8mm X 7mm X 1000mm, e.g. [here on shop.swiss-composite.ch](https://shop.swiss-composite.ch/pi.php/Halbfabrikate/Rohre/Vierkant-Rohre/CFK-Vierkantrohr-8x8-7x7mm.html)
- - Carbon Rods R 3mm X 2mm X 1000mm, e.g. [here on shop.swiss-composite.ch](https://shop.swiss-composite.ch/pi.php/Halbfabrikate/Rohre/CFK-Rohre-pultrudiert-pullwinding/Carbon-Microtubes-100cm-x-20-3mm.html)
+ - Carbon square tube R 8mm X 7mm X 1000mm, e.g. [here on shop.swiss-composite.ch](https://www.shop.swiss-composite.ch/de/produkt/cfk-vierkantrohr-8x8-7x7mm)
+ - Carbon Rods R 3mm X 2mm X 1000mm, e.g. [here on shop.swiss-composite.ch](https://www.shop.swiss-composite.ch/de/produkt/carbon-microtubes-100cm-x-20-3mm)
- Required lengths:
- square tube: 8 pieces with length of 248mm
- rods: 12x328mm, 6x465mm
diff --git a/docs/ko/frames_plane/reptile_dragon_2.md b/docs/ko/frames_plane/reptile_dragon_2.md
index cf761afce0..f8751129d0 100644
--- a/docs/ko/frames_plane/reptile_dragon_2.md
+++ b/docs/ko/frames_plane/reptile_dragon_2.md
@@ -56,7 +56,7 @@ Key build features
- MS4525DO differential pressure module and pitot tube
-- [Caddx Vista FPV air unit](https://caddxfpv.com/collections/vista-kit)
+- [Caddx Vista FPV air unit](https://www.caddxfpv.com/collections/vista-kit)
- [Emax ES08MA ii](https://emaxmodel.com/products/emax-es08ma-ii-12g-mini-metal-gear-analog-servo-for-rc-model-robot-pwm-servo)
@@ -66,7 +66,7 @@ Key build features
- [5V BEC](https://www.readymaderc.com/products/details/rmrc-3a-power-regulator-5-to-6-volt-ubec)
-- [6s2p 18650 LiIon flight battery](https://www.upgradeenergytech.com/product-page/6s-22-2v-5600mah-30c-dark-lithium-liion-drone-battery) (select XT60 connector)
+- [6s2p 18650 LiIon flight battery](https://www.upgradeenergytech.com/products/red-6s1p-5000mah-molicel-p50b) (select XT60 connector)
- [Custom designed 3D printed parts](https://github.com/PX4/PX4-Autopilot/raw/main/docs/assets/airframes/fw/reptile_dragon_2/rd2_3d_printed_parts.zip)
- ARK6X carrier mount
@@ -97,7 +97,7 @@ The airplane needs some assembly out of the box.
Servos, wings, and the tail will need to be installed.
:::info
-For this portion of assembly, the instructions included with the kit should be sufficent, but some helpful tips are listed below.
+For this portion of assembly, the instructions included with the kit should be sufficient, but some helpful tips are listed below.
:::
### Gluing Foam
@@ -225,7 +225,7 @@ An alternative carrier board is the Holybro Pixhawk 5X carrier.
The carrier comes installed in a plastic case.
While the case does look nice, it is extra weight, so the carrier was removed from the case.
-Once removed from the case, the ARK6X was installed, and a protective cover fitted ontop.
+Once removed from the case, the ARK6X was installed, and a protective cover fitted on top.
@@ -353,7 +353,7 @@ For more information see [TBS Crossfire (CRSF) Telemetry](../telemetry/crsf_tele
### `msp_osd` Module
-The `msp_osd` module steams MSP telemetry to a selected serial port.
+The `msp_osd` module streams MSP telemetry to a selected serial port.
The Caddx Vista Air Unit supports listening to MSP telemetry and will show the received telemetry values in its OSD (on screen display).
1. In the PX4 board config tool, navigate to the `drivers` submenu, then scroll down to highlight `OSD`.
diff --git a/docs/ko/frames_plane/turbo_timber_evolution.md b/docs/ko/frames_plane/turbo_timber_evolution.md
index bf5b5988a0..31bdc80f00 100644
--- a/docs/ko/frames_plane/turbo_timber_evolution.md
+++ b/docs/ko/frames_plane/turbo_timber_evolution.md
@@ -50,7 +50,7 @@ Key Build Features:
- MS4525DO differential pressure module and pitot tube
-- [Caddx Vista FPV air unit](https://caddxfpv.com/collections/vista-kit)
+- [Caddx Vista FPV air unit](https://www.caddxfpv.com/collections/vista-kit)
- [DJI FPV Goggles](https://www.dji.com/fpv)
@@ -74,7 +74,7 @@ Servos and linkages have already been installed, and the only real remaining wor
For this portion of the assembly, simply follow the manual.
:::info
-[Some reports](https://www.rcgroups.com/forums/showthread.php?3904021-NEW-E-flite-Turbo-Timber-Evolution-1-5m-%C2%96-Smartest-Most-Capable-Durable-Timber-Yet/page50) have indicated that the stock ESC bundled with the airplane has an issue with overheating.
+[Some reports](https://www.rcgroups.com/forums/showthread.php?3904021-NEW-E-flite-Turbo-Timber-Evolution-1-5m/page50) have indicated that the stock ESC bundled with the airplane has an issue with overheating.
As this build will be especially heavy, and therefore likely demand higher average power from the ESC, the stock 60A ESC was replaced with an 80A Turnigy PLUSH-32 during testing.
The stock motor was also replaced with a [higher power motor](https://hobbyking.com/en_us/turnigy-aerodrive-sk3-3548-840kv-brushless-outrunner-motor.html).
@@ -90,7 +90,7 @@ A long M3 nylon screw and a washer on the underside, followed by a washer and st
-
+
## Pitot Pod
@@ -150,7 +150,7 @@ Power for the servo and lighting will be provided by the "BEC" power supply in t
The TTE is very flexible when it comes to battery options.
I use both a 3.6Ah 4S Turnigy pack as well as a Upgrade Energy 4s2p liion pack.
-While the 3.6Ah LiPo is inexpensive, nearly twice the flight time (24 minutes vs 12 minutes) can be acheived with the Upgrade Energy Liion pack.
+While the 3.6Ah LiPo is inexpensive, nearly twice the flight time (24 minutes vs 12 minutes) can be achieved with the Upgrade Energy Liion pack.
@@ -177,10 +177,10 @@ Similarly, a JST PH to std spaced headers adapter was made, and it was also left
#### 무선 수신기
-A custom cable was made to connect the ExpressLRS RX ([RC Reciever](../getting_started/rc_transmitter_receiver.md)) to the Pixhawk 4 Mini.
+A custom cable was made to connect the ExpressLRS RX ([RC Receiver](../getting_started/rc_transmitter_receiver.md)) to the Pixhawk 4 Mini.
Because the Pixhawk 4 Mini has limited uarts, the RX was connected to RC input which does not have a TX pin.
-This means that the RX will only send control data to the FCU but telemtry cannot be sent to the RX from the FCU.
+This means that the RX will only send control data to the FCU but telemetry cannot be sent to the RX from the FCU.
Heatshrink was used to secure the dupont connector of the cable such that it cannot back out off the headers of the ExpressLRS RX.
#### FPV Pod & Airspeed Cable
@@ -189,7 +189,7 @@ Another custom cable was made to connect the Caddx Vista FPV transmitter to the
A Molex microfit was added close to the Vista so that it could be easily disconnected without needing to gain access to the Pixhawk.
As the name implies, the `UART/I2C B` port provides both a UART and I2C interface.
This port is split with the custom cable and one side provides power and data to the I2C airspeed sensor, while the other side provides power and UART TX/RX to the Caddx Vista.
-From the UART/I2C B port, 5V, GND, and I2C SCL/SDA, are connected to the I2C airspeed sensor, while just serial RX and TX are connected to the Caddx Vista (Ground is provided the seperate battery power/gnd leads for the Vista)
+From the UART/I2C B port, 5V, GND, and I2C SCL/SDA, are connected to the I2C airspeed sensor, while just serial RX and TX are connected to the Caddx Vista (Ground is provided the separate battery power/gnd leads for the Vista)
The [msp_osd](../modules/modules_driver.md#msp-osd) module is used to stream telemetry to the Caddx Vista which can be seen on the DJI Goggles with the "custom OSD" feature enabled.
@@ -204,7 +204,7 @@ Heatshrink was used to electrically insulate the bare board and the radio was in
Overall, this build was a success.
-Even with the added weight of the Pixhawk 4 Mini installation, the airplane balances well and has plenty of power to retain its original STOL characterisitics.
+Even with the added weight of the Pixhawk 4 Mini installation, the airplane balances well and has plenty of power to retain its original STOL characteristics.
PX4 is easily capable of stabilizing the airplane and fine tuning of the rate loops were accomplished using [fixed-wing autotuning](../config/autotune_fw.md).
The results of tuning can be found in the [parameter file linked below](#parameter-file).
diff --git a/docs/ko/frames_plane/wing_wing_z84.md b/docs/ko/frames_plane/wing_wing_z84.md
index f76275ae14..298dfdaf07 100644
--- a/docs/ko/frames_plane/wing_wing_z84.md
+++ b/docs/ko/frames_plane/wing_wing_z84.md
@@ -33,7 +33,7 @@ Any small (>=12A) ESC will do:
- FrSky D4R-II 수신기 또는 동급 (설명서에 따라 PPM 합계 출력으로 점퍼됨)
- [Mini telemetry set](../flight_controller/pixfalcon.md#availability) for Holybro pix32
- [Digital airspeed sensor](../flight_controller/pixfalcon.md#availability) for Holybro pix32 / Pixfalcon
-- 1800 mAh 2S LiPo Battery - e.g. [Team Orion 1800mAh 7.4V 50C 2S1P](https://teamorion.com/en/batteries-en/lipo/soft-case/team-orion-lipo-1800-2s-7-4v-50c-xt60-en/)
+- 1800 mAh 2S LiPo Battery - e.g. Team Orion 1800mAh 7.4V 50C 2S1P with XT 60 plug.
### 권장 예비 부품
diff --git a/docs/ko/frames_sub/bluerov2.md b/docs/ko/frames_sub/bluerov2.md
index 49c4870366..ae43036907 100644
--- a/docs/ko/frames_sub/bluerov2.md
+++ b/docs/ko/frames_sub/bluerov2.md
@@ -2,21 +2,25 @@
@@ -29,6 +33,15 @@ The vehicle will then match the configuration documented in the [Airframe Refere
- **MAIN7:** motor 7 CCW, stern starboard vertical, propeller CW
- **MAIN8:** motor 8 CCW, stern port vertical, propeller CCW
+## Manual Modes
+
+| Mode | 설명 |
+| -------- | ---------------------------------------------------------------------------------------------------------------------------------------------------- |
+| Manual | Direct manual control of yaw and thrust. |
+| Acro | Manual control of yaw/thrust, but keeps roll/pitch zero |
+| Altitude | Manual control of x/y thrust and yaw. Control of height with PID, manually controlled by user. Keeps roll/pitch zero |
+| Position | Controls x/y/z and yaw. Manually controlled by user. Keeps roll/pitch zero |
+
## 기체 설정
BlueROV2 does not come with PX4 installed.
diff --git a/docs/ko/frames_vtol/tailsitter.md b/docs/ko/frames_vtol/tailsitter.md
index 2bb1d4c4d5..8ce9063e61 100644
--- a/docs/ko/frames_vtol/tailsitter.md
+++ b/docs/ko/frames_vtol/tailsitter.md
@@ -91,7 +91,7 @@ This section contains videos that are specific to Tailsitter VTOL (videos that a
-
+
diff --git a/docs/ko/frames_vtol/vtol_quadplane_falcon_vertigo_hybrid_rtf_dropix.md b/docs/ko/frames_vtol/vtol_quadplane_falcon_vertigo_hybrid_rtf_dropix.md
index 2e390ce6dc..587208e4c4 100644
--- a/docs/ko/frames_vtol/vtol_quadplane_falcon_vertigo_hybrid_rtf_dropix.md
+++ b/docs/ko/frames_vtol/vtol_quadplane_falcon_vertigo_hybrid_rtf_dropix.md
@@ -36,7 +36,7 @@ RTF 키트에는 RC 수신기와 텔레메트리를 제외하고, 시스템에
- 푸셔 모터 전원 시스템
- 탄소 섬유 튜브 및 마운트
- G10 모터 마운트
-- 1 x [3700mah 4S 30C Lipo battery](https://www.overlander.co.uk/batteries/lipo-batteries/power-packs/3700mah-4s-14-8v-25c-lipo-battery-overlander-sport.html)
+- 1 x [3700mah 4S 30C Lipo battery](https://wheelspinmodels.co.uk/i/3700mah-4s-14.8v-25c-lipo-battery-overlander-262221/)
- Dropix power distribution board and cable
이 키트는 라디오 수신기 또는 텔레메트리(선택 사항)는 제공하지 않습니다.
diff --git a/docs/ko/frames_vtol/vtol_quadplane_foxtech_loong_2160.md b/docs/ko/frames_vtol/vtol_quadplane_foxtech_loong_2160.md
index ad64afc43e..88f32dca27 100644
--- a/docs/ko/frames_vtol/vtol_quadplane_foxtech_loong_2160.md
+++ b/docs/ko/frames_vtol/vtol_quadplane_foxtech_loong_2160.md
@@ -43,14 +43,14 @@ The following options have been tested:
- [Holybro PM08D Power Module (alternative to Auterion PM)](https://holybro.com/collections/power-modules-pdbs/products/pm08d-digital-power-module-14s-200a)
- [GPS F9P (included in Skynode eval. kit)](../gps_compass/rtk_gps_holybro_h-rtk-f9p.md)
- [GPS M9N (cheaper alternative to F9P)](../gps_compass/rtk_gps_holybro_h-rtk-m8p.md)
-- [Airspeed sensor (included in Skynode eval. kit)](https://www.dualrc.com/parts/airspeed-sensor-sdp33) — recommended for improved safety and performance
+- [Airspeed sensor (included in Skynode eval. kit)](https://www.dualrc.com/parts/p/airspeed-sensor-sdp33) — recommended for improved safety and performance
- [Airspeed sensor (cheaper alternative)](https://holybro.com/products/digital-air-speed-sensor-ms4525do)
- [Lidar Lightware lw20-c (included in Skynode eval. kit)](../sensor/sfxx_lidar.md) (Optional)
- [Lidar Seeed Studio PSK-CM8JL65-CC5 (cheaper alternative)](https://www.seeedstudio.com/PSK-CM8JL65-CC5-Infrared-Distance-Measuring-Sensor-p-4028.html) (Optional)
- [Radio (RC) System](../getting_started/rc_transmitter_receiver.md) of your preference
-- [Groundstation and Radio link](https://holybro.com/collections/rc-radio-transmitter-receiver/products/skydroid-h12?variant=42940989931709)
+- [Groundstation and Radio link](https://holybro.com/products/skydroid-h12)
- [USB-C extension cable](https://www.digitec.ch/en/s1/product/powerguard-usb-c-usb-c-025-m-usb-cables-22529949?dbq=1&gclid=Cj0KCQjw2cWgBhDYARIsALggUhrh-z-7DSU0wKfLBVa8filkXLQaxUpi7pC0ffQyRzLng8Ph01h2R1gaAp0mEALw_wcB&gclsrc=aw.ds)
-- [I2C Splitter](https://www.3dxr.co.uk/autopilots-c2/the-cube-aka-pixhawk-2-1-c9/cube-cables-accessories-sensors-c15/cubepilot-i2c-can-splitter-jst-gh-4pin-p2840)
+- [I2C Splitter](https://www.3dxr.co.uk/autopilots-c2/the-cube-aka-pixhawk-2-1-c9/cube-cables-accessories-sensors-c15/cubepilot-i2c-can-splitter-jst-gh-4pin-hx4-06152-p2840)
- [3D-Printed mounts](https://github.com/PX4/PX4-Autopilot/raw/main/docs/assets/airframes/vtol/foxtech_loong_2160/loong-3d-prints.zip)
- 1x Baseplate
- 1x Stack-fixture
@@ -305,7 +305,7 @@ To load the file:
- If the [Lidar Lightware lw20-c (included in Skynode eval. kit)](../sensor/sfxx_lidar.md) is used, [SENS_EN_SF1XX](../advanced_config/parameter_reference.md#SENS_EN_SF1XX) needs to be set to 6 (SF/LW/20c).
- Make that the correct airspeed sensor is selected.
- If you use the recommended [SDP33 airspeed sensor](https://www.dualrc.com/parts/airspeed-sensor-sdp33) no changes will be needed as [SENS_EN_SDP3X](../advanced_config/parameter_reference.md#SENS_EN_SDP3X) is enabled (set to `1`) in the parameter file.
+ If you use the recommended [SDP33 airspeed sensor](https://www.dualrc.com/parts/p/airspeed-sensor-sdp33) no changes will be needed as [SENS_EN_SDP3X](../advanced_config/parameter_reference.md#SENS_EN_SDP3X) is enabled (set to `1`) in the parameter file.
### Sensor Calibration
diff --git a/docs/ko/frames_vtol/vtol_tailsitter_caipiroshka_pixracer.md b/docs/ko/frames_vtol/vtol_tailsitter_caipiroshka_pixracer.md
index 7cb8848371..6580d0bba2 100644
--- a/docs/ko/frames_vtol/vtol_tailsitter_caipiroshka_pixracer.md
+++ b/docs/ko/frames_vtol/vtol_tailsitter_caipiroshka_pixracer.md
@@ -4,7 +4,7 @@ The Caipiroshka VTOL is a slightly modified _TBS Caipirinha_.
:::info
The _TBS Caipirinha_ has been superseded and is no longer available.
-These instructions _should_ work with the updated vehicle: [TBS Caipirinha 2](https://team-blacksheep.com/products/prod:tbs_caipi2_pnp).
+These instructions _should_ work with the updated vehicle: [TBS Caipirinha 2](https://www.team-blacksheep.com/products/prod:tbs_caipi2_pnp).
부품 목록에서 다른 여러 구성 요소도 업데이트 되었습니다.
:::
@@ -12,7 +12,7 @@ These instructions _should_ work with the updated vehicle: [TBS Caipirinha 2](ht
## 부품 목록
-- TBS Caipirinha Wing (no longer available - try [TBS Caipirinha 2](https://team-blacksheep.com/products/prod:tbs_caipi2_pnp))
+- TBS Caipirinha Wing (no longer available - try [TBS Caipirinha 2](https://www.team-blacksheep.com/products/prod:tbs_caipi2_pnp))
- Left and right 3D-printed motor mount (design files)
- CW 8045 propeller ([Eflight store](https://www.banggood.com/GEMFAN-Carbon-Nylon-8045-CWCCW-Propeller-For-Quadcopters-1-Pair-p-950874.html))
- CCW 8045 propeller ([Eflight store](https://www.banggood.com/GEMFAN-Carbon-Nylon-8045-CWCCW-Propeller-For-Quadcopters-1-Pair-p-950874.html))
@@ -24,7 +24,7 @@ These instructions _should_ work with the updated vehicle: [TBS Caipirinha 2](ht
- [GetFPV](https://www.getfpv.com/lumenier-30a-blheli-s-esc-opto-2-4s.html)
- BEC (3A, 5-5.3V) (출력 레일 용 5V 전원 공급 장치로 작동 할 수없는 ESC를 사용하는 경우에만 필요)
- 3S 2200 mA 리포 배터리
- - Team Orion 3S 11.1V 50 C ([Hobbyshop store](https://www.hobbyshop.ch/modellbau-elektronik/akku/team-orion-lipo-2200-3s-11-1v-50c-xt60-ori60163.html))
+ - Team Orion 3S 11.1V 50 C ([Hobbyshop store](https://www.hobbyshop.ch/team-orion-lipo-2200-3s-11-1v-50c-xt60-ori60163.html))
- [Pixracer autopilot board + power module](../flight_controller/pixracer.md)
- [Digital airspeed sensor](https://hobbyking.com/en_us/hkpilot-32-digital-air-speed-sensor-and-pitot-tube-set.html)
diff --git a/docs/ko/frames_vtol/vtol_tiltrotor_omp_hobby_zmo_fpv.md b/docs/ko/frames_vtol/vtol_tiltrotor_omp_hobby_zmo_fpv.md
index f8f16bf6d9..5e42675263 100644
--- a/docs/ko/frames_vtol/vtol_tiltrotor_omp_hobby_zmo_fpv.md
+++ b/docs/ko/frames_vtol/vtol_tiltrotor_omp_hobby_zmo_fpv.md
@@ -25,9 +25,9 @@ Depending on the final takeoff weight the hover time might be limited (there is
## 구매처
-- [OMP-Hobby](https://www.omphobby.com/OMPHOBBY-ZMO-VTOL-FPV-Aircraft-With-DJI-Goggles-And-Remote-Controller-p3069854.html)
- [GetFPV](https://www.getfpv.com/omphobby-zmo-z3-vtol-fpv-1200mm-arf-plane-kit-no-fpv-system.html)
- [FoxtechFPV](https://www.foxtechfpv.com/zmo-pro-fpv-vtol.html)
+- [RMRC](https://www.readymaderc.com/products/details/omp-hobby-zmo-vtol-fpv-airplane-rtf-goggles-radio)
## 비행 콘트롤러
@@ -43,7 +43,7 @@ The approximate maximum size of the FC is: 50x110x22mm
- [GPS F9P (included in Skynode eval. kit)](../gps_compass/rtk_gps_holybro_h-rtk-f9p.md)
- [GPS M9N (cheaper alternative to F9P)](../gps_compass/rtk_gps_holybro_h-rtk-m8p.md)
-- [Airspeed sensor (included in Skynode eval. kit)](https://www.dualrc.com/parts/airspeed-sensor-sdp33) — recommended for improved safety and performance
+- [Airspeed sensor (included in Skynode eval. kit)](https://www.dualrc.com/parts/p/airspeed-sensor-sdp33) — recommended for improved safety and performance
- [Airspeed sensor (cheaper alternative)](https://holybro.com/products/digital-air-speed-sensor-ms4525do)
- [Lidar Lightware lw20-c (included in Skynode eval. kit)](../sensor/sfxx_lidar.md) (Optional)
- [Lidar Seeed Studio PSK-CM8JL65-CC5 (cheaper alternative)](https://www.seeedstudio.com/PSK-CM8JL65-CC5-Infrared-Distance-Measuring-Sensor-p-4028.html) (Optional)
@@ -79,7 +79,7 @@ The following tools were used for this build.
### Preparations
Remove the original flight controller, ESC and wing connector cables.
-Also remove the the propellers.
+Also remove the propellers.
This will help you with the handling of the vehicle and will reduce the risk of an injury due to an unintentional motor startup.
ZMO FPV in it's original state.
@@ -101,7 +101,7 @@ Flight controller and wing connectors removed from the vehicle.
4. Shorten the rear motor wires and solder them as shown in the picture into place.
-5. Solder signal and GND wires to the PWM input ot the ESC.
+5. Solder signal and GND wires to the PWM input to the ESC.
@@ -293,7 +293,7 @@ To load the file:
The airspeed sensor can be enabled in the [Parameters](../advanced_config/parameters.md#finding-updating-parameters) tab.
-- If the [recommended airspeed sensor (SDP33)](https://www.dualrc.com/parts/airspeed-sensor-sdp33) is used, `SENS_EN_SDP3X` needs to be enabled.
+- If the [recommended airspeed sensor (SDP33)](https://www.dualrc.com/parts/p/airspeed-sensor-sdp33) is used, `SENS_EN_SDP3X` needs to be enabled.
- If the [Lidar Lightware lw20-c (included in Skynode eval. kit)](../sensor/sfxx_lidar.md) is used, `SENS_EN_SF1XX` needs to be set to 6 (SF/LW/20c).
### Sensor Calibration
diff --git a/docs/ko/getting_started/flight_reporting.md b/docs/ko/getting_started/flight_reporting.md
index 1cce986830..02cffd153f 100644
--- a/docs/ko/getting_started/flight_reporting.md
+++ b/docs/ko/getting_started/flight_reporting.md
@@ -38,7 +38,7 @@ For more information see [Settings > MAVLink Settings > MAVLink 2 Logging (PX4 o
## PX4 개발자가 검토할 로그 파일 공유
-The [Flight Review](https://logs.px4.io/) log file link can be shared for discussion in the [support forums](../contribute/support.md#forums-and-chat) or a [Github issue](../index.md#reporting-bugs-issues).
+The [Flight Review](https://logs.px4.io/) log file link can be shared for discussion in the [support forums](../contribute/support.md#forums-and-chat) or a [Github issue](../contribute/support.md#issue-bug-reporting).
## 로그 설정
diff --git a/docs/ko/getting_started/rc_transmitter_receiver.md b/docs/ko/getting_started/rc_transmitter_receiver.md
index 071945f2d7..0c7c31e120 100644
--- a/docs/ko/getting_started/rc_transmitter_receiver.md
+++ b/docs/ko/getting_started/rc_transmitter_receiver.md
@@ -3,13 +3,15 @@
A Radio Control (RC) system can be used to _manually_ control your vehicle from a handheld RC controller.
This topic provides an overview of how RC works, how to choose an appropriate radio system for your vehicle, and how to connect it to your flight controller.
-:::tip
-PX4 can also be manually controlled using a [Joystick](../config/joystick.md) or gamepad-like controller: this is different to an RC system!
-The [COM_RC_IN_MODE](../advanced_config/parameter_reference.md#COM_RC_IN_MODE) parameter [can be set](../advanced_config/parameters.md) to choose whether RC (default), Joystick, both, or neither, are enabled.
+:::info
+PX4 does not require a manual control system for autonomous flight modes.
:::
-:::info
-PX4 does not require a remote control system for autonomous flight modes.
+:::tip
+PX4 can also be [manually controlled](../config/manual_control.md) using a [Joystick](../config/joystick.md) or gamepad-like controller.
+
+By default PX4 will latch the first valid controller it discovers and use it until the vehicle reboots.
+If you have multiple controllers and you want to define their priority see [Manual Control > PX4 Configuration](../config/manual_control.md#px4-configuration).
:::
## 무선 조종기 작동 방법
diff --git a/docs/ko/gps_compass/gps_cuav_neo_3.md b/docs/ko/gps_compass/gps_cuav_neo_3.md
index df1e935bf9..022d24faa2 100644
--- a/docs/ko/gps_compass/gps_cuav_neo_3.md
+++ b/docs/ko/gps_compass/gps_cuav_neo_3.md
@@ -47,7 +47,7 @@ It integrates Ublox M9N, IST8310, three-color LED lights and safety switches, an
## 구매처
-- [CUAV](https://cuav.en.alibaba.com/product/1600217379204-820872629/CUAV_NEO_3_M9N_GPS_Module_for_Pixhawk_Compass_gps_tracker_navigation_gps.html?spm=a2700.shop_oth.74.1.636e28725EvVHb)
+- [CUAV](https://www.alibaba.com/product-detail/CUAV_NEO_3_M9N_GPS_Module_for_Pixhawk_Compass_gps_tracker_navigation_gps_1600217379204.html)
## 배선
diff --git a/docs/ko/gps_compass/gps_cuav_neo_3pro.md b/docs/ko/gps_compass/gps_cuav_neo_3pro.md
index 970a9e43bc..55fdfb33b3 100644
--- a/docs/ko/gps_compass/gps_cuav_neo_3pro.md
+++ b/docs/ko/gps_compass/gps_cuav_neo_3pro.md
@@ -41,7 +41,7 @@ It integrates UBLOX M9N, STM32F4 MCU, RM3100 compass, three-color LED light and
## 구매처
-- [CUAV](https://cuav.en.alibaba.com/product/1600165544920-820872629/Free_shipping_CUAV_Neo_3_pro_drone_UAVCAN_GNSS_processor_STM32F412_autopilot_ublox_M9N_positioning_RM3100_compass_uav_gps_module.html?spm=a2700.shop_oth.74.2.636e28725EvVHb)
+- [CUAV](https://www.alibaba.com/product-detail/Free_shipping_CUAV_Neo_3_pro_drone_UAVCAN_GNSS_processor_STM32F412_autopilot_ublox_M9N_positioning_RM3100_compass_uav_gps_module_1600165544920.html)
## 배선
diff --git a/docs/ko/gps_compass/index.md b/docs/ko/gps_compass/index.md
index d6afb08543..15308c843a 100644
--- a/docs/ko/gps_compass/index.md
+++ b/docs/ko/gps_compass/index.md
@@ -187,9 +187,9 @@ Some of GNSS terms that are useful for interpreting the data include:
- `DOP`: Dilution of position (dimensionless).
This is a measure of the geometric quality of satellite positions and their effect on the precision of the GPS receiver's calculations.
- `EPH`: Standard deviation of horizontal position error (metres).
- This represents the the uncertainty in the GPS fix latitude and longitude.
+ This represents the uncertainty in the GPS fix latitude and longitude.
- `EPV`: Standard deviation of vertical position error (metres).
- This represents the the uncertainty in the GPS fix altitude.
+ This represents the uncertainty in the GPS fix altitude.
### DOP vs EPH/EPV
diff --git a/docs/ko/gps_compass/magnetometer.md b/docs/ko/gps_compass/magnetometer.md
index 5474b68bbd..2c46339587 100644
--- a/docs/ko/gps_compass/magnetometer.md
+++ b/docs/ko/gps_compass/magnetometer.md
@@ -22,7 +22,7 @@ If it fails before flight, arming will be denied.
### Compass Parts
PX4 can be used with many magnetometer parts, including: Bosch BMM 150 MEMS (via I2C bus), HMC5883 / HMC5983 (I2C or SPI), IST8310 (I2C), LIS3MDL (I2C or SPI), RM3100, and more.
-Other supported magnetometer parts and their busses can be inferred from the drivers listed in [Modules Reference: Magnetometer (Driver)](../modules/modules_driver_magnetometer.md).
+Other supported magnetometer parts and their buses can be inferred from the drivers listed in [Modules Reference: Magnetometer (Driver)](../modules/modules_driver_magnetometer.md).
These parts are included in stand alone compass modules, combined compass/GNSS modules, and also in many flight controllers,
@@ -55,7 +55,7 @@ This list contains stand-alone magnetometer modules (without GNSS).
Internal compasses are not recommended for real use as a heading source, because the performance is almost always very poor.
-This is particularly true on on small vehicles where the flight controller has to be mounted close to motor/ESC power lines and other sources of electromagnetic interference.
+This is particularly true on small vehicles where the flight controller has to be mounted close to motor/ESC power lines and other sources of electromagnetic interference.
While they may be better on larger vehicles (e.g. VTOL), where it is possible to reduce electromagnetic interference by mounting the flight controller a long way from power supply lines, an external compass will almost always be better.
:::tip
diff --git a/docs/ko/gps_compass/rtk_gps.md b/docs/ko/gps_compass/rtk_gps.md
index 8b0e09ca86..8107f4ff1d 100644
--- a/docs/ko/gps_compass/rtk_gps.md
+++ b/docs/ko/gps_compass/rtk_gps.md
@@ -14,7 +14,7 @@ Some RTK GNSS setups can provide yaw/heading information, as an alternative to t
## 지원되는 RTK 장치
-PX4 supports the [u-blox M8P](https://www.u-blox.com/en/product/neo-m8p), [u-blox F9P](https://www.u-blox.com/en/product/zed-f9p-module) and the [Trimble MB-Two](https://oemgnss.trimble.com/en/products/receiver-modules/mb-two) GPS, and products that incorporate them.
+PX4 supports the [u-blox M8P](https://www.u-blox.com/en/product/neo-m8p-series), [u-blox F9P](https://www.u-blox.com/en/product/zed-f9p-module) and the [Trimble MB-Two](https://oemgnss.trimble.com/en/products/receiver-modules/mb-two) GPS, and products that incorporate them.
:::note
일부 RTK 모듈은 특정 기능(베이스 또는 로버)으로만 사용할 수 있는 반면, 다른 모듈은 서로 교환하여 사용할 수 있습니다.
@@ -58,7 +58,7 @@ It also highlights devices that connect via the CAN bus, and those which support
| [Septentrio AsteRx-m3 Pro](../gps_compass/septentrio_asterx-rib.md) | AsteRx | ✓ | | [Septentrio Dual Antenna] | ✓ |
| [Septentrio mosaic-go](../gps_compass/septentrio_mosaic-go.md) | mosaic X5 / mosaic H | ✓ | | [Septentrio Dual Antenna] | ✓ |
| [SIRIUS RTK GNSS ROVER (F9P)](https://store-drotek.com/911-sirius-rtk-gnss-rover-f9p.html) | F9P | ✓ | | [Dual F9P] | |
-| [SparkFun GPS-RTK2 Board - ZED-F9P](https://www.sparkfun.com/products/15136) | F9P | ✓ | | [Dual F9P] | |
+| [SparkFun GPS-RTK2 Board - ZED-F9P](https://www.sparkfun.com/sparkfun-gps-rtk2-board-zed-f9p-qwiic-gps-15136.html) | F9P | ✓ | | [Dual F9P] | |
| [Trimble MB-Two](../gps_compass/rtk_gps_trimble_mb_two.md) | F9P | ✓ | | ✓ | |
diff --git a/docs/ko/gps_compass/rtk_gps_cuav_c-rtk-9ps.md b/docs/ko/gps_compass/rtk_gps_cuav_c-rtk-9ps.md
index 148c69608e..8ee956fd67 100644
--- a/docs/ko/gps_compass/rtk_gps_cuav_c-rtk-9ps.md
+++ b/docs/ko/gps_compass/rtk_gps_cuav_c-rtk-9ps.md
@@ -1,6 +1,6 @@
# CUAV C-RTK 9Ps
-The CUAV [C-RTK 9Ps](https://www.cuav.net/en/c_rtk_9ps/) is a multi-satellite, multi-band, centimeter-level, RTK GNSS system.
+The CUAV [C-RTK 9Ps](https://www.cuav.net/en/c-rtk-9ps-en/) is a multi-satellite, multi-band, centimeter-level, RTK GNSS system.
The module simultaneously receives GPS, GLONASS, Galileo and Beidou satellite signals, enabling faster positioning and higher accuracy.
It also supports [RTK GPS Heading](../gps_compass/u-blox_f9p_heading.md) using dual modules.
@@ -12,7 +12,7 @@ This is ideal for survey drones, agricultural drones and other application scena
## 구매처
-[cuav Store](https://store.cuav.net/shop/c-rtk-9ps/)
+[cuav Store](https://store.cuav.net/?route=product%2Fproduct&path=61&product_id=187)
## 사양
diff --git a/docs/ko/gps_compass/rtk_gps_cuav_c-rtk.md b/docs/ko/gps_compass/rtk_gps_cuav_c-rtk.md
index 52a2c14024..2a3e7952cc 100644
--- a/docs/ko/gps_compass/rtk_gps_cuav_c-rtk.md
+++ b/docs/ko/gps_compass/rtk_gps_cuav_c-rtk.md
@@ -1,6 +1,6 @@
# CUAV C-RTK
-The [CUAV C-RTK GPS receiver](https://www.cuav.net/en/c_rtk_9ps/) is an [RTK GPS module](../gps_compass/rtk_gps.md) for the mass market.
+The [CUAV C-RTK GPS receiver](https://www.cuav.net/en/c-rtk-9ps-en/) is an [RTK GPS module](../gps_compass/rtk_gps.md) for the mass market.
완전한 RTK 시스템은 2개 이상의 C-RTK 모듈 \(하나는 기지국용, 다른 하나는 항공기용\)으로 구성됩니다. RTK를 사용하면 PX4는 일반 GPS에서 제공하는 것 보다 훨씬 더 정확한 센티미터 수준의 정확도로 위치를 파악할 수 있습니다.
@@ -8,7 +8,7 @@ The [CUAV C-RTK GPS receiver](https://www.cuav.net/en/c_rtk_9ps/) is an [RTK GPS
## 구매처
- [cuav taobao](https://item.taobao.com/item.htm?id=565380634341&spm=2014.21600712.0.0)
-- [cuav aliexpress](https://www.aliexpress.com/store/product/CUAV-NEW-Flight-Controller-GPS-C-RTK-differential-positioning-navigation-module-GPS-for-PIX4-Pixhawk-pixhack/3257035_32853894248.html?spm=2114.12010608.0.0.75592fadQKPPEn)
+- [cuav aliexpress](https://www.aliexpress.com/item/32853894248.html?spm=2114.12010608.0.0.75592fadQKPPEn)
## 설정
@@ -16,7 +16,7 @@ RTK setup and use on PX4 via _QGroundControl_ is largely plug and play \(see [RT
## 배선
-C-RTK GPS comes with a cable that terminates in a 6-pin connector and 4-pin connector that are compatible with [Pixhack v3](https://doc.cuav.net/flight-controller/pixhack/en/quick-start-pixhack-v3x.html#gps--compass).
+C-RTK GPS comes with a cable that terminates in a 6-pin connector and 4-pin connector that are compatible with [Pixhack v3](../flight_controller/pixhack_v3.md).
6핀 커넥터는 RTK GPS 용 인터페이스를 제공하며 비행 콘트롤러의 GPS 포트에 연결하여야합니다.
4핀 커넥터는 두 번째 GPS로 사용하기 위한 (옵션) m8n (표준) GPS 인터페이스입니다.
diff --git a/docs/ko/gps_compass/rtk_gps_cuav_c-rtk2.md b/docs/ko/gps_compass/rtk_gps_cuav_c-rtk2.md
index 6aea7d8563..14269d956a 100644
--- a/docs/ko/gps_compass/rtk_gps_cuav_c-rtk2.md
+++ b/docs/ko/gps_compass/rtk_gps_cuav_c-rtk2.md
@@ -1,6 +1,6 @@
# CUAV C-RTK2 GNSS Module (RTK/PPK)
-The [CUAV C-RTK2 receiver](https://www.cuav.net/en/c_rtk_9ps/) is a high-performance PPK/RTK positioning module created by CUAV for professional applications such as drone aerial surveying and mapping.
+The [CUAV C-RTK2 receiver](https://www.cuav.net/en/c-rtk-9ps-en/) is a high-performance PPK/RTK positioning module created by CUAV for professional applications such as drone aerial surveying and mapping.
It has a high-precision IMU and positioning module, and can reduce the number of required [control points](https://www.youtube.com/watch?v=3k7v5aXyuKQ) by more than to 80%.
In addition to surveying/mapping, it is suitable for many other use-cases, including: agricultural plant protection and drone swarms.
@@ -10,7 +10,7 @@ In addition to surveying/mapping, it is suitable for many other use-cases, inclu
- High-performance H7 processor
- High precision industrial grade IMU
-- Support RTK and save RAW raw data (PPK) at the same time
+- Support RTK and save raw data (PPK) at the same time
- Multi-satellite and multi-frequency receivers
- UAVCAN/Dronecan protocol
- Support hotshoe and shutter trigger
@@ -18,7 +18,7 @@ In addition to surveying/mapping, it is suitable for many other use-cases, inclu
## 구매처
-- [CUAV Store](https://store.cuav.net/shop/c-rtk-2/)
+- [CUAV Store](https://store.cuav.net/?route=product%2Fproduct&product_id=159)
- [CUAV aliexpress](https://pt.aliexpress.com/item/1005003754165772.html?spm=a2g0o.store_pc_groupList.8148356.13.2f893550i0NE4o)
# 요약
diff --git a/docs/ko/gps_compass/rtk_gps_datagnss_nano_hrtk.md b/docs/ko/gps_compass/rtk_gps_datagnss_nano_hrtk.md
index 4db5b0567e..29845a96b9 100644
--- a/docs/ko/gps_compass/rtk_gps_datagnss_nano_hrtk.md
+++ b/docs/ko/gps_compass/rtk_gps_datagnss_nano_hrtk.md
@@ -90,7 +90,7 @@ Note that for the base we recommend the [NANO RTK Receiver](https://www.datagnss
-See to [How to setup Base station](https://wiki.datagnss.com/index.php/GEM1305-autopilot#Base_station_setup) for information on how to configure the module for use as a base station (not including step 6 and later, for which you would QGroundControl instead of Mission Planner).
+See to [How to setup Base station](https://docs.datagnss.com/#Base_station_setup) for information on how to configure the module for use as a base station (not including step 6 and later, for which you would QGroundControl instead of Mission Planner).
### Rover Setup (PX4)
@@ -111,13 +111,12 @@ GPS and RTK configuration on PX4 via _QGroundControl_ is plug and play (see [RTK
## Resources
-- [NANO RTK Receiver 2D drawing file](https://wiki.datagnss.com/images/3/31/EVK-DG-1206_V.2.0.pdf)
- [NANO HRTK Receiver Wiki](https://docs.datagnss.com/gnss/rtk_receiver/NANO/nano-helix-rtk/) (DATAGNSS WiKi)
- [HED-10L Heading RTK Receiver](https://docs.datagnss.com/gnss/rtk_receiver/HED-10L/)
## More information
-- [NANO RTK Receiver](https://docs.datagnss.com/gnss/rtk_receiver/NANO/nano-rtk-receiver)
+- [NANO RTK Receiver](https://docs.datagnss.com/gnss/rtk_receiver/NANO/nano-rtk-receiver/)
- [HELIX Antenna for RTK](https://www.datagnss.com/collections/rtk-antenna/products/smart-helix-antenna)
- [RTK Antenna AGR6302G](https://www.datagnss.com/collections/rtk-antenna/products/antenna-agr6302g)
- [AT400 RTK Antenna](https://www.datagnss.com/collections/rtk-antenna/products/at400-multi-band-antenna-for-rtk)
diff --git a/docs/ko/gps_compass/rtk_gps_drotek_xl.md b/docs/ko/gps_compass/rtk_gps_drotek_xl.md
index 7b032cad86..b67ca1c93e 100644
--- a/docs/ko/gps_compass/rtk_gps_drotek_xl.md
+++ b/docs/ko/gps_compass/rtk_gps_drotek_xl.md
@@ -2,7 +2,7 @@
:::info
This module appears to have been discontinued, and is no longer on the Drotek site (September 2023).
-The last documentation was in [PX4 v1.13 here](https://docs.px4.io/v1.13/en/gps_compass/rtk_gps_drotek_xl.html)
+The last documentation was in [PX4 v1.13 here](https://docs.px4.io/v1.13/en/gps_compass/rtk_gps_drotek_xl)
:::
diff --git a/docs/ko/gps_compass/rtk_gps_gem1305.md b/docs/ko/gps_compass/rtk_gps_gem1305.md
index a10248fed2..05589e0039 100644
--- a/docs/ko/gps_compass/rtk_gps_gem1305.md
+++ b/docs/ko/gps_compass/rtk_gps_gem1305.md
@@ -77,7 +77,7 @@ The 1.25mm pitch 6P connector (from left: PIN1 to PIN6) supports UART for GNSS a
## 하드웨어 설정
RTK requires a base RTK module attached to the ground station, and a rover RTK module on the vehicle.
-The data from the base needs to be transmitted to the drone via telemetry radio and inputed into the RTK receiver on the rover.
+The data from the base needs to be transmitted to the drone via telemetry radio and inputted into the RTK receiver on the rover.
@@ -93,7 +93,7 @@ Note that for the base we recommend the [NANO RTK Receiver](https://www.datagnss
-See to [How to setup Base station](https://wiki.datagnss.com/index.php/GEM1305-autopilot#Base_station_setup) for information on how to configure the module for use as a base station (not including step 6 and later, for which you would QGroundControl instead of Mission Planner).
+See to [How to setup Base station](https://docs.datagnss.com/#Base_station_setup) for information on how to configure the module for use as a base station (not including step 6 and later, for which you would QGroundControl instead of Mission Planner).
### Rover Setup (PX4)
@@ -115,14 +115,13 @@ GPS and RTK configuration on PX4 via _QGroundControl_ is plug and play (see [RTK
## Resources
-- [NANO RTK Receiver 2D drawing file](https://wiki.datagnss.com/images/3/31/EVK-DG-1206_V.2.0.pdf)
- [GEM1305 Wiki](https://docs.datagnss.com/gnss/rtk_receiver/GEM1305/) (DATAGNSS WiKi)
- [HED-10L Heading RTK Receiver](https://docs.datagnss.com/gnss/rtk_receiver/HED-10L/)
- [NANO HRTK Receiver](https://docs.datagnss.com/gnss/rtk_receiver/NANO/nano-helix-rtk/)
## More information
-- [NANO RTK Receiver](https://www.datagnss.com/collections/evk/products/tau951m-1312-tiny-evk)
+- [NANO RTK Receiver](https://www.datagnss.com/products/nano-rtk-receiver)
- [HELIX Antenna for RTK](https://www.datagnss.com/collections/rtk-antenna/products/smart-helix-antenna)
- [RTK Antenna AGR6302G](https://www.datagnss.com/collections/rtk-antenna/products/antenna-agr6302g)
- [AT400 RTK Antenna](https://www.datagnss.com/collections/rtk-antenna/products/at400-multi-band-antenna-for-rtk)
diff --git a/docs/ko/gps_compass/rtk_gps_hex_hereplus.md b/docs/ko/gps_compass/rtk_gps_hex_hereplus.md
index af20afe92a..0f01c3f646 100644
--- a/docs/ko/gps_compass/rtk_gps_hex_hereplus.md
+++ b/docs/ko/gps_compass/rtk_gps_hex_hereplus.md
@@ -5,7 +5,7 @@
:::info
This GPS is no longer available for purchase but is still compatible with PX4.
-Usage documentation can be found in [PX4v1.11 docs](https://docs.px4.io/v1.11/en/gps_compass/rtk_gps_hex_hereplus.html)
+Usage documentation can be found in [PX4v1.11 docs](https://docs.px4.io/v1.11/en/gps_compass/rtk_gps_hex_hereplus)
:::
The **Here+ RTK GPS receiver** is a small, light and energy efficient [RTK GPS module](../gps_compass/rtk_gps.md), based on the u-blox M8P. RTK를 사용하면 PX4는 일반 GPS에서 제공하는 것 보다 훨씬 더 정확한 센티미터 수준의 정확도로 위치를 파악할 수 있습니다.
diff --git a/docs/ko/gps_compass/rtk_gps_holybro_h-rtk-f9p.md b/docs/ko/gps_compass/rtk_gps_holybro_h-rtk-f9p.md
index aa56937f56..8044dcd28d 100644
--- a/docs/ko/gps_compass/rtk_gps_holybro_h-rtk-f9p.md
+++ b/docs/ko/gps_compass/rtk_gps_holybro_h-rtk-f9p.md
@@ -19,7 +19,7 @@ Using RTK allows PX4 to get its position with centimetre-level accuracy, which i
## 구매처
- [H-RTK F9P (Holybro Website)](https://holybro.com/products/h-rtk-f9p-gnss-series)
-- [H-RTK Accessories (Holybro Website)](https://holybro.com/collections/h-rtk-gps)
+- [H-RTK Accessories (Holybro Website)](https://holybro.com/collections/gps)
## 설정
@@ -50,6 +50,6 @@ The cables/connectors may need to be modified in order to connect to other fligh
## GPS 소품
-[H-RTK Mount (Holybro Website)](https://holybro.com/products/vertical-mount-for-h-rtk-helical)
+[H-RTK Mount (Holybro Website)](https://holybro.com/collections/gps-accessories/products/vertical-mount-for-h-rtk-helical)
diff --git a/docs/ko/gps_compass/rtk_gps_holybro_h-rtk-m8p.md b/docs/ko/gps_compass/rtk_gps_holybro_h-rtk-m8p.md
index 7a62557d76..d2f983c492 100644
--- a/docs/ko/gps_compass/rtk_gps_holybro_h-rtk-m8p.md
+++ b/docs/ko/gps_compass/rtk_gps_holybro_h-rtk-m8p.md
@@ -2,9 +2,10 @@
:::warning
This GNSS has been discontinued, and is no longer commercially available.
+Replaced by [Holybro H-RTK F9P GNSS](../gps_compass/rtk_gps_holybro_h-rtk-f9p.md).
:::
-The [Holybro H-RTK M8P GNSS](https://holybro.com/collections/standard-h-rtk-series/products/h-rtk-m8p-gnss-series) is an [RTK GNSS module](../gps_compass/rtk_gps.md) series for the mass market.
+The _Holybro H-RTK M8P GNSS_ is an [RTK GNSS module](../gps_compass/rtk_gps.md) series for the mass market.
This family is similar to the [H-RTK M9P](../gps_compass/rtk_gps_holybro_h-rtk-f9p.md) series but uses the smaller, lighter, and less expensive M8P u-blox RTK GNSS module (which still provides far superior position resolution than previous generations\_.
Holybro H-RTK M8P에는 세 가지 모델이 있으며, 각각 다른 요구 사항을 충족하기 위해 서로 다른 안테나 디자인을 사용합니다.
@@ -16,7 +17,7 @@ RTK를 사용하면 PX4는 일반 GPS에서 제공하는 것 보다 훨씬 더
## 구매처
-- [H-RTK M8P (GPS RTK Mounts)](https://holybro.com/products/vertical-mount-for-h-rtk-helical)
+- Discontinued.
## 설정
@@ -30,9 +31,7 @@ All H-RTK GNSS models come with a GH 10-pin connector/cable that is compatible w
The cables/connectors may need to be modified in order to connect to other flight controller boards (see [pin map](#pin_map)below).
:::
-
-
-## 핀 맵
+## Pin Map {#pin_map}
diff --git a/docs/ko/gps_compass/rtk_gps_holybro_unicore_um982.md b/docs/ko/gps_compass/rtk_gps_holybro_unicore_um982.md
index 69d2c0de92..af8d6e1264 100644
--- a/docs/ko/gps_compass/rtk_gps_holybro_unicore_um982.md
+++ b/docs/ko/gps_compass/rtk_gps_holybro_unicore_um982.md
@@ -1,10 +1,10 @@
# Holybro H-RTK Unicore UM982 GPS
-The [Holybro H-RTK Unicore UM982 GPS](https://holybro.com/products/h-rtk-um982) is an multi-band high-precision [RTK GNSS System](../gps_compass/rtk_gps.md) launched by Holybro.
+The [Holybro H-RTK Unicore UM982 GPS](https://holybro.com/products/h-rtk-unicore-um982) is an multi-band high-precision [RTK GNSS System](../gps_compass/rtk_gps.md) launched by Holybro.
-This module is based on the [Unicore UM982 Chip](https://en.unicorecomm.com/products/detail/24), which supports RTK positioning and dual-antenna heading calculation.
+This module is based on the [Unicore UM982 Chip](https://en.unicore.com/products/dual-antenna-gnss-um982/), which supports RTK positioning and dual-antenna heading calculation.
This means that it can generate a moving baseline headline/yaw determinations for autopilots with just one GPS module and dual antennas - a magnetometer is not needed.
Unlike when using a module such as the U-blox F9P, where you would need [two U-blox F9P modules to compute a heading angle](../gps_compass/u-blox_f9p_heading.md), with the Unicore UM982 GPS, you only need one GPS module!
@@ -20,7 +20,7 @@ Additional technical information can be found at [Holybro Technical Documentatio
## 구매처
-- [Holybro Website](https://holybro.com/products/h-rtk-um982)
+- [Holybro Website](https://holybro.com/products/h-rtk-unicore-um982)
## 배선
diff --git a/docs/ko/gps_compass/rtk_gps_locosys_r1.md b/docs/ko/gps_compass/rtk_gps_locosys_r1.md
index 0e608794ce..06025daca0 100644
--- a/docs/ko/gps_compass/rtk_gps_locosys_r1.md
+++ b/docs/ko/gps_compass/rtk_gps_locosys_r1.md
@@ -26,7 +26,7 @@ For an equivalent GPS module with a compass try: [LOCOSYS Hawk R2](../gps_compas
- Fast TTFF at low signal level
- Free hybrid ephemeris prediction to achieve faster cold start
- Default 5Hz, up to 10 Hz update rate (SBAS support 5Hz only).
-- Build-in super capacitor to reserve system data for rapid satellite acquisition
+- Built-in super capacitor to reserve system data for rapid satellite acquisition
diff --git a/docs/ko/gps_compass/rtk_gps_locosys_r2.md b/docs/ko/gps_compass/rtk_gps_locosys_r2.md
index d2c9f493f0..534b964f34 100644
--- a/docs/ko/gps_compass/rtk_gps_locosys_r2.md
+++ b/docs/ko/gps_compass/rtk_gps_locosys_r2.md
@@ -22,8 +22,8 @@ The fast time-to-first-fix, RTK convergence, superior sensitivity, low power con
- Fast TTFF at low signal level
- Free hybrid ephemeris prediction to achieve faster cold start
- Default 5Hz, up to 10 Hz update rate (SBAS support 5Hz only)
-- Build-in super capacitor to reserve system data for rapid satellite acquisition
-- Build-in 3 axis compass function
+- Built-in super capacitor to reserve system data for rapid satellite acquisition
+- Built-in 3 axis compass function
- Three LED indicator for Power, PPS and Data transmit
diff --git a/docs/ko/gps_compass/septentrio.md b/docs/ko/gps_compass/septentrio.md
index 2160154b9e..eb31f237cd 100644
--- a/docs/ko/gps_compass/septentrio.md
+++ b/docs/ko/gps_compass/septentrio.md
@@ -10,7 +10,7 @@ Certain receivers are recommended for autopilot applications because of their ph
Dual-antenna, ultra-low-power GNSS rover receiver with support for heading.
-- [AsteRx-m3 Pro+](https://www.septentrio.com/en/products/gps/gnss-boards/asterx-m3-pro-plus)
+- [AsteRx-m3 Pro+](https://www.septentrio.com/en/products/gnss-receivers/gnss-boards/asterx-m3-pro-plus)
Dual-antenna, ultra-low-power versatile GNSS rover and base receiver with support for heading.
@@ -19,7 +19,7 @@ Certain receivers are recommended for autopilot applications because of their ph
Single-antenna evaluation kit with support for L5 frequency band, based on the mosaic-X5 GNSS
receiver module.
-- [mosaic-go heading](https://www.septentrio.com/en/products/gps/gnss-receiver-modules/mosaic-h-evaluation-kit)
+- [mosaic-go heading](https://www.septentrio.com/en/products/gnss-receivers/gnss-receiver-modules/mosaic-h-evaluation-kit)
Dual-antenna evaluation kit with support for heading, based on the mosaic-H GNSS receiver module.
diff --git a/docs/ko/gps_compass/septentrio_mosaic-go.md b/docs/ko/gps_compass/septentrio_mosaic-go.md
index 87dcc69e74..5e7fcd0772 100644
--- a/docs/ko/gps_compass/septentrio_mosaic-go.md
+++ b/docs/ko/gps_compass/septentrio_mosaic-go.md
@@ -2,8 +2,8 @@
The Septentrio mosaic-go receivers are evaluation kits for their mosaic-X5 and mosaic-H receiver modules.
Because of their small size and low weight, they are ideal for autopilot applications.
-The available variants are the [mosaic-go](https://www.septentrio.com/en/products/gps/gnss-receiver-modules/mosaic-go-evaluation-kit)
-and [mosaic-go heading](https://www.septentrio.com/en/products/gps/gnss-receiver-modules/mosaic-h-evaluation-kit).
+The available variants are the [mosaic-go](https://www.septentrio.com/en/products/gnss-receivers/gnss-receiver-modules/mosaic-go-evaluation-kit)
+and [mosaic-go heading](https://www.septentrio.com/en/products/gnss-receivers/gnss-receiver-modules/mosaic-h-evaluation-kit).
@@ -108,7 +108,7 @@ To enable multi-antenna attitude determination, follow the following procedure:
These can be compensated for with the heading parameters provided by the Septentrio driver in PX4.
:::info
-For optimal heading results, the two antennas should be seperated by at least 30cm / 11.8 in (ideally 50cm / 19.7in or more).
+For optimal heading results, the two antennas should be separated by at least 30cm / 11.8 in (ideally 50cm / 19.7in or more).
For additional configuration of the dual antenna setup, please refer to our [Knowledge Base](https://support.septentrio.com/l/858493/2022-04-19/xgrqd) or the [hardware manual](https://web.septentrio.com/l/858493/2022-04-19/xgrql).
:::
diff --git a/docs/ko/gps_compass/u-blox_f9p_heading.md b/docs/ko/gps_compass/u-blox_f9p_heading.md
index b7f672d078..e0640b3111 100644
--- a/docs/ko/gps_compass/u-blox_f9p_heading.md
+++ b/docs/ko/gps_compass/u-blox_f9p_heading.md
@@ -10,7 +10,7 @@ This feature works on F9P devices that support CAN or expose the GPS UART2 port.
The following devices are supported:
- [ARK RTK GPS](https://arkelectron.com/product/ark-rtk-gps/) (arkelectron.com)
-- [SparkFun GPS-RTK2 Board - ZED-F9P](https://www.sparkfun.com/products/15136) (www.sparkfun.com)
+- [SparkFun GPS-RTK2 Board - ZED-F9P](https://www.sparkfun.com/sparkfun-gps-rtk2-board-zed-f9p-qwiic-gps-15136.html) (www.sparkfun.com)
- [SIRIUS RTK GNSS ROVER (F9P)](https://store-drotek.com/911-sirius-rtk-gnss-rover-f9p.html) (store-drotek.com)
- [mRo u-blox ZED-F9 RTK L1/L2 GPS](https://store.mrobotics.io/product-p/m10020d.htm) (store.mrobotics.io)
- [Holybro H-RTK F9P Helical or Base](https://holybro.com/products/h-rtk-f9p-gnss-series) (Holybro Store)
diff --git a/docs/ko/hardware/board_support_guide.md b/docs/ko/hardware/board_support_guide.md
index ad5dec6778..63183773a5 100644
--- a/docs/ko/hardware/board_support_guide.md
+++ b/docs/ko/hardware/board_support_guide.md
@@ -57,7 +57,7 @@ PX4는 일반적으로 상업적으로 사용 가능한 보드만 지원하므
### VER and REV ID (Hardware Revision and Version Sensing) {#ver_rev_id}
FMUv5 이상에는 전기 감지 메커니즘이 있습니다.
-선택적 구성 데이터와 결합된 이 감지는 필수 장치 및 전원 공급 장치 구성과 관련하여 하드웨어 구성을 정의합니다. Manufacturers must obtain the VER and REV ID from PX4 board maintainers by issuing a PR to ammend the [DS-018 Pixhawk standard](https://github.com/pixhawk/Pixhawk-Standards) for board versions and revisions.
+선택적 구성 데이터와 결합된 이 감지는 필수 장치 및 전원 공급 장치 구성과 관련하여 하드웨어 구성을 정의합니다. Manufacturers must obtain the VER and REV ID from PX4 board maintainers by issuing a PR to amend the [DS-018 Pixhawk standard](https://github.com/pixhawk/Pixhawk-Standards) for board versions and revisions.
Because these boards are 100% compliant with the Pixhawk standard, the values assigned for VER and REV ID are the defaults for that FMU Version.
@@ -97,7 +97,7 @@ _New_ experimental boards are allocated [VER and REV IDs](#ver_rev_id) based on
이 범주에는 PX4 프로젝트 또는 제조업체에서 지원하지 않고 "실험적" 지원에 해당하지 않는 모든 보드가 포함됩니다.
- 보드는 우리가 이미 지원하는 것과 문서상 어느 정도 호환되며 "실험적"으로 올리려면, 최소한의 노력이 필요하지만 개발 팀이나 제조업체 모두 현재 이를 추구하지 않습니다.
-- Manufacturer/Owner of hardware violates our [Code of Conduct](https://discuss.px4.io/t/code-of-conduct/13655)
+- Manufacturer/Owner of hardware violates our [Code of Conduct](https://discuss.px4.io/t/px4-community-code-of-conduct/13655)
- 라이선스 제한으로 인해 보드 지원을 추가하는 데 필요한 도구/libs/drivers/etc가 호환되지 않는 것으로 간주되는 비공개 소스
- 보드가 일반 요구 사항에 명시된 최소 요구 사항을 충족하지 않습니다.
diff --git a/docs/ko/hardware/drone_parts.md b/docs/ko/hardware/drone_parts.md
index fe395f1b44..94c826c1ad 100644
--- a/docs/ko/hardware/drone_parts.md
+++ b/docs/ko/hardware/drone_parts.md
@@ -1,4 +1,4 @@
-# Hardware Hardware Selection & Setup
+# Hardware Selection & Setup
PX4 완제품 기체와 자체 제작 드론의 부품들에 대하여 설명합니다.
diff --git a/docs/ko/index.md b/docs/ko/index.md
index 339b6ecf6c..bc3b4a558c 100644
--- a/docs/ko/index.md
+++ b/docs/ko/index.md
@@ -5,7 +5,7 @@ const { site } = useData();
# PX4 Autopilot 사용자 안내서
-[](https://github.com/PX4/PX4-Autopilot/releases) [](https://discuss.px4.io//) [](https://discord.gg/dronecode)
+[](https://github.com/PX4/PX4-Autopilot/releases) [](https://discuss.px4.io//) [](https://discord.com/invite/dronecode)
PX4 is an open-source autopilot for drones and autonomous vehicles. It runs on multirotors, fixed-wing, VTOL, helicopters, rovers, and more. This guide covers everything from assembly and configuration to flight operations and development.
@@ -49,7 +49,7 @@ Read [Operations](config/operations.md) to understand safety features and failsa
## 지원
-Get help on the [discussion forums](https://discuss.px4.io/) or [Discord](https://discord.gg/dronecode). See the [Support](contribute/support.md) page for diagnosing problems, reporting bugs, and joining the [weekly dev call](contribute/dev_call.md).
+Get help on the [discussion forums](https://discuss.px4.io/) or [Discord](https://discord.com/invite/dronecode). See the [Support](contribute/support.md) page for diagnosing problems, reporting bugs, and joining the [weekly dev call](contribute/dev_call.md).
## 기여
@@ -94,9 +94,9 @@ The calendar default timezone is Central European Time (CET).
## 운영 방법
-The PX4 Autopilot project is hosted by the [Dronecode Foundation](https://www.dronecode.org/), a [Linux Foundation](https://www.linuxfoundation.org/) Collaborative Project. Dronecode holds all PX4 trademarks and serves as the project's legal guardian, ensuring vendor-neutral stewardship. No single company owns the name or controls the roadmap. The source code is licensed under the [BSD 3-Clause](https://opensource.org/license/BSD-3-Clause) license, so you are free to use, modify, and distribute it in your own projects.
+The PX4 Autopilot project is hosted by the [Dronecode Foundation](https://dronecode.org/), a [Linux Foundation](https://www.linuxfoundation.org/) Collaborative Project. Dronecode holds all PX4 trademarks and serves as the project's legal guardian, ensuring vendor-neutral stewardship. No single company owns the name or controls the roadmap. The source code is licensed under the [BSD 3-Clause](https://opensource.org/license/BSD-3-Clause) license, so you are free to use, modify, and distribute it in your own projects.
-
+
diff --git a/docs/ko/mavlink/adding_messages.md b/docs/ko/mavlink/adding_messages.md
index 275e8de7d5..87de83d3f9 100644
--- a/docs/ko/mavlink/adding_messages.md
+++ b/docs/ko/mavlink/adding_messages.md
@@ -39,7 +39,7 @@ Once the message headers for your definitions are generated in the PX4 build, yo
The first step in debugging is to confirm that any messages you've created are being sent/received as you expect.
-You should should first use the `uorb top []` command to verify in real-time that your message is published and the rate (see [uORB Messaging](../middleware/uorb.md#uorb-top-command)).
+You should first use the `uorb top []` command to verify in real-time that your message is published and the rate (see [uORB Messaging](../middleware/uorb.md#uorb-top-command)).
This approach can also be used to test incoming messages that publish a uORB topic (for other messages you might use `printf` in your code and test in SITL).
There are several approaches you can use to view MAVLink traffic:
@@ -82,16 +82,16 @@ So if you have created a custom message in PX4 you won't be able to use it unles
### Updating QGroundControl
-You will need to [Build QGroundControl](https://docs.qgroundcontrol.com/master/en/qgc-dev-guide/getting_started/index.html) including a pre-built C library that contains your custom messages.
+You will need to [Build QGroundControl](https://docs.qgroundcontrol.com/master/en/qgc-dev-guide/getting_started/index.html) with your custom messages included.
-QGC uses a pre-built C library that must be located at [/qgroundcontrol/libs/mavlink/include/mavlink](https://github.com/mavlink/qgroundcontrol/tree/master/libs/mavlink/include/mavlink) in the QGC source.
+QGC fetches MAVLink via CMake using settings defined in [`cmake/CustomOptions.cmake`](https://github.com/mavlink/qgroundcontrol/blob/master/cmake/CustomOptions.cmake).
+The key variables are `QGC_MAVLINK_GIT_REPO` (the MAVLink repository to fetch), `QGC_MAVLINK_GIT_TAG` (a specific commit or tag), and `QGC_MAVLINK_DIALECT` (the dialect, default: `all`).
+To use a custom MAVLink repository or dialect, override these in a `CustomOverrides.cmake` file in the QGC source root.
-By default this is pre-included as a submodule from but you can [generate your own MAVLink Libraries](https://mavlink.io/en/getting_started/generate_libraries.html).
+QGC uses the **all** dialect by default, which includes **common.xml**.
+You can include your messages in either file, or [generate your own MAVLink Libraries](https://mavlink.io/en/getting_started/generate_libraries.html).
-QGC uses the **all.xml** dialect by default, which includes **common.xml**.
-You can include your messages in either file.
-
-Note that if you use your own _custom dialect_ then it should include **ArduPilotMega.xml** (or it will miss all the existing messages), and you will need to change the dialect used by setting it in [`MAVLINK_CONF`](https://github.com/mavlink/qgroundcontrol/blob/master/QGCExternalLibs.pri#L52) when running _qmake_.
+Note that if you use your own _custom dialect_ then it should include **all.xml** (or it may miss all the existing messages), and you will need to set `QGC_MAVLINK_DIALECT` accordingly in `CustomOverrides.cmake`.
### Updating MAVSDK
diff --git a/docs/ko/mavlink/index.md b/docs/ko/mavlink/index.md
index 53ed4c4a1f..c5e4bd47f1 100644
--- a/docs/ko/mavlink/index.md
+++ b/docs/ko/mavlink/index.md
@@ -77,7 +77,7 @@ You will need to work with the [MAVLink team](https://mavlink.io/en/contributing
:::
PX4 includes the [mavlink/mavlink](https://github.com/mavlink/mavlink) repo as a submodule under [/src/modules/mavlink](https://github.com/PX4/PX4-Autopilot/tree/main/src/modules/mavlink).
-This contains XML definition files in [/mavlink/messages/1.0/](https://github.com/mavlink/mavlink/blob/master/message_definitions/v1.0/).
+This contains XML definition files in [/mavlink/messages/1.0/](https://github.com/mavlink/mavlink/tree/master/message_definitions/v1.0).
The build toolchain generates the MAVLink 2 C header files at build time.
The XML file for which headers files are generated may be defined in the [PX4 kconfig board configuration](../hardware/porting_guide_config.md#px4-board-configuration-kconfig) on a per-board basis, using the variable `CONFIG_MAVLINK_DIALECT`:
diff --git a/docs/ko/middleware/dds_topics.md b/docs/ko/middleware/dds_topics.md
index 642635db4c..514379d670 100644
--- a/docs/ko/middleware/dds_topics.md
+++ b/docs/ko/middleware/dds_topics.md
@@ -70,7 +70,6 @@ This document shows a markdown-rendered version of [dds_topics.yaml](https://git
| /fmu/in/vehicle_torque_setpoint | [px4_msgs::msg::VehicleTorqueSetpoint](../msg_docs/VehicleTorqueSetpoint.md) |
| /fmu/in/actuator_motors | [px4_msgs::msg::ActuatorMotors](../msg_docs/ActuatorMotors.md) |
| /fmu/in/actuator_servos | [px4_msgs::msg::ActuatorServos](../msg_docs/ActuatorServos.md) |
-| /fmu/in/aux_global_position | [px4_msgs::msg::VehicleGlobalPosition](../msg_docs/VehicleGlobalPosition.md) |
| /fmu/in/fixed_wing_longitudinal_setpoint | [px4_msgs::msg::FixedWingLongitudinalSetpoint](../msg_docs/FixedWingLongitudinalSetpoint.md) |
| /fmu/in/fixed_wing_lateral_setpoint | [px4_msgs::msg::FixedWingLateralSetpoint](../msg_docs/FixedWingLateralSetpoint.md) |
| /fmu/in/longitudinal_control_configuration | [px4_msgs::msg::LongitudinalControlConfiguration](../msg_docs/LongitudinalControlConfiguration.md) |
@@ -85,7 +84,9 @@ This document shows a markdown-rendered version of [dds_topics.yaml](https://git
## Subscriptions Multi
-None
+| Topic | 형식 | Route Field | Max Instances |
+| --------------------------------------------------------------------- | --------------------------------------------------------------------------------------------------------------------------------------------------------- | ----------- | ------------- |
+| /fmu/in/aux_global_position | [px4_msgs::msg::AuxGlobalPosition](../msg_docs/AuxGlobalPosition.md) | `id` | 4 |
## Not Exported
@@ -95,200 +96,203 @@ They are not build into the module, and hence are neither published or subscribe
:::details
See messages
-- [GpioIn](../msg_docs/GpioIn.md)
-- [SystemPower](../msg_docs/SystemPower.md)
-- [LandingTargetInnovations](../msg_docs/LandingTargetInnovations.md)
-- [VehicleOpticalFlow](../msg_docs/VehicleOpticalFlow.md)
-- [LandingTargetPose](../msg_docs/LandingTargetPose.md)
-- [EstimatorGpsStatus](../msg_docs/EstimatorGpsStatus.md)
-- [EstimatorBias](../msg_docs/EstimatorBias.md)
-- [ParameterSetValueResponse](../msg_docs/ParameterSetValueResponse.md)
-- [LogMessage](../msg_docs/LogMessage.md)
-- [PowerMonitor](../msg_docs/PowerMonitor.md)
-- [VehicleConstraints](../msg_docs/VehicleConstraints.md)
-- [SensorAirflow](../msg_docs/SensorAirflow.md)
-- [ArmingCheckRequestV0](../msg_docs/ArmingCheckRequestV0.md)
-- [ActuatorArmed](../msg_docs/ActuatorArmed.md)
-- [HoverThrustEstimate](../msg_docs/HoverThrustEstimate.md)
-- [LaunchDetectionStatus](../msg_docs/LaunchDetectionStatus.md)
-- [DifferentialPressure](../msg_docs/DifferentialPressure.md)
-- [MagnetometerBiasEstimate](../msg_docs/MagnetometerBiasEstimate.md)
-- [PwmInput](../msg_docs/PwmInput.md)
-- [OrbTestMedium](../msg_docs/OrbTestMedium.md)
-- [QshellReq](../msg_docs/QshellReq.md)
-- [GeofenceStatus](../msg_docs/GeofenceStatus.md)
-- [RcChannels](../msg_docs/RcChannels.md)
-- [Cpuload](../msg_docs/Cpuload.md)
-- [DebugArray](../msg_docs/DebugArray.md)
-- [FlightPhaseEstimation](../msg_docs/FlightPhaseEstimation.md)
-- [Mission](../msg_docs/Mission.md)
-- [Airspeed](../msg_docs/Airspeed.md)
-- [LedControl](../msg_docs/LedControl.md)
-- [HealthReport](../msg_docs/HealthReport.md)
-- [FixedWingLateralGuidanceStatus](../msg_docs/FixedWingLateralGuidanceStatus.md)
-- [FigureEightStatus](../msg_docs/FigureEightStatus.md)
-- [EstimatorInnovations](../msg_docs/EstimatorInnovations.md)
-- [VehicleImuStatus](../msg_docs/VehicleImuStatus.md)
-- [VehicleLocalPositionSetpoint](../msg_docs/VehicleLocalPositionSetpoint.md)
-- [InputRc](../msg_docs/InputRc.md)
-- [UavcanParameterRequest](../msg_docs/UavcanParameterRequest.md)
-- [FixedWingRunwayControl](../msg_docs/FixedWingRunwayControl.md)
-- [SensorCorrection](../msg_docs/SensorCorrection.md)
-- [ControlAllocatorStatus](../msg_docs/ControlAllocatorStatus.md)
-- [AirspeedValidatedV0](../msg_docs/AirspeedValidatedV0.md)
-- [CanInterfaceStatus](../msg_docs/CanInterfaceStatus.md)
-- [SensorSelection](../msg_docs/SensorSelection.md)
-- [DeviceInformation](../msg_docs/DeviceInformation.md)
-- [CameraTrigger](../msg_docs/CameraTrigger.md)
-- [SensorAccel](../msg_docs/SensorAccel.md)
-- [ActuatorServosTrim](../msg_docs/ActuatorServosTrim.md)
-- [SensorsStatusImu](../msg_docs/SensorsStatusImu.md)
-- [EstimatorBias3d](../msg_docs/EstimatorBias3d.md)
-- [GimbalManagerStatus](../msg_docs/GimbalManagerStatus.md)
-- [BatteryStatusV0](../msg_docs/BatteryStatusV0.md)
-- [OpenDroneIdSelfId](../msg_docs/OpenDroneIdSelfId.md)
-- [VehicleImu](../msg_docs/VehicleImu.md)
-- [MissionResult](../msg_docs/MissionResult.md)
-- [SensorAccelFifo](../msg_docs/SensorAccelFifo.md)
-- [DistanceSensorModeChangeRequest](../msg_docs/DistanceSensorModeChangeRequest.md)
-- [SensorPreflightMag](../msg_docs/SensorPreflightMag.md)
-- [OrbTest](../msg_docs/OrbTest.md)
-- [PositionControllerLandingStatus](../msg_docs/PositionControllerLandingStatus.md)
-- [FuelTankStatus](../msg_docs/FuelTankStatus.md)
-- [OpenDroneIdSystem](../msg_docs/OpenDroneIdSystem.md)
-- [OrbitStatus](../msg_docs/OrbitStatus.md)
-- [Px4ioStatus](../msg_docs/Px4ioStatus.md)
-- [RtlStatus](../msg_docs/RtlStatus.md)
-- [ButtonEvent](../msg_docs/ButtonEvent.md)
-- [VehicleLocalPositionV0](../msg_docs/VehicleLocalPositionV0.md)
-- [DebugValue](../msg_docs/DebugValue.md)
-- [ParameterSetUsedRequest](../msg_docs/ParameterSetUsedRequest.md)
-- [RoverSpeedStatus](../msg_docs/RoverSpeedStatus.md)
-- [SensorHygrometer](../msg_docs/SensorHygrometer.md)
-- [OpenDroneIdOperatorId](../msg_docs/OpenDroneIdOperatorId.md)
-- [InternalCombustionEngineStatus](../msg_docs/InternalCombustionEngineStatus.md)
-- [GpioOut](../msg_docs/GpioOut.md)
-- [ActuatorTest](../msg_docs/ActuatorTest.md)
-- [SensorBaro](../msg_docs/SensorBaro.md)
-- [PositionControllerStatus](../msg_docs/PositionControllerStatus.md)
-- [PurePursuitStatus](../msg_docs/PurePursuitStatus.md)
-- [RoverRateStatus](../msg_docs/RoverRateStatus.md)
-- [TecsStatus](../msg_docs/TecsStatus.md)
-- [PpsCapture](../msg_docs/PpsCapture.md)
-- [RaptorStatus](../msg_docs/RaptorStatus.md)
-- [EventV0](../msg_docs/EventV0.md)
-- [GpioRequest](../msg_docs/GpioRequest.md)
-- [FollowTargetEstimator](../msg_docs/FollowTargetEstimator.md)
-- [MagWorkerData](../msg_docs/MagWorkerData.md)
-- [FollowTarget](../msg_docs/FollowTarget.md)
-- [EstimatorAidSource1d](../msg_docs/EstimatorAidSource1d.md)
-- [GimbalDeviceSetAttitude](../msg_docs/GimbalDeviceSetAttitude.md)
-- [SensorGnssRelative](../msg_docs/SensorGnssRelative.md)
-- [ActionRequest](../msg_docs/ActionRequest.md)
-- [NavigatorMissionItem](../msg_docs/NavigatorMissionItem.md)
-- [GpsInjectData](../msg_docs/GpsInjectData.md)
-- [VehicleStatusV0](../msg_docs/VehicleStatusV0.md)
-- [DronecanNodeStatus](../msg_docs/DronecanNodeStatus.md)
-- [UlogStream](../msg_docs/UlogStream.md)
-- [DebugKeyValue](../msg_docs/DebugKeyValue.md)
-- [NavigatorStatus](../msg_docs/NavigatorStatus.md)
-- [MountOrientation](../msg_docs/MountOrientation.md)
-- [RcParameterMap](../msg_docs/RcParameterMap.md)
-- [AdcReport](../msg_docs/AdcReport.md)
-- [EstimatorSensorBias](../msg_docs/EstimatorSensorBias.md)
-- [InternalCombustionEngineControl](../msg_docs/InternalCombustionEngineControl.md)
-- [MavlinkLog](../msg_docs/MavlinkLog.md)
-- [VehicleMagnetometer](../msg_docs/VehicleMagnetometer.md)
- [GpioConfig](../msg_docs/GpioConfig.md)
-- [GainCompression](../msg_docs/GainCompression.md)
-- [DebugVect](../msg_docs/DebugVect.md)
-- [ArmingCheckReplyV0](../msg_docs/ArmingCheckReplyV0.md)
-- [VehicleAttitudeSetpointV0](../msg_docs/VehicleAttitudeSetpointV0.md)
-- [FollowTargetStatus](../msg_docs/FollowTargetStatus.md)
-- [RtlTimeEstimate](../msg_docs/RtlTimeEstimate.md)
-- [RoverAttitudeStatus](../msg_docs/RoverAttitudeStatus.md)
-- [SensorUwb](../msg_docs/SensorUwb.md)
-- [YawEstimatorStatus](../msg_docs/YawEstimatorStatus.md)
-- [VelocityLimits](../msg_docs/VelocityLimits.md)
-- [TrajectorySetpoint6dof](../msg_docs/TrajectorySetpoint6dof.md)
-- [OpenDroneIdArmStatus](../msg_docs/OpenDroneIdArmStatus.md)
-- [EscStatus](../msg_docs/EscStatus.md)
-- [GimbalManagerInformation](../msg_docs/GimbalManagerInformation.md)
-- [HeaterStatus](../msg_docs/HeaterStatus.md)
-- [EstimatorSelectorStatus](../msg_docs/EstimatorSelectorStatus.md)
-- [GeofenceResult](../msg_docs/GeofenceResult.md)
-- [PowerButtonState](../msg_docs/PowerButtonState.md)
-- [Rpm](../msg_docs/Rpm.md)
-- [WheelEncoders](../msg_docs/WheelEncoders.md)
-- [LoggerStatus](../msg_docs/LoggerStatus.md)
-- [CellularStatus](../msg_docs/CellularStatus.md)
-- [TuneControl](../msg_docs/TuneControl.md)
-- [ConfigOverridesV0](../msg_docs/ConfigOverridesV0.md)
-- [GimbalManagerSetAttitude](../msg_docs/GimbalManagerSetAttitude.md)
-- [OrbTestLarge](../msg_docs/OrbTestLarge.md)
-- [BatteryInfo](../msg_docs/BatteryInfo.md)
-- [CameraStatus](../msg_docs/CameraStatus.md)
-- [QshellRetval](../msg_docs/QshellRetval.md)
-- [SensorMag](../msg_docs/SensorMag.md)
-- [RateCtrlStatus](../msg_docs/RateCtrlStatus.md)
-- [TaskStackInfo](../msg_docs/TaskStackInfo.md)
-- [EstimatorAidSource2d](../msg_docs/EstimatorAidSource2d.md)
-- [AirspeedWind](../msg_docs/AirspeedWind.md)
-- [AutotuneAttitudeControlStatus](../msg_docs/AutotuneAttitudeControlStatus.md)
-- [GimbalDeviceInformation](../msg_docs/GimbalDeviceInformation.md)
-- [GpsDump](../msg_docs/GpsDump.md)
-- [SensorTemp](../msg_docs/SensorTemp.md)
-- [ParameterResetRequest](../msg_docs/ParameterResetRequest.md)
-- [TiltrotorExtraControls](../msg_docs/TiltrotorExtraControls.md)
-- [SensorsStatus](../msg_docs/SensorsStatus.md)
-- [EstimatorStatus](../msg_docs/EstimatorStatus.md)
-- [FailureDetectorStatus](../msg_docs/FailureDetectorStatus.md)
-- [VehicleAirData](../msg_docs/VehicleAirData.md)
-- [ActuatorControlsStatus](../msg_docs/ActuatorControlsStatus.md)
-- [TakeoffStatus](../msg_docs/TakeoffStatus.md)
-- [GeneratorStatus](../msg_docs/GeneratorStatus.md)
-- [SensorGyroFifo](../msg_docs/SensorGyroFifo.md)
-- [VehicleAngularVelocity](../msg_docs/VehicleAngularVelocity.md)
-- [LandingGearWheel](../msg_docs/LandingGearWheel.md)
-- [ParameterSetValueRequest](../msg_docs/ParameterSetValueRequest.md)
-- [RegisterExtComponentReplyV0](../msg_docs/RegisterExtComponentReplyV0.md)
-- [RaptorInput](../msg_docs/RaptorInput.md)
-- [SensorGyro](../msg_docs/SensorGyro.md)
-- [ParameterUpdate](../msg_docs/ParameterUpdate.md)
-- [NormalizedUnsignedSetpoint](../msg_docs/NormalizedUnsignedSetpoint.md)
-- [PositionSetpoint](../msg_docs/PositionSetpoint.md)
-- [EstimatorStates](../msg_docs/EstimatorStates.md)
-- [ActuatorOutputs](../msg_docs/ActuatorOutputs.md)
-- [ManualControlSwitches](../msg_docs/ManualControlSwitches.md)
-- [UavcanParameterValue](../msg_docs/UavcanParameterValue.md)
-- [VehicleAngularAccelerationSetpoint](../msg_docs/VehicleAngularAccelerationSetpoint.md)
-- [EstimatorEventFlags](../msg_docs/EstimatorEventFlags.md)
-- [SensorGnssStatus](../msg_docs/SensorGnssStatus.md)
-- [GimbalManagerSetManualControl](../msg_docs/GimbalManagerSetManualControl.md)
-- [HomePositionV0](../msg_docs/HomePositionV0.md)
-- [FixedWingLateralStatus](../msg_docs/FixedWingLateralStatus.md)
-- [SatelliteInfo](../msg_docs/SatelliteInfo.md)
-- [IrlockReport](../msg_docs/IrlockReport.md)
-- [Ping](../msg_docs/Ping.md)
-- [CameraCapture](../msg_docs/CameraCapture.md)
-- [Vtx](../msg_docs/Vtx.md)
-- [Ekf2Timestamps](../msg_docs/Ekf2Timestamps.md)
-- [RegisterExtComponentRequestV0](../msg_docs/RegisterExtComponentRequestV0.md)
-- [EscReport](../msg_docs/EscReport.md)
-- [Gripper](../msg_docs/Gripper.md)
-- [UlogStreamAck](../msg_docs/UlogStreamAck.md)
-- [SensorGyroFft](../msg_docs/SensorGyroFft.md)
-- [VehicleRoi](../msg_docs/VehicleRoi.md)
-- [VehicleAcceleration](../msg_docs/VehicleAcceleration.md)
-- [NeuralControl](../msg_docs/NeuralControl.md)
-- [DatamanResponse](../msg_docs/DatamanResponse.md)
-- [GimbalControls](../msg_docs/GimbalControls.md)
-- [MavlinkTunnel](../msg_docs/MavlinkTunnel.md)
-- [EstimatorAidSource3d](../msg_docs/EstimatorAidSource3d.md)
-- [DatamanRequest](../msg_docs/DatamanRequest.md)
+- [MavlinkLog](../msg_docs/MavlinkLog.md)
- [Event](../msg_docs/Event.md)
-- [RadioStatus](../msg_docs/RadioStatus.md)
-- [VehicleOpticalFlowVel](../msg_docs/VehicleOpticalFlowVel.md)
+- [EstimatorBias3d](../msg_docs/EstimatorBias3d.md)
+- [MagWorkerData](../msg_docs/MagWorkerData.md)
+- [OrbTest](../msg_docs/OrbTest.md)
+- [RtlTimeEstimate](../msg_docs/RtlTimeEstimate.md)
+- [EventV0](../msg_docs/EventV0.md)
+- [TiltrotorExtraControls](../msg_docs/TiltrotorExtraControls.md)
+- [EstimatorBias](../msg_docs/EstimatorBias.md)
+- [QshellRetval](../msg_docs/QshellRetval.md)
- [IridiumsbdStatus](../msg_docs/IridiumsbdStatus.md)
+- [GpioIn](../msg_docs/GpioIn.md)
+- [Px4ioStatus](../msg_docs/Px4ioStatus.md)
+- [UavcanParameterRequest](../msg_docs/UavcanParameterRequest.md)
+- [RegisterExtComponentReplyV0](../msg_docs/RegisterExtComponentReplyV0.md)
+- [Airspeed](../msg_docs/Airspeed.md)
+- [SensorMag](../msg_docs/SensorMag.md)
+- [QshellReq](../msg_docs/QshellReq.md)
+- [RcChannels](../msg_docs/RcChannels.md)
+- [FuelTankStatus](../msg_docs/FuelTankStatus.md)
+- [ParameterSetValueResponse](../msg_docs/ParameterSetValueResponse.md)
+- [VehicleOpticalFlowVel](../msg_docs/VehicleOpticalFlowVel.md)
+- [ActuatorControlsStatus](../msg_docs/ActuatorControlsStatus.md)
+- [TecsStatus](../msg_docs/TecsStatus.md)
+- [CameraStatus](../msg_docs/CameraStatus.md)
+- [FollowTargetStatus](../msg_docs/FollowTargetStatus.md)
+- [DistanceSensorModeChangeRequest](../msg_docs/DistanceSensorModeChangeRequest.md)
+- [DatamanRequest](../msg_docs/DatamanRequest.md)
+- [SensorAccel](../msg_docs/SensorAccel.md)
+- [HomePositionV0](../msg_docs/HomePositionV0.md)
+- [VehicleMagnetometer](../msg_docs/VehicleMagnetometer.md)
+- [SensorGnssStatus](../msg_docs/SensorGnssStatus.md)
+- [GimbalDeviceInformation](../msg_docs/GimbalDeviceInformation.md)
+- [VehicleGlobalPositionV0](../msg_docs/VehicleGlobalPositionV0.md)
+- [OrbitStatus](../msg_docs/OrbitStatus.md)
+- [RcParameterMap](../msg_docs/RcParameterMap.md)
+- [PowerButtonState](../msg_docs/PowerButtonState.md)
+- [GpioRequest](../msg_docs/GpioRequest.md)
+- [VehicleRoi](../msg_docs/VehicleRoi.md)
+- [EstimatorEventFlags](../msg_docs/EstimatorEventFlags.md)
+- [VehicleStatusV0](../msg_docs/VehicleStatusV0.md)
+- [YawEstimatorStatus](../msg_docs/YawEstimatorStatus.md)
+- [ParameterSetValueRequest](../msg_docs/ParameterSetValueRequest.md)
+- [LandingTargetInnovations](../msg_docs/LandingTargetInnovations.md)
+- [EscStatus](../msg_docs/EscStatus.md)
+- [GimbalManagerSetManualControl](../msg_docs/GimbalManagerSetManualControl.md)
+- [OpenDroneIdSystem](../msg_docs/OpenDroneIdSystem.md)
+- [SensorHygrometer](../msg_docs/SensorHygrometer.md)
+- [GpioOut](../msg_docs/GpioOut.md)
+- [FlightPhaseEstimation](../msg_docs/FlightPhaseEstimation.md)
+- [ActionRequest](../msg_docs/ActionRequest.md)
+- [GimbalControls](../msg_docs/GimbalControls.md)
+- [MountOrientation](../msg_docs/MountOrientation.md)
+- [LedControl](../msg_docs/LedControl.md)
+- [UlogStreamAck](../msg_docs/UlogStreamAck.md)
+- [EstimatorAidSource1d](../msg_docs/EstimatorAidSource1d.md)
+- [DronecanNodeStatus](../msg_docs/DronecanNodeStatus.md)
+- [VehicleConstraints](../msg_docs/VehicleConstraints.md)
+- [VehicleAirData](../msg_docs/VehicleAirData.md)
+- [BatteryInfo](../msg_docs/BatteryInfo.md)
+- [GimbalManagerInformation](../msg_docs/GimbalManagerInformation.md)
+- [RaptorInput](../msg_docs/RaptorInput.md)
+- [RoverAttitudeStatus](../msg_docs/RoverAttitudeStatus.md)
+- [Ekf2Timestamps](../msg_docs/Ekf2Timestamps.md)
+- [PositionControllerStatus](../msg_docs/PositionControllerStatus.md)
+- [VehicleImu](../msg_docs/VehicleImu.md)
+- [AirspeedValidatedV0](../msg_docs/AirspeedValidatedV0.md)
+- [VehicleAngularAccelerationSetpoint](../msg_docs/VehicleAngularAccelerationSetpoint.md)
+- [ConfigOverridesV0](../msg_docs/ConfigOverridesV0.md)
+- [EstimatorAidSource2d](../msg_docs/EstimatorAidSource2d.md)
+- [SensorUwb](../msg_docs/SensorUwb.md)
+- [LogMessage](../msg_docs/LogMessage.md)
+- [EstimatorSelectorStatus](../msg_docs/EstimatorSelectorStatus.md)
+- [VehicleStatusV1](../msg_docs/VehicleStatusV1.md)
+- [ActuatorServosTrim](../msg_docs/ActuatorServosTrim.md)
+- [SensorGnssRelative](../msg_docs/SensorGnssRelative.md)
+- [LandingGearWheel](../msg_docs/LandingGearWheel.md)
+- [SensorTemp](../msg_docs/SensorTemp.md)
+- [SensorGyro](../msg_docs/SensorGyro.md)
+- [PowerMonitor](../msg_docs/PowerMonitor.md)
+- [UavcanParameterValue](../msg_docs/UavcanParameterValue.md)
+- [TrajectorySetpoint6dof](../msg_docs/TrajectorySetpoint6dof.md)
+- [HeaterStatus](../msg_docs/HeaterStatus.md)
+- [SensorAirflow](../msg_docs/SensorAirflow.md)
+- [TakeoffStatus](../msg_docs/TakeoffStatus.md)
+- [ControlAllocatorStatus](../msg_docs/ControlAllocatorStatus.md)
+- [LoggerStatus](../msg_docs/LoggerStatus.md)
+- [TuneControl](../msg_docs/TuneControl.md)
+- [GpsDump](../msg_docs/GpsDump.md)
+- [WheelEncoders](../msg_docs/WheelEncoders.md)
+- [PurePursuitStatus](../msg_docs/PurePursuitStatus.md)
+- [VehicleAcceleration](../msg_docs/VehicleAcceleration.md)
+- [EstimatorGpsStatus](../msg_docs/EstimatorGpsStatus.md)
+- [MagnetometerBiasEstimate](../msg_docs/MagnetometerBiasEstimate.md)
+- [ManualControlSwitches](../msg_docs/ManualControlSwitches.md)
+- [SensorPreflightMag](../msg_docs/SensorPreflightMag.md)
+- [HealthReport](../msg_docs/HealthReport.md)
+- [SensorGyroFifo](../msg_docs/SensorGyroFifo.md)
+- [GpsInjectData](../msg_docs/GpsInjectData.md)
+- [OpenDroneIdArmStatus](../msg_docs/OpenDroneIdArmStatus.md)
+- [EscReport](../msg_docs/EscReport.md)
+- [DebugKeyValue](../msg_docs/DebugKeyValue.md)
+- [ActuatorOutputs](../msg_docs/ActuatorOutputs.md)
+- [GimbalDeviceSetAttitude](../msg_docs/GimbalDeviceSetAttitude.md)
+- [LandingTargetPose](../msg_docs/LandingTargetPose.md)
+- [GeofenceStatus](../msg_docs/GeofenceStatus.md)
+- [FailureDetectorStatus](../msg_docs/FailureDetectorStatus.md)
+- [MavlinkTunnel](../msg_docs/MavlinkTunnel.md)
+- [SensorCorrection](../msg_docs/SensorCorrection.md)
+- [ParameterUpdate](../msg_docs/ParameterUpdate.md)
+- [RateCtrlStatus](../msg_docs/RateCtrlStatus.md)
+- [DifferentialPressure](../msg_docs/DifferentialPressure.md)
+- [PositionSetpoint](../msg_docs/PositionSetpoint.md)
+- [OpenDroneIdOperatorId](../msg_docs/OpenDroneIdOperatorId.md)
+- [OrbTestMedium](../msg_docs/OrbTestMedium.md)
+- [SensorsStatusImu](../msg_docs/SensorsStatusImu.md)
+- [EstimatorStatus](../msg_docs/EstimatorStatus.md)
+- [SensorAccelFifo](../msg_docs/SensorAccelFifo.md)
+- [VehicleLocalPositionSetpoint](../msg_docs/VehicleLocalPositionSetpoint.md)
+- [RegisterExtComponentRequestV0](../msg_docs/RegisterExtComponentRequestV0.md)
+- [VehicleCommandAckV0](../msg_docs/VehicleCommandAckV0.md)
+- [EstimatorStates](../msg_docs/EstimatorStates.md)
+- [CameraCapture](../msg_docs/CameraCapture.md)
+- [RadioStatus](../msg_docs/RadioStatus.md)
+- [EstimatorSensorBias](../msg_docs/EstimatorSensorBias.md)
+- [SensorsStatus](../msg_docs/SensorsStatus.md)
+- [VehicleAttitudeSetpointV0](../msg_docs/VehicleAttitudeSetpointV0.md)
+- [NeuralControl](../msg_docs/NeuralControl.md)
+- [FixedWingLateralStatus](../msg_docs/FixedWingLateralStatus.md)
+- [EstimatorAidSource3d](../msg_docs/EstimatorAidSource3d.md)
+- [FollowTargetEstimator](../msg_docs/FollowTargetEstimator.md)
+- [GimbalManagerStatus](../msg_docs/GimbalManagerStatus.md)
+- [GeofenceResult](../msg_docs/GeofenceResult.md)
+- [SystemPower](../msg_docs/SystemPower.md)
+- [NavigatorMissionItem](../msg_docs/NavigatorMissionItem.md)
+- [VehicleImuStatus](../msg_docs/VehicleImuStatus.md)
+- [ArmingCheckReplyV0](../msg_docs/ArmingCheckReplyV0.md)
+- [CameraTrigger](../msg_docs/CameraTrigger.md)
+- [NormalizedUnsignedSetpoint](../msg_docs/NormalizedUnsignedSetpoint.md)
+- [RoverRateStatus](../msg_docs/RoverRateStatus.md)
+- [NavigatorStatus](../msg_docs/NavigatorStatus.md)
+- [VehicleLocalPositionV0](../msg_docs/VehicleLocalPositionV0.md)
+- [VelocityLimits](../msg_docs/VelocityLimits.md)
+- [Gripper](../msg_docs/Gripper.md)
+- [Mission](../msg_docs/Mission.md)
+- [RtlStatus](../msg_docs/RtlStatus.md)
+- [GainCompression](../msg_docs/GainCompression.md)
+- [DatamanResponse](../msg_docs/DatamanResponse.md)
+- [BatteryStatusV0](../msg_docs/BatteryStatusV0.md)
+- [SensorGyroFft](../msg_docs/SensorGyroFft.md)
+- [DeviceInformation](../msg_docs/DeviceInformation.md)
+- [UlogStream](../msg_docs/UlogStream.md)
+- [SensorSelection](../msg_docs/SensorSelection.md)
+- [DebugVect](../msg_docs/DebugVect.md)
+- [PpsCapture](../msg_docs/PpsCapture.md)
+- [OrbTestLarge](../msg_docs/OrbTestLarge.md)
+- [EstimatorInnovations](../msg_docs/EstimatorInnovations.md)
+- [PositionControllerLandingStatus](../msg_docs/PositionControllerLandingStatus.md)
+- [FigureEightStatus](../msg_docs/FigureEightStatus.md)
+- [ActuatorArmed](../msg_docs/ActuatorArmed.md)
+- [InternalCombustionEngineControl](../msg_docs/InternalCombustionEngineControl.md)
+- [OpenDroneIdSelfId](../msg_docs/OpenDroneIdSelfId.md)
+- [FollowTarget](../msg_docs/FollowTarget.md)
+- [DebugArray](../msg_docs/DebugArray.md)
+- [DebugValue](../msg_docs/DebugValue.md)
+- [Rpm](../msg_docs/Rpm.md)
+- [HoverThrustEstimate](../msg_docs/HoverThrustEstimate.md)
+- [CellularStatus](../msg_docs/CellularStatus.md)
+- [ButtonEvent](../msg_docs/ButtonEvent.md)
+- [ArmingCheckRequestV0](../msg_docs/ArmingCheckRequestV0.md)
+- [VehicleOpticalFlow](../msg_docs/VehicleOpticalFlow.md)
+- [PwmInput](../msg_docs/PwmInput.md)
+- [LaunchDetectionStatus](../msg_docs/LaunchDetectionStatus.md)
+- [RaptorStatus](../msg_docs/RaptorStatus.md)
+- [FixedWingLateralGuidanceStatus](../msg_docs/FixedWingLateralGuidanceStatus.md)
+- [ParameterSetUsedRequest](../msg_docs/ParameterSetUsedRequest.md)
+- [SensorBaro](../msg_docs/SensorBaro.md)
+- [InternalCombustionEngineStatus](../msg_docs/InternalCombustionEngineStatus.md)
+- [InputRc](../msg_docs/InputRc.md)
+- [AirspeedWind](../msg_docs/AirspeedWind.md)
+- [CanInterfaceStatus](../msg_docs/CanInterfaceStatus.md)
+- [Vtx](../msg_docs/Vtx.md)
+- [GimbalManagerSetAttitude](../msg_docs/GimbalManagerSetAttitude.md)
+- [SatelliteInfo](../msg_docs/SatelliteInfo.md)
+- [TaskStackInfo](../msg_docs/TaskStackInfo.md)
+- [RoverSpeedStatus](../msg_docs/RoverSpeedStatus.md)
+- [GeneratorStatus](../msg_docs/GeneratorStatus.md)
+- [MissionResult](../msg_docs/MissionResult.md)
+- [ParameterResetRequest](../msg_docs/ParameterResetRequest.md)
+- [ActuatorTest](../msg_docs/ActuatorTest.md)
+- [IrlockReport](../msg_docs/IrlockReport.md)
+- [AdcReport](../msg_docs/AdcReport.md)
+- [FixedWingRunwayControl](../msg_docs/FixedWingRunwayControl.md)
+- [AutotuneAttitudeControlStatus](../msg_docs/AutotuneAttitudeControlStatus.md)
+- [Ping](../msg_docs/Ping.md)
+- [VehicleAngularVelocity](../msg_docs/VehicleAngularVelocity.md)
+- [Cpuload](../msg_docs/Cpuload.md)
:::
diff --git a/docs/ko/middleware/micrortps.md b/docs/ko/middleware/micrortps.md
index f54335d412..a84ccde4ab 100644
--- a/docs/ko/middleware/micrortps.md
+++ b/docs/ko/middleware/micrortps.md
@@ -3,4 +3,4 @@
[arguments...]
## rgbled
-Source: [drivers/lights/rgbled](https://github.com/PX4/PX4-Autopilot/tree/main/src/drivers/lights/rgbled)
+Source: [drivers/lights/rgbled_ncp5623c](https://github.com/PX4/PX4-Autopilot/tree/main/src/drivers/lights/rgbled_ncp5623c)
### Usage {#rgbled_usage}
@@ -1124,7 +1124,9 @@ rgbled [arguments...]
[-f ] bus frequency in kHz
[-q] quiet startup (no message if no device found)
[-a ] I2C address
- default: 85
+ default: 57
+ [-o ] RGB PWM Assignment
+ default: 123
stop
diff --git a/docs/ko/modules/modules_driver_distance_sensor.md b/docs/ko/modules/modules_driver_distance_sensor.md
index 3d34e69be4..f1ca2664f9 100644
--- a/docs/ko/modules/modules_driver_distance_sensor.md
+++ b/docs/ko/modules/modules_driver_distance_sensor.md
@@ -98,13 +98,56 @@ leddar_one [arguments...]
stop Stop driver
```
+## lightware_grf_serial
+
+Source: [drivers/distance_sensor/lightware_grf_serial](https://github.com/PX4/PX4-Autopilot/tree/main/src/drivers/distance_sensor/lightware_grf_serial)
+
+### 설명
+
+Serial bus driver for the Lightware GRF Laser rangefinder.
+
+### 설정
+
+https://docs.px4.io/main/en/sensor/grf_lidar
+
+### 매개변수
+
+https://docs.px4.io/main/en/advanced_config/parameter_reference#GRF_SENS_MODEL
+https://docs.px4.io/main/en/advanced_config/parameter_reference#GRF_RATE_CFG
+https://docs.px4.io/main/en/advanced_config/parameter_reference#SENS_EN_GRF_CFG
+
+### 예
+
+Attempt to start driver on a specified serial device.
+
+```
+lightware_grf_serial start -d /dev/ttyS1
+```
+
+Stop driver
+
+```
+lightware_grf_serial stop
+```
+
+### Usage {#lightware_grf_serial_usage}
+
+```
+lightware_grf_serial [arguments...]
+ Commands:
+ start Start driver
+ -d Serial device
+
+ stop Stop driver
+```
+
## lightware_laser_i2c
Source: [drivers/distance_sensor/lightware_laser_i2c](https://github.com/PX4/PX4-Autopilot/tree/main/src/drivers/distance_sensor/lightware_laser_i2c)
### 설명
-I2C bus driver for Lightware SFxx series LIDAR rangefinders: SF10/a, SF10/b, SF10/c, SF11/c, SF/LW20, SF30/d.
+I2C bus driver for Lightware LIDAR rangefinders: SF10/a, SF10/b, SF10/c, SF11/c, SF/LW20, SF/LW30/d, GRF250, GRF500.
Setup/usage information: https://docs.px4.io/main/en/sensor/sfxx_lidar.html
@@ -122,8 +165,6 @@ lightware_laser_i2c [arguments...]
[-q] quiet startup (no message if no device found)
[-a ] I2C address
default: 102
- [-R ] Sensor rotation - downward facing by default
- default: 25
stop
diff --git a/docs/ko/modules/modules_driver_ins.md b/docs/ko/modules/modules_driver_ins.md
index ca390b9321..d6c7d98d43 100644
--- a/docs/ko/modules/modules_driver_ins.md
+++ b/docs/ko/modules/modules_driver_ins.md
@@ -9,7 +9,7 @@ Source: [drivers/ins/microstrain](https://github.com/PX4/PX4-Autopilot/tree/main
MicroStrain by HBK Inertial Sensor Driver.
Currently supports the following sensors:
--[CV7-AR](https://www.hbkworld.com/en/products/transducers/inertial-sensors/vertical-reference-units--vru-/3dm-cv7-ar) -[CV7-AHRS](https://www.hbkworld.com/en/products/transducers/inertial-sensors/attitude-and-heading-reference-systems--ahrs-/3dm-cv7-ahrs) -[CV7-INS](https://www.hbkworld.com/en/products/transducers/inertial-sensors/inertial-navigation-systems--ins-/3dm-cv7-ins) -[CV7-GNSS/INS](https://www.hbkworld.com/en/products/transducers/inertial-sensors/inertial-navigation-systems--ins-/3dm-cv7-gnss-ins)
+-[CV7-AR](https://www.hbkworld.com/en/products/transducers/inertial-sensors/vertical-reference-units--vru-/3dm-cv7-ar) -[CV7-AHRS](https://www.hbkworld.com/en/products/transducers/inertial-sensors/attitude-and-heading-reference-systems--ahrs-/3dm-cv7-ahrs) -[CV7-INS](https://www.hbkworld.com/en/products/transducers/inertial-sensors/navigation/3dm-cv7-ins) -[CV7-GNSS/INS](https://www.hbkworld.com/en/products/transducers/inertial-sensors/navigation/3dm-cv7-gnss-ins)
This driver is not included in the firmware by default.
Include the module in firmware by setting the
diff --git a/docs/ko/modules/modules_estimator.md b/docs/ko/modules/modules_estimator.md
index c4f57f3fff..7c80f73d98 100644
--- a/docs/ko/modules/modules_estimator.md
+++ b/docs/ko/modules/modules_estimator.md
@@ -49,7 +49,7 @@ Source: [modules/ekf2](https://github.com/PX4/PX4-Autopilot/tree/main/src/module
확장 칼만 필터를 사용한 태도 및 위치 추정기입니다. 멀티콥터와 고정익에 사용됩니다.
-The documentation can be found on the [ECL/EKF Overview & Tuning](https://docs.px4.io/main/en/advanced_config/tuning_the_ecl_ekf.html) page.
+The documentation can be found on the [ECL/EKF Overview & Tuning](../advanced_config/tuning_the_ecl_ekf.md) page.
ekf2 can be started in replay mode (`-r`): in this mode, it does not access the system time, but only uses the
timestamps from the sensor topics.
diff --git a/docs/ko/modules/modules_system.md b/docs/ko/modules/modules_system.md
index 8be479bba8..bd3753acec 100644
--- a/docs/ko/modules/modules_system.md
+++ b/docs/ko/modules/modules_system.md
@@ -321,7 +321,7 @@ Source: [drivers/heater](https://github.com/PX4/PX4-Autopilot/tree/main/src/driv
### 설명
-Background process running periodically on the LP work queue to regulate IMU temperature at a setpoint.
+Background process running periodically on the INS{i} queue to regulate IMU temperature at a setpoint.
This task can be started at boot from the startup scripts by setting SENS_EN_THERMAL or via CLI.
@@ -732,7 +732,7 @@ The module is typically used together with uORB publisher rules, to specify whic
The replay module will just publish all messages that are found in the log. It also applies the parameters from
the log.
-The replay procedure is documented on the [System-wide Replay](https://docs.px4.io/main/en/debug/system_wide_replay.html)
+The replay procedure is documented on the [System-wide Replay](../debug/system_wide_replay.md)
page.
### Usage {#replay_usage}
@@ -921,6 +921,30 @@ system_power_simulation [arguments...]
status print status info
```
+## task_watchdog
+
+Source: [modules/task_watchdog](https://github.com/PX4/PX4-Autopilot/tree/main/src/modules/task_watchdog)
+
+### 설명
+
+Detects when a higher-priority task starves the system by running too long.
+When starvation is detected, dumps the offending task's registers and stack,
+and saves a cpuload snapshot.
+
+### Usage {#task_watchdog_usage}
+
+```
+task_watchdog [arguments...]
+ Commands:
+ start
+
+ trigger Manually trigger the watchdog
+
+ stop
+
+ status print status info
+```
+
## tattu_can
Source: [drivers/tattu_can](https://github.com/PX4/PX4-Autopilot/tree/main/src/drivers/tattu_can)
diff --git a/docs/ko/msg_docs/ActionRequest.md b/docs/ko/msg_docs/ActionRequest.md
index 94f8d7d693..00753e7a53 100644
--- a/docs/ko/msg_docs/ActionRequest.md
+++ b/docs/ko/msg_docs/ActionRequest.md
@@ -25,26 +25,26 @@ Request are published by `manual_control` and subscribed by the `commander` and
### ACTION {#ACTION}
-| 명칭 | 형식 | Value | 설명 |
-| ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- | ------- | ----- | ---------------------------------------------------------------------------------------- |
-| ACTION_DISARM | `uint8` | 0 | Disarm vehicle |
-| ACTION_ARM | `uint8` | 1 | Arm vehicle |
-| ACTION_TOGGLE_ARMING | `uint8` | 2 | Toggle arming |
-| ACTION_UNKILL | `uint8` | 3 | Revert a kill action |
-| ACTION_KILL | `uint8` | 4 | Kill vehicle (instantly stop the motors) |
-| ACTION_SWITCH_MODE | `uint8` | 5 | Switch mode. The target mode is set in the `mode` field. |
-| ACTION_VTOL_TRANSITION_TO_MULTICOPTER | `uint8` | 6 | Transition to hover flight |
-| ACTION_VTOL_TRANSITION_TO_FIXEDWING | `uint8` | 7 | Transition to fast forward flight |
-| ACTION_TERMINATION | `uint8` | 8 | Irreversibly output failsafe values on all outputs, trigger parachute |
+| 명칭 | 형식 | Value | 설명 |
+| ----------------------------------------------------------------------------------------------------------------------------------------------------------------------------- | ------- | ----- | ---------------------------------------------------------------------------------------- |
+| ACTION_DISARM | `uint8` | 0 | Disarm vehicle |
+| ACTION_ARM | `uint8` | 1 | Arm vehicle |
+| ACTION_TOGGLE_ARMING | `uint8` | 2 | Toggle arming |
+| ACTION_UNKILL | `uint8` | 3 | Revert a kill action |
+| ACTION_KILL | `uint8` | 4 | Kill vehicle (instantly stop the motors) |
+| ACTION_SWITCH_MODE | `uint8` | 5 | Switch mode. The target mode is set in the `mode` field. |
+| ACTION_VTOL_TRANSITION_TO_MULTICOPTER | `uint8` | 6 | Transition to hover flight |
+| ACTION_VTOL_TRANSITION_TO_FIXEDWING | `uint8` | 7 | Transition to fast forward flight |
+| ACTION_TERMINATION | `uint8` | 8 | Irreversibly output failsafe values on all outputs, trigger parachute |
### SOURCE {#SOURCE}
-| 명칭 | 형식 | Value | 설명 |
-| ---------------------------------------------------------------------------------------------------------------------- | ------- | ----- | --------------------------------------------------------------- |
-| SOURCE_STICK_GESTURE | `uint8` | 0 | Triggered by holding the sticks in a certain position |
-| SOURCE_RC_SWITCH | `uint8` | 1 | Triggered by an RC switch moving into a certain position |
-| SOURCE_RC_BUTTON | `uint8` | 2 | Triggered by a momentary button on the RC being pressed or held |
-| SOURCE_RC_MODE_SLOT | `uint8` | 3 | Mode change through the RC mode selection mechanism |
+| 명칭 | 형식 | Value | 설명 |
+| -------------------------------------------------------------------------------------------------------------------- | ------- | ----- | --------------------------------------------------------------- |
+| SOURCE_STICK_GESTURE | `uint8` | 0 | Triggered by holding the sticks in a certain position |
+| SOURCE_RC_SWITCH | `uint8` | 1 | Triggered by an RC switch moving into a certain position |
+| SOURCE_RC_BUTTON | `uint8` | 2 | Triggered by a momentary button on the RC being pressed or held |
+| SOURCE_RC_MODE_SLOT | `uint8` | 3 | Mode change through the RC mode selection mechanism |
## Source Message
@@ -60,26 +60,26 @@ Click here to see original file
# It allows mapping triggers from various external interfaces like RC channels or MAVLink to cause an action.
# Request are published by `manual_control` and subscribed by the `commander` and `vtol_att_control` modules.
-uint64 timestamp # [us] Time since system start
+uint64 timestamp # [us] Time since system start
-uint8 action # [@enum ACTION] Requested action
-uint8 ACTION_DISARM = 0 # Disarm vehicle
-uint8 ACTION_ARM = 1 # Arm vehicle
-uint8 ACTION_TOGGLE_ARMING = 2 # Toggle arming
-uint8 ACTION_UNKILL = 3 # Revert a kill action
-uint8 ACTION_KILL = 4 # Kill vehicle (instantly stop the motors)
-uint8 ACTION_SWITCH_MODE = 5 # Switch mode. The target mode is set in the `mode` field.
-uint8 ACTION_VTOL_TRANSITION_TO_MULTICOPTER = 6 # Transition to hover flight
-uint8 ACTION_VTOL_TRANSITION_TO_FIXEDWING = 7 # Transition to fast forward flight
-uint8 ACTION_TERMINATION = 8 # Irreversibly output failsafe values on all outputs, trigger parachute
+uint8 action # [@enum ACTION] Requested action
+uint8 ACTION_DISARM = 0 # Disarm vehicle
+uint8 ACTION_ARM = 1 # Arm vehicle
+uint8 ACTION_TOGGLE_ARMING = 2 # Toggle arming
+uint8 ACTION_UNKILL = 3 # Revert a kill action
+uint8 ACTION_KILL = 4 # Kill vehicle (instantly stop the motors)
+uint8 ACTION_SWITCH_MODE = 5 # Switch mode. The target mode is set in the `mode` field.
+uint8 ACTION_VTOL_TRANSITION_TO_MULTICOPTER = 6 # Transition to hover flight
+uint8 ACTION_VTOL_TRANSITION_TO_FIXEDWING = 7 # Transition to fast forward flight
+uint8 ACTION_TERMINATION = 8 # Irreversibly output failsafe values on all outputs, trigger parachute
-uint8 source # [@enum SOURCE] Request trigger type, such as a switch, button or gesture
-uint8 SOURCE_STICK_GESTURE = 0 # Triggered by holding the sticks in a certain position
-uint8 SOURCE_RC_SWITCH = 1 # Triggered by an RC switch moving into a certain position
-uint8 SOURCE_RC_BUTTON = 2 # Triggered by a momentary button on the RC being pressed or held
-uint8 SOURCE_RC_MODE_SLOT = 3 # Mode change through the RC mode selection mechanism
+uint8 source # [@enum SOURCE] Request trigger type, such as a switch, button or gesture
+uint8 SOURCE_STICK_GESTURE = 0 # Triggered by holding the sticks in a certain position
+uint8 SOURCE_RC_SWITCH = 1 # Triggered by an RC switch moving into a certain position
+uint8 SOURCE_RC_BUTTON = 2 # Triggered by a momentary button on the RC being pressed or held
+uint8 SOURCE_RC_MODE_SLOT = 3 # Mode change through the RC mode selection mechanism
-uint8 mode # Requested mode. Only applies when `action` is `ACTION_SWITCH_MODE`. Values for this field are defined by the `vehicle_status_s::NAVIGATION_STATE_*` enumeration.
+uint8 mode # Requested mode. Only applies when `action` is `ACTION_SWITCH_MODE`. Values for this field are defined by the `vehicle_status_s::NAVIGATION_STATE_*` enumeration.
```
:::
diff --git a/docs/ko/msg_docs/ActuatorMotors.md b/docs/ko/msg_docs/ActuatorMotors.md
index eb794ef1c6..6ae1e7f28f 100644
--- a/docs/ko/msg_docs/ActuatorMotors.md
+++ b/docs/ko/msg_docs/ActuatorMotors.md
@@ -18,15 +18,15 @@ Published by the vehicle's allocation and consumed by the ESC protocol drivers e
| timestamp | `uint64` | us | | Time since system start |
| timestamp_sample | `uint64` | us | | Sampling timestamp of the data this control response is based on |
| reversible_flags | `uint16` | | | Bitset indicating which motors are configured to be reversible |
-| control | `float32[12]` | | [-1 : 1] | Normalized thrust. where 1 means maximum positive thrust, -1 maximum negative (if not supported by the output, <0 maps to NaN). NaN maps to disarmed (stop the motors) |
+| control | `float32[12]` | | [-1 : 1] | Normalized thrust. Where 1 means maximum positive thrust, -1 maximum negative (if not supported by the output, <0 maps to NaN). NaN maps to disarmed (stop the motors) |
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ----------------------------------------------------------------------------------------------------------- | -------- | ----- | -- |
-| MESSAGE_VERSION | `uint32` | 0 | |
-| ACTUATOR_FUNCTION_MOTOR1 | `uint8` | 101 | |
-| NUM_CONTROLS | `uint8` | 12 | |
+| 명칭 | 형식 | Value | 설명 |
+| --------------------------------------------------------------------------------------------------------- | -------- | ----- | -- |
+| MESSAGE_VERSION | `uint32` | 0 | |
+| ACTUATOR_FUNCTION_MOTOR1 | `uint8` | 101 | |
+| NUM_CONTROLS | `uint8` | 12 | |
## Source Message
@@ -43,15 +43,15 @@ Click here to see original file
uint32 MESSAGE_VERSION = 0
-uint64 timestamp # [us] Time since system start
-uint64 timestamp_sample # [us] Sampling timestamp of the data this control response is based on
+uint64 timestamp # [us] Time since system start
+uint64 timestamp_sample # [us] Sampling timestamp of the data this control response is based on
-uint16 reversible_flags # [-] Bitset indicating which motors are configured to be reversible
+uint16 reversible_flags # [-] Bitset indicating which motors are configured to be reversible
-uint8 ACTUATOR_FUNCTION_MOTOR1 = 101 #
+uint8 ACTUATOR_FUNCTION_MOTOR1 = 101
-uint8 NUM_CONTROLS = 12 #
-float32[12] control # [@range -1, 1] Normalized thrust. where 1 means maximum positive thrust, -1 maximum negative (if not supported by the output, <0 maps to NaN). NaN maps to disarmed (stop the motors)
+uint8 NUM_CONTROLS = 12
+float32[12] control # [@range -1, 1] Normalized thrust. Where 1 means maximum positive thrust, -1 maximum negative (if not supported by the output, <0 maps to NaN). NaN maps to disarmed (stop the motors)
```
:::
diff --git a/docs/ko/msg_docs/ActuatorOutputs.md b/docs/ko/msg_docs/ActuatorOutputs.md
index cbdaacf727..10a809e645 100644
--- a/docs/ko/msg_docs/ActuatorOutputs.md
+++ b/docs/ko/msg_docs/ActuatorOutputs.md
@@ -16,10 +16,10 @@ pageClass: is-wide-page
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ------------------------------------------------------------------------------------------------------------------------------------- | ------- | ----- | ------------------- |
-| NUM_ACTUATOR_OUTPUTS | `uint8` | 16 | |
-| NUM_ACTUATOR_OUTPUT_GROUPS | `uint8` | 4 | for sanity checking |
+| 명칭 | 형식 | Value | 설명 |
+| ---------------------------------------------------------------------------------------------------------------------------------- | ------- | ----- | ------------------- |
+| NUM_ACTUATOR_OUTPUTS | `uint8` | 16 | |
+| NUM_ACTUATOR_OUTPUT_GROUPS | `uint8` | 4 | for sanity checking |
## Source Message
diff --git a/docs/ko/msg_docs/ActuatorServos.md b/docs/ko/msg_docs/ActuatorServos.md
index 41776a04f5..23358da50b 100644
--- a/docs/ko/msg_docs/ActuatorServos.md
+++ b/docs/ko/msg_docs/ActuatorServos.md
@@ -21,10 +21,10 @@ Published by the vehicle's allocation and consumed by the actuator output driver
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| -------------------------------------------------------------------- | -------- | ----- | -- |
-| MESSAGE_VERSION | `uint32` | 0 | |
-| NUM_CONTROLS | `uint8` | 8 | |
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------------ | -------- | ----- | -- |
+| MESSAGE_VERSION | `uint32` | 0 | |
+| NUM_CONTROLS | `uint8` | 8 | |
## Source Message
@@ -41,11 +41,11 @@ Click here to see original file
uint32 MESSAGE_VERSION = 0
-uint64 timestamp # [us] Time since system start
-uint64 timestamp_sample # [us] Sampling timestamp of the data this control response is based on
+uint64 timestamp # [us] Time since system start
+uint64 timestamp_sample # [us] Sampling timestamp of the data this control response is based on
-uint8 NUM_CONTROLS = 8 #
-float32[8] control # [-] [@range -1, 1] Normalized output. 1 means maximum positive position. -1 maximum negative position (if not supported by the output, <0 maps to NaN). NaN maps to disarmed.
+uint8 NUM_CONTROLS = 8
+float32[8] control # [-] [@range -1, 1] Normalized output. 1 means maximum positive position. -1 maximum negative position (if not supported by the output, <0 maps to NaN). NaN maps to disarmed.
```
:::
diff --git a/docs/ko/msg_docs/ActuatorServosTrim.md b/docs/ko/msg_docs/ActuatorServosTrim.md
index f507eb06b5..ea248b526b 100644
--- a/docs/ko/msg_docs/ActuatorServosTrim.md
+++ b/docs/ko/msg_docs/ActuatorServosTrim.md
@@ -6,7 +6,7 @@ pageClass: is-wide-page
Servo trims, added as offset to servo outputs.
-**TOPICS:** actuator_servostrim
+**TOPICS:** actuator_servos_trim
## Fields
@@ -17,9 +17,9 @@ Servo trims, added as offset to servo outputs.
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| -------------------------------------------------------------- | ------- | ----- | -- |
-| NUM_CONTROLS | `uint8` | 8 | |
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------ | ------- | ----- | -- |
+| NUM_CONTROLS | `uint8` | 8 | |
## Source Message
diff --git a/docs/ko/msg_docs/ActuatorTest.md b/docs/ko/msg_docs/ActuatorTest.md
index ffb159486c..c63e5fb98b 100644
--- a/docs/ko/msg_docs/ActuatorTest.md
+++ b/docs/ko/msg_docs/ActuatorTest.md
@@ -18,15 +18,15 @@ pageClass: is-wide-page
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ------------------------------------------------------------------------------------------------------- | ------- | ----- | -------------------------------------------------------------------------------------------------------------------- |
-| ACTION_RELEASE_CONTROL | `uint8` | 0 | exit test mode for the given function |
-| ACTION_DO_CONTROL | `uint8` | 1 | enable actuator test mode |
-| FUNCTION_MOTOR1 | `uint8` | 101 | |
-| MAX_NUM_MOTORS | `uint8` | 12 | |
-| FUNCTION_SERVO1 | `uint8` | 201 | |
-| MAX_NUM_SERVOS | `uint8` | 8 | |
-| ORB_QUEUE_LENGTH | `uint8` | 16 | > = MAX_NUM_MOTORS to support code in esc_calibration |
+| 명칭 | 형식 | Value | 설명 |
+| ----------------------------------------------------------------------------------------------------- | ------- | ----- | -------------------------------------------------------------------------------------------------------------------- |
+| ACTION_RELEASE_CONTROL | `uint8` | 0 | exit test mode for the given function |
+| ACTION_DO_CONTROL | `uint8` | 1 | enable actuator test mode |
+| FUNCTION_MOTOR1 | `uint8` | 101 | |
+| MAX_NUM_MOTORS | `uint8` | 12 | |
+| FUNCTION_SERVO1 | `uint8` | 201 | |
+| MAX_NUM_SERVOS | `uint8` | 8 | |
+| ORB_QUEUE_LENGTH | `uint8` | 16 | > = MAX_NUM_MOTORS to support code in esc_calibration |
## Source Message
diff --git a/docs/ko/msg_docs/AirspeedValidated.md b/docs/ko/msg_docs/AirspeedValidated.md
index aeffcc6904..33d43f1764 100644
--- a/docs/ko/msg_docs/AirspeedValidated.md
+++ b/docs/ko/msg_docs/AirspeedValidated.md
@@ -30,20 +30,20 @@ Used by controllers, estimators and for airspeed reporting to operator.
### SOURCE {#SOURCE}
-| 명칭 | 형식 | Value | 설명 |
-| -------------------------------------------------------------------------------------------------------------------------------- | ------ | ----- | ----------------------- |
-| SOURCE_DISABLED | `int8` | -1 | Disabled |
-| SOURCE_GROUND_MINUS_WIND | `int8` | 0 | Ground speed minus wind |
-| SOURCE_SENSOR_1 | `int8` | 1 | Sensor 1 |
-| SOURCE_SENSOR_2 | `int8` | 2 | Sensor 2 |
-| SOURCE_SENSOR_3 | `int8` | 3 | Sensor 3 |
-| SOURCE_SYNTHETIC | `int8` | 4 | Synthetic airspeed |
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------------------------------------------------------------------------ | ------ | ----- | ----------------------- |
+| SOURCE_DISABLED | `int8` | -1 | Disabled |
+| SOURCE_GROUND_MINUS_WIND | `int8` | 0 | Ground speed minus wind |
+| SOURCE_SENSOR_1 | `int8` | 1 | Sensor 1 |
+| SOURCE_SENSOR_2 | `int8` | 2 | Sensor 2 |
+| SOURCE_SENSOR_3 | `int8` | 3 | Sensor 3 |
+| SOURCE_SYNTHETIC | `int8` | 4 | Synthetic airspeed |
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| -------------------------------------------------------------------- | -------- | ----- | -- |
-| MESSAGE_VERSION | `uint32` | 1 | |
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------------ | -------- | ----- | -- |
+| MESSAGE_VERSION | `uint32` | 1 | |
## Source Message
@@ -58,28 +58,27 @@ Click here to see original file
# Provides information about airspeed (indicated, true, calibrated) and the source of the data.
# Used by controllers, estimators and for airspeed reporting to operator.
-
uint32 MESSAGE_VERSION = 1
-uint64 timestamp # [us] Time since system start
+uint64 timestamp # [us] Time since system start
-float32 indicated_airspeed_m_s # [m/s] [@invalid NaN] Indicated airspeed (IAS)
-float32 calibrated_airspeed_m_s # [m/s] [@invalid NaN] Calibrated airspeed (CAS)
-float32 true_airspeed_m_s # [m/s] [@invalid NaN] True airspeed (TAS)
+float32 indicated_airspeed_m_s # [m/s] [@invalid NaN] Indicated airspeed (IAS)
+float32 calibrated_airspeed_m_s # [m/s] [@invalid NaN] Calibrated airspeed (CAS)
+float32 true_airspeed_m_s # [m/s] [@invalid NaN] True airspeed (TAS)
-int8 airspeed_source # [@enum SOURCE] Source of currently published airspeed values
-int8 SOURCE_DISABLED = -1 # Disabled
-int8 SOURCE_GROUND_MINUS_WIND = 0 # Ground speed minus wind
-int8 SOURCE_SENSOR_1 = 1 # Sensor 1
-int8 SOURCE_SENSOR_2 = 2 # Sensor 2
-int8 SOURCE_SENSOR_3 = 3 # Sensor 3
-int8 SOURCE_SYNTHETIC = 4 # Synthetic airspeed
+int8 airspeed_source # [@enum SOURCE] Source of currently published airspeed values
+int8 SOURCE_DISABLED = -1 # Disabled
+int8 SOURCE_GROUND_MINUS_WIND = 0 # Ground speed minus wind
+int8 SOURCE_SENSOR_1 = 1 # Sensor 1
+int8 SOURCE_SENSOR_2 = 2 # Sensor 2
+int8 SOURCE_SENSOR_3 = 3 # Sensor 3
+int8 SOURCE_SYNTHETIC = 4 # Synthetic airspeed
-float32 calibrated_ground_minus_wind_m_s # [m/s] [@invalid NaN] CAS calculated from groundspeed - windspeed, where windspeed is estimated based on a zero-sideslip assumption
-float32 calibraded_airspeed_synth_m_s # [m/s] [@invalid NaN] Synthetic airspeed
-float32 airspeed_derivative_filtered # [m/s^2] Filtered indicated airspeed derivative
-float32 throttle_filtered # [-] Filtered fixed-wing throttle
-float32 pitch_filtered # [rad] Filtered pitch
+float32 calibrated_ground_minus_wind_m_s # [m/s] [@invalid NaN] CAS calculated from groundspeed - windspeed, where windspeed is estimated based on a zero-sideslip assumption
+float32 calibraded_airspeed_synth_m_s # [m/s] [@invalid NaN] Synthetic airspeed
+float32 airspeed_derivative_filtered # [m/s^2] Filtered indicated airspeed derivative
+float32 throttle_filtered # [-] Filtered fixed-wing throttle
+float32 pitch_filtered # [rad] Filtered pitch
```
:::
diff --git a/docs/ko/msg_docs/AirspeedValidatedV0.md b/docs/ko/msg_docs/AirspeedValidatedV0.md
index e311b1e496..2b22c48b39 100644
--- a/docs/ko/msg_docs/AirspeedValidatedV0.md
+++ b/docs/ko/msg_docs/AirspeedValidatedV0.md
@@ -4,7 +4,7 @@ pageClass: is-wide-page
# AirspeedValidatedV0 (UORB message)
-**TOPICS:** airspeed_validatedv0
+**TOPICS:** airspeed_validated_v0
## Fields
@@ -24,9 +24,9 @@ pageClass: is-wide-page
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| -------------------------------------------------------------------- | -------- | ----- | -- |
-| MESSAGE_VERSION | `uint32` | 0 | |
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------------ | -------- | ----- | -- |
+| MESSAGE_VERSION | `uint32` | 0 | |
## Source Message
diff --git a/docs/ko/msg_docs/AirspeedWind.md b/docs/ko/msg_docs/AirspeedWind.md
index a3aaf9ab46..21f4b2f06d 100644
--- a/docs/ko/msg_docs/AirspeedWind.md
+++ b/docs/ko/msg_docs/AirspeedWind.md
@@ -35,12 +35,12 @@ subscribed to by any other modules.
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ---------------------------------------------------------------------------------------------------------------------- | ------- | ----- | ----------------------------------------------------------------------------------------------------- |
-| SOURCE_AS_BETA_ONLY | `uint8` | 0 | Wind estimate only based on synthetic sideslip fusion |
-| SOURCE_AS_SENSOR_1 | `uint8` | 1 | Combined synthetic sideslip and airspeed fusion (data from first airspeed sensor) |
-| SOURCE_AS_SENSOR_2 | `uint8` | 2 | Combined synthetic sideslip and airspeed fusion (data from second airspeed sensor) |
-| SOURCE_AS_SENSOR_3 | `uint8` | 3 | Combined synthetic sideslip and airspeed fusion (data from third airspeed sensor) |
+| 명칭 | 형식 | Value | 설명 |
+| -------------------------------------------------------------------------------------------------------------------- | ------- | ----- | ----------------------------------------------------------------------------------------------------- |
+| SOURCE_AS_BETA_ONLY | `uint8` | 0 | Wind estimate only based on synthetic sideslip fusion |
+| SOURCE_AS_SENSOR_1 | `uint8` | 1 | Combined synthetic sideslip and airspeed fusion (data from first airspeed sensor) |
+| SOURCE_AS_SENSOR_2 | `uint8` | 2 | Combined synthetic sideslip and airspeed fusion (data from second airspeed sensor) |
+| SOURCE_AS_SENSOR_3 | `uint8` | 3 | Combined synthetic sideslip and airspeed fusion (data from third airspeed sensor) |
## Source Message
diff --git a/docs/ko/msg_docs/ArmingCheckReply.md b/docs/ko/msg_docs/ArmingCheckReply.md
index bf5e6d21d7..1d138c66d8 100644
--- a/docs/ko/msg_docs/ArmingCheckReply.md
+++ b/docs/ko/msg_docs/ArmingCheckReply.md
@@ -13,7 +13,7 @@ The request is sent regularly to all registered ROS modes, even while armed, so
Note that the external component is identified by its registration_id, which is allocated to the component during registration (arming_check_id in RegisterExtComponentReply).
The message is not used by internal/FMU components, as their mode requirements are known at compile time.
-**TOPICS:** arming_checkreply
+**TOPICS:** arming_check_reply
## Fields
@@ -45,16 +45,16 @@ The message is not used by internal/FMU components, as their mode requirements a
### HEALTH_COMPONENT_INDEX {#HEALTH_COMPONENT_INDEX}
-| 명칭 | 형식 | Value | 설명 |
-| -------------------------------------------------------------------------------------------------------------------------------------- | ------- | ----- | --------------------------------------------------------- |
-| HEALTH_COMPONENT_INDEX_NONE | `uint8` | 0 | Index of health component for which this response applies |
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------------------------------------------------------------------------------ | ------- | ----- | --------------------------------------------------------- |
+| HEALTH_COMPONENT_INDEX_NONE | `uint8` | 0 | Index of health component for which this response applies |
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ------------------------------------------------------------------------------------------- | -------- | ----- | -- |
-| MESSAGE_VERSION | `uint32` | 1 | |
-| ORB_QUEUE_LENGTH | `uint8` | 4 | |
+| 명칭 | 형식 | Value | 설명 |
+| ----------------------------------------------------------------------------------------- | -------- | ----- | -- |
+| MESSAGE_VERSION | `uint32` | 1 | |
+| ORB_QUEUE_LENGTH | `uint8` | 4 | |
## Source Message
@@ -73,40 +73,40 @@ Click here to see original file
# Note that the external component is identified by its registration_id, which is allocated to the component during registration (arming_check_id in RegisterExtComponentReply).
# The message is not used by internal/FMU components, as their mode requirements are known at compile time.
-uint32 MESSAGE_VERSION = 1
+uint32 MESSAGE_VERSION = 1
uint64 timestamp # [us] Time since system start.
-uint8 request_id # [-] Id of ArmingCheckRequest for which this is a response
-uint8 registration_id # [-] Id of external component emitting this response
+uint8 request_id # [-] Id of ArmingCheckRequest for which this is a response
+uint8 registration_id # [-] Id of external component emitting this response
-uint8 HEALTH_COMPONENT_INDEX_NONE = 0 # Index of health component for which this response applies
+uint8 HEALTH_COMPONENT_INDEX_NONE = 0 # Index of health component for which this response applies
-uint8 health_component_index # [@enum HEALTH_COMPONENT_INDEX]
-bool health_component_is_present # Unused. Intended for use with health events interface (health_component_t in events.json)
-bool health_component_warning # Unused. Intended for use with health events interface (health_component_t in events.json)
-bool health_component_error # Unused. Intended for use with health events interface (health_component_t in events.json)
+uint8 health_component_index # [@enum HEALTH_COMPONENT_INDEX]
+bool health_component_is_present # Unused. Intended for use with health events interface (health_component_t in events.json)
+bool health_component_warning # Unused. Intended for use with health events interface (health_component_t in events.json)
+bool health_component_error # Unused. Intended for use with health events interface (health_component_t in events.json)
-bool can_arm_and_run # True if the component can arm. For navigation mode components, true if the component can arm in the mode or switch to the mode when already armed
+bool can_arm_and_run # True if the component can arm. For navigation mode components, true if the component can arm in the mode or switch to the mode when already armed
-uint8 num_events # Number of queued failure messages (Event) in the events field
+uint8 num_events # Number of queued failure messages (Event) in the events field
-Event[5] events # Arming failure reasons (Queue of events to report to GCS)
+Event[5] events # Arming failure reasons (Queue of events to report to GCS)
# Mode requirements
-bool mode_req_angular_velocity # Requires angular velocity estimate (e.g. from gyroscope)
-bool mode_req_attitude # Requires an attitude estimate
-bool mode_req_local_alt # Requires a local altitude estimate
-bool mode_req_local_position # Requires a local position estimate
-bool mode_req_local_position_relaxed # Requires a more relaxed global position estimate
-bool mode_req_global_position # Requires a global position estimate
-bool mode_req_global_position_relaxed # Requires a relaxed global position estimate
-bool mode_req_mission # Requires an uploaded mission
-bool mode_req_home_position # Requires a home position (such as RTL/Return mode)
-bool mode_req_prevent_arming # Prevent arming (such as in Land mode)
-bool mode_req_manual_control # Requires a manual controller
+bool mode_req_angular_velocity # Requires angular velocity estimate (e.g. from gyroscope)
+bool mode_req_attitude # Requires an attitude estimate
+bool mode_req_local_alt # Requires a local altitude estimate
+bool mode_req_local_position # Requires a local position estimate
+bool mode_req_local_position_relaxed # Requires a more relaxed global position estimate
+bool mode_req_global_position # Requires a global position estimate
+bool mode_req_global_position_relaxed # Requires a relaxed global position estimate
+bool mode_req_mission # Requires an uploaded mission
+bool mode_req_home_position # Requires a home position (such as RTL/Return mode)
+bool mode_req_prevent_arming # Prevent arming (such as in Land mode)
+bool mode_req_manual_control # Requires a manual controller
-uint8 ORB_QUEUE_LENGTH = 4
+uint8 ORB_QUEUE_LENGTH = 4
```
:::
diff --git a/docs/ko/msg_docs/ArmingCheckReplyV0.md b/docs/ko/msg_docs/ArmingCheckReplyV0.md
index 10a7bd8602..b5bf63dfce 100644
--- a/docs/ko/msg_docs/ArmingCheckReplyV0.md
+++ b/docs/ko/msg_docs/ArmingCheckReplyV0.md
@@ -4,7 +4,7 @@ pageClass: is-wide-page
# ArmingCheckReplyV0 (UORB message)
-**TOPICS:** arming_checkreplyv0
+**TOPICS:** arming_check_reply_v0
## Fields
@@ -33,11 +33,11 @@ pageClass: is-wide-page
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| -------------------------------------------------------------------------------------------------------------------------------------- | -------- | ----- | -- |
-| MESSAGE_VERSION | `uint32` | 0 | |
-| HEALTH_COMPONENT_INDEX_NONE | `uint8` | 0 | |
-| ORB_QUEUE_LENGTH | `uint8` | 4 | |
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------------------------------------------------------------------------------ | -------- | ----- | -- |
+| MESSAGE_VERSION | `uint32` | 0 | |
+| HEALTH_COMPONENT_INDEX_NONE | `uint8` | 0 | |
+| ORB_QUEUE_LENGTH | `uint8` | 4 | |
## Source Message
diff --git a/docs/ko/msg_docs/ArmingCheckRequest.md b/docs/ko/msg_docs/ArmingCheckRequest.md
index d67cf35311..4c854266aa 100644
--- a/docs/ko/msg_docs/ArmingCheckRequest.md
+++ b/docs/ko/msg_docs/ArmingCheckRequest.md
@@ -13,7 +13,7 @@ The request is sent regularly, even while armed, so that the FMU always knows th
The reply will include the published request_id, allowing correlation of all arming check information for a particular request.
The reply will also include the registration_id for each external component, provided to it during the registration process (RegisterExtComponentReply).
-**TOPICS:** arming_checkrequest
+**TOPICS:** arming_check_request
## Fields
@@ -25,9 +25,9 @@ The reply will also include the registration_id for each external component, pro
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| -------------------------------------------------------------------- | -------- | ----- | -- |
-| MESSAGE_VERSION | `uint32` | 1 | |
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------------ | -------- | ----- | -- |
+| MESSAGE_VERSION | `uint32` | 1 | |
## Source Message
@@ -48,9 +48,9 @@ Click here to see original file
uint32 MESSAGE_VERSION = 1
-uint64 timestamp # [us] Time since system start
+uint64 timestamp # [us] Time since system start
-uint8 request_id # [-] Id of this request. Allows correlation with associated ArmingCheckReply messages.
+uint8 request_id # [-] Id of this request. Allows correlation with associated ArmingCheckReply messages.
uint32 valid_registrations_mask # [-] Bitmask of valid registration ID's (the bit is also cleared if flagged as unresponsive)
```
diff --git a/docs/ko/msg_docs/ArmingCheckRequestV0.md b/docs/ko/msg_docs/ArmingCheckRequestV0.md
index 1014b8f53e..4fa228b580 100644
--- a/docs/ko/msg_docs/ArmingCheckRequestV0.md
+++ b/docs/ko/msg_docs/ArmingCheckRequestV0.md
@@ -13,7 +13,7 @@ The request is sent regularly, even while armed, so that the FMU always knows th
The reply will include the published request_id, allowing correlation of all arming check information for a particular request.
The reply will also include the registration_id for each external component, provided to it during the registration process (RegisterExtComponentReply).
-**TOPICS:** arming_checkrequestv0
+**TOPICS:** arming_check_request_v0
## Fields
@@ -24,9 +24,9 @@ The reply will also include the registration_id for each external component, pro
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| -------------------------------------------------------------------- | -------- | ----- | -- |
-| MESSAGE_VERSION | `uint32` | 0 | |
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------------ | -------- | ----- | -- |
+| MESSAGE_VERSION | `uint32` | 0 | |
## Source Message
diff --git a/docs/ko/msg_docs/AutotuneAttitudeControlStatus.md b/docs/ko/msg_docs/AutotuneAttitudeControlStatus.md
index 6831460328..fe1edac6bc 100644
--- a/docs/ko/msg_docs/AutotuneAttitudeControlStatus.md
+++ b/docs/ko/msg_docs/AutotuneAttitudeControlStatus.md
@@ -11,7 +11,7 @@ and is subscribed to by the respective attitude controllers to command rate setp
The rate_sp field is consumed by the controllers, while the remaining fields (model coefficients, gains, filters, and autotune state) are used for logging and debugging.
-**TOPICS:** autotune_attitudecontrol_status
+**TOPICS:** autotune_attitude_control_status
## Fields
@@ -37,25 +37,25 @@ The rate_sp field is consumed by the controllers, while the remaining fields (mo
### STATE {#STATE}
-| 명칭 | 형식 | Value | 설명 |
-| ---------------------------------------------------------------------------------------------------------------------------------------------- | ------- | ----- | ------------------------------------------------------------------------------------------- |
-| STATE_IDLE | `uint8` | 0 | Idle (not running) |
-| STATE_INIT | `uint8` | 1 | Initialize filters and setup |
-| STATE_ROLL_AMPLITUDE_DETECTION | `uint8` | 2 | FW only: determine required excitation amplitude (roll) |
-| STATE_ROLL | `uint8` | 3 | Roll-axis excitation and model identification |
-| STATE_ROLL_PAUSE | `uint8` | 4 | Pause to return to level flight |
-| STATE_PITCH_AMPLITUDE_DETECTION | `uint8` | 5 | FW only: determine required excitation amplitude (pitch) |
-| STATE_PITCH | `uint8` | 6 | Pitch-axis excitation and model identification |
-| STATE_PITCH_PAUSE | `uint8` | 7 | Pause to return to level flight |
-| STATE_YAW_AMPLITUDE_DETECTION | `uint8` | 8 | FW only: determine required excitation amplitude (yaw) |
-| STATE_YAW | `uint8` | 9 | Yaw-axis excitation and model identification |
-| STATE_YAW_PAUSE | `uint8` | 10 | Pause to return to level flight |
-| STATE_VERIFICATION | `uint8` | 11 | Verify model and candidate gains |
-| STATE_APPLY | `uint8` | 12 | Apply gains |
-| STATE_TEST | `uint8` | 13 | Test gains in closed-loop |
-| STATE_COMPLETE | `uint8` | 14 | Tuning completed successfully |
-| STATE_FAIL | `uint8` | 15 | Tuning failed (model invalid or controller unstable) |
-| STATE_WAIT_FOR_DISARM | `uint8` | 16 | Waiting for disarm before finalizing |
+| 명칭 | 형식 | Value | 설명 |
+| -------------------------------------------------------------------------------------------------------------------------------------------- | ------- | ----- | ------------------------------------------------------------------------------------------- |
+| STATE_IDLE | `uint8` | 0 | Idle (not running) |
+| STATE_INIT | `uint8` | 1 | Initialize filters and setup |
+| STATE_ROLL_AMPLITUDE_DETECTION | `uint8` | 2 | FW only: determine required excitation amplitude (roll) |
+| STATE_ROLL | `uint8` | 3 | Roll-axis excitation and model identification |
+| STATE_ROLL_PAUSE | `uint8` | 4 | Pause to return to level flight |
+| STATE_PITCH_AMPLITUDE_DETECTION | `uint8` | 5 | FW only: determine required excitation amplitude (pitch) |
+| STATE_PITCH | `uint8` | 6 | Pitch-axis excitation and model identification |
+| STATE_PITCH_PAUSE | `uint8` | 7 | Pause to return to level flight |
+| STATE_YAW_AMPLITUDE_DETECTION | `uint8` | 8 | FW only: determine required excitation amplitude (yaw) |
+| STATE_YAW | `uint8` | 9 | Yaw-axis excitation and model identification |
+| STATE_YAW_PAUSE | `uint8` | 10 | Pause to return to level flight |
+| STATE_VERIFICATION | `uint8` | 11 | Verify model and candidate gains |
+| STATE_APPLY | `uint8` | 12 | Apply gains |
+| STATE_TEST | `uint8` | 13 | Test gains in closed-loop |
+| STATE_COMPLETE | `uint8` | 14 | Tuning completed successfully |
+| STATE_FAIL | `uint8` | 15 | Tuning failed (model invalid or controller unstable) |
+| STATE_WAIT_FOR_DISARM | `uint8` | 16 | Waiting for disarm before finalizing |
## Source Message
diff --git a/docs/ko/msg_docs/AuxGlobalPosition.md b/docs/ko/msg_docs/AuxGlobalPosition.md
new file mode 100644
index 0000000000..881504a091
--- /dev/null
+++ b/docs/ko/msg_docs/AuxGlobalPosition.md
@@ -0,0 +1,90 @@
+---
+pageClass: is-wide-page
+---
+
+# AuxGlobalPosition (UORB message)
+
+Auxiliary global position.
+
+This message provides global position data from an external source such as
+pseudolites, visual navigation, or other positioning system.
+
+**TOPICS:** aux_global_position
+
+## Fields
+
+| 명칭 | 형식 | Unit [Frame] | Range/Enum | 설명 |
+| ------------------------------------------------------------------------------------ | --------- | ---------------------------------------------------------------- | ----------------- | --------------------------------------------------------------------------------------------------------------------------------------------------------------------- |
+| timestamp | `uint64` | us | | Time since system start |
+| timestamp_sample | `uint64` | us | | Timestamp of the raw data |
+| id | `uint8` | | | Unique identifier for the AGP source |
+| source | `uint8` | | [SOURCE](#SOURCE) | Source type of the position data (based on mavlink::GLOBAL_POSITION_SRC) |
+| lat | `float64` | deg | | Latitude in WGS84 |
+| lon | `float64` | deg | | Longitude in WGS84 |
+| alt | `float32` | m | | Altitude above mean sea level (AMSL) (Invalid: NaN) |
+| eph | `float32` | m | | Std dev of horizontal position, lower bounded by NOISE param (Invalid: NaN) |
+| epv | `float32` | m | | Std dev of vertical position, lower bounded by NOISE param (Invalid: NaN) |
+| lat_lon_reset_counter | `uint8` | | | Counter for reset events on horizontal position coordinates |
+
+## Enums
+
+### SOURCE {#SOURCE}
+
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------------------ | ------- | ----- | -------------- |
+| SOURCE_UNKNOWN | `uint8` | 0 | Unknown source |
+| SOURCE_GNSS | `uint8` | 1 | GNSS |
+| SOURCE_VISION | `uint8` | 2 | Vision |
+| SOURCE_PSEUDOLITES | `uint8` | 3 | Pseudolites |
+| SOURCE_TERRAIN | `uint8` | 4 | Terrain |
+| SOURCE_MAGNETIC | `uint8` | 5 | Magnetic |
+| SOURCE_ESTIMATOR | `uint8` | 6 | 추정기 |
+
+## Constants
+
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------------ | -------- | ----- | -- |
+| MESSAGE_VERSION | `uint32` | 1 | |
+
+## Source Message
+
+[Source file (GitHub)](https://github.com/PX4/PX4-Autopilot/blob/main/msg/versioned/AuxGlobalPosition.msg)
+
+:::details
+Click here to see original file
+
+```c
+# Auxiliary global position
+#
+# This message provides global position data from an external source such as
+# pseudolites, visual navigation, or other positioning system.
+
+uint32 MESSAGE_VERSION = 1
+
+uint64 timestamp # [us] Time since system start
+uint64 timestamp_sample # [us] Timestamp of the raw data
+
+uint8 id # [-] Unique identifier for the AGP source
+uint8 source # [@enum SOURCE] Source type of the position data (based on mavlink::GLOBAL_POSITION_SRC)
+uint8 SOURCE_UNKNOWN = 0 # Unknown source
+uint8 SOURCE_GNSS = 1 # GNSS
+uint8 SOURCE_VISION = 2 # Vision
+uint8 SOURCE_PSEUDOLITES = 3 # Pseudolites
+uint8 SOURCE_TERRAIN = 4 # Terrain
+uint8 SOURCE_MAGNETIC = 5 # Magnetic
+uint8 SOURCE_ESTIMATOR = 6 # Estimator
+
+# lat, lon: required for horizontal position fusion, alt: required for vertical position fusion
+float64 lat # [deg] Latitude in WGS84
+float64 lon # [deg] Longitude in WGS84
+float32 alt # [m] [@invalid NaN] Altitude above mean sea level (AMSL)
+
+float32 eph # [m] [@invalid NaN] Std dev of horizontal position, lower bounded by NOISE param
+float32 epv # [m] [@invalid NaN] Std dev of vertical position, lower bounded by NOISE param
+
+uint8 lat_lon_reset_counter # [-] Counter for reset events on horizontal position coordinates
+
+# TOPICS aux_global_position
+```
+
+:::
diff --git a/docs/ko/msg_docs/BatteryStatus.md b/docs/ko/msg_docs/BatteryStatus.md
index 9058d50080..0809a57da3 100644
--- a/docs/ko/msg_docs/BatteryStatus.md
+++ b/docs/ko/msg_docs/BatteryStatus.md
@@ -25,7 +25,7 @@ Battery instance information is also logged and streamed in MAVLink telemetry.
| remaining | `float32` | | [0 : 1] | Remaining capacity (Invalid: -1) |
| scale | `float32` | | [1 : -] | Scaling factor to compensate for lower actuation power caused by voltage sag (Invalid: -1) |
| time_remaining_s | `float32` | s | | Predicted time remaining until battery is empty under previous averaged load (Invalid: NaN) |
-| temperature | `float32` | °C | | Temperature of the battery (Invalid: NaN) |
+| temperature | `float32` | degC | | Temperature of the battery (Invalid: NaN) |
| cell_count | `uint8` | | | Number of cells (Invalid: 0) |
| source | `uint8` | | [SOURCE](#SOURCE) | Battery source |
| priority | `uint8` | | | Zero based priority is the connection on the Power Controller V1..Vn AKA BrickN-1 |
@@ -59,52 +59,52 @@ Battery instance information is also logged and streamed in MAVLink telemetry.
### SOURCE {#SOURCE}
-| 명칭 | 형식 | Value | 설명 |
-| ------------------------------------------------------------------------------------------------- | ------- | ----- | ----------------------------------------------------------------- |
-| SOURCE_POWER_MODULE | `uint8` | 0 | Power module (analog ADC or I2C power monitor) |
-| SOURCE_EXTERNAL | `uint8` | 1 | External (MAVLink, CAN, or external driver) |
-| SOURCE_ESCS | `uint8` | 2 | ESCs (via ESC telemetry) |
+| 명칭 | 형식 | Value | 설명 |
+| ----------------------------------------------------------------------------------------------- | ------- | ----- | ----------------------------------------------------------------- |
+| SOURCE_POWER_MODULE | `uint8` | 0 | Power module (analog ADC or I2C power monitor) |
+| SOURCE_EXTERNAL | `uint8` | 1 | External (MAVLink, CAN, or external driver) |
+| SOURCE_ESCS | `uint8` | 2 | ESCs (via ESC telemetry) |
### WARNING {#WARNING}
-| 명칭 | 형식 | Value | 설명 |
-| ------------------------------------------------------------------------ | ------- | ----- | -------------------------------------------- |
-| WARNING_NONE | `uint8` | 0 | No battery low voltage warning active |
-| WARNING_LOW | `uint8` | 1 | Low voltage warning |
-| WARNING_CRITICAL | `uint8` | 2 | Critical voltage, return / abort immediately |
-| WARNING_EMERGENCY | `uint8` | 3 | Immediate landing required |
-| WARNING_FAILED | `uint8` | 4 | Battery has failed completely |
+| 명칭 | 형식 | Value | 설명 |
+| ---------------------------------------------------------------------- | ------- | ----- | -------------------------------------------- |
+| WARNING_NONE | `uint8` | 0 | No battery low voltage warning active |
+| WARNING_LOW | `uint8` | 1 | Low voltage warning |
+| WARNING_CRITICAL | `uint8` | 2 | Critical voltage, return / abort immediately |
+| WARNING_EMERGENCY | `uint8` | 3 | Immediate landing required |
+| WARNING_FAILED | `uint8` | 4 | Battery has failed completely |
### STATE {#STATE}
-| 명칭 | 형식 | Value | 설명 |
-| -------------------------------------------------------------------- | ------- | ----- | ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ |
-| STATE_UNHEALTHY | `uint8` | 6 | Battery is diagnosed to be defective or an error occurred, usage is discouraged / prohibited. Possible causes (faults) are listed in faults field |
-| STATE_CHARGING | `uint8` | 7 | Battery is charging |
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------------ | ------- | ----- | ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ |
+| STATE_UNHEALTHY | `uint8` | 6 | Battery is diagnosed to be defective or an error occurred, usage is discouraged / prohibited. Possible causes (faults) are listed in faults field |
+| STATE_CHARGING | `uint8` | 7 | Battery is charging |
### FAULT {#FAULT}
-| 명칭 | 형식 | Value | 설명 |
-| ---------------------------------------------------------------------------------------------------------------------- | ------- | ----- | --------------------------------------------------------------------------------------------------------------------------------- |
-| FAULT_DEEP_DISCHARGE | `uint8` | 0 | Battery has deep discharged |
-| FAULT_SPIKES | `uint8` | 1 | Voltage spikes |
-| FAULT_CELL_FAIL | `uint8` | 2 | One or more cells have failed |
-| FAULT_OVER_CURRENT | `uint8` | 3 | Over-current |
-| FAULT_OVER_TEMPERATURE | `uint8` | 4 | Over-temperature |
-| FAULT_UNDER_TEMPERATURE | `uint8` | 5 | Under-temperature fault |
-| FAULT_INCOMPATIBLE_VOLTAGE | `uint8` | 6 | Vehicle voltage is not compatible with this battery (batteries on same power rail should have similar voltage) |
-| FAULT_INCOMPATIBLE_FIRMWARE | `uint8` | 7 | Battery firmware is not compatible with current autopilot firmware |
-| FAULT_INCOMPATIBLE_MODEL | `uint8` | 8 | Battery model is not supported by the system |
-| FAULT_HARDWARE_FAILURE | `uint8` | 9 | Hardware problem |
-| FAULT_FAILED_TO_ARM | `uint8` | 10 | Battery had a problem while arming |
-| FAULT_COUNT | `uint8` | 11 | Counter. Keep this as last element |
+| 명칭 | 형식 | Value | 설명 |
+| -------------------------------------------------------------------------------------------------------------------- | ------- | ----- | --------------------------------------------------------------------------------------------------------------------------------- |
+| FAULT_DEEP_DISCHARGE | `uint8` | 0 | Battery has deep discharged |
+| FAULT_SPIKES | `uint8` | 1 | Voltage spikes |
+| FAULT_CELL_FAIL | `uint8` | 2 | One or more cells have failed |
+| FAULT_OVER_CURRENT | `uint8` | 3 | Over-current |
+| FAULT_OVER_TEMPERATURE | `uint8` | 4 | Over-temperature |
+| FAULT_UNDER_TEMPERATURE | `uint8` | 5 | Under-temperature fault |
+| FAULT_INCOMPATIBLE_VOLTAGE | `uint8` | 6 | Vehicle voltage is not compatible with this battery (batteries on same power rail should have similar voltage) |
+| FAULT_INCOMPATIBLE_FIRMWARE | `uint8` | 7 | Battery firmware is not compatible with current autopilot firmware |
+| FAULT_INCOMPATIBLE_MODEL | `uint8` | 8 | Battery model is not supported by the system |
+| FAULT_HARDWARE_FAILURE | `uint8` | 9 | Hardware problem |
+| FAULT_FAILED_TO_ARM | `uint8` | 10 | Battery had a problem while arming |
+| FAULT_COUNT | `uint8` | 11 | Counter. Keep this as last element |
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| -------------------------------------------------------------------- | -------- | ----- | -- |
-| MESSAGE_VERSION | `uint32` | 1 | |
-| MAX_INSTANCES | `uint8` | 3 | |
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------------ | -------- | ----- | -- |
+| MESSAGE_VERSION | `uint32` | 1 | |
+| MAX_INSTANCES | `uint8` | 3 | |
## Source Message
@@ -123,76 +123,75 @@ Click here to see original file
uint32 MESSAGE_VERSION = 1
uint8 MAX_INSTANCES = 3
-uint64 timestamp # [us] Time since system start
+uint64 timestamp # [us] Time since system start
-bool connected # Whether or not a battery is connected. For power modules this is based on a voltage threshold.
-float32 voltage_v # [V] [@invalid 0] Battery voltage
-float32 current_a # [A] [@invalid -1] Battery current
-float32 current_average_a # [A] [@invalid -1] Battery current average (for FW average in level flight)
-float32 discharged_mah # [mAh] [@invalid -1] Discharged amount
-float32 remaining # [@range 0,1] [@invalid -1] Remaining capacity
-float32 scale # [-] [@range 1,] [@invalid -1] Scaling factor to compensate for lower actuation power caused by voltage sag
-float32 time_remaining_s # [s] [@invalid NaN] Predicted time remaining until battery is empty under previous averaged load
-float32 temperature # [°C] [@invalid NaN] Temperature of the battery
-uint8 cell_count # [-] [@invalid 0] Number of cells
+bool connected # Whether or not a battery is connected. For power modules this is based on a voltage threshold.
+float32 voltage_v # [V] [@invalid 0] Battery voltage
+float32 current_a # [A] [@invalid -1] Battery current
+float32 current_average_a # [A] [@invalid -1] Battery current average (for FW average in level flight)
+float32 discharged_mah # [mAh] [@invalid -1] Discharged amount
+float32 remaining # [@range 0,1] [@invalid -1] Remaining capacity
+float32 scale # [-] [@range 1,] [@invalid -1] Scaling factor to compensate for lower actuation power caused by voltage sag
+float32 time_remaining_s # [s] [@invalid NaN] Predicted time remaining until battery is empty under previous averaged load
+float32 temperature # [degC] [@invalid NaN] Temperature of the battery
+uint8 cell_count # [-] [@invalid 0] Number of cells
+uint8 source # [@enum SOURCE] Battery source
+uint8 SOURCE_POWER_MODULE = 0 # Power module (analog ADC or I2C power monitor)
+uint8 SOURCE_EXTERNAL = 1 # External (MAVLink, CAN, or external driver)
+uint8 SOURCE_ESCS = 2 # ESCs (via ESC telemetry)
-uint8 source # [@enum SOURCE] Battery source
-uint8 SOURCE_POWER_MODULE = 0 # Power module (analog ADC or I2C power monitor)
-uint8 SOURCE_EXTERNAL = 1 # External (MAVLink, CAN, or external driver)
-uint8 SOURCE_ESCS = 2 # ESCs (via ESC telemetry)
+uint8 priority # [-] Zero based priority is the connection on the Power Controller V1..Vn AKA BrickN-1
+uint16 capacity # [mAh] Capacity of the battery when fully charged
+uint16 cycle_count # [-] Number of discharge cycles the battery has experienced
+uint16 average_time_to_empty # [minutes] Predicted remaining battery capacity based on the average rate of discharge
+uint16 manufacture_date # [-] Manufacture date, part of serial number of the battery pack. Formatted as: Day + Month×32 + (Year–1980)×512
+uint16 state_of_health # [%] [@range 0, 100] State of health. FullChargeCapacity/DesignCapacity
+uint16 max_error # [%] [@range 1, 100] Max error, expected margin of error in the state-of-charge calculation
+uint8 id # [-] ID number of a battery. Should be unique and consistent for the lifetime of a vehicle. 1-indexed
+uint16 interface_error # [-] Interface error counter
-uint8 priority # [-] Zero based priority is the connection on the Power Controller V1..Vn AKA BrickN-1
-uint16 capacity # [mAh] Capacity of the battery when fully charged
-uint16 cycle_count # [-] Number of discharge cycles the battery has experienced
-uint16 average_time_to_empty # [minutes] Predicted remaining battery capacity based on the average rate of discharge
-uint16 manufacture_date # [-] Manufacture date, part of serial number of the battery pack. Formatted as: Day + Month×32 + (Year–1980)×512
-uint16 state_of_health # [%] [@range 0, 100] State of health. FullChargeCapacity/DesignCapacity
-uint16 max_error # [%] [@range 1, 100] Max error, expected margin of error in the state-of-charge calculation
-uint8 id # [-] ID number of a battery. Should be unique and consistent for the lifetime of a vehicle. 1-indexed
-uint16 interface_error # [-] Interface error counter
+float32[14] voltage_cell_v # [V] [@invalid 0] Battery individual cell voltages
+float32 max_cell_voltage_delta # [V] Max difference between individual cell voltages
-float32[14] voltage_cell_v # [V] [@invalid 0] Battery individual cell voltages
-float32 max_cell_voltage_delta # [V] Max difference between individual cell voltages
+bool is_powering_off # Power off event imminent indication, false if unknown
+bool is_required # Set if the battery is explicitly required before arming
-bool is_powering_off # Power off event imminent indication, false if unknown
-bool is_required # Set if the battery is explicitly required before arming
+uint8 warning # [@enum WARNING STATE] Current battery warning
+uint8 WARNING_NONE = 0 # No battery low voltage warning active
+uint8 WARNING_LOW = 1 # Low voltage warning
+uint8 WARNING_CRITICAL = 2 # Critical voltage, return / abort immediately
+uint8 WARNING_EMERGENCY = 3 # Immediate landing required
+uint8 WARNING_FAILED = 4 # Battery has failed completely
+uint8 STATE_UNHEALTHY = 6 # Battery is diagnosed to be defective or an error occurred, usage is discouraged / prohibited. Possible causes (faults) are listed in faults field
+uint8 STATE_CHARGING = 7 # Battery is charging
-uint8 warning # [@enum WARNING STATE] Current battery warning
-uint8 WARNING_NONE = 0 # No battery low voltage warning active
-uint8 WARNING_LOW = 1 # Low voltage warning
-uint8 WARNING_CRITICAL = 2 # Critical voltage, return / abort immediately
-uint8 WARNING_EMERGENCY = 3 # Immediate landing required
-uint8 WARNING_FAILED = 4 # Battery has failed completely
-uint8 STATE_UNHEALTHY = 6 # Battery is diagnosed to be defective or an error occurred, usage is discouraged / prohibited. Possible causes (faults) are listed in faults field
-uint8 STATE_CHARGING = 7 # Battery is charging
+uint16 faults # [@enum FAULT] Smart battery supply status/fault flags (bitmask) for health indication
+uint8 FAULT_DEEP_DISCHARGE = 0 # Battery has deep discharged
+uint8 FAULT_SPIKES = 1 # Voltage spikes
+uint8 FAULT_CELL_FAIL= 2 # One or more cells have failed
+uint8 FAULT_OVER_CURRENT = 3 # Over-current
+uint8 FAULT_OVER_TEMPERATURE = 4 # Over-temperature
+uint8 FAULT_UNDER_TEMPERATURE = 5 # Under-temperature fault
+uint8 FAULT_INCOMPATIBLE_VOLTAGE = 6 # Vehicle voltage is not compatible with this battery (batteries on same power rail should have similar voltage)
+uint8 FAULT_INCOMPATIBLE_FIRMWARE = 7 # Battery firmware is not compatible with current autopilot firmware
+uint8 FAULT_INCOMPATIBLE_MODEL = 8 # Battery model is not supported by the system
+uint8 FAULT_HARDWARE_FAILURE = 9 # Hardware problem
+uint8 FAULT_FAILED_TO_ARM = 10 # Battery had a problem while arming
+uint8 FAULT_COUNT = 11 # Counter. Keep this as last element
-uint16 faults # [@enum FAULT] Smart battery supply status/fault flags (bitmask) for health indication
-uint8 FAULT_DEEP_DISCHARGE = 0 # Battery has deep discharged
-uint8 FAULT_SPIKES = 1 # Voltage spikes
-uint8 FAULT_CELL_FAIL= 2 # One or more cells have failed
-uint8 FAULT_OVER_CURRENT = 3 # Over-current
-uint8 FAULT_OVER_TEMPERATURE = 4 # Over-temperature
-uint8 FAULT_UNDER_TEMPERATURE = 5 # Under-temperature fault
-uint8 FAULT_INCOMPATIBLE_VOLTAGE = 6 # Vehicle voltage is not compatible with this battery (batteries on same power rail should have similar voltage)
-uint8 FAULT_INCOMPATIBLE_FIRMWARE = 7 # Battery firmware is not compatible with current autopilot firmware
-uint8 FAULT_INCOMPATIBLE_MODEL = 8 # Battery model is not supported by the system
-uint8 FAULT_HARDWARE_FAILURE = 9 # Hardware problem
-uint8 FAULT_FAILED_TO_ARM = 10 # Battery had a problem while arming
-uint8 FAULT_COUNT = 11 # Counter. Keep this as last element
+float32 full_charge_capacity_wh # [Wh] Compensated battery capacity
+float32 remaining_capacity_wh # [Wh] Compensated battery capacity remaining
+uint16 over_discharge_count # [-] Number of battery overdischarge
+float32 nominal_voltage # [V] Nominal voltage of the battery pack
-float32 full_charge_capacity_wh # [Wh] Compensated battery capacity
-float32 remaining_capacity_wh # [Wh] Compensated battery capacity remaining
-uint16 over_discharge_count # [-] Number of battery overdischarge
-float32 nominal_voltage # [V] Nominal voltage of the battery pack
-
-float32 internal_resistance_estimate # [Ohm] Internal resistance per cell estimate
-float32 ocv_estimate # [V] Open circuit voltage estimate
-float32 ocv_estimate_filtered # [V] Filtered open circuit voltage estimate
-float32 volt_based_soc_estimate # [-] [@range 0, 1] Normalized volt based state of charge estimate
-float32 voltage_prediction # [V] Predicted voltage
-float32 prediction_error # [V] Prediction error
-float32 estimation_covariance_norm # [-] Norm of the covariance matrix
+float32 internal_resistance_estimate # [Ohm] Internal resistance per cell estimate
+float32 ocv_estimate # [V] Open circuit voltage estimate
+float32 ocv_estimate_filtered # [V] Filtered open circuit voltage estimate
+float32 volt_based_soc_estimate # [-] [@range 0, 1] Normalized volt based state of charge estimate
+float32 voltage_prediction # [V] Predicted voltage
+float32 prediction_error # [V] Prediction error
+float32 estimation_covariance_norm # [-] Norm of the covariance matrix
```
:::
diff --git a/docs/ko/msg_docs/BatteryStatusV0.md b/docs/ko/msg_docs/BatteryStatusV0.md
index 569b955594..6859b3c3e3 100644
--- a/docs/ko/msg_docs/BatteryStatusV0.md
+++ b/docs/ko/msg_docs/BatteryStatusV0.md
@@ -10,7 +10,7 @@ Battery status information for up to 4 battery instances.
These are populated from power module and smart battery device drivers, and one battery updated from MAVLink.
Battery instance information is also logged and streamed in MAVLink telemetry.
-**TOPICS:** battery_statusv0
+**TOPICS:** battery_status_v0
## Fields
@@ -60,52 +60,52 @@ Battery instance information is also logged and streamed in MAVLink telemetry.
### SOURCE {#SOURCE}
-| 명칭 | 형식 | Value | 설명 |
-| ------------------------------------------------------------------------------------------------- | ------- | ----- | ----------------------------------------------------------------- |
-| SOURCE_POWER_MODULE | `uint8` | 0 | Power module (analog ADC or I2C power monitor) |
-| SOURCE_EXTERNAL | `uint8` | 1 | External (MAVLink, CAN, or external driver) |
-| SOURCE_ESCS | `uint8` | 2 | ESCs (via ESC telemetry) |
+| 명칭 | 형식 | Value | 설명 |
+| ----------------------------------------------------------------------------------------------- | ------- | ----- | ----------------------------------------------------------------- |
+| SOURCE_POWER_MODULE | `uint8` | 0 | Power module (analog ADC or I2C power monitor) |
+| SOURCE_EXTERNAL | `uint8` | 1 | External (MAVLink, CAN, or external driver) |
+| SOURCE_ESCS | `uint8` | 2 | ESCs (via ESC telemetry) |
### WARNING {#WARNING}
-| 명칭 | 형식 | Value | 설명 |
-| ------------------------------------------------------------------------ | ------- | ----- | -------------------------------------------- |
-| WARNING_NONE | `uint8` | 0 | No battery low voltage warning active |
-| WARNING_LOW | `uint8` | 1 | Low voltage warning |
-| WARNING_CRITICAL | `uint8` | 2 | Critical voltage, return / abort immediately |
-| WARNING_EMERGENCY | `uint8` | 3 | Immediate landing required |
-| WARNING_FAILED | `uint8` | 4 | Battery has failed completely |
+| 명칭 | 형식 | Value | 설명 |
+| ---------------------------------------------------------------------- | ------- | ----- | -------------------------------------------- |
+| WARNING_NONE | `uint8` | 0 | No battery low voltage warning active |
+| WARNING_LOW | `uint8` | 1 | Low voltage warning |
+| WARNING_CRITICAL | `uint8` | 2 | Critical voltage, return / abort immediately |
+| WARNING_EMERGENCY | `uint8` | 3 | Immediate landing required |
+| WARNING_FAILED | `uint8` | 4 | Battery has failed completely |
### STATE {#STATE}
-| 명칭 | 형식 | Value | 설명 |
-| -------------------------------------------------------------------- | ------- | ----- | ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ |
-| STATE_UNHEALTHY | `uint8` | 6 | Battery is diagnosed to be defective or an error occurred, usage is discouraged / prohibited. Possible causes (faults) are listed in faults field |
-| STATE_CHARGING | `uint8` | 7 | Battery is charging |
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------------ | ------- | ----- | ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ |
+| STATE_UNHEALTHY | `uint8` | 6 | Battery is diagnosed to be defective or an error occurred, usage is discouraged / prohibited. Possible causes (faults) are listed in faults field |
+| STATE_CHARGING | `uint8` | 7 | Battery is charging |
### FAULT {#FAULT}
-| 명칭 | 형식 | Value | 설명 |
-| ---------------------------------------------------------------------------------------------------------------------- | ------- | ----- | --------------------------------------------------------------------------------------------------------------------------------- |
-| FAULT_DEEP_DISCHARGE | `uint8` | 0 | Battery has deep discharged |
-| FAULT_SPIKES | `uint8` | 1 | Voltage spikes |
-| FAULT_CELL_FAIL | `uint8` | 2 | One or more cells have failed |
-| FAULT_OVER_CURRENT | `uint8` | 3 | Over-current |
-| FAULT_OVER_TEMPERATURE | `uint8` | 4 | Over-temperature |
-| FAULT_UNDER_TEMPERATURE | `uint8` | 5 | Under-temperature fault |
-| FAULT_INCOMPATIBLE_VOLTAGE | `uint8` | 6 | Vehicle voltage is not compatible with this battery (batteries on same power rail should have similar voltage) |
-| FAULT_INCOMPATIBLE_FIRMWARE | `uint8` | 7 | Battery firmware is not compatible with current autopilot firmware |
-| FAULT_INCOMPATIBLE_MODEL | `uint8` | 8 | Battery model is not supported by the system |
-| FAULT_HARDWARE_FAILURE | `uint8` | 9 | Hardware problem |
-| FAULT_FAILED_TO_ARM | `uint8` | 10 | Battery had a problem while arming |
-| FAULT_COUNT | `uint8` | 11 | Counter. Keep this as last element |
+| 명칭 | 형식 | Value | 설명 |
+| -------------------------------------------------------------------------------------------------------------------- | ------- | ----- | --------------------------------------------------------------------------------------------------------------------------------- |
+| FAULT_DEEP_DISCHARGE | `uint8` | 0 | Battery has deep discharged |
+| FAULT_SPIKES | `uint8` | 1 | Voltage spikes |
+| FAULT_CELL_FAIL | `uint8` | 2 | One or more cells have failed |
+| FAULT_OVER_CURRENT | `uint8` | 3 | Over-current |
+| FAULT_OVER_TEMPERATURE | `uint8` | 4 | Over-temperature |
+| FAULT_UNDER_TEMPERATURE | `uint8` | 5 | Under-temperature fault |
+| FAULT_INCOMPATIBLE_VOLTAGE | `uint8` | 6 | Vehicle voltage is not compatible with this battery (batteries on same power rail should have similar voltage) |
+| FAULT_INCOMPATIBLE_FIRMWARE | `uint8` | 7 | Battery firmware is not compatible with current autopilot firmware |
+| FAULT_INCOMPATIBLE_MODEL | `uint8` | 8 | Battery model is not supported by the system |
+| FAULT_HARDWARE_FAILURE | `uint8` | 9 | Hardware problem |
+| FAULT_FAILED_TO_ARM | `uint8` | 10 | Battery had a problem while arming |
+| FAULT_COUNT | `uint8` | 11 | Counter. Keep this as last element |
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| -------------------------------------------------------------------- | -------- | ----- | -- |
-| MESSAGE_VERSION | `uint32` | 0 | |
-| MAX_INSTANCES | `uint8` | 4 | |
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------------ | -------- | ----- | -- |
+| MESSAGE_VERSION | `uint32` | 0 | |
+| MAX_INSTANCES | `uint8` | 4 | |
## Source Message
diff --git a/docs/ko/msg_docs/ButtonEvent.md b/docs/ko/msg_docs/ButtonEvent.md
index 26b8256910..464887c736 100644
--- a/docs/ko/msg_docs/ButtonEvent.md
+++ b/docs/ko/msg_docs/ButtonEvent.md
@@ -15,9 +15,9 @@ pageClass: is-wide-page
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ------------------------------------------------------------------------------------------- | ------- | ----- | -- |
-| ORB_QUEUE_LENGTH | `uint8` | 2 | |
+| 명칭 | 형식 | Value | 설명 |
+| ----------------------------------------------------------------------------------------- | ------- | ----- | -- |
+| ORB_QUEUE_LENGTH | `uint8` | 2 | |
## Source Message
diff --git a/docs/ko/msg_docs/CameraTrigger.md b/docs/ko/msg_docs/CameraTrigger.md
index c59b50d542..07ae75942e 100644
--- a/docs/ko/msg_docs/CameraTrigger.md
+++ b/docs/ko/msg_docs/CameraTrigger.md
@@ -17,9 +17,9 @@ pageClass: is-wide-page
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ------------------------------------------------------------------------------------------- | -------- | ----- | -- |
-| ORB_QUEUE_LENGTH | `uint32` | 2 | |
+| 명칭 | 형식 | Value | 설명 |
+| ----------------------------------------------------------------------------------------- | -------- | ----- | -- |
+| ORB_QUEUE_LENGTH | `uint32` | 2 | |
## Source Message
diff --git a/docs/ko/msg_docs/CanInterfaceStatus.md b/docs/ko/msg_docs/CanInterfaceStatus.md
index e00ec7c3ae..f777bc55e6 100644
--- a/docs/ko/msg_docs/CanInterfaceStatus.md
+++ b/docs/ko/msg_docs/CanInterfaceStatus.md
@@ -4,7 +4,7 @@ pageClass: is-wide-page
# CanInterfaceStatus (UORB message)
-**TOPICS:** can_interfacestatus
+**TOPICS:** can_interface_status
## Fields
diff --git a/docs/ko/msg_docs/CellularStatus.md b/docs/ko/msg_docs/CellularStatus.md
index d5a547f472..fb0c17c251 100644
--- a/docs/ko/msg_docs/CellularStatus.md
+++ b/docs/ko/msg_docs/CellularStatus.md
@@ -27,40 +27,40 @@ This is currently used only for logging cell status from MAVLink.
### STATUS_FLAG {#STATUS_FLAG}
-| 명칭 | 형식 | Value | 설명 |
-| ------------------------------------------------------------------------------------------------------------- | -------- | ----- | --------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- |
-| STATUS_FLAG_UNKNOWN | `uint16` | 1 | State unknown or not reportable |
-| STATUS_FLAG_FAILED | `uint16` | 2 | Modem is unusable |
-| STATUS_FLAG_INITIALIZING | `uint16` | 4 | Modem is being initialized |
-| STATUS_FLAG_LOCKED | `uint16` | 8 | Modem is locked |
-| STATUS_FLAG_DISABLED | `uint16` | 16 | Modem is not enabled and is powered down |
-| STATUS_FLAG_DISABLING | `uint16` | 32 | Modem is currently transitioning to the STATUS_FLAG_DISABLED state |
-| STATUS_FLAG_ENABLING | `uint16` | 64 | Modem is currently transitioning to the STATUS_FLAG_ENABLED state |
-| STATUS_FLAG_ENABLED | `uint16` | 128 | Modem is enabled and powered on but not registered with a network provider and not available for data connections |
-| STATUS_FLAG_SEARCHING | `uint16` | 256 | Modem is searching for a network provider to register |
-| STATUS_FLAG_REGISTERED | `uint16` | 512 | Modem is registered with a network provider, and data connections and messaging may be available for use |
-| STATUS_FLAG_DISCONNECTING | `uint16` | 1024 | Modem is disconnecting and deactivating the last active packet data bearer. This state will not be entered if more than one packet data bearer is active and one of the active bearers is deactivated |
-| STATUS_FLAG_CONNECTING | `uint16` | 2048 | Modem is activating and connecting the first packet data bearer. Subsequent bearer activations when another bearer is already active do not cause this state to be entered |
-| STATUS_FLAG_CONNECTED | `uint16` | 4096 | One or more packet data bearers is active and connected |
+| 명칭 | 형식 | Value | 설명 |
+| ----------------------------------------------------------------------------------------------------------- | -------- | ----- | --------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- |
+| STATUS_FLAG_UNKNOWN | `uint16` | 1 | State unknown or not reportable |
+| STATUS_FLAG_FAILED | `uint16` | 2 | Modem is unusable |
+| STATUS_FLAG_INITIALIZING | `uint16` | 4 | Modem is being initialized |
+| STATUS_FLAG_LOCKED | `uint16` | 8 | Modem is locked |
+| STATUS_FLAG_DISABLED | `uint16` | 16 | Modem is not enabled and is powered down |
+| STATUS_FLAG_DISABLING | `uint16` | 32 | Modem is currently transitioning to the STATUS_FLAG_DISABLED state |
+| STATUS_FLAG_ENABLING | `uint16` | 64 | Modem is currently transitioning to the STATUS_FLAG_ENABLED state |
+| STATUS_FLAG_ENABLED | `uint16` | 128 | Modem is enabled and powered on but not registered with a network provider and not available for data connections |
+| STATUS_FLAG_SEARCHING | `uint16` | 256 | Modem is searching for a network provider to register |
+| STATUS_FLAG_REGISTERED | `uint16` | 512 | Modem is registered with a network provider, and data connections and messaging may be available for use |
+| STATUS_FLAG_DISCONNECTING | `uint16` | 1024 | Modem is disconnecting and deactivating the last active packet data bearer. This state will not be entered if more than one packet data bearer is active and one of the active bearers is deactivated |
+| STATUS_FLAG_CONNECTING | `uint16` | 2048 | Modem is activating and connecting the first packet data bearer. Subsequent bearer activations when another bearer is already active do not cause this state to be entered |
+| STATUS_FLAG_CONNECTED | `uint16` | 4096 | One or more packet data bearers is active and connected |
### FAILURE_REASON {#FAILURE_REASON}
-| 명칭 | 형식 | Value | 설명 |
-| ------------------------------------------------------------------------------------------------------------------------------------ | ------- | ----- | ----------------------------------------------- |
-| FAILURE_REASON_NONE | `uint8` | 0 | No error |
-| FAILURE_REASON_UNKNOWN | `uint8` | 1 | Error state is unknown |
-| FAILURE_REASON_SIM_MISSING | `uint8` | 2 | SIM is required for the modem but missing |
-| FAILURE_REASON_SIM_ERROR | `uint8` | 3 | SIM is available, but not usable for connection |
+| 명칭 | 형식 | Value | 설명 |
+| ---------------------------------------------------------------------------------------------------------------------------------- | ------- | ----- | ----------------------------------------------- |
+| FAILURE_REASON_NONE | `uint8` | 0 | No error |
+| FAILURE_REASON_UNKNOWN | `uint8` | 1 | Error state is unknown |
+| FAILURE_REASON_SIM_MISSING | `uint8` | 2 | SIM is required for the modem but missing |
+| FAILURE_REASON_SIM_ERROR | `uint8` | 3 | SIM is available, but not usable for connection |
### CELLULAR_NETWORK_RADIO_TYPE {#CELLULAR_NETWORK_RADIO_TYPE}
-| 명칭 | 형식 | Value | 설명 |
-| ----------------------------------------------------------------------------------------------------------------------------------------------------------------------- | ------- | ----- | ----- |
-| CELLULAR_NETWORK_RADIO_TYPE_NONE | `uint8` | 0 | None |
-| CELLULAR_NETWORK_RADIO_TYPE_GSM | `uint8` | 1 | GSM |
-| CELLULAR_NETWORK_RADIO_TYPE_CDMA | `uint8` | 2 | CDMA |
-| CELLULAR_NETWORK_RADIO_TYPE_WCDMA | `uint8` | 3 | WCDMA |
-| CELLULAR_NETWORK_RADIO_TYPE_LTE | `uint8` | 4 | LTE |
+| 명칭 | 형식 | Value | 설명 |
+| --------------------------------------------------------------------------------------------------------------------------------------------------------------------- | ------- | ----- | ----- |
+| CELLULAR_NETWORK_RADIO_TYPE_NONE | `uint8` | 0 | None |
+| CELLULAR_NETWORK_RADIO_TYPE_GSM | `uint8` | 1 | GSM |
+| CELLULAR_NETWORK_RADIO_TYPE_CDMA | `uint8` | 2 | CDMA |
+| CELLULAR_NETWORK_RADIO_TYPE_WCDMA | `uint8` | 3 | WCDMA |
+| CELLULAR_NETWORK_RADIO_TYPE_LTE | `uint8` | 4 | LTE |
## Source Message
diff --git a/docs/ko/msg_docs/ConfigOverrides.md b/docs/ko/msg_docs/ConfigOverrides.md
index cb1c45cbee..750c091ab6 100644
--- a/docs/ko/msg_docs/ConfigOverrides.md
+++ b/docs/ko/msg_docs/ConfigOverrides.md
@@ -22,12 +22,12 @@ Configurable overrides by (external) modes or mode executors.
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ---------------------------------------------------------------------------------------------------------------------------------- | -------- | ----- | -- |
-| MESSAGE_VERSION | `uint32` | 1 | |
-| SOURCE_TYPE_MODE | `int8` | 0 | |
-| SOURCE_TYPE_MODE_EXECUTOR | `int8` | 1 | |
-| ORB_QUEUE_LENGTH | `uint8` | 4 | |
+| 명칭 | 형식 | Value | 설명 |
+| -------------------------------------------------------------------------------------------------------------------------------- | -------- | ----- | -- |
+| MESSAGE_VERSION | `uint32` | 1 | |
+| SOURCE_TYPE_MODE | `int8` | 0 | |
+| SOURCE_TYPE_MODE_EXECUTOR | `int8` | 1 | |
+| ORB_QUEUE_LENGTH | `uint8` | 4 | |
## Source Message
diff --git a/docs/ko/msg_docs/ConfigOverridesV0.md b/docs/ko/msg_docs/ConfigOverridesV0.md
index a7dcaf2a98..bb4b184712 100644
--- a/docs/ko/msg_docs/ConfigOverridesV0.md
+++ b/docs/ko/msg_docs/ConfigOverridesV0.md
@@ -21,12 +21,12 @@ Configurable overrides by (external) modes or mode executors.
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ---------------------------------------------------------------------------------------------------------------------------------- | -------- | ----- | -- |
-| MESSAGE_VERSION | `uint32` | 0 | |
-| SOURCE_TYPE_MODE | `int8` | 0 | |
-| SOURCE_TYPE_MODE_EXECUTOR | `int8` | 1 | |
-| ORB_QUEUE_LENGTH | `uint8` | 4 | |
+| 명칭 | 형식 | Value | 설명 |
+| -------------------------------------------------------------------------------------------------------------------------------- | -------- | ----- | -- |
+| MESSAGE_VERSION | `uint32` | 0 | |
+| SOURCE_TYPE_MODE | `int8` | 0 | |
+| SOURCE_TYPE_MODE_EXECUTOR | `int8` | 1 | |
+| ORB_QUEUE_LENGTH | `uint8` | 4 | |
## Source Message
diff --git a/docs/ko/msg_docs/ControlAllocatorStatus.md b/docs/ko/msg_docs/ControlAllocatorStatus.md
index 4239807f5a..42632fd7f6 100644
--- a/docs/ko/msg_docs/ControlAllocatorStatus.md
+++ b/docs/ko/msg_docs/ControlAllocatorStatus.md
@@ -4,7 +4,7 @@ pageClass: is-wide-page
# ControlAllocatorStatus (UORB message)
-**TOPICS:** control_allocatorstatus
+**TOPICS:** control_allocator_status
## Fields
@@ -21,13 +21,13 @@ pageClass: is-wide-page
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ------------------------------------------------------------------------------------------------------------------------------------------ | ------ | ----- | ----------------------------------------------------------------------------------------------------------------------------------------------------- |
-| ACTUATOR_SATURATION_OK | `int8` | 0 | The actuator is not saturated |
-| ACTUATOR_SATURATION_UPPER_DYN | `int8` | 1 | The actuator is saturated (with a value <= the desired value) because it cannot increase its value faster |
-| ACTUATOR_SATURATION_UPPER | `int8` | 2 | The actuator is saturated (with a value <= the desired value) because it has reached its maximum value |
-| ACTUATOR_SATURATION_LOWER_DYN | `int8` | -1 | The actuator is saturated (with a value >= the desired value) because it cannot decrease its value faster |
-| ACTUATOR_SATURATION_LOWER | `int8` | -2 | The actuator is saturated (with a value >= the desired value) because it has reached its minimum value |
+| 명칭 | 형식 | Value | 설명 |
+| ---------------------------------------------------------------------------------------------------------------------------------------- | ------ | ----- | ----------------------------------------------------------------------------------------------------------------------------------------------------- |
+| ACTUATOR_SATURATION_OK | `int8` | 0 | The actuator is not saturated |
+| ACTUATOR_SATURATION_UPPER_DYN | `int8` | 1 | The actuator is saturated (with a value <= the desired value) because it cannot increase its value faster |
+| ACTUATOR_SATURATION_UPPER | `int8` | 2 | The actuator is saturated (with a value <= the desired value) because it has reached its maximum value |
+| ACTUATOR_SATURATION_LOWER_DYN | `int8` | -1 | The actuator is saturated (with a value >= the desired value) because it cannot decrease its value faster |
+| ACTUATOR_SATURATION_LOWER | `int8` | -2 | The actuator is saturated (with a value >= the desired value) because it has reached its minimum value |
## Source Message
diff --git a/docs/ko/msg_docs/DatamanResponse.md b/docs/ko/msg_docs/DatamanResponse.md
index fd41bf5a34..b404859c45 100644
--- a/docs/ko/msg_docs/DatamanResponse.md
+++ b/docs/ko/msg_docs/DatamanResponse.md
@@ -20,14 +20,14 @@ pageClass: is-wide-page
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| -------------------------------------------------------------------------------------------------------------------------------------- | ------- | ----- | -- |
-| STATUS_SUCCESS | `uint8` | 0 | |
-| STATUS_FAILURE_ID_ERR | `uint8` | 1 | |
-| STATUS_FAILURE_NO_DATA | `uint8` | 2 | |
-| STATUS_FAILURE_READ_FAILED | `uint8` | 3 | |
-| STATUS_FAILURE_WRITE_FAILED | `uint8` | 4 | |
-| STATUS_FAILURE_CLEAR_FAILED | `uint8` | 5 | |
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------------------------------------------------------------------------------ | ------- | ----- | -- |
+| STATUS_SUCCESS | `uint8` | 0 | |
+| STATUS_FAILURE_ID_ERR | `uint8` | 1 | |
+| STATUS_FAILURE_NO_DATA | `uint8` | 2 | |
+| STATUS_FAILURE_READ_FAILED | `uint8` | 3 | |
+| STATUS_FAILURE_WRITE_FAILED | `uint8` | 4 | |
+| STATUS_FAILURE_CLEAR_FAILED | `uint8` | 5 | |
## Source Message
diff --git a/docs/ko/msg_docs/DebugArray.md b/docs/ko/msg_docs/DebugArray.md
index 80918ae97f..67b715fa2a 100644
--- a/docs/ko/msg_docs/DebugArray.md
+++ b/docs/ko/msg_docs/DebugArray.md
@@ -17,9 +17,9 @@ pageClass: is-wide-page
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ---------------------------------------------------------- | ------- | ----- | -- |
-| ARRAY_SIZE | `uint8` | 58 | |
+| 명칭 | 형식 | Value | 설명 |
+| -------------------------------------------------------- | ------- | ----- | -- |
+| ARRAY_SIZE | `uint8` | 58 | |
## Source Message
diff --git a/docs/ko/msg_docs/DebugKeyValue.md b/docs/ko/msg_docs/DebugKeyValue.md
index 1ed3816e57..3734a5f61b 100644
--- a/docs/ko/msg_docs/DebugKeyValue.md
+++ b/docs/ko/msg_docs/DebugKeyValue.md
@@ -4,7 +4,7 @@ pageClass: is-wide-page
# DebugKeyValue (UORB message)
-**TOPICS:** debug_keyvalue
+**TOPICS:** debug_key_value
## Fields
diff --git a/docs/ko/msg_docs/DeviceInformation.md b/docs/ko/msg_docs/DeviceInformation.md
index af01a4f244..5183964ddb 100644
--- a/docs/ko/msg_docs/DeviceInformation.md
+++ b/docs/ko/msg_docs/DeviceInformation.md
@@ -17,8 +17,7 @@ as well as tracking of the used firmware versions on the devices.
| ------------------------------------- | ---------- | ---------------------------------------------------------------- | ----------------------------------------------------------------------------------------------------------------------------------------------------------------------- | ------------------------------------------------------------------------------------------------------------------------------- |
| timestamp | `uint64` | | | time since system start (microseconds) |
| device_type | `uint8` | | [DEVICE_TYPE](#DEVICE_TYPE) | Type of the device. Matches MAVLink DEVICE_TYPE enum |
-| vendor_name | `char[32]` | | | Name of the device vendor |
-| model_name | `char[32]` | | | Name of the device model |
+| name | `char[80]` | | | Name of device e.g. DroneCAN node name |
| `uint32` | | | Unique device ID for the sensor. Does not change between power cycles. (Invalid: 0 if not available) | |
| firmware_version | `char[24]` | | | Firmware version. (Invalid: empty if not available) |
| hardware_version | `char[24]` | | | Hardware version. (Invalid: empty if not available) |
@@ -28,24 +27,24 @@ as well as tracking of the used firmware versions on the devices.
### DEVICE_TYPE {#DEVICE_TYPE}
-| 명칭 | 형식 | Value | 설명 |
-| -------------------------------------------------------------------------------------------------------------------------------------------------- | ------- | ----- | ---------------------- |
-| DEVICE_TYPE_GENERIC | `uint8` | 0 | Generic/unknown sensor |
-| DEVICE_TYPE_AIRSPEED | `uint8` | 1 | 풍속 센서 |
-| DEVICE_TYPE_ESC | `uint8` | 2 | ESC |
-| DEVICE_TYPE_SERVO | `uint8` | 3 | Servo |
-| DEVICE_TYPE_GPS | `uint8` | 4 | GPS |
-| DEVICE_TYPE_MAGNETOMETER | `uint8` | 5 | 자기 센서 |
-| DEVICE_TYPE_PARACHUTE | `uint8` | 6 | 낙하산 |
-| DEVICE_TYPE_RANGEFINDER | `uint8` | 7 | Rangefinder |
-| DEVICE_TYPE_WINCH | `uint8` | 8 | Winch |
-| DEVICE_TYPE_BAROMETER | `uint8` | 9 | 기압계 |
-| DEVICE_TYPE_OPTICAL_FLOW | `uint8` | 10 | Optical flow |
-| DEVICE_TYPE_ACCELEROMETER | `uint8` | 11 | Accelerometer |
-| DEVICE_TYPE_GYROSCOPE | `uint8` | 12 | Gyroscope |
-| DEVICE_TYPE_DIFFERENTIAL_PRESSURE | `uint8` | 13 | Differential pressure |
-| DEVICE_TYPE_BATTERY | `uint8` | 14 | Battery |
-| DEVICE_TYPE_HYGROMETER | `uint8` | 15 | Hygrometer |
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------------------------------------------------------------------------------------------ | ------- | ----- | ---------------------- |
+| DEVICE_TYPE_GENERIC | `uint8` | 0 | Generic/unknown sensor |
+| DEVICE_TYPE_AIRSPEED | `uint8` | 1 | 풍속 센서 |
+| DEVICE_TYPE_ESC | `uint8` | 2 | ESC |
+| DEVICE_TYPE_SERVO | `uint8` | 3 | Servo |
+| DEVICE_TYPE_GPS | `uint8` | 4 | GPS |
+| DEVICE_TYPE_MAGNETOMETER | `uint8` | 5 | 자기 센서 |
+| DEVICE_TYPE_PARACHUTE | `uint8` | 6 | 낙하산 |
+| DEVICE_TYPE_RANGEFINDER | `uint8` | 7 | Rangefinder |
+| DEVICE_TYPE_WINCH | `uint8` | 8 | Winch |
+| DEVICE_TYPE_BAROMETER | `uint8` | 9 | 기압계 |
+| DEVICE_TYPE_OPTICAL_FLOW | `uint8` | 10 | Optical flow |
+| DEVICE_TYPE_ACCELEROMETER | `uint8` | 11 | Accelerometer |
+| DEVICE_TYPE_GYROSCOPE | `uint8` | 12 | Gyroscope |
+| DEVICE_TYPE_DIFFERENTIAL_PRESSURE | `uint8` | 13 | Differential pressure |
+| DEVICE_TYPE_BATTERY | `uint8` | 14 | Battery |
+| DEVICE_TYPE_HYGROMETER | `uint8` | 15 | Hygrometer |
## Source Message
@@ -63,7 +62,6 @@ Click here to see original file
uint64 timestamp # time since system start (microseconds)
uint8 device_type # [@enum DEVICE_TYPE] Type of the device. Matches MAVLink DEVICE_TYPE enum
-
uint8 DEVICE_TYPE_GENERIC = 0 # Generic/unknown sensor
uint8 DEVICE_TYPE_AIRSPEED = 1 # Airspeed sensor
uint8 DEVICE_TYPE_ESC = 2 # ESC
@@ -81,8 +79,7 @@ uint8 DEVICE_TYPE_DIFFERENTIAL_PRESSURE = 13 # Differential pressure
uint8 DEVICE_TYPE_BATTERY = 14 # Battery
uint8 DEVICE_TYPE_HYGROMETER = 15 # Hygrometer
-char[32] vendor_name # Name of the device vendor
-char[32] model_name # Name of the device model
+char[80] name # Name of device e.g. DroneCAN node name
uint32 device_id # [-] [@invalid 0 if not available] Unique device ID for the sensor. Does not change between power cycles.
char[24] firmware_version # [-] [@invalid empty if not available] Firmware version.
diff --git a/docs/ko/msg_docs/DistanceSensor.md b/docs/ko/msg_docs/DistanceSensor.md
index d66f400c91..16747401fc 100644
--- a/docs/ko/msg_docs/DistanceSensor.md
+++ b/docs/ko/msg_docs/DistanceSensor.md
@@ -28,30 +28,30 @@ DISTANCE_SENSOR message data.
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| -------------------------------------------------------------------------------------------------------------------------------------------- | ------- | ----- | ----------------------------------------------------------------------------------------------------------------- |
-| MAV_DISTANCE_SENSOR_LASER | `uint8` | 0 | |
-| MAV_DISTANCE_SENSOR_ULTRASOUND | `uint8` | 1 | |
-| MAV_DISTANCE_SENSOR_INFRARED | `uint8` | 2 | |
-| MAV_DISTANCE_SENSOR_RADAR | `uint8` | 3 | |
-| ROTATION_YAW_0 | `uint8` | 0 | MAV_SENSOR_ROTATION_NONE |
-| ROTATION_YAW_45 | `uint8` | 1 | MAV_SENSOR_ROTATION_YAW_45 |
-| ROTATION_YAW_90 | `uint8` | 2 | MAV_SENSOR_ROTATION_YAW_90 |
-| ROTATION_YAW_135 | `uint8` | 3 | MAV_SENSOR_ROTATION_YAW_135 |
-| ROTATION_YAW_180 | `uint8` | 4 | MAV_SENSOR_ROTATION_YAW_180 |
-| ROTATION_YAW_225 | `uint8` | 5 | MAV_SENSOR_ROTATION_YAW_225 |
-| ROTATION_YAW_270 | `uint8` | 6 | MAV_SENSOR_ROTATION_YAW_270 |
-| ROTATION_YAW_315 | `uint8` | 7 | MAV_SENSOR_ROTATION_YAW_315 |
-| ROTATION_FORWARD_FACING | `uint8` | 0 | MAV_SENSOR_ROTATION_NONE |
-| ROTATION_RIGHT_FACING | `uint8` | 2 | MAV_SENSOR_ROTATION_YAW_90 |
-| ROTATION_BACKWARD_FACING | `uint8` | 4 | MAV_SENSOR_ROTATION_YAW_180 |
-| ROTATION_LEFT_FACING | `uint8` | 6 | MAV_SENSOR_ROTATION_YAW_270 |
-| ROTATION_UPWARD_FACING | `uint8` | 24 | MAV_SENSOR_ROTATION_PITCH_90 |
-| ROTATION_DOWNWARD_FACING | `uint8` | 25 | MAV_SENSOR_ROTATION_PITCH_270 |
-| ROTATION_CUSTOM | `uint8` | 100 | MAV_SENSOR_ROTATION_CUSTOM |
-| MODE_UNKNOWN | `uint8` | 0 | |
-| MODE_ENABLED | `uint8` | 1 | |
-| MODE_DISABLED | `uint8` | 2 | |
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------------------------------------------------------------------------------------ | ------- | ----- | ----------------------------------------------------------------------------------------------------------------- |
+| MAV_DISTANCE_SENSOR_LASER | `uint8` | 0 | |
+| MAV_DISTANCE_SENSOR_ULTRASOUND | `uint8` | 1 | |
+| MAV_DISTANCE_SENSOR_INFRARED | `uint8` | 2 | |
+| MAV_DISTANCE_SENSOR_RADAR | `uint8` | 3 | |
+| ROTATION_YAW_0 | `uint8` | 0 | MAV_SENSOR_ROTATION_NONE |
+| ROTATION_YAW_45 | `uint8` | 1 | MAV_SENSOR_ROTATION_YAW_45 |
+| ROTATION_YAW_90 | `uint8` | 2 | MAV_SENSOR_ROTATION_YAW_90 |
+| ROTATION_YAW_135 | `uint8` | 3 | MAV_SENSOR_ROTATION_YAW_135 |
+| ROTATION_YAW_180 | `uint8` | 4 | MAV_SENSOR_ROTATION_YAW_180 |
+| ROTATION_YAW_225 | `uint8` | 5 | MAV_SENSOR_ROTATION_YAW_225 |
+| ROTATION_YAW_270 | `uint8` | 6 | MAV_SENSOR_ROTATION_YAW_270 |
+| ROTATION_YAW_315 | `uint8` | 7 | MAV_SENSOR_ROTATION_YAW_315 |
+| ROTATION_FORWARD_FACING | `uint8` | 0 | MAV_SENSOR_ROTATION_NONE |
+| ROTATION_RIGHT_FACING | `uint8` | 2 | MAV_SENSOR_ROTATION_YAW_90 |
+| ROTATION_BACKWARD_FACING | `uint8` | 4 | MAV_SENSOR_ROTATION_YAW_180 |
+| ROTATION_LEFT_FACING | `uint8` | 6 | MAV_SENSOR_ROTATION_YAW_270 |
+| ROTATION_UPWARD_FACING | `uint8` | 24 | MAV_SENSOR_ROTATION_PITCH_90 |
+| ROTATION_DOWNWARD_FACING | `uint8` | 25 | MAV_SENSOR_ROTATION_PITCH_270 |
+| ROTATION_CUSTOM | `uint8` | 100 | MAV_SENSOR_ROTATION_CUSTOM |
+| MODE_UNKNOWN | `uint8` | 0 | |
+| MODE_ENABLED | `uint8` | 1 | |
+| MODE_DISABLED | `uint8` | 2 | |
## Source Message
diff --git a/docs/ko/msg_docs/DistanceSensorModeChangeRequest.md b/docs/ko/msg_docs/DistanceSensorModeChangeRequest.md
index 8c222c5d97..50fcfdc283 100644
--- a/docs/ko/msg_docs/DistanceSensorModeChangeRequest.md
+++ b/docs/ko/msg_docs/DistanceSensorModeChangeRequest.md
@@ -4,7 +4,7 @@ pageClass: is-wide-page
# DistanceSensorModeChangeRequest (UORB message)
-**TOPICS:** distance_sensormode_changerequest
+**TOPICS:** distance_sensor_mode_change_request
## Fields
@@ -15,10 +15,10 @@ pageClass: is-wide-page
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ------------------------------------------------------------ | ------- | ----- | -- |
-| REQUEST_OFF | `uint8` | 0 | |
-| REQUEST_ON | `uint8` | 1 | |
+| 명칭 | 형식 | Value | 설명 |
+| ---------------------------------------------------------- | ------- | ----- | -- |
+| REQUEST_OFF | `uint8` | 0 | |
+| REQUEST_ON | `uint8` | 1 | |
## Source Message
diff --git a/docs/ko/msg_docs/DronecanNodeStatus.md b/docs/ko/msg_docs/DronecanNodeStatus.md
index 7a4cbd8f7a..1243556fd6 100644
--- a/docs/ko/msg_docs/DronecanNodeStatus.md
+++ b/docs/ko/msg_docs/DronecanNodeStatus.md
@@ -4,7 +4,7 @@ pageClass: is-wide-page
# DronecanNodeStatus (UORB message)
-**TOPICS:** dronecan_nodestatus
+**TOPICS:** dronecan_node_status
## Fields
@@ -20,17 +20,17 @@ pageClass: is-wide-page
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| --------------------------------------------------------------------------------------------------- | ------- | ----- | ----------------------------------------------------------------------------------------------- |
-| HEALTH_OK | `uint8` | 0 | The node is functioning properly. |
-| HEALTH_WARNING | `uint8` | 1 | A critical parameter went out of range or the node encountered a minor failure. |
-| HEALTH_ERROR | `uint8` | 2 | The node encountered a major failure. |
-| HEALTH_CRITICAL | `uint8` | 3 | The node suffered a fatal malfunction. |
-| MODE_OPERATIONAL | `uint8` | 0 | Normal operating mode. |
-| MODE_INITIALIZATION | `uint8` | 1 | Initialization is in progress; this mode is entered immediately after startup. |
-| MODE_MAINTENANCE | `uint8` | 2 | 예: calibration, the bootloader is running, etc. |
-| MODE_SOFTWARE_UPDATE | `uint8` | 3 | New software/firmware is being loaded. |
-| MODE_OFFLINE | `uint8` | 7 | The node is no longer available. |
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------------------------------------------- | ------- | ----- | ----------------------------------------------------------------------------------------------- |
+| HEALTH_OK | `uint8` | 0 | The node is functioning properly. |
+| HEALTH_WARNING | `uint8` | 1 | A critical parameter went out of range or the node encountered a minor failure. |
+| HEALTH_ERROR | `uint8` | 2 | The node encountered a major failure. |
+| HEALTH_CRITICAL | `uint8` | 3 | The node suffered a fatal malfunction. |
+| MODE_OPERATIONAL | `uint8` | 0 | Normal operating mode. |
+| MODE_INITIALIZATION | `uint8` | 1 | Initialization is in progress; this mode is entered immediately after startup. |
+| MODE_MAINTENANCE | `uint8` | 2 | 예: calibration, the bootloader is running, etc. |
+| MODE_SOFTWARE_UPDATE | `uint8` | 3 | New software/firmware is being loaded. |
+| MODE_OFFLINE | `uint8` | 7 | The node is no longer available. |
## Source Message
diff --git a/docs/ko/msg_docs/Ekf2Timestamps.md b/docs/ko/msg_docs/Ekf2Timestamps.md
index 844d062050..86c1d98964 100644
--- a/docs/ko/msg_docs/Ekf2Timestamps.md
+++ b/docs/ko/msg_docs/Ekf2Timestamps.md
@@ -23,9 +23,9 @@ this message contains the (relative) timestamps of the sensor inputs used by EKF
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| --------------------------------------------------------------------------------------------------------------- | ------- | ----- | ------------------------------------------------------------- |
-| RELATIVE_TIMESTAMP_INVALID | `int16` | 32767 | (0x7fff) If one of the relative timestamps |
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------------------------------------------------------- | ------- | ----- | ------------------------------------------------------------- |
+| RELATIVE_TIMESTAMP_INVALID | `int16` | 32767 | (0x7fff) If one of the relative timestamps |
## Source Message
diff --git a/docs/ko/msg_docs/EscReport.md b/docs/ko/msg_docs/EscReport.md
index 9ad39f92cd..a19159d2b5 100644
--- a/docs/ko/msg_docs/EscReport.md
+++ b/docs/ko/msg_docs/EscReport.md
@@ -16,6 +16,7 @@ pageClass: is-wide-page
| esc_voltage | `float32` | | | Voltage measured from current ESC [V] - if supported |
| esc_current | `float32` | | | Current measured from current ESC [A] - if supported |
| esc_temperature | `float32` | | | Temperature measured from current ESC [degC] - if supported |
+| motor_temperature | `int16` | | | Temperature measured from current motor [degC] - if supported |
| esc_address | `uint8` | | | Address of current ESC (in most cases 1-8 / must be set by driver) |
| esc_cmdcount | `uint8` | | | Counter of number of commands |
| esc_state | `uint8` | | | State of ESC - depend on Vendor |
@@ -25,31 +26,31 @@ pageClass: is-wide-page
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| -------------------------------------------------------------------------------------------------------------------------------------------- | ------- | ----- | ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ |
-| ACTUATOR_FUNCTION_MOTOR1 | `uint8` | 101 | |
-| ACTUATOR_FUNCTION_MOTOR2 | `uint8` | 102 | |
-| ACTUATOR_FUNCTION_MOTOR3 | `uint8` | 103 | |
-| ACTUATOR_FUNCTION_MOTOR4 | `uint8` | 104 | |
-| ACTUATOR_FUNCTION_MOTOR5 | `uint8` | 105 | |
-| ACTUATOR_FUNCTION_MOTOR6 | `uint8` | 106 | |
-| ACTUATOR_FUNCTION_MOTOR7 | `uint8` | 107 | |
-| ACTUATOR_FUNCTION_MOTOR8 | `uint8` | 108 | |
-| ACTUATOR_FUNCTION_MOTOR9 | `uint8` | 109 | |
-| ACTUATOR_FUNCTION_MOTOR10 | `uint8` | 110 | |
-| ACTUATOR_FUNCTION_MOTOR11 | `uint8` | 111 | |
-| ACTUATOR_FUNCTION_MOTOR12 | `uint8` | 112 | |
-| FAILURE_OVER_CURRENT | `uint8` | 0 | (1 << 0) |
-| FAILURE_OVER_VOLTAGE | `uint8` | 1 | (1 << 1) |
-| FAILURE_MOTOR_OVER_TEMPERATURE | `uint8` | 2 | (1 << 2) |
-| FAILURE_OVER_RPM | `uint8` | 3 | (1 << 3) |
-| FAILURE_INCONSISTENT_CMD | `uint8` | 4 | (1 << 4) Set if ESC received an inconsistent command (i.e out of boundaries) |
-| FAILURE_MOTOR_STUCK | `uint8` | 5 | (1 << 5) |
-| FAILURE_GENERIC | `uint8` | 6 | (1 << 6) |
-| FAILURE_MOTOR_WARN_TEMPERATURE | `uint8` | 7 | (1 << 7) |
-| FAILURE_WARN_ESC_TEMPERATURE | `uint8` | 8 | (1 << 8) |
-| FAILURE_OVER_ESC_TEMPERATURE | `uint8` | 9 | (1 << 9) |
-| ESC_FAILURE_COUNT | `uint8` | 10 | Counter - keep it as last element! |
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------------------------------------------------------------------------------------ | ------- | ----- | ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ |
+| ACTUATOR_FUNCTION_MOTOR1 | `uint8` | 101 | |
+| ACTUATOR_FUNCTION_MOTOR2 | `uint8` | 102 | |
+| ACTUATOR_FUNCTION_MOTOR3 | `uint8` | 103 | |
+| ACTUATOR_FUNCTION_MOTOR4 | `uint8` | 104 | |
+| ACTUATOR_FUNCTION_MOTOR5 | `uint8` | 105 | |
+| ACTUATOR_FUNCTION_MOTOR6 | `uint8` | 106 | |
+| ACTUATOR_FUNCTION_MOTOR7 | `uint8` | 107 | |
+| ACTUATOR_FUNCTION_MOTOR8 | `uint8` | 108 | |
+| ACTUATOR_FUNCTION_MOTOR9 | `uint8` | 109 | |
+| ACTUATOR_FUNCTION_MOTOR10 | `uint8` | 110 | |
+| ACTUATOR_FUNCTION_MOTOR11 | `uint8` | 111 | |
+| ACTUATOR_FUNCTION_MOTOR12 | `uint8` | 112 | |
+| FAILURE_OVER_CURRENT | `uint8` | 0 | (1 << 0) |
+| FAILURE_OVER_VOLTAGE | `uint8` | 1 | (1 << 1) |
+| FAILURE_MOTOR_OVER_TEMPERATURE | `uint8` | 2 | (1 << 2) |
+| FAILURE_OVER_RPM | `uint8` | 3 | (1 << 3) |
+| FAILURE_INCONSISTENT_CMD | `uint8` | 4 | (1 << 4) Set if ESC received an inconsistent command (i.e out of boundaries) |
+| FAILURE_MOTOR_STUCK | `uint8` | 5 | (1 << 5) |
+| FAILURE_GENERIC | `uint8` | 6 | (1 << 6) |
+| FAILURE_MOTOR_WARN_TEMPERATURE | `uint8` | 7 | (1 << 7) |
+| FAILURE_WARN_ESC_TEMPERATURE | `uint8` | 8 | (1 << 8) |
+| FAILURE_OVER_ESC_TEMPERATURE | `uint8` | 9 | (1 << 9) |
+| ESC_FAILURE_COUNT | `uint8` | 10 | Counter - keep it as last element! |
## Source Message
@@ -65,6 +66,7 @@ int32 esc_rpm # Motor RPM, negative for reverse rotation [RPM] - if support
float32 esc_voltage # Voltage measured from current ESC [V] - if supported
float32 esc_current # Current measured from current ESC [A] - if supported
float32 esc_temperature # Temperature measured from current ESC [degC] - if supported
+int16 motor_temperature # Temperature measured from current motor [degC] - if supported
uint8 esc_address # Address of current ESC (in most cases 1-8 / must be set by driver)
uint8 esc_cmdcount # Counter of number of commands
diff --git a/docs/ko/msg_docs/EscStatus.md b/docs/ko/msg_docs/EscStatus.md
index e3678d9ff0..6165263b91 100644
--- a/docs/ko/msg_docs/EscStatus.md
+++ b/docs/ko/msg_docs/EscStatus.md
@@ -20,15 +20,15 @@ pageClass: is-wide-page
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| -------------------------------------------------------------------------------------------------------------------------------------- | ------- | ----- | ---------------------------------------------------------------------------------------------------- |
-| CONNECTED_ESC_MAX | `uint8` | 8 | The number of ESCs supported. Current (Q2/2013) we support 8 ESCs |
-| ESC_CONNECTION_TYPE_PPM | `uint8` | 0 | Traditional PPM ESC |
-| ESC_CONNECTION_TYPE_SERIAL | `uint8` | 1 | Serial Bus connected ESC |
-| ESC_CONNECTION_TYPE_ONESHOT | `uint8` | 2 | One Shot PPM |
-| ESC_CONNECTION_TYPE_I2C | `uint8` | 3 | I2C |
-| ESC_CONNECTION_TYPE_CAN | `uint8` | 4 | CAN-Bus |
-| ESC_CONNECTION_TYPE_DSHOT | `uint8` | 5 | DShot |
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------------------------------------------------------------------------------ | ------- | ----- | ---------------------------------------------------------------------------------------------------- |
+| CONNECTED_ESC_MAX | `uint8` | 8 | The number of ESCs supported. Current (Q2/2013) we support 8 ESCs |
+| ESC_CONNECTION_TYPE_PPM | `uint8` | 0 | Traditional PPM ESC |
+| ESC_CONNECTION_TYPE_SERIAL | `uint8` | 1 | Serial Bus connected ESC |
+| ESC_CONNECTION_TYPE_ONESHOT | `uint8` | 2 | One Shot PPM |
+| ESC_CONNECTION_TYPE_I2C | `uint8` | 3 | I2C |
+| ESC_CONNECTION_TYPE_CAN | `uint8` | 4 | CAN-Bus |
+| ESC_CONNECTION_TYPE_DSHOT | `uint8` | 5 | DShot |
## Source Message
diff --git a/docs/ko/msg_docs/EstimatorEventFlags.md b/docs/ko/msg_docs/EstimatorEventFlags.md
index f4f6350ab1..e7776f8656 100644
--- a/docs/ko/msg_docs/EstimatorEventFlags.md
+++ b/docs/ko/msg_docs/EstimatorEventFlags.md
@@ -4,7 +4,7 @@ pageClass: is-wide-page
# EstimatorEventFlags (UORB message)
-**TOPICS:** estimator_eventflags
+**TOPICS:** estimator_event_flags
## Fields
diff --git a/docs/ko/msg_docs/EstimatorGpsStatus.md b/docs/ko/msg_docs/EstimatorGpsStatus.md
index b7a4b3c9ff..1cb6e33e9b 100644
--- a/docs/ko/msg_docs/EstimatorGpsStatus.md
+++ b/docs/ko/msg_docs/EstimatorGpsStatus.md
@@ -4,7 +4,7 @@ pageClass: is-wide-page
# EstimatorGpsStatus (UORB message)
-**TOPICS:** estimator_gpsstatus
+**TOPICS:** estimator_gps_status
## Fields
diff --git a/docs/ko/msg_docs/EstimatorSelectorStatus.md b/docs/ko/msg_docs/EstimatorSelectorStatus.md
index a908697306..7f5d943721 100644
--- a/docs/ko/msg_docs/EstimatorSelectorStatus.md
+++ b/docs/ko/msg_docs/EstimatorSelectorStatus.md
@@ -4,7 +4,7 @@ pageClass: is-wide-page
# EstimatorSelectorStatus (UORB message)
-**TOPICS:** estimator_selectorstatus
+**TOPICS:** estimator_selector_status
## Fields
diff --git a/docs/ko/msg_docs/EstimatorSensorBias.md b/docs/ko/msg_docs/EstimatorSensorBias.md
index babb6a5532..7f2ca119e1 100644
--- a/docs/ko/msg_docs/EstimatorSensorBias.md
+++ b/docs/ko/msg_docs/EstimatorSensorBias.md
@@ -6,7 +6,7 @@ pageClass: is-wide-page
Sensor readings and in-run biases in SI-unit form. Sensor readings are compensated for static offsets,. scale errors, in-run bias and thermal drift (if thermal compensation is enabled and available).
-**TOPICS:** estimator_sensorbias
+**TOPICS:** estimator_sensor_bias
## Fields
diff --git a/docs/ko/msg_docs/EstimatorStatus.md b/docs/ko/msg_docs/EstimatorStatus.md
index bbc1a2b612..d97f0fec95 100644
--- a/docs/ko/msg_docs/EstimatorStatus.md
+++ b/docs/ko/msg_docs/EstimatorStatus.md
@@ -51,52 +51,52 @@ pageClass: is-wide-page
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- | ------- | ----- | ------------------------------------------------------------------------------------------------- |
-| GPS_CHECK_FAIL_GPS_FIX | `uint8` | 0 | 0 : insufficient fix type (no 3D solution) |
-| GPS_CHECK_FAIL_MIN_SAT_COUNT | `uint8` | 1 | 1 : minimum required sat count fail |
-| GPS_CHECK_FAIL_MAX_PDOP | `uint8` | 2 | 2 : maximum allowed PDOP fail |
-| GPS_CHECK_FAIL_MAX_HORZ_ERR | `uint8` | 3 | 3 : maximum allowed horizontal position error fail |
-| GPS_CHECK_FAIL_MAX_VERT_ERR | `uint8` | 4 | 4 : maximum allowed vertical position error fail |
-| GPS_CHECK_FAIL_MAX_SPD_ERR | `uint8` | 5 | 5 : maximum allowed speed error fail |
-| GPS_CHECK_FAIL_MAX_HORZ_DRIFT | `uint8` | 6 | 6 : maximum allowed horizontal position drift fail - requires stationary vehicle |
-| GPS_CHECK_FAIL_MAX_VERT_DRIFT | `uint8` | 7 | 7 : maximum allowed vertical position drift fail - requires stationary vehicle |
-| GPS_CHECK_FAIL_MAX_HORZ_SPD_ERR | `uint8` | 8 | 8 : maximum allowed horizontal speed fail - requires stationary vehicle |
-| GPS_CHECK_FAIL_MAX_VERT_SPD_ERR | `uint8` | 9 | 9 : maximum allowed vertical velocity discrepancy fail |
-| GPS_CHECK_FAIL_SPOOFED | `uint8` | 10 | 10 : GPS signal is spoofed |
-| GPS_CHECK_FAIL_JAMMED | `uint8` | 11 | 11 : GPS signal is jammed |
-| CS_TILT_ALIGN | `uint8` | 0 | 0 - true if the filter tilt alignment is complete |
-| CS_YAW_ALIGN | `uint8` | 1 | 1 - true if the filter yaw alignment is complete |
-| CS_GNSS_POS | `uint8` | 2 | 2 - true if GNSS position measurements are being fused |
-| CS_OPT_FLOW | `uint8` | 3 | 3 - true if optical flow measurements are being fused |
-| CS_MAG_HDG | `uint8` | 4 | 4 - true if a simple magnetic yaw heading is being fused |
-| CS_MAG_3D | `uint8` | 5 | 5 - true if 3-axis magnetometer measurement are being fused |
-| CS_MAG_DEC | `uint8` | 6 | 6 - true if synthetic magnetic declination measurements are being fused |
-| CS_IN_AIR | `uint8` | 7 | 7 - true when thought to be airborne |
-| CS_WIND | `uint8` | 8 | 8 - true when wind velocity is being estimated |
-| CS_BARO_HGT | `uint8` | 9 | 9 - true when baro data is being fused |
-| CS_RNG_HGT | `uint8` | 10 | 10 - true when range finder data is being fused for height aiding |
-| CS_GPS_HGT | `uint8` | 11 | 11 - true when GPS altitude is being fused |
-| CS_EV_POS | `uint8` | 12 | 12 - true when local position data from external vision is being fused |
-| CS_EV_YAW | `uint8` | 13 | 13 - true when yaw data from external vision measurements is being fused |
-| CS_EV_HGT | `uint8` | 14 | 14 - true when height data from external vision measurements is being fused |
-| CS_BETA | `uint8` | 15 | 15 - true when synthetic sideslip measurements are being fused |
-| CS_MAG_FIELD | `uint8` | 16 | 16 - true when only the magnetic field states are updated by the magnetometer |
-| CS_FIXED_WING | `uint8` | 17 | 17 - true when thought to be operating as a fixed wing vehicle with constrained sideslip |
-| CS_MAG_FAULT | `uint8` | 18 | 18 - true when the magnetometer has been declared faulty and is no longer being used |
-| CS_ASPD | `uint8` | 19 | 19 - true when airspeed measurements are being fused |
-| CS_GND_EFFECT | `uint8` | 20 | 20 - true when when protection from ground effect induced static pressure rise is active |
-| CS_RNG_STUCK | `uint8` | 21 | 21 - true when a stuck range finder sensor has been detected |
-| CS_GPS_YAW | `uint8` | 22 | 22 - true when yaw (not ground course) data from a GPS receiver is being fused |
-| CS_MAG_ALIGNED | `uint8` | 23 | 23 - true when the in-flight mag field alignment has been completed |
-| CS_EV_VEL | `uint8` | 24 | 24 - true when local frame velocity data fusion from external vision measurements is intended |
-| CS_SYNTHETIC_MAG_Z | `uint8` | 25 | 25 - true when we are using a synthesized measurement for the magnetometer Z component |
-| CS_VEHICLE_AT_REST | `uint8` | 26 | 26 - true when the vehicle is at rest |
-| CS_GPS_YAW_FAULT | `uint8` | 27 | 27 - true when the GNSS heading has been declared faulty and is no longer being used |
-| CS_RNG_FAULT | `uint8` | 28 | 28 - true when the range finder has been declared faulty and is no longer being used |
-| CS_GNSS_VEL | `uint8` | 44 | 44 - true if GNSS velocity measurement fusion is intended |
-| CS_GNSS_FAULT | `uint8` | 45 | 45 - true if GNSS measurements have been declared faulty and are no longer used |
-| CS_YAW_MANUAL | `uint8` | 46 | 46 - true if yaw has been set manually |
+| 명칭 | 형식 | Value | 설명 |
+| ----------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- | ------- | ----- | ------------------------------------------------------------------------------------------------- |
+| GPS_CHECK_FAIL_GPS_FIX | `uint8` | 0 | 0 : insufficient fix type (no 3D solution) |
+| GPS_CHECK_FAIL_MIN_SAT_COUNT | `uint8` | 1 | 1 : minimum required sat count fail |
+| GPS_CHECK_FAIL_MAX_PDOP | `uint8` | 2 | 2 : maximum allowed PDOP fail |
+| GPS_CHECK_FAIL_MAX_HORZ_ERR | `uint8` | 3 | 3 : maximum allowed horizontal position error fail |
+| GPS_CHECK_FAIL_MAX_VERT_ERR | `uint8` | 4 | 4 : maximum allowed vertical position error fail |
+| GPS_CHECK_FAIL_MAX_SPD_ERR | `uint8` | 5 | 5 : maximum allowed speed error fail |
+| GPS_CHECK_FAIL_MAX_HORZ_DRIFT | `uint8` | 6 | 6 : maximum allowed horizontal position drift fail - requires stationary vehicle |
+| GPS_CHECK_FAIL_MAX_VERT_DRIFT | `uint8` | 7 | 7 : maximum allowed vertical position drift fail - requires stationary vehicle |
+| GPS_CHECK_FAIL_MAX_HORZ_SPD_ERR | `uint8` | 8 | 8 : maximum allowed horizontal speed fail - requires stationary vehicle |
+| GPS_CHECK_FAIL_MAX_VERT_SPD_ERR | `uint8` | 9 | 9 : maximum allowed vertical velocity discrepancy fail |
+| GPS_CHECK_FAIL_SPOOFED | `uint8` | 10 | 10 : GPS signal is spoofed |
+| GPS_CHECK_FAIL_JAMMED | `uint8` | 11 | 11 : GPS signal is jammed |
+| CS_TILT_ALIGN | `uint8` | 0 | 0 - true if the filter tilt alignment is complete |
+| CS_YAW_ALIGN | `uint8` | 1 | 1 - true if the filter yaw alignment is complete |
+| CS_GNSS_POS | `uint8` | 2 | 2 - true if GNSS position measurements are being fused |
+| CS_OPT_FLOW | `uint8` | 3 | 3 - true if optical flow measurements are being fused |
+| CS_MAG_HDG | `uint8` | 4 | 4 - true if a simple magnetic yaw heading is being fused |
+| CS_MAG_3D | `uint8` | 5 | 5 - true if 3-axis magnetometer measurement are being fused |
+| CS_MAG_DEC | `uint8` | 6 | 6 - true if synthetic magnetic declination measurements are being fused |
+| CS_IN_AIR | `uint8` | 7 | 7 - true when thought to be airborne |
+| CS_WIND | `uint8` | 8 | 8 - true when wind velocity is being estimated |
+| CS_BARO_HGT | `uint8` | 9 | 9 - true when baro data is being fused |
+| CS_RNG_HGT | `uint8` | 10 | 10 - true when range finder data is being fused for height aiding |
+| CS_GPS_HGT | `uint8` | 11 | 11 - true when GPS altitude is being fused |
+| CS_EV_POS | `uint8` | 12 | 12 - true when local position data from external vision is being fused |
+| CS_EV_YAW | `uint8` | 13 | 13 - true when yaw data from external vision measurements is being fused |
+| CS_EV_HGT | `uint8` | 14 | 14 - true when height data from external vision measurements is being fused |
+| CS_BETA | `uint8` | 15 | 15 - true when synthetic sideslip measurements are being fused |
+| CS_MAG_FIELD | `uint8` | 16 | 16 - true when only the magnetic field states are updated by the magnetometer |
+| CS_FIXED_WING | `uint8` | 17 | 17 - true when thought to be operating as a fixed wing vehicle with constrained sideslip |
+| CS_MAG_FAULT | `uint8` | 18 | 18 - true when the magnetometer has been declared faulty and is no longer being used |
+| CS_ASPD | `uint8` | 19 | 19 - true when airspeed measurements are being fused |
+| CS_GND_EFFECT | `uint8` | 20 | 20 - true when when protection from ground effect induced static pressure rise is active |
+| CS_RNG_STUCK | `uint8` | 21 | 21 - true when a stuck range finder sensor has been detected |
+| CS_GPS_YAW | `uint8` | 22 | 22 - true when yaw (not ground course) data from a GPS receiver is being fused |
+| CS_MAG_ALIGNED | `uint8` | 23 | 23 - true when the in-flight mag field alignment has been completed |
+| CS_EV_VEL | `uint8` | 24 | 24 - true when local frame velocity data fusion from external vision measurements is intended |
+| CS_SYNTHETIC_MAG_Z | `uint8` | 25 | 25 - true when we are using a synthesized measurement for the magnetometer Z component |
+| CS_VEHICLE_AT_REST | `uint8` | 26 | 26 - true when the vehicle is at rest |
+| CS_GPS_YAW_FAULT | `uint8` | 27 | 27 - true when the GNSS heading has been declared faulty and is no longer being used |
+| CS_RNG_FAULT | `uint8` | 28 | 28 - true when the range finder has been declared faulty and is no longer being used |
+| CS_GNSS_VEL | `uint8` | 44 | 44 - true if GNSS velocity measurement fusion is intended |
+| CS_GNSS_FAULT | `uint8` | 45 | 45 - true if GNSS measurements have been declared faulty and are no longer used |
+| CS_YAW_MANUAL | `uint8` | 46 | 46 - true if yaw has been set manually |
## Source Message
diff --git a/docs/ko/msg_docs/EstimatorStatusFlags.md b/docs/ko/msg_docs/EstimatorStatusFlags.md
index 0b907904f0..47e4d64a49 100644
--- a/docs/ko/msg_docs/EstimatorStatusFlags.md
+++ b/docs/ko/msg_docs/EstimatorStatusFlags.md
@@ -4,7 +4,7 @@ pageClass: is-wide-page
# EstimatorStatusFlags (UORB message)
-**TOPICS:** estimator_statusflags
+**TOPICS:** estimator_status_flags
## Fields
diff --git a/docs/ko/msg_docs/Event.md b/docs/ko/msg_docs/Event.md
index 6fa988c3fd..b196dd7a08 100644
--- a/docs/ko/msg_docs/Event.md
+++ b/docs/ko/msg_docs/Event.md
@@ -20,10 +20,10 @@ Events interface.
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ------------------------------------------------------------------------------------------- | -------- | ----- | -- |
-| MESSAGE_VERSION | `uint32` | 1 | |
-| ORB_QUEUE_LENGTH | `uint8` | 16 | |
+| 명칭 | 형식 | Value | 설명 |
+| ----------------------------------------------------------------------------------------- | -------- | ----- | -- |
+| MESSAGE_VERSION | `uint32` | 1 | |
+| ORB_QUEUE_LENGTH | `uint8` | 16 | |
## Source Message
diff --git a/docs/ko/msg_docs/EventV0.md b/docs/ko/msg_docs/EventV0.md
index 4bc23e839a..5a85824724 100644
--- a/docs/ko/msg_docs/EventV0.md
+++ b/docs/ko/msg_docs/EventV0.md
@@ -6,7 +6,7 @@ pageClass: is-wide-page
this message is required here in the msg_old folder because other msg are depending on it. Events interface.
-**TOPICS:** eventv0
+**TOPICS:** event_v0
## Fields
@@ -20,10 +20,10 @@ this message is required here in the msg_old folder because other msg are depend
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ------------------------------------------------------------------------------------------- | -------- | ----- | -- |
-| MESSAGE_VERSION | `uint32` | 0 | |
-| ORB_QUEUE_LENGTH | `uint8` | 16 | |
+| 명칭 | 형식 | Value | 설명 |
+| ----------------------------------------------------------------------------------------- | -------- | ----- | -- |
+| MESSAGE_VERSION | `uint32` | 0 | |
+| ORB_QUEUE_LENGTH | `uint8` | 16 | |
## Source Message
diff --git a/docs/ko/msg_docs/FailsafeFlags.md b/docs/ko/msg_docs/FailsafeFlags.md
index 04514b37ba..bce2f09387 100644
--- a/docs/ko/msg_docs/FailsafeFlags.md
+++ b/docs/ko/msg_docs/FailsafeFlags.md
@@ -46,6 +46,10 @@ The flag comments are used as label for the failsafe state machine simulation
| battery_warning | `uint8` | | | Battery warning level (see BatteryStatus.msg) |
| battery_low_remaining_time | `bool` | | | Low battery based on remaining flight time |
| battery_unhealthy | `bool` | | | Battery unhealthy |
+| fd_critical_failure | `bool` | | | Critical failure (attitude/altitude limit exceeded, or external ATS) |
+| fd_esc_arming_failure | `bool` | | | ESC failed to arm |
+| fd_imbalanced_prop | `bool` | | | Imbalanced propeller detected |
+| fd_motor_failure | `bool` | | | Motor failure |
| geofence_breached | `bool` | | | Geofence breached (one or multiple) |
| mission_failure | `bool` | | | Mission failure |
| vtol_fixed_wing_system_failure | `bool` | | | vehicle in fixed-wing system failure failsafe mode (after quad-chute) |
@@ -53,10 +57,7 @@ The flag comments are used as label for the failsafe state machine simulation
| flight_time_limit_exceeded | `bool` | | | Maximum flight time exceeded |
| position_accuracy_low | `bool` | | | Position estimate has dropped below threshold, but is currently still declared valid |
| navigator_failure | `bool` | | | Navigator failed to execute a mode |
-| fd_critical_failure | `bool` | | | Critical failure (attitude/altitude limit exceeded, or external ATS) |
-| fd_esc_arming_failure | `bool` | | | ESC failed to arm |
-| fd_imbalanced_prop | `bool` | | | Imbalanced propeller detected |
-| fd_motor_failure | `bool` | | | Motor failure |
+| parachute_unhealthy | `bool` | | | Parachute system missing or unhealthy |
## Source Message
@@ -112,6 +113,12 @@ uint8 battery_warning # Battery warning level (see BatteryStatus
bool battery_low_remaining_time # Low battery based on remaining flight time
bool battery_unhealthy # Battery unhealthy
+# Failure detector
+bool fd_critical_failure # Critical failure (attitude/altitude limit exceeded, or external ATS)
+bool fd_esc_arming_failure # ESC failed to arm
+bool fd_imbalanced_prop # Imbalanced propeller detected
+bool fd_motor_failure # Motor failure
+
# Other
bool geofence_breached # Geofence breached (one or multiple)
bool mission_failure # Mission failure
@@ -120,12 +127,7 @@ bool wind_limit_exceeded # Wind limit exceeded
bool flight_time_limit_exceeded # Maximum flight time exceeded
bool position_accuracy_low # Position estimate has dropped below threshold, but is currently still declared valid
bool navigator_failure # Navigator failed to execute a mode
-
-# Failure detector
-bool fd_critical_failure # Critical failure (attitude/altitude limit exceeded, or external ATS)
-bool fd_esc_arming_failure # ESC failed to arm
-bool fd_imbalanced_prop # Imbalanced propeller detected
-bool fd_motor_failure # Motor failure
+bool parachute_unhealthy # Parachute system missing or unhealthy
```
:::
diff --git a/docs/ko/msg_docs/FailureDetectorStatus.md b/docs/ko/msg_docs/FailureDetectorStatus.md
index 9b4de32cae..35100c0056 100644
--- a/docs/ko/msg_docs/FailureDetectorStatus.md
+++ b/docs/ko/msg_docs/FailureDetectorStatus.md
@@ -4,7 +4,7 @@ pageClass: is-wide-page
# FailureDetectorStatus (UORB message)
-**TOPICS:** failure_detectorstatus
+**TOPICS:** failure_detector_status
## Fields
diff --git a/docs/ko/msg_docs/FigureEightStatus.md b/docs/ko/msg_docs/FigureEightStatus.md
index 375d856181..5687ddfba6 100644
--- a/docs/ko/msg_docs/FigureEightStatus.md
+++ b/docs/ko/msg_docs/FigureEightStatus.md
@@ -4,7 +4,7 @@ pageClass: is-wide-page
# FigureEightStatus (UORB message)
-**TOPICS:** figure_eightstatus
+**TOPICS:** figure_eight_status
## Fields
diff --git a/docs/ko/msg_docs/FixedWingLateralGuidanceStatus.md b/docs/ko/msg_docs/FixedWingLateralGuidanceStatus.md
index c8f636e377..9419c5989e 100644
--- a/docs/ko/msg_docs/FixedWingLateralGuidanceStatus.md
+++ b/docs/ko/msg_docs/FixedWingLateralGuidanceStatus.md
@@ -6,7 +6,7 @@ pageClass: is-wide-page
Fixed Wing Lateral Guidance Status message. Published by fw_pos_control module to report the resultant lateral setpoints and NPFG debug outputs.
-**TOPICS:** fixed_winglateral_guidancestatus
+**TOPICS:** fixed_wing_lateral_guidance_status
## Fields
diff --git a/docs/ko/msg_docs/FixedWingLateralSetpoint.md b/docs/ko/msg_docs/FixedWingLateralSetpoint.md
index c0ecdb3a9e..2b04265811 100644
--- a/docs/ko/msg_docs/FixedWingLateralSetpoint.md
+++ b/docs/ko/msg_docs/FixedWingLateralSetpoint.md
@@ -4,24 +4,27 @@ pageClass: is-wide-page
# FixedWingLateralSetpoint (UORB message)
-Fixed Wing Lateral Setpoint message. Used by the fw_lateral_longitudinal_control module. At least one of course, airspeed_direction, or lateral_acceleration must be finite.
+Fixed Wing Lateral Setpoint message.
-**TOPICS:** fixed_winglateral_setpoint
+Used by the fw_lateral_longitudinal_control module
+At least one of course, airspeed_direction, or lateral_acceleration must be finite.
+
+**TOPICS:** fixed_wing_lateral_setpoint
## Fields
| 명칭 | 형식 | Unit [Frame] | Range/Enum | 설명 |
| ----------------------------------------- | --------- | ---------------------------------------------------------------- | ------------------------------------------------------------------------------ | ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ |
-| timestamp | `uint64` | | | time since system start (microseconds) |
+| timestamp | `uint64` | us | | Time since system start |
| course | `float32` | rad | [-pi : pi] | Desired direction of travel over ground w.r.t (true) North. NAN if not controlled directly. |
| airspeed_direction | `float32` | rad | [-pi : pi] | Desired horizontal angle of airspeed vector w.r.t. (true) North. Same as vehicle heading if in the absence of sideslip. NAN if not controlled directly, takes precedence over course if finite. |
-| lateral_acceleration | `float32` | FRD | | Lateral acceleration setpoint. NAN if not controlled directly, used as feedforward if either course setpoint or airspeed_direction is finite. |
+| lateral_acceleration | `float32` | m/s^2 [FRD] | | Lateral acceleration setpoint. NAN if not controlled directly, used as feedforward if either course setpoint or airspeed_direction is finite. |
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| -------------------------------------------------------------------- | -------- | ----- | -- |
-| MESSAGE_VERSION | `uint32` | 0 | |
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------------ | -------- | ----- | -- |
+| MESSAGE_VERSION | `uint32` | 0 | |
## Source Message
@@ -32,16 +35,17 @@ Click here to see original file
```c
# Fixed Wing Lateral Setpoint message
+#
# Used by the fw_lateral_longitudinal_control module
# At least one of course, airspeed_direction, or lateral_acceleration must be finite.
uint32 MESSAGE_VERSION = 0
-uint64 timestamp # time since system start (microseconds)
+uint64 timestamp # [us] Time since system start
-float32 course # [rad] [@range -pi, pi] Desired direction of travel over ground w.r.t (true) North. NAN if not controlled directly.
-float32 airspeed_direction # [rad] [@range -pi, pi] Desired horizontal angle of airspeed vector w.r.t. (true) North. Same as vehicle heading if in the absence of sideslip. NAN if not controlled directly, takes precedence over course if finite.
-float32 lateral_acceleration # [m/s^2] [FRD] Lateral acceleration setpoint. NAN if not controlled directly, used as feedforward if either course setpoint or airspeed_direction is finite.
+float32 course # [rad] [@range -pi, pi] Desired direction of travel over ground w.r.t (true) North. NAN if not controlled directly.
+float32 airspeed_direction # [rad] [@range -pi, pi] Desired horizontal angle of airspeed vector w.r.t. (true) North. Same as vehicle heading if in the absence of sideslip. NAN if not controlled directly, takes precedence over course if finite.
+float32 lateral_acceleration # [m/s^2] [@frame FRD] Lateral acceleration setpoint. NAN if not controlled directly, used as feedforward if either course setpoint or airspeed_direction is finite.
```
:::
diff --git a/docs/ko/msg_docs/FixedWingLateralStatus.md b/docs/ko/msg_docs/FixedWingLateralStatus.md
index 442146c4d8..34ec390be1 100644
--- a/docs/ko/msg_docs/FixedWingLateralStatus.md
+++ b/docs/ko/msg_docs/FixedWingLateralStatus.md
@@ -6,7 +6,7 @@ pageClass: is-wide-page
Fixed Wing Lateral Status message. Published by the fw_lateral_longitudinal_control module to report the resultant lateral setpoint.
-**TOPICS:** fixed_winglateral_status
+**TOPICS:** fixed_wing_lateral_status
## Fields
diff --git a/docs/ko/msg_docs/FixedWingLongitudinalSetpoint.md b/docs/ko/msg_docs/FixedWingLongitudinalSetpoint.md
index 2ba24c7f5f..04e46510b3 100644
--- a/docs/ko/msg_docs/FixedWingLongitudinalSetpoint.md
+++ b/docs/ko/msg_docs/FixedWingLongitudinalSetpoint.md
@@ -4,26 +4,30 @@ pageClass: is-wide-page
# FixedWingLongitudinalSetpoint (UORB message)
-Fixed Wing Longitudinal Setpoint message. Used by the fw_lateral_longitudinal_control module. If pitch_direct and throttle_direct are not both finite, then the controller relies on altitude/height_rate and equivalent_airspeed to control vertical motion. If both altitude and height_rate are NAN, the controller maintains the current altitude.
+Fixed Wing Longitudinal Setpoint message.
-**TOPICS:** fixed_winglongitudinal_setpoint
+Used by the fw_lateral_longitudinal_control module
+If pitch_direct and throttle_direct are not both finite, then the controller relies on altitude/height_rate and equivalent_airspeed to control vertical motion.
+If both altitude and height_rate are NAN, the controller maintains the current altitude.
+
+**TOPICS:** fixed_wing_longitudinal_setpoint
## Fields
| 명칭 | 형식 | Unit [Frame] | Range/Enum | 설명 |
| ---------------------------------------- | --------- | ---------------------------------------------------------------- | ------------------------------------------------------------------------------ | ------------------------------------------------------------------------------------------------------- |
-| timestamp | `uint64` | | | time since system start (microseconds) |
+| timestamp | `uint64` | us | | Time since system start |
| altitude | `float32` | m | | Altitude setpoint AMSL, not controlled directly if NAN or if height_rate is finite |
-| height_rate | `float32` | ENU | | Scalar height rate setpoint. NAN if not controlled directly |
+| height_rate | `float32` | m/s [ENU] | | Scalar height rate setpoint. NAN if not controlled directly |
| equivalent_airspeed | `float32` | m/s | [0 : inf] | Scalar equivalent airspeed setpoint. NAN if system default should be used |
-| pitch_direct | `float32` | FRD | [-pi : pi] | NAN if not controlled, overrides total energy controller |
+| pitch_direct | `float32` | rad [FRD] | [-pi : pi] | NAN if not controlled, overrides total energy controller |
| throttle_direct | `float32` | norm | [0 : 1] | NAN if not controlled, overrides total energy controller |
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| -------------------------------------------------------------------- | -------- | ----- | -- |
-| MESSAGE_VERSION | `uint32` | 0 | |
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------------ | -------- | ----- | -- |
+| MESSAGE_VERSION | `uint32` | 0 | |
## Source Message
@@ -34,19 +38,20 @@ Click here to see original file
```c
# Fixed Wing Longitudinal Setpoint message
+#
# Used by the fw_lateral_longitudinal_control module
# If pitch_direct and throttle_direct are not both finite, then the controller relies on altitude/height_rate and equivalent_airspeed to control vertical motion.
# If both altitude and height_rate are NAN, the controller maintains the current altitude.
uint32 MESSAGE_VERSION = 0
-uint64 timestamp # time since system start (microseconds)
+uint64 timestamp # [us] Time since system start
-float32 altitude # [m] Altitude setpoint AMSL, not controlled directly if NAN or if height_rate is finite
-float32 height_rate # [m/s] [ENU] Scalar height rate setpoint. NAN if not controlled directly
-float32 equivalent_airspeed # [m/s] [@range 0, inf] Scalar equivalent airspeed setpoint. NAN if system default should be used
-float32 pitch_direct # [rad] [@range -pi, pi] [FRD] NAN if not controlled, overrides total energy controller
-float32 throttle_direct # [norm] [@range 0,1] NAN if not controlled, overrides total energy controller
+float32 altitude # [m] Altitude setpoint AMSL, not controlled directly if NAN or if height_rate is finite
+float32 height_rate # [m/s] [@frame ENU] Scalar height rate setpoint. NAN if not controlled directly
+float32 equivalent_airspeed # [m/s] [@range 0, inf] Scalar equivalent airspeed setpoint. NAN if system default should be used
+float32 pitch_direct # [rad] [@range -pi, pi] [@frame FRD] NAN if not controlled, overrides total energy controller
+float32 throttle_direct # [norm] [@range 0,1] NAN if not controlled, overrides total energy controller
```
:::
diff --git a/docs/ko/msg_docs/FixedWingRunwayControl.md b/docs/ko/msg_docs/FixedWingRunwayControl.md
index b05ac86b18..7208f6374d 100644
--- a/docs/ko/msg_docs/FixedWingRunwayControl.md
+++ b/docs/ko/msg_docs/FixedWingRunwayControl.md
@@ -6,7 +6,7 @@ pageClass: is-wide-page
Auxiliary control fields for fixed-wing runway takeoff/landing.
-**TOPICS:** fixed_wingrunway_control
+**TOPICS:** fixed_wing_runway_control
## Fields
@@ -19,12 +19,12 @@ Auxiliary control fields for fixed-wing runway takeoff/landing.
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ------------------------------------------------------------------------------------------------------------------------------ | ------- | ----- | -------------------------------------------------------------------------------- |
-| STATE_THROTTLE_RAMP | `uint8` | 0 | ramping up throttle |
-| STATE_CLAMPED_TO_RUNWAY | `uint8` | 1 | clamped to runway, controlling yaw directly (wheel or rudder) |
-| STATE_CLIMBOUT | `uint8` | 2 | climbout to safe height before navigation |
-| STATE_FLYING | `uint8` | 3 | navigate freely |
+| 명칭 | 형식 | Value | 설명 |
+| ---------------------------------------------------------------------------------------------------------------------------- | ------- | ----- | -------------------------------------------------------------------------------- |
+| STATE_THROTTLE_RAMP | `uint8` | 0 | ramping up throttle |
+| STATE_CLAMPED_TO_RUNWAY | `uint8` | 1 | clamped to runway, controlling yaw directly (wheel or rudder) |
+| STATE_CLIMBOUT | `uint8` | 2 | climbout to safe height before navigation |
+| STATE_FLYING | `uint8` | 3 | navigate freely |
## Source Message
diff --git a/docs/ko/msg_docs/FlightPhaseEstimation.md b/docs/ko/msg_docs/FlightPhaseEstimation.md
index b859adfc27..2d88790c67 100644
--- a/docs/ko/msg_docs/FlightPhaseEstimation.md
+++ b/docs/ko/msg_docs/FlightPhaseEstimation.md
@@ -4,7 +4,7 @@ pageClass: is-wide-page
# FlightPhaseEstimation (UORB message)
-**TOPICS:** flight_phaseestimation
+**TOPICS:** flight_phase_estimation
## Fields
@@ -15,12 +15,12 @@ pageClass: is-wide-page
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| --------------------------------------------------------------------------------------------------- | ------- | ----- | ------------------------------- |
-| FLIGHT_PHASE_UNKNOWN | `uint8` | 0 | vehicle flight phase is unknown |
-| FLIGHT_PHASE_LEVEL | `uint8` | 1 | Vehicle is in level flight |
-| FLIGHT_PHASE_DESCEND | `uint8` | 2 | vehicle is in descend |
-| FLIGHT_PHASE_CLIMB | `uint8` | 3 | vehicle is climbing |
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------------------------------------------- | ------- | ----- | ------------------------------- |
+| FLIGHT_PHASE_UNKNOWN | `uint8` | 0 | vehicle flight phase is unknown |
+| FLIGHT_PHASE_LEVEL | `uint8` | 1 | Vehicle is in level flight |
+| FLIGHT_PHASE_DESCEND | `uint8` | 2 | vehicle is in descend |
+| FLIGHT_PHASE_CLIMB | `uint8` | 3 | vehicle is climbing |
## Source Message
diff --git a/docs/ko/msg_docs/FollowTargetEstimator.md b/docs/ko/msg_docs/FollowTargetEstimator.md
index 799cab3655..fe7c845bcf 100644
--- a/docs/ko/msg_docs/FollowTargetEstimator.md
+++ b/docs/ko/msg_docs/FollowTargetEstimator.md
@@ -4,7 +4,7 @@ pageClass: is-wide-page
# FollowTargetEstimator (UORB message)
-**TOPICS:** follow_targetestimator
+**TOPICS:** follow_target_estimator
## Fields
diff --git a/docs/ko/msg_docs/FollowTargetStatus.md b/docs/ko/msg_docs/FollowTargetStatus.md
index 7fe978c12a..a0fd16599e 100644
--- a/docs/ko/msg_docs/FollowTargetStatus.md
+++ b/docs/ko/msg_docs/FollowTargetStatus.md
@@ -4,7 +4,7 @@ pageClass: is-wide-page
# FollowTargetStatus (UORB message)
-**TOPICS:** follow_targetstatus
+**TOPICS:** follow_target_status
## Fields
diff --git a/docs/ko/msg_docs/FuelTankStatus.md b/docs/ko/msg_docs/FuelTankStatus.md
index 82da178157..b7c26d2339 100644
--- a/docs/ko/msg_docs/FuelTankStatus.md
+++ b/docs/ko/msg_docs/FuelTankStatus.md
@@ -4,7 +4,7 @@ pageClass: is-wide-page
# FuelTankStatus (UORB message)
-**TOPICS:** fuel_tankstatus
+**TOPICS:** fuel_tank_status
## Fields
@@ -22,11 +22,11 @@ pageClass: is-wide-page
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| -------------------------------------------------------------------------------------------------------------------------- | ------- | ----- | --------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- |
-| MAV_FUEL_TYPE_UNKNOWN | `uint8` | 0 | fuel type not specified. Fuel levels are normalized (i.e., maximum is 1, and other levels are relative to 1). |
-| MAV_FUEL_TYPE_LIQUID | `uint8` | 1 | represents generic liquid fuels, such as gasoline or diesel. Fuel levels are measured in millilitres (ml), and flow rates in millilitres per second (ml/s). |
-| MAV_FUEL_TYPE_GAS | `uint8` | 2 | represents a gas fuel, such as hydrogen, methane, or propane. Fuel levels are in kilo-Pascal (kPa), and flow rates are in milliliters per second (ml/s). |
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------------------------------------------------------------------ | ------- | ----- | --------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- |
+| MAV_FUEL_TYPE_UNKNOWN | `uint8` | 0 | fuel type not specified. Fuel levels are normalized (i.e., maximum is 1, and other levels are relative to 1). |
+| MAV_FUEL_TYPE_LIQUID | `uint8` | 1 | represents generic liquid fuels, such as gasoline or diesel. Fuel levels are measured in millilitres (ml), and flow rates in millilitres per second (ml/s). |
+| MAV_FUEL_TYPE_GAS | `uint8` | 2 | represents a gas fuel, such as hydrogen, methane, or propane. Fuel levels are in kilo-Pascal (kPa), and flow rates are in milliliters per second (ml/s). |
## Source Message
diff --git a/docs/ko/msg_docs/GeneratorStatus.md b/docs/ko/msg_docs/GeneratorStatus.md
index 838563a7c9..d190cc30c4 100644
--- a/docs/ko/msg_docs/GeneratorStatus.md
+++ b/docs/ko/msg_docs/GeneratorStatus.md
@@ -25,31 +25,31 @@ pageClass: is-wide-page
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ | -------- | ------- | -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- |
-| STATUS_FLAG_OFF | `uint64` | 1 | Generator is off. |
-| STATUS_FLAG_READY | `uint64` | 2 | Generator is ready to start generating power. |
-| STATUS_FLAG_GENERATING | `uint64` | 4 | Generator is generating power. |
-| STATUS_FLAG_CHARGING | `uint64` | 8 | Generator is charging the batteries (generating enough power to charge and provide the load). |
-| STATUS_FLAG_REDUCED_POWER | `uint64` | 16 | Generator is operating at a reduced maximum power. |
-| STATUS_FLAG_MAXPOWER | `uint64` | 32 | Generator is providing the maximum output. |
-| STATUS_FLAG_OVERTEMP_WARNING | `uint64` | 64 | Generator is near the maximum operating temperature, cooling is insufficient. |
-| STATUS_FLAG_OVERTEMP_FAULT | `uint64` | 128 | Generator hit the maximum operating temperature and shutdown. |
-| STATUS_FLAG_ELECTRONICS_OVERTEMP_WARNING | `uint64` | 256 | Power electronics are near the maximum operating temperature, cooling is insufficient. |
-| STATUS_FLAG_ELECTRONICS_OVERTEMP_FAULT | `uint64` | 512 | Power electronics hit the maximum operating temperature and shutdown. |
-| STATUS_FLAG_ELECTRONICS_FAULT | `uint64` | 1024 | Power electronics experienced a fault and shutdown. |
-| STATUS_FLAG_POWERSOURCE_FAULT | `uint64` | 2048 | The power source supplying the generator failed e.g. mechanical generator stopped, tether is no longer providing power, solar cell is in shade, hydrogen reaction no longer happening. |
-| STATUS_FLAG_COMMUNICATION_WARNING | `uint64` | 4096 | Generator controller having communication problems. |
-| STATUS_FLAG_COOLING_WARNING | `uint64` | 8192 | Power electronic or generator cooling system error. |
-| STATUS_FLAG_POWER_RAIL_FAULT | `uint64` | 16384 | Generator controller power rail experienced a fault. |
-| STATUS_FLAG_OVERCURRENT_FAULT | `uint64` | 32768 | Generator controller exceeded the overcurrent threshold and shutdown to prevent damage. |
-| STATUS_FLAG_BATTERY_OVERCHARGE_CURRENT_FAULT | `uint64` | 65536 | Generator controller detected a high current going into the batteries and shutdown to prevent battery damage. |
-| STATUS_FLAG_OVERVOLTAGE_FAULT | `uint64` | 131072 | Generator controller exceeded it's overvoltage threshold and shutdown to prevent it exceeding the voltage rating. |
-| STATUS_FLAG_BATTERY_UNDERVOLT_FAULT | `uint64` | 262144 | Batteries are under voltage (generator will not start). |
-| STATUS_FLAG_START_INHIBITED | `uint64` | 524288 | Generator start is inhibited by e.g. a safety switch. |
-| STATUS_FLAG_MAINTENANCE_REQUIRED | `uint64` | 1048576 | Generator requires maintenance. |
-| STATUS_FLAG_WARMING_UP | `uint64` | 2097152 | Generator is not ready to generate yet. |
-| STATUS_FLAG_IDLE | `uint64` | 4194304 | Generator is idle. |
+| 명칭 | 형식 | Value | 설명 |
+| ---------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- | -------- | ------- | -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- |
+| STATUS_FLAG_OFF | `uint64` | 1 | Generator is off. |
+| STATUS_FLAG_READY | `uint64` | 2 | Generator is ready to start generating power. |
+| STATUS_FLAG_GENERATING | `uint64` | 4 | Generator is generating power. |
+| STATUS_FLAG_CHARGING | `uint64` | 8 | Generator is charging the batteries (generating enough power to charge and provide the load). |
+| STATUS_FLAG_REDUCED_POWER | `uint64` | 16 | Generator is operating at a reduced maximum power. |
+| STATUS_FLAG_MAXPOWER | `uint64` | 32 | Generator is providing the maximum output. |
+| STATUS_FLAG_OVERTEMP_WARNING | `uint64` | 64 | Generator is near the maximum operating temperature, cooling is insufficient. |
+| STATUS_FLAG_OVERTEMP_FAULT | `uint64` | 128 | Generator hit the maximum operating temperature and shutdown. |
+| STATUS_FLAG_ELECTRONICS_OVERTEMP_WARNING | `uint64` | 256 | Power electronics are near the maximum operating temperature, cooling is insufficient. |
+| STATUS_FLAG_ELECTRONICS_OVERTEMP_FAULT | `uint64` | 512 | Power electronics hit the maximum operating temperature and shutdown. |
+| STATUS_FLAG_ELECTRONICS_FAULT | `uint64` | 1024 | Power electronics experienced a fault and shutdown. |
+| STATUS_FLAG_POWERSOURCE_FAULT | `uint64` | 2048 | The power source supplying the generator failed e.g. mechanical generator stopped, tether is no longer providing power, solar cell is in shade, hydrogen reaction no longer happening. |
+| STATUS_FLAG_COMMUNICATION_WARNING | `uint64` | 4096 | Generator controller having communication problems. |
+| STATUS_FLAG_COOLING_WARNING | `uint64` | 8192 | Power electronic or generator cooling system error. |
+| STATUS_FLAG_POWER_RAIL_FAULT | `uint64` | 16384 | Generator controller power rail experienced a fault. |
+| STATUS_FLAG_OVERCURRENT_FAULT | `uint64` | 32768 | Generator controller exceeded the overcurrent threshold and shutdown to prevent damage. |
+| STATUS_FLAG_BATTERY_OVERCHARGE_CURRENT_FAULT | `uint64` | 65536 | Generator controller detected a high current going into the batteries and shutdown to prevent battery damage. |
+| STATUS_FLAG_OVERVOLTAGE_FAULT | `uint64` | 131072 | Generator controller exceeded it's overvoltage threshold and shutdown to prevent it exceeding the voltage rating. |
+| STATUS_FLAG_BATTERY_UNDERVOLT_FAULT | `uint64` | 262144 | Batteries are under voltage (generator will not start). |
+| STATUS_FLAG_START_INHIBITED | `uint64` | 524288 | Generator start is inhibited by e.g. a safety switch. |
+| STATUS_FLAG_MAINTENANCE_REQUIRED | `uint64` | 1048576 | Generator requires maintenance. |
+| STATUS_FLAG_WARMING_UP | `uint64` | 2097152 | Generator is not ready to generate yet. |
+| STATUS_FLAG_IDLE | `uint64` | 4194304 | Generator is idle. |
## Source Message
diff --git a/docs/ko/msg_docs/GeofenceResult.md b/docs/ko/msg_docs/GeofenceResult.md
index f6c650b707..ae89ed1a2b 100644
--- a/docs/ko/msg_docs/GeofenceResult.md
+++ b/docs/ko/msg_docs/GeofenceResult.md
@@ -18,14 +18,14 @@ pageClass: is-wide-page
## Constants
-\| Name | Type | Value | Description |
-\| ------------------------------------------------------- | ------- | ----- | ------------------------------- | ------ |
-\| GF_ACTION_NONE | `uint8` | 0 | no action on geofence violation |
-\| GF_ACTION_WARN | `uint8` | 1 | critical mavlink message |
-\| GF_ACTION_LOITER | `uint8` | 2 | switch to AUTO | LOITER |
-\| GF_ACTION_RTL | `uint8` | 3 | switch to AUTO | RTL |
-\| GF_ACTION_TERMINATE | `uint8` | 4 | flight termination |
-\| GF_ACTION_LAND | `uint8` | 5 | switch to AUTO | LAND |
+\| Name | Type | Value | Description |
+\| ----------------------------------------------------- | ------- | ----- | ------------------------------- | ------ |
+\| GF_ACTION_NONE | `uint8` | 0 | no action on geofence violation |
+\| GF_ACTION_WARN | `uint8` | 1 | critical mavlink message |
+\| GF_ACTION_LOITER | `uint8` | 2 | switch to AUTO | LOITER |
+\| GF_ACTION_RTL | `uint8` | 3 | switch to AUTO | RTL |
+\| GF_ACTION_TERMINATE | `uint8` | 4 | flight termination |
+\| GF_ACTION_LAND | `uint8` | 5 | switch to AUTO | LAND |
## Source Message
diff --git a/docs/ko/msg_docs/GeofenceStatus.md b/docs/ko/msg_docs/GeofenceStatus.md
index a12563d15e..383ec9f1b8 100644
--- a/docs/ko/msg_docs/GeofenceStatus.md
+++ b/docs/ko/msg_docs/GeofenceStatus.md
@@ -16,10 +16,10 @@ pageClass: is-wide-page
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| --------------------------------------------------------------------------------------------- | ------- | ----- | -- |
-| GF_STATUS_LOADING | `uint8` | 0 | |
-| GF_STATUS_READY | `uint8` | 1 | |
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------------------------------------- | ------- | ----- | -- |
+| GF_STATUS_LOADING | `uint8` | 0 | |
+| GF_STATUS_READY | `uint8` | 1 | |
## Source Message
diff --git a/docs/ko/msg_docs/GimbalControls.md b/docs/ko/msg_docs/GimbalControls.md
index 2757e77784..22c6de1a76 100644
--- a/docs/ko/msg_docs/GimbalControls.md
+++ b/docs/ko/msg_docs/GimbalControls.md
@@ -16,11 +16,11 @@ pageClass: is-wide-page
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ------------------------------------------------------------ | ------- | ----- | -- |
-| INDEX_ROLL | `uint8` | 0 | |
-| INDEX_PITCH | `uint8` | 1 | |
-| INDEX_YAW | `uint8` | 2 | |
+| 명칭 | 형식 | Value | 설명 |
+| ---------------------------------------------------------- | ------- | ----- | -- |
+| INDEX_ROLL | `uint8` | 0 | |
+| INDEX_PITCH | `uint8` | 1 | |
+| INDEX_YAW | `uint8` | 2 | |
## Source Message
diff --git a/docs/ko/msg_docs/GimbalDeviceAttitudeStatus.md b/docs/ko/msg_docs/GimbalDeviceAttitudeStatus.md
index 83ee93aa44..a947b14c06 100644
--- a/docs/ko/msg_docs/GimbalDeviceAttitudeStatus.md
+++ b/docs/ko/msg_docs/GimbalDeviceAttitudeStatus.md
@@ -4,7 +4,7 @@ pageClass: is-wide-page
# GimbalDeviceAttitudeStatus (UORB message)
-**TOPICS:** gimbal_deviceattitude_status
+**TOPICS:** gimbal_device_attitude_status
## Fields
@@ -26,15 +26,15 @@ pageClass: is-wide-page
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- | -------- | ----- | -- |
-| DEVICE_FLAGS_RETRACT | `uint16` | 1 | |
-| DEVICE_FLAGS_NEUTRAL | `uint16` | 2 | |
-| DEVICE_FLAGS_ROLL_LOCK | `uint16` | 4 | |
-| DEVICE_FLAGS_PITCH_LOCK | `uint16` | 8 | |
-| DEVICE_FLAGS_YAW_LOCK | `uint16` | 16 | |
-| DEVICE_FLAGS_YAW_IN_VEHICLE_FRAME | `uint16` | 32 | |
-| DEVICE_FLAGS_YAW_IN_EARTH_FRAME | `uint16` | 64 | |
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ | -------- | ----- | -- |
+| DEVICE_FLAGS_RETRACT | `uint16` | 1 | |
+| DEVICE_FLAGS_NEUTRAL | `uint16` | 2 | |
+| DEVICE_FLAGS_ROLL_LOCK | `uint16` | 4 | |
+| DEVICE_FLAGS_PITCH_LOCK | `uint16` | 8 | |
+| DEVICE_FLAGS_YAW_LOCK | `uint16` | 16 | |
+| DEVICE_FLAGS_YAW_IN_VEHICLE_FRAME | `uint16` | 32 | |
+| DEVICE_FLAGS_YAW_IN_EARTH_FRAME | `uint16` | 64 | |
## Source Message
diff --git a/docs/ko/msg_docs/GimbalDeviceInformation.md b/docs/ko/msg_docs/GimbalDeviceInformation.md
index 19b6db7b88..6e3e0b1ca3 100644
--- a/docs/ko/msg_docs/GimbalDeviceInformation.md
+++ b/docs/ko/msg_docs/GimbalDeviceInformation.md
@@ -4,7 +4,7 @@ pageClass: is-wide-page
# GimbalDeviceInformation (UORB message)
-**TOPICS:** gimbal_deviceinformation
+**TOPICS:** gimbal_device_information
## Fields
@@ -29,20 +29,20 @@ pageClass: is-wide-page
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ----------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- | -------- | ----- | -- |
-| GIMBAL_DEVICE_CAP_FLAGS_HAS_RETRACT | `uint32` | 1 | |
-| GIMBAL_DEVICE_CAP_FLAGS_HAS_NEUTRAL | `uint32` | 2 | |
-| GIMBAL_DEVICE_CAP_FLAGS_HAS_ROLL_AXIS | `uint32` | 4 | |
-| GIMBAL_DEVICE_CAP_FLAGS_HAS_ROLL_FOLLOW | `uint32` | 8 | |
-| GIMBAL_DEVICE_CAP_FLAGS_HAS_ROLL_LOCK | `uint32` | 16 | |
-| GIMBAL_DEVICE_CAP_FLAGS_HAS_PITCH_AXIS | `uint32` | 32 | |
-| GIMBAL_DEVICE_CAP_FLAGS_HAS_PITCH_FOLLOW | `uint32` | 64 | |
-| GIMBAL_DEVICE_CAP_FLAGS_HAS_PITCH_LOCK | `uint32` | 128 | |
-| GIMBAL_DEVICE_CAP_FLAGS_HAS_YAW_AXIS | `uint32` | 256 | |
-| GIMBAL_DEVICE_CAP_FLAGS_HAS_YAW_FOLLOW | `uint32` | 512 | |
-| GIMBAL_DEVICE_CAP_FLAGS_HAS_YAW_LOCK | `uint32` | 1024 | |
-| GIMBAL_DEVICE_CAP_FLAGS_SUPPORTS_INFINITE_YAW | `uint32` | 2048 | |
+| 명칭 | 형식 | Value | 설명 |
+| --------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- | -------- | ----- | -- |
+| GIMBAL_DEVICE_CAP_FLAGS_HAS_RETRACT | `uint32` | 1 | |
+| GIMBAL_DEVICE_CAP_FLAGS_HAS_NEUTRAL | `uint32` | 2 | |
+| GIMBAL_DEVICE_CAP_FLAGS_HAS_ROLL_AXIS | `uint32` | 4 | |
+| GIMBAL_DEVICE_CAP_FLAGS_HAS_ROLL_FOLLOW | `uint32` | 8 | |
+| GIMBAL_DEVICE_CAP_FLAGS_HAS_ROLL_LOCK | `uint32` | 16 | |
+| GIMBAL_DEVICE_CAP_FLAGS_HAS_PITCH_AXIS | `uint32` | 32 | |
+| GIMBAL_DEVICE_CAP_FLAGS_HAS_PITCH_FOLLOW | `uint32` | 64 | |
+| GIMBAL_DEVICE_CAP_FLAGS_HAS_PITCH_LOCK | `uint32` | 128 | |
+| GIMBAL_DEVICE_CAP_FLAGS_HAS_YAW_AXIS | `uint32` | 256 | |
+| GIMBAL_DEVICE_CAP_FLAGS_HAS_YAW_FOLLOW | `uint32` | 512 | |
+| GIMBAL_DEVICE_CAP_FLAGS_HAS_YAW_LOCK | `uint32` | 1024 | |
+| GIMBAL_DEVICE_CAP_FLAGS_SUPPORTS_INFINITE_YAW | `uint32` | 2048 | |
## Source Message
diff --git a/docs/ko/msg_docs/GimbalDeviceSetAttitude.md b/docs/ko/msg_docs/GimbalDeviceSetAttitude.md
index 4ddac878bb..771841e98c 100644
--- a/docs/ko/msg_docs/GimbalDeviceSetAttitude.md
+++ b/docs/ko/msg_docs/GimbalDeviceSetAttitude.md
@@ -4,7 +4,7 @@ pageClass: is-wide-page
# GimbalDeviceSetAttitude (UORB message)
-**TOPICS:** gimbal_deviceset_attitude
+**TOPICS:** gimbal_device_set_attitude
## Fields
@@ -21,13 +21,13 @@ pageClass: is-wide-page
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ----------------------------------------------------------------------------------------------------------------------------------------------------------------- | -------- | ----- | -- |
-| GIMBAL_DEVICE_FLAGS_RETRACT | `uint32` | 1 | |
-| GIMBAL_DEVICE_FLAGS_NEUTRAL | `uint32` | 2 | |
-| GIMBAL_DEVICE_FLAGS_ROLL_LOCK | `uint32` | 4 | |
-| GIMBAL_DEVICE_FLAGS_PITCH_LOCK | `uint32` | 8 | |
-| GIMBAL_DEVICE_FLAGS_YAW_LOCK | `uint32` | 16 | |
+| 명칭 | 형식 | Value | 설명 |
+| --------------------------------------------------------------------------------------------------------------------------------------------------------------- | -------- | ----- | -- |
+| GIMBAL_DEVICE_FLAGS_RETRACT | `uint32` | 1 | |
+| GIMBAL_DEVICE_FLAGS_NEUTRAL | `uint32` | 2 | |
+| GIMBAL_DEVICE_FLAGS_ROLL_LOCK | `uint32` | 4 | |
+| GIMBAL_DEVICE_FLAGS_PITCH_LOCK | `uint32` | 8 | |
+| GIMBAL_DEVICE_FLAGS_YAW_LOCK | `uint32` | 16 | |
## Source Message
diff --git a/docs/ko/msg_docs/GimbalManagerInformation.md b/docs/ko/msg_docs/GimbalManagerInformation.md
index bbc7286498..5dd0fea9a9 100644
--- a/docs/ko/msg_docs/GimbalManagerInformation.md
+++ b/docs/ko/msg_docs/GimbalManagerInformation.md
@@ -4,7 +4,7 @@ pageClass: is-wide-page
# GimbalManagerInformation (UORB message)
-**TOPICS:** gimbal_managerinformation
+**TOPICS:** gimbal_manager_information
## Fields
@@ -22,22 +22,22 @@ pageClass: is-wide-page
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ | -------- | ------ | -- |
-| GIMBAL_MANAGER_CAP_FLAGS_HAS_RETRACT | `uint32` | 1 | |
-| GIMBAL_MANAGER_CAP_FLAGS_HAS_NEUTRAL | `uint32` | 2 | |
-| GIMBAL_MANAGER_CAP_FLAGS_HAS_ROLL_AXIS | `uint32` | 4 | |
-| GIMBAL_MANAGER_CAP_FLAGS_HAS_ROLL_FOLLOW | `uint32` | 8 | |
-| GIMBAL_MANAGER_CAP_FLAGS_HAS_ROLL_LOCK | `uint32` | 16 | |
-| GIMBAL_MANAGER_CAP_FLAGS_HAS_PITCH_AXIS | `uint32` | 32 | |
-| GIMBAL_MANAGER_CAP_FLAGS_HAS_PITCH_FOLLOW | `uint32` | 64 | |
-| GIMBAL_MANAGER_CAP_FLAGS_HAS_PITCH_LOCK | `uint32` | 128 | |
-| GIMBAL_MANAGER_CAP_FLAGS_HAS_YAW_AXIS | `uint32` | 256 | |
-| GIMBAL_MANAGER_CAP_FLAGS_HAS_YAW_FOLLOW | `uint32` | 512 | |
-| GIMBAL_MANAGER_CAP_FLAGS_HAS_YAW_LOCK | `uint32` | 1024 | |
-| GIMBAL_MANAGER_CAP_FLAGS_SUPPORTS_INFINITE_YAW | `uint32` | 2048 | |
-| GIMBAL_MANAGER_CAP_FLAGS_CAN_POINT_LOCATION_LOCAL | `uint32` | 65536 | |
-| GIMBAL_MANAGER_CAP_FLAGS_CAN_POINT_LOCATION_GLOBAL | `uint32` | 131072 | |
+| 명칭 | 형식 | Value | 설명 |
+| ---------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- | -------- | ------ | -- |
+| GIMBAL_MANAGER_CAP_FLAGS_HAS_RETRACT | `uint32` | 1 | |
+| GIMBAL_MANAGER_CAP_FLAGS_HAS_NEUTRAL | `uint32` | 2 | |
+| GIMBAL_MANAGER_CAP_FLAGS_HAS_ROLL_AXIS | `uint32` | 4 | |
+| GIMBAL_MANAGER_CAP_FLAGS_HAS_ROLL_FOLLOW | `uint32` | 8 | |
+| GIMBAL_MANAGER_CAP_FLAGS_HAS_ROLL_LOCK | `uint32` | 16 | |
+| GIMBAL_MANAGER_CAP_FLAGS_HAS_PITCH_AXIS | `uint32` | 32 | |
+| GIMBAL_MANAGER_CAP_FLAGS_HAS_PITCH_FOLLOW | `uint32` | 64 | |
+| GIMBAL_MANAGER_CAP_FLAGS_HAS_PITCH_LOCK | `uint32` | 128 | |
+| GIMBAL_MANAGER_CAP_FLAGS_HAS_YAW_AXIS | `uint32` | 256 | |
+| GIMBAL_MANAGER_CAP_FLAGS_HAS_YAW_FOLLOW | `uint32` | 512 | |
+| GIMBAL_MANAGER_CAP_FLAGS_HAS_YAW_LOCK | `uint32` | 1024 | |
+| GIMBAL_MANAGER_CAP_FLAGS_SUPPORTS_INFINITE_YAW | `uint32` | 2048 | |
+| GIMBAL_MANAGER_CAP_FLAGS_CAN_POINT_LOCATION_LOCAL | `uint32` | 65536 | |
+| GIMBAL_MANAGER_CAP_FLAGS_CAN_POINT_LOCATION_GLOBAL | `uint32` | 131072 | |
## Source Message
diff --git a/docs/ko/msg_docs/GimbalManagerSetAttitude.md b/docs/ko/msg_docs/GimbalManagerSetAttitude.md
index 538cb79b54..99197472ea 100644
--- a/docs/ko/msg_docs/GimbalManagerSetAttitude.md
+++ b/docs/ko/msg_docs/GimbalManagerSetAttitude.md
@@ -4,7 +4,7 @@ pageClass: is-wide-page
# GimbalManagerSetAttitude (UORB message)
-**TOPICS:** gimbal_managerset_attitude
+**TOPICS:** gimbal_manager_set_attitude
## Fields
@@ -24,14 +24,14 @@ pageClass: is-wide-page
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ------------------------------------------------------------------------------------------------------------------------------------------------------------------- | -------- | ----- | -- |
-| GIMBAL_MANAGER_FLAGS_RETRACT | `uint32` | 1 | |
-| GIMBAL_MANAGER_FLAGS_NEUTRAL | `uint32` | 2 | |
-| GIMBAL_MANAGER_FLAGS_ROLL_LOCK | `uint32` | 4 | |
-| GIMBAL_MANAGER_FLAGS_PITCH_LOCK | `uint32` | 8 | |
-| GIMBAL_MANAGER_FLAGS_YAW_LOCK | `uint32` | 16 | |
-| ORB_QUEUE_LENGTH | `uint8` | 2 | |
+| 명칭 | 형식 | Value | 설명 |
+| ----------------------------------------------------------------------------------------------------------------------------------------------------------------- | -------- | ----- | -- |
+| GIMBAL_MANAGER_FLAGS_RETRACT | `uint32` | 1 | |
+| GIMBAL_MANAGER_FLAGS_NEUTRAL | `uint32` | 2 | |
+| GIMBAL_MANAGER_FLAGS_ROLL_LOCK | `uint32` | 4 | |
+| GIMBAL_MANAGER_FLAGS_PITCH_LOCK | `uint32` | 8 | |
+| GIMBAL_MANAGER_FLAGS_YAW_LOCK | `uint32` | 16 | |
+| ORB_QUEUE_LENGTH | `uint8` | 2 | |
## Source Message
diff --git a/docs/ko/msg_docs/GimbalManagerSetManualControl.md b/docs/ko/msg_docs/GimbalManagerSetManualControl.md
index b3bca540a0..8c0a0bb642 100644
--- a/docs/ko/msg_docs/GimbalManagerSetManualControl.md
+++ b/docs/ko/msg_docs/GimbalManagerSetManualControl.md
@@ -4,7 +4,7 @@ pageClass: is-wide-page
# GimbalManagerSetManualControl (UORB message)
-**TOPICS:** gimbal_managerset_manualcontrol
+**TOPICS:** gimbal_manager_set_manual_control
## Fields
@@ -24,13 +24,13 @@ pageClass: is-wide-page
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ------------------------------------------------------------------------------------------------------------------------------------------------------------------- | -------- | ----- | -- |
-| GIMBAL_MANAGER_FLAGS_RETRACT | `uint32` | 1 | |
-| GIMBAL_MANAGER_FLAGS_NEUTRAL | `uint32` | 2 | |
-| GIMBAL_MANAGER_FLAGS_ROLL_LOCK | `uint32` | 4 | |
-| GIMBAL_MANAGER_FLAGS_PITCH_LOCK | `uint32` | 8 | |
-| GIMBAL_MANAGER_FLAGS_YAW_LOCK | `uint32` | 16 | |
+| 명칭 | 형식 | Value | 설명 |
+| ----------------------------------------------------------------------------------------------------------------------------------------------------------------- | -------- | ----- | -- |
+| GIMBAL_MANAGER_FLAGS_RETRACT | `uint32` | 1 | |
+| GIMBAL_MANAGER_FLAGS_NEUTRAL | `uint32` | 2 | |
+| GIMBAL_MANAGER_FLAGS_ROLL_LOCK | `uint32` | 4 | |
+| GIMBAL_MANAGER_FLAGS_PITCH_LOCK | `uint32` | 8 | |
+| GIMBAL_MANAGER_FLAGS_YAW_LOCK | `uint32` | 16 | |
## Source Message
diff --git a/docs/ko/msg_docs/GimbalManagerStatus.md b/docs/ko/msg_docs/GimbalManagerStatus.md
index a664c44f05..eb870c1504 100644
--- a/docs/ko/msg_docs/GimbalManagerStatus.md
+++ b/docs/ko/msg_docs/GimbalManagerStatus.md
@@ -4,7 +4,7 @@ pageClass: is-wide-page
# GimbalManagerStatus (UORB message)
-**TOPICS:** gimbal_managerstatus
+**TOPICS:** gimbal_manager_status
## Fields
diff --git a/docs/ko/msg_docs/GotoSetpoint.md b/docs/ko/msg_docs/GotoSetpoint.md
index eca8aaf6cf..2f89625e7c 100644
--- a/docs/ko/msg_docs/GotoSetpoint.md
+++ b/docs/ko/msg_docs/GotoSetpoint.md
@@ -4,7 +4,13 @@ pageClass: is-wide-page
# GotoSetpoint (UORB message)
-Position and (optional) heading setpoints with corresponding speed constraints. Setpoints are intended as inputs to position and heading smoothers, respectively. Setpoints do not need to be kinematically consistent. Optional heading setpoints may be specified as controlled by the respective flag. Unset optional setpoints are not controlled. Unset optional constraints default to vehicle specifications.
+Position and (optional) heading setpoints with corresponding speed constraints.
+
+Setpoints are intended as inputs to position and heading smoothers, respectively.
+Setpoints do not need to be kinematically consistent.
+Optional heading setpoints may be specified as controlled by the respective flag.
+Unset optional setpoints are not controlled.
+Unset optional constraints default to vehicle specifications.
**TOPICS:** goto_setpoint
@@ -12,22 +18,22 @@ Position and (optional) heading setpoints with corresponding speed constraints.
| 명칭 | 형식 | Unit [Frame] | Range/Enum | 설명 |
| ----------------------------------------------------------------------------------------------------------------- | ------------ | ---------------------------------------------------------------- | ---------- | --------------------------------------------------------------------------------------------------------------------------------------------------------------- |
-| timestamp | `uint64` | | | time since system start (microseconds) |
-| position | `float32[3]` | m | | NED local world frame |
+| timestamp | `uint64` | us | | Time since system start |
+| position | `float32[3]` | m [NED] | | NED local world frame |
| flag_control_heading | `bool` | | | true if heading is to be controlled |
| heading | `float32` | | | (optional) [rad] [-pi,pi] from North |
| flag_set_max_horizontal_speed | `bool` | | | true if setting a non-default horizontal speed limit |
-| max_horizontal_speed | `float32` | | | (optional) [m/s] maximum speed (absolute) in the NE-plane |
+| max_horizontal_speed | `float32` | m/s | | (optional) Maximum speed (absolute) in the NE-plane |
| flag_set_max_vertical_speed | `bool` | | | true if setting a non-default vertical speed limit |
-| max_vertical_speed | `float32` | | | (optional) [m/s] maximum speed (absolute) in the D-axis |
+| max_vertical_speed | `float32` | m/s | | (optional) Maximum speed (absolute) in the D-axis |
| flag_set_max_heading_rate | `bool` | | | true if setting a non-default heading rate limit |
-| max_heading_rate | `float32` | | | (optional) [rad/s] maximum heading rate (absolute) |
+| max_heading_rate | `float32` | rad/s | | (optional) Maximum heading rate (absolute) |
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| -------------------------------------------------------------------- | -------- | ----- | -- |
-| MESSAGE_VERSION | `uint32` | 0 | |
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------------ | -------- | ----- | -- |
+| MESSAGE_VERSION | `uint32` | 0 | |
## Source Message
@@ -38,31 +44,32 @@ Click here to see original file
```c
# Position and (optional) heading setpoints with corresponding speed constraints
-# Setpoints are intended as inputs to position and heading smoothers, respectively
-# Setpoints do not need to be kinematically consistent
-# Optional heading setpoints may be specified as controlled by the respective flag
-# Unset optional setpoints are not controlled
-# Unset optional constraints default to vehicle specifications
+#
+# Setpoints are intended as inputs to position and heading smoothers, respectively.
+# Setpoints do not need to be kinematically consistent.
+# Optional heading setpoints may be specified as controlled by the respective flag.
+# Unset optional setpoints are not controlled.
+# Unset optional constraints default to vehicle specifications.
uint32 MESSAGE_VERSION = 0
-uint64 timestamp # time since system start (microseconds)
+uint64 timestamp # [us] Time since system start
# setpoints
-float32[3] position # [m] NED local world frame
+float32[3] position # [m] [@frame NED] NED local world frame
bool flag_control_heading # true if heading is to be controlled
float32 heading # (optional) [rad] [-pi,pi] from North
# constraints
bool flag_set_max_horizontal_speed # true if setting a non-default horizontal speed limit
-float32 max_horizontal_speed # (optional) [m/s] maximum speed (absolute) in the NE-plane
+float32 max_horizontal_speed # [m/s] (optional) Maximum speed (absolute) in the NE-plane
bool flag_set_max_vertical_speed # true if setting a non-default vertical speed limit
-float32 max_vertical_speed # (optional) [m/s] maximum speed (absolute) in the D-axis
+float32 max_vertical_speed # [m/s] (optional) Maximum speed (absolute) in the D-axis
bool flag_set_max_heading_rate # true if setting a non-default heading rate limit
-float32 max_heading_rate # (optional) [rad/s] maximum heading rate (absolute)
+float32 max_heading_rate # [rad/s] (optional) Maximum heading rate (absolute)
```
:::
diff --git a/docs/ko/msg_docs/GpioConfig.md b/docs/ko/msg_docs/GpioConfig.md
index fba68b892d..afd713d6d3 100644
--- a/docs/ko/msg_docs/GpioConfig.md
+++ b/docs/ko/msg_docs/GpioConfig.md
@@ -20,19 +20,19 @@ GPIO configuration.
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ---------------------------------------------------------------------------------------------------------- | -------- | ----- | ------ |
-| INPUT | `uint32` | 0 | 0x0000 |
-| OUTPUT | `uint32` | 1 | 0x0001 |
-| PULLUP | `uint32` | 16 | 0x0010 |
-| PULLDOWN | `uint32` | 32 | 0x0020 |
-| OPENDRAIN | `uint32` | 256 | 0x0100 |
-| INPUT_FLOATING | `uint32` | 0 | 0x0000 |
-| INPUT_PULLUP | `uint32` | 16 | 0x0010 |
-| INPUT_PULLDOWN | `uint32` | 32 | 0x0020 |
-| OUTPUT_PUSHPULL | `uint32` | 0 | 0x0000 |
-| OUTPUT_OPENDRAIN | `uint32` | 256 | 0x0100 |
-| OUTPUT_OPENDRAIN_PULLUP | `uint32` | 272 | 0x0110 |
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------------------------------------------------- | -------- | ----- | ------ |
+| INPUT | `uint32` | 0 | 0x0000 |
+| OUTPUT | `uint32` | 1 | 0x0001 |
+| PULLUP | `uint32` | 16 | 0x0010 |
+| PULLDOWN | `uint32` | 32 | 0x0020 |
+| OPENDRAIN | `uint32` | 256 | 0x0100 |
+| INPUT_FLOATING | `uint32` | 0 | 0x0000 |
+| INPUT_PULLUP | `uint32` | 16 | 0x0010 |
+| INPUT_PULLDOWN | `uint32` | 32 | 0x0020 |
+| OUTPUT_PUSHPULL | `uint32` | 0 | 0x0000 |
+| OUTPUT_OPENDRAIN | `uint32` | 256 | 0x0100 |
+| OUTPUT_OPENDRAIN_PULLUP | `uint32` | 272 | 0x0110 |
## Source Message
diff --git a/docs/ko/msg_docs/GpioIn.md b/docs/ko/msg_docs/GpioIn.md
index 5bbaf4ae51..8ef9a7e3bd 100644
--- a/docs/ko/msg_docs/GpioIn.md
+++ b/docs/ko/msg_docs/GpioIn.md
@@ -18,9 +18,9 @@ GPIO mask and state.
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ---------------------------------------------------------------- | ------- | ----- | -- |
-| MAX_INSTANCES | `uint8` | 8 | |
+| 명칭 | 형식 | Value | 설명 |
+| -------------------------------------------------------------- | ------- | ----- | -- |
+| MAX_INSTANCES | `uint8` | 8 | |
## Source Message
diff --git a/docs/ko/msg_docs/GpsDump.md b/docs/ko/msg_docs/GpsDump.md
index a0afd2f854..cc6d37a6fe 100644
--- a/docs/ko/msg_docs/GpsDump.md
+++ b/docs/ko/msg_docs/GpsDump.md
@@ -20,11 +20,11 @@ This message is used to dump the raw gps communication to the log.
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ------------------------------------------------------------------------------------------- | ------- | ----- | -- |
-| INSTANCE_MAIN | `uint8` | 0 | |
-| INSTANCE_SECONDARY | `uint8` | 1 | |
-| ORB_QUEUE_LENGTH | `uint8` | 16 | |
+| 명칭 | 형식 | Value | 설명 |
+| ----------------------------------------------------------------------------------------- | ------- | ----- | -- |
+| INSTANCE_MAIN | `uint8` | 0 | |
+| INSTANCE_SECONDARY | `uint8` | 1 | |
+| ORB_QUEUE_LENGTH | `uint8` | 16 | |
## Source Message
diff --git a/docs/ko/msg_docs/GpsInjectData.md b/docs/ko/msg_docs/GpsInjectData.md
index 041afba713..39de9ec10e 100644
--- a/docs/ko/msg_docs/GpsInjectData.md
+++ b/docs/ko/msg_docs/GpsInjectData.md
@@ -4,7 +4,7 @@ pageClass: is-wide-page
# GpsInjectData (UORB message)
-**TOPICS:** gps_injectdata
+**TOPICS:** gps_inject_data
## Fields
@@ -18,10 +18,10 @@ pageClass: is-wide-page
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ------------------------------------------------------------------------------------------- | ------- | ----- | -- |
-| ORB_QUEUE_LENGTH | `uint8` | 8 | |
-| MAX_INSTANCES | `uint8` | 2 | |
+| 명칭 | 형식 | Value | 설명 |
+| ----------------------------------------------------------------------------------------- | ------- | ----- | -- |
+| ORB_QUEUE_LENGTH | `uint8` | 8 | |
+| MAX_INSTANCES | `uint8` | 2 | |
## Source Message
diff --git a/docs/ko/msg_docs/Gripper.md b/docs/ko/msg_docs/Gripper.md
index 86e1393f8e..9046e0510e 100644
--- a/docs/ko/msg_docs/Gripper.md
+++ b/docs/ko/msg_docs/Gripper.md
@@ -17,10 +17,10 @@ pageClass: is-wide-page
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| -------------------------------------------------------------------- | ------ | ----- | -- |
-| COMMAND_GRAB | `int8` | 0 | |
-| COMMAND_RELEASE | `int8` | 1 | |
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------------ | ------ | ----- | -- |
+| COMMAND_GRAB | `int8` | 0 | |
+| COMMAND_RELEASE | `int8` | 1 | |
## Source Message
diff --git a/docs/ko/msg_docs/HeaterStatus.md b/docs/ko/msg_docs/HeaterStatus.md
index d587e119d5..663b0ae165 100644
--- a/docs/ko/msg_docs/HeaterStatus.md
+++ b/docs/ko/msg_docs/HeaterStatus.md
@@ -25,10 +25,10 @@ pageClass: is-wide-page
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ---------------------------------------------------------- | ------- | ----- | -- |
-| MODE_GPIO | `uint8` | 1 | |
-| MODE_PX4IO | `uint8` | 2 | |
+| 명칭 | 형식 | Value | 설명 |
+| -------------------------------------------------------- | ------- | ----- | -- |
+| MODE_GPIO | `uint8` | 1 | |
+| MODE_PX4IO | `uint8` | 2 | |
## Source Message
diff --git a/docs/ko/msg_docs/HomePosition.md b/docs/ko/msg_docs/HomePosition.md
index 1dca6ffb41..1952ef623f 100644
--- a/docs/ko/msg_docs/HomePosition.md
+++ b/docs/ko/msg_docs/HomePosition.md
@@ -30,9 +30,9 @@ GPS home position in WGS84 coordinates.
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| -------------------------------------------------------------------- | -------- | ----- | -- |
-| MESSAGE_VERSION | `uint32` | 1 | |
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------------ | -------- | ----- | -- |
+| MESSAGE_VERSION | `uint32` | 1 | |
## Source Message
diff --git a/docs/ko/msg_docs/HomePositionV0.md b/docs/ko/msg_docs/HomePositionV0.md
index 8fcde53cb5..96c499ab26 100644
--- a/docs/ko/msg_docs/HomePositionV0.md
+++ b/docs/ko/msg_docs/HomePositionV0.md
@@ -6,7 +6,7 @@ pageClass: is-wide-page
GPS home position in WGS84 coordinates.
-**TOPICS:** home_positionv0
+**TOPICS:** home_position_v0
## Fields
@@ -28,9 +28,9 @@ GPS home position in WGS84 coordinates.
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| -------------------------------------------------------------------- | -------- | ----- | -- |
-| MESSAGE_VERSION | `uint32` | 0 | |
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------------ | -------- | ----- | -- |
+| MESSAGE_VERSION | `uint32` | 0 | |
## Source Message
diff --git a/docs/ko/msg_docs/HoverThrustEstimate.md b/docs/ko/msg_docs/HoverThrustEstimate.md
index d39e2dea3d..4352290705 100644
--- a/docs/ko/msg_docs/HoverThrustEstimate.md
+++ b/docs/ko/msg_docs/HoverThrustEstimate.md
@@ -4,7 +4,7 @@ pageClass: is-wide-page
# HoverThrustEstimate (UORB message)
-**TOPICS:** hover_thrustestimate
+**TOPICS:** hover_thrust_estimate
## Fields
diff --git a/docs/ko/msg_docs/InputRc.md b/docs/ko/msg_docs/InputRc.md
index 130ad9ada4..be71c98fc2 100644
--- a/docs/ko/msg_docs/InputRc.md
+++ b/docs/ko/msg_docs/InputRc.md
@@ -28,26 +28,26 @@ pageClass: is-wide-page
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ------------------------------------------------------------------------------------------------------------------------------------------------------------------- | ------- | ----- | -------------------------------------------------------------------------------------------------------------------------------- |
-| RC_INPUT_SOURCE_UNKNOWN | `uint8` | 0 | |
-| RC_INPUT_SOURCE_PX4FMU_PPM | `uint8` | 1 | |
-| RC_INPUT_SOURCE_PX4IO_PPM | `uint8` | 2 | |
-| RC_INPUT_SOURCE_PX4IO_SPEKTRUM | `uint8` | 3 | |
-| RC_INPUT_SOURCE_PX4IO_SBUS | `uint8` | 4 | |
-| RC_INPUT_SOURCE_PX4IO_ST24 | `uint8` | 5 | |
-| RC_INPUT_SOURCE_MAVLINK | `uint8` | 6 | |
-| RC_INPUT_SOURCE_QURT | `uint8` | 7 | |
-| RC_INPUT_SOURCE_PX4FMU_SPEKTRUM | `uint8` | 8 | |
-| RC_INPUT_SOURCE_PX4FMU_SBUS | `uint8` | 9 | |
-| RC_INPUT_SOURCE_PX4FMU_ST24 | `uint8` | 10 | |
-| RC_INPUT_SOURCE_PX4FMU_SUMD | `uint8` | 11 | |
-| RC_INPUT_SOURCE_PX4FMU_DSM | `uint8` | 12 | |
-| RC_INPUT_SOURCE_PX4IO_SUMD | `uint8` | 13 | |
-| RC_INPUT_SOURCE_PX4FMU_CRSF | `uint8` | 14 | |
-| RC_INPUT_SOURCE_PX4FMU_GHST | `uint8` | 15 | |
-| RC_INPUT_MAX_CHANNELS | `uint8` | 18 | Maximum number of R/C input channels in the system. S.Bus has up to 18 channels. |
-| RSSI_MAX | `int8` | 100 | |
+| 명칭 | 형식 | Value | 설명 |
+| ----------------------------------------------------------------------------------------------------------------------------------------------------------------- | ------- | ----- | -------------------------------------------------------------------------------------------------------------------------------- |
+| RC_INPUT_SOURCE_UNKNOWN | `uint8` | 0 | |
+| RC_INPUT_SOURCE_PX4FMU_PPM | `uint8` | 1 | |
+| RC_INPUT_SOURCE_PX4IO_PPM | `uint8` | 2 | |
+| RC_INPUT_SOURCE_PX4IO_SPEKTRUM | `uint8` | 3 | |
+| RC_INPUT_SOURCE_PX4IO_SBUS | `uint8` | 4 | |
+| RC_INPUT_SOURCE_PX4IO_ST24 | `uint8` | 5 | |
+| RC_INPUT_SOURCE_MAVLINK | `uint8` | 6 | |
+| RC_INPUT_SOURCE_QURT | `uint8` | 7 | |
+| RC_INPUT_SOURCE_PX4FMU_SPEKTRUM | `uint8` | 8 | |
+| RC_INPUT_SOURCE_PX4FMU_SBUS | `uint8` | 9 | |
+| RC_INPUT_SOURCE_PX4FMU_ST24 | `uint8` | 10 | |
+| RC_INPUT_SOURCE_PX4FMU_SUMD | `uint8` | 11 | |
+| RC_INPUT_SOURCE_PX4FMU_DSM | `uint8` | 12 | |
+| RC_INPUT_SOURCE_PX4IO_SUMD | `uint8` | 13 | |
+| RC_INPUT_SOURCE_PX4FMU_CRSF | `uint8` | 14 | |
+| RC_INPUT_SOURCE_PX4FMU_GHST | `uint8` | 15 | |
+| RC_INPUT_MAX_CHANNELS | `uint8` | 18 | Maximum number of R/C input channels in the system. S.Bus has up to 18 channels. |
+| RSSI_MAX | `int8` | 100 | |
## Source Message
diff --git a/docs/ko/msg_docs/InternalCombustionEngineControl.md b/docs/ko/msg_docs/InternalCombustionEngineControl.md
index a7d6822f00..9ba4466e4a 100644
--- a/docs/ko/msg_docs/InternalCombustionEngineControl.md
+++ b/docs/ko/msg_docs/InternalCombustionEngineControl.md
@@ -4,7 +4,7 @@ pageClass: is-wide-page
# InternalCombustionEngineControl (UORB message)
-**TOPICS:** internal_combustionengine_control
+**TOPICS:** internal_combustion_engine_control
## Fields
diff --git a/docs/ko/msg_docs/InternalCombustionEngineStatus.md b/docs/ko/msg_docs/InternalCombustionEngineStatus.md
index 99fc9fae60..73d177f43c 100644
--- a/docs/ko/msg_docs/InternalCombustionEngineStatus.md
+++ b/docs/ko/msg_docs/InternalCombustionEngineStatus.md
@@ -4,7 +4,7 @@ pageClass: is-wide-page
# InternalCombustionEngineStatus (UORB message)
-**TOPICS:** internal_combustionengine_status
+**TOPICS:** internal_combustion_engine_status
## Fields
@@ -36,36 +36,36 @@ pageClass: is-wide-page
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| --------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- | -------- | ------ | -------------------------------------------------------------------------------------- |
-| STATE_STOPPED | `uint8` | 0 | The engine is not running. This is the default state. |
-| STATE_STARTING | `uint8` | 1 | The engine is starting. This is a transient state. |
-| STATE_RUNNING | `uint8` | 2 | The engine is running normally. |
-| STATE_FAULT | `uint8` | 3 | The engine can no longer function. |
-| FLAG_GENERAL_ERROR | `uint32` | 1 | General error. |
-| FLAG_CRANKSHAFT_SENSOR_ERROR_SUPPORTED | `uint32` | 2 | Error of the crankshaft sensor. This flag is optional. |
-| FLAG_CRANKSHAFT_SENSOR_ERROR | `uint32` | 4 | |
-| FLAG_TEMPERATURE_SUPPORTED | `uint32` | 8 | Temperature levels. These flags are optional |
-| FLAG_TEMPERATURE_BELOW_NOMINAL | `uint32` | 16 | Under-temperature warning |
-| FLAG_TEMPERATURE_ABOVE_NOMINAL | `uint32` | 32 | Over-temperature warning |
-| FLAG_TEMPERATURE_OVERHEATING | `uint32` | 64 | Critical overheating |
-| FLAG_TEMPERATURE_EGT_ABOVE_NOMINAL | `uint32` | 128 | Exhaust gas over-temperature warning |
-| FLAG_FUEL_PRESSURE_SUPPORTED | `uint32` | 256 | Fuel pressure. These flags are optional |
-| FLAG_FUEL_PRESSURE_BELOW_NOMINAL | `uint32` | 512 | Under-pressure warning |
-| FLAG_FUEL_PRESSURE_ABOVE_NOMINAL | `uint32` | 1024 | Over-pressure warning |
-| FLAG_DETONATION_SUPPORTED | `uint32` | 2048 | Detonation warning. This flag is optional. |
-| FLAG_DETONATION_OBSERVED | `uint32` | 4096 | Detonation condition observed warning |
-| FLAG_MISFIRE_SUPPORTED | `uint32` | 8192 | Misfire warning. This flag is optional. |
-| FLAG_MISFIRE_OBSERVED | `uint32` | 16384 | Misfire condition observed warning |
-| FLAG_OIL_PRESSURE_SUPPORTED | `uint32` | 32768 | Oil pressure. These flags are optional |
-| FLAG_OIL_PRESSURE_BELOW_NOMINAL | `uint32` | 65536 | Under-pressure warning |
-| FLAG_OIL_PRESSURE_ABOVE_NOMINAL | `uint32` | 131072 | Over-pressure warning |
-| FLAG_DEBRIS_SUPPORTED | `uint32` | 262144 | Debris warning. This flag is optional |
-| FLAG_DEBRIS_DETECTED | `uint32` | 524288 | Detection of debris warning |
-| SPARK_PLUG_SINGLE | `uint8` | 0 | |
-| SPARK_PLUG_FIRST_ACTIVE | `uint8` | 1 | |
-| SPARK_PLUG_SECOND_ACTIVE | `uint8` | 2 | |
-| SPARK_PLUG_BOTH_ACTIVE | `uint8` | 3 | |
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- | -------- | ------ | -------------------------------------------------------------------------------------- |
+| STATE_STOPPED | `uint8` | 0 | The engine is not running. This is the default state. |
+| STATE_STARTING | `uint8` | 1 | The engine is starting. This is a transient state. |
+| STATE_RUNNING | `uint8` | 2 | The engine is running normally. |
+| STATE_FAULT | `uint8` | 3 | The engine can no longer function. |
+| FLAG_GENERAL_ERROR | `uint32` | 1 | General error. |
+| FLAG_CRANKSHAFT_SENSOR_ERROR_SUPPORTED | `uint32` | 2 | Error of the crankshaft sensor. This flag is optional. |
+| FLAG_CRANKSHAFT_SENSOR_ERROR | `uint32` | 4 | |
+| FLAG_TEMPERATURE_SUPPORTED | `uint32` | 8 | Temperature levels. These flags are optional |
+| FLAG_TEMPERATURE_BELOW_NOMINAL | `uint32` | 16 | Under-temperature warning |
+| FLAG_TEMPERATURE_ABOVE_NOMINAL | `uint32` | 32 | Over-temperature warning |
+| FLAG_TEMPERATURE_OVERHEATING | `uint32` | 64 | Critical overheating |
+| FLAG_TEMPERATURE_EGT_ABOVE_NOMINAL | `uint32` | 128 | Exhaust gas over-temperature warning |
+| FLAG_FUEL_PRESSURE_SUPPORTED | `uint32` | 256 | Fuel pressure. These flags are optional |
+| FLAG_FUEL_PRESSURE_BELOW_NOMINAL | `uint32` | 512 | Under-pressure warning |
+| FLAG_FUEL_PRESSURE_ABOVE_NOMINAL | `uint32` | 1024 | Over-pressure warning |
+| FLAG_DETONATION_SUPPORTED | `uint32` | 2048 | Detonation warning. This flag is optional. |
+| FLAG_DETONATION_OBSERVED | `uint32` | 4096 | Detonation condition observed warning |
+| FLAG_MISFIRE_SUPPORTED | `uint32` | 8192 | Misfire warning. This flag is optional. |
+| FLAG_MISFIRE_OBSERVED | `uint32` | 16384 | Misfire condition observed warning |
+| FLAG_OIL_PRESSURE_SUPPORTED | `uint32` | 32768 | Oil pressure. These flags are optional |
+| FLAG_OIL_PRESSURE_BELOW_NOMINAL | `uint32` | 65536 | Under-pressure warning |
+| FLAG_OIL_PRESSURE_ABOVE_NOMINAL | `uint32` | 131072 | Over-pressure warning |
+| FLAG_DEBRIS_SUPPORTED | `uint32` | 262144 | Debris warning. This flag is optional |
+| FLAG_DEBRIS_DETECTED | `uint32` | 524288 | Detection of debris warning |
+| SPARK_PLUG_SINGLE | `uint8` | 0 | |
+| SPARK_PLUG_FIRST_ACTIVE | `uint8` | 1 | |
+| SPARK_PLUG_SECOND_ACTIVE | `uint8` | 2 | |
+| SPARK_PLUG_BOTH_ACTIVE | `uint8` | 3 | |
## Source Message
diff --git a/docs/ko/msg_docs/LandingGear.md b/docs/ko/msg_docs/LandingGear.md
index 3781f1816e..018f490094 100644
--- a/docs/ko/msg_docs/LandingGear.md
+++ b/docs/ko/msg_docs/LandingGear.md
@@ -15,11 +15,11 @@ pageClass: is-wide-page
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| -------------------------------------------------------- | ------ | ----- | ---------------------- |
-| GEAR_UP | `int8` | 1 | landing gear up |
-| GEAR_DOWN | `int8` | -1 | landing gear down |
-| GEAR_KEEP | `int8` | 0 | keep the current state |
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------ | ------ | ----- | ---------------------- |
+| GEAR_UP | `int8` | 1 | landing gear up |
+| GEAR_DOWN | `int8` | -1 | landing gear down |
+| GEAR_KEEP | `int8` | 0 | keep the current state |
## Source Message
diff --git a/docs/ko/msg_docs/LandingGearWheel.md b/docs/ko/msg_docs/LandingGearWheel.md
index a815e88f5f..6b890aec5d 100644
--- a/docs/ko/msg_docs/LandingGearWheel.md
+++ b/docs/ko/msg_docs/LandingGearWheel.md
@@ -4,7 +4,7 @@ pageClass: is-wide-page
# LandingGearWheel (UORB message)
-**TOPICS:** landing_gearwheel
+**TOPICS:** landing_gear_wheel
## Fields
diff --git a/docs/ko/msg_docs/LandingTargetInnovations.md b/docs/ko/msg_docs/LandingTargetInnovations.md
index e82715c4a9..685eef10ce 100644
--- a/docs/ko/msg_docs/LandingTargetInnovations.md
+++ b/docs/ko/msg_docs/LandingTargetInnovations.md
@@ -4,7 +4,7 @@ pageClass: is-wide-page
# LandingTargetInnovations (UORB message)
-**TOPICS:** landing_targetinnovations
+**TOPICS:** landing_target_innovations
## Fields
diff --git a/docs/ko/msg_docs/LandingTargetPose.md b/docs/ko/msg_docs/LandingTargetPose.md
index 404e715203..c39dc87b5d 100644
--- a/docs/ko/msg_docs/LandingTargetPose.md
+++ b/docs/ko/msg_docs/LandingTargetPose.md
@@ -6,7 +6,7 @@ pageClass: is-wide-page
Relative position of precision land target in navigation (body fixed, north aligned, NED) and inertial (world fixed, north aligned, NED) frames.
-**TOPICS:** landing_targetpose
+**TOPICS:** landing_target_pose
## Fields
diff --git a/docs/ko/msg_docs/LateralControlConfiguration.md b/docs/ko/msg_docs/LateralControlConfiguration.md
index cac7d54072..04ea25be03 100644
--- a/docs/ko/msg_docs/LateralControlConfiguration.md
+++ b/docs/ko/msg_docs/LateralControlConfiguration.md
@@ -4,22 +4,24 @@ pageClass: is-wide-page
# LateralControlConfiguration (UORB message)
-Fixed Wing Lateral Control Configuration message. Used by the fw_lateral_longitudinal_control module to constrain FixedWingLateralSetpoint messages.
+Fixed Wing Lateral Control Configuration message.
-**TOPICS:** lateral_controlconfiguration
+Used by the fw_lateral_longitudinal_control module to constrain FixedWingLateralSetpoint messages.
+
+**TOPICS:** lateral_control_configuration
## Fields
| 명칭 | 형식 | Unit [Frame] | Range/Enum | 설명 |
| ----------------------------------------------------------- | --------- | ---------------------------------------------------------------- | ---------- | ----------------------------------------------------------------------------------------------------------------------------------------- |
-| timestamp | `uint64` | | | time since system start (microseconds) |
-| lateral_accel_max | `float32` | m/s^2 | | currently maps to a maximum roll angle, accel_max = tan(roll_max) \* GRAVITY |
+| timestamp | `uint64` | us | | Time since system start |
+| lateral_accel_max | `float32` | m/s^2 | | Currently maps to a maximum roll angle, accel_max = tan(roll_max) \* GRAVITY |
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| -------------------------------------------------------------------- | -------- | ----- | -- |
-| MESSAGE_VERSION | `uint32` | 0 | |
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------------ | -------- | ----- | -- |
+| MESSAGE_VERSION | `uint32` | 0 | |
## Source Message
@@ -30,13 +32,14 @@ Click here to see original file
```c
# Fixed Wing Lateral Control Configuration message
+#
# Used by the fw_lateral_longitudinal_control module to constrain FixedWingLateralSetpoint messages.
uint32 MESSAGE_VERSION = 0
-uint64 timestamp # time since system start (microseconds)
+uint64 timestamp # [us] Time since system start
-float32 lateral_accel_max # [m/s^2] currently maps to a maximum roll angle, accel_max = tan(roll_max) * GRAVITY
+float32 lateral_accel_max # [m/s^2] Currently maps to a maximum roll angle, accel_max = tan(roll_max) * GRAVITY
```
:::
diff --git a/docs/ko/msg_docs/LaunchDetectionStatus.md b/docs/ko/msg_docs/LaunchDetectionStatus.md
index 5ef459164b..4a4a814dde 100644
--- a/docs/ko/msg_docs/LaunchDetectionStatus.md
+++ b/docs/ko/msg_docs/LaunchDetectionStatus.md
@@ -6,22 +6,23 @@ pageClass: is-wide-page
Status of the launch detection state machine (fixed-wing only).
-**TOPICS:** launch_detectionstatus
+**TOPICS:** launch_detection_status
## Fields
-| 명칭 | 형식 | Unit [Frame] | Range/Enum | 설명 |
-| ---------------------------------------------------------------- | -------- | ---------------------------------------------------------------- | ---------- | --------------------------------------------------------- |
-| timestamp | `uint64` | | | time since system start (microseconds) |
-| launch_detection_state | `uint8` | | | |
+| 명칭 | 형식 | Unit [Frame] | Range/Enum | 설명 |
+| ------------------------------------------------------------------------------------------------ | -------- | ---------------------------------------------------------------- | ---------- | -------------------------------------------------------------------------------------------------------------------------------- |
+| timestamp | `uint64` | | | time since system start (microseconds) |
+| launch_detection_state | `uint8` | | | |
+| selected_control_surface_disarmed | `bool` | | | flag indicating whether selected actuators should kept disarmed (have to be configured in control allocation) |
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ----------------------------------------------------------------------------------------------------------------------------------------------------------------------------- | ------- | ----- | ----------------------------------------------------------------------------------------------------------------------------------------------------------------------- |
-| STATE_WAITING_FOR_LAUNCH | `uint8` | 0 | waiting for launch |
-| STATE_LAUNCH_DETECTED_DISABLED_MOTOR | `uint8` | 1 | launch detected, but keep motor(s) disabled (e.g. because it can't spin freely while on catapult) |
-| STATE_FLYING | `uint8` | 2 | launch detected, use normal takeoff/flying configuration |
+| 명칭 | 형식 | Value | 설명 |
+| --------------------------------------------------------------------------------------------------------------------------------------------------------------------------- | ------- | ----- | ----------------------------------------------------------------------------------------------------------------------------------------------------------------------- |
+| STATE_WAITING_FOR_LAUNCH | `uint8` | 0 | waiting for launch |
+| STATE_LAUNCH_DETECTED_DISABLED_MOTOR | `uint8` | 1 | launch detected, but keep motor(s) disabled (e.g. because it can't spin freely while on catapult) |
+| STATE_FLYING | `uint8` | 2 | launch detected, use normal takeoff/flying configuration |
## Source Message
@@ -40,6 +41,8 @@ uint8 STATE_LAUNCH_DETECTED_DISABLED_MOTOR = 1 # launch detected, but keep moto
uint8 STATE_FLYING = 2 # launch detected, use normal takeoff/flying configuration
uint8 launch_detection_state
+
+bool selected_control_surface_disarmed # [-] flag indicating whether selected actuators should kept disarmed (have to be configured in control allocation)
```
:::
diff --git a/docs/ko/msg_docs/LedControl.md b/docs/ko/msg_docs/LedControl.md
index 3ee8b926aa..3edd88a45e 100644
--- a/docs/ko/msg_docs/LedControl.md
+++ b/docs/ko/msg_docs/LedControl.md
@@ -21,27 +21,27 @@ LED control: control a single or multiple LED's. These are the externally visibl
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| --------------------------------------------------------------------------------------------- | ------- | ----- | ------------------------------------------------------------------------------------------------------------------------------------------------ |
-| COLOR_OFF | `uint8` | 0 | this is only used in the drivers |
-| COLOR_RED | `uint8` | 1 | |
-| COLOR_GREEN | `uint8` | 2 | |
-| COLOR_BLUE | `uint8` | 3 | |
-| COLOR_YELLOW | `uint8` | 4 | |
-| COLOR_PURPLE | `uint8` | 5 | |
-| COLOR_AMBER | `uint8` | 6 | |
-| COLOR_CYAN | `uint8` | 7 | |
-| COLOR_WHITE | `uint8` | 8 | |
-| MODE_OFF | `uint8` | 0 | turn LED off |
-| MODE_ON | `uint8` | 1 | turn LED on |
-| MODE_DISABLED | `uint8` | 2 | disable this priority (switch to lower priority setting) |
-| MODE_BLINK_SLOW | `uint8` | 3 | |
-| MODE_BLINK_NORMAL | `uint8` | 4 | |
-| MODE_BLINK_FAST | `uint8` | 5 | |
-| MODE_BREATHE | `uint8` | 6 | continuously increase & decrease brightness (solid color if driver does not support it) |
-| MODE_FLASH | `uint8` | 7 | two fast blinks (on/off) with timing as in MODE_BLINK_FAST and then off for a while |
-| MAX_PRIORITY | `uint8` | 2 | maximum priority (minimum is 0) |
-| ORB_QUEUE_LENGTH | `uint8` | 8 | needs to match BOARD_MAX_LEDS |
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------------------------------------- | ------- | ----- | ------------------------------------------------------------------------------------------------------------------------------------------------ |
+| COLOR_OFF | `uint8` | 0 | this is only used in the drivers |
+| COLOR_RED | `uint8` | 1 | |
+| COLOR_GREEN | `uint8` | 2 | |
+| COLOR_BLUE | `uint8` | 3 | |
+| COLOR_YELLOW | `uint8` | 4 | |
+| COLOR_PURPLE | `uint8` | 5 | |
+| COLOR_AMBER | `uint8` | 6 | |
+| COLOR_CYAN | `uint8` | 7 | |
+| COLOR_WHITE | `uint8` | 8 | |
+| MODE_OFF | `uint8` | 0 | turn LED off |
+| MODE_ON | `uint8` | 1 | turn LED on |
+| MODE_DISABLED | `uint8` | 2 | disable this priority (switch to lower priority setting) |
+| MODE_BLINK_SLOW | `uint8` | 3 | |
+| MODE_BLINK_NORMAL | `uint8` | 4 | |
+| MODE_BLINK_FAST | `uint8` | 5 | |
+| MODE_BREATHE | `uint8` | 6 | continuously increase & decrease brightness (solid color if driver does not support it) |
+| MODE_FLASH | `uint8` | 7 | two fast blinks (on/off) with timing as in MODE_BLINK_FAST and then off for a while |
+| MAX_PRIORITY | `uint8` | 2 | maximum priority (minimum is 0) |
+| ORB_QUEUE_LENGTH | `uint8` | 8 | needs to match BOARD_MAX_LEDS |
## Source Message
diff --git a/docs/ko/msg_docs/LogMessage.md b/docs/ko/msg_docs/LogMessage.md
index 96b04eb262..52a96f62d5 100644
--- a/docs/ko/msg_docs/LogMessage.md
+++ b/docs/ko/msg_docs/LogMessage.md
@@ -18,9 +18,9 @@ A logging message, output with PX4_WARN, PX4_ERR, PX4_INFO.
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ------------------------------------------------------------------------------------------- | ------- | ----- | -- |
-| ORB_QUEUE_LENGTH | `uint8` | 4 | |
+| 명칭 | 형식 | Value | 설명 |
+| ----------------------------------------------------------------------------------------- | ------- | ----- | -- |
+| ORB_QUEUE_LENGTH | `uint8` | 4 | |
## Source Message
diff --git a/docs/ko/msg_docs/LoggerStatus.md b/docs/ko/msg_docs/LoggerStatus.md
index 59f5a9bb25..1a56229f34 100644
--- a/docs/ko/msg_docs/LoggerStatus.md
+++ b/docs/ko/msg_docs/LoggerStatus.md
@@ -24,13 +24,13 @@ pageClass: is-wide-page
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ------------------------------------------------------------------------------------------------- | ------- | ----- | -------------------------------------------------------------------------------------------- |
-| LOGGER_TYPE_FULL | `uint8` | 0 | Normal, full size log |
-| LOGGER_TYPE_MISSION | `uint8` | 1 | reduced mission log (e.g. for geotagging) |
-| BACKEND_FILE | `uint8` | 1 | |
-| BACKEND_MAVLINK | `uint8` | 2 | |
-| BACKEND_ALL | `uint8` | 3 | |
+| 명칭 | 형식 | Value | 설명 |
+| ----------------------------------------------------------------------------------------------- | ------- | ----- | -------------------------------------------------------------------------------------------- |
+| LOGGER_TYPE_FULL | `uint8` | 0 | Normal, full size log |
+| LOGGER_TYPE_MISSION | `uint8` | 1 | reduced mission log (e.g. for geotagging) |
+| BACKEND_FILE | `uint8` | 1 | |
+| BACKEND_MAVLINK | `uint8` | 2 | |
+| BACKEND_ALL | `uint8` | 3 | |
## Source Message
diff --git a/docs/ko/msg_docs/LongitudinalControlConfiguration.md b/docs/ko/msg_docs/LongitudinalControlConfiguration.md
index a9d7c67f20..38c777329f 100644
--- a/docs/ko/msg_docs/LongitudinalControlConfiguration.md
+++ b/docs/ko/msg_docs/LongitudinalControlConfiguration.md
@@ -4,30 +4,33 @@ pageClass: is-wide-page
# LongitudinalControlConfiguration (UORB message)
-Fixed Wing Longitudinal Control Configuration message. Used by the fw_lateral_longitudinal_control module and TECS to constrain FixedWingLongitudinalSetpoint messages. and configure the resultant setpoints.
+Fixed Wing Longitudinal Control Configuration message.
-**TOPICS:** longitudinal_controlconfiguration
+Used by the fw_lateral_longitudinal_control module and TECS to constrain FixedWingLongitudinalSetpoint messages
+and configure the resultant setpoints.
+
+**TOPICS:** longitudinal_control_configuration
## Fields
| 명칭 | 형식 | Unit [Frame] | Range/Enum | 설명 |
| ------------------------------------------------------------------------------------------- | --------- | ---------------------------------------------------------------- | ------------------------------------------------------------------------------ | ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- |
-| timestamp | `uint64` | | | time since system start (microseconds) |
-| pitch_min | `float32` | rad | [-pi : pi] | defaults to FW_P_LIM_MIN if NAN. |
-| pitch_max | `float32` | rad | [-pi : pi] | defaults to FW_P_LIM_MAX if NAN. |
-| throttle_min | `float32` | norm | [0 : 1] | deaults to FW_THR_MIN if NAN. |
-| throttle_max | `float32` | norm | [0 : 1] | defaults to FW_THR_MAX if NAN. |
-| climb_rate_target | `float32` | m/s | | target climbrate to change altitude. Defaults to FW_T_CLIMB_MAX if NAN. Not used if height_rate is directly set in FixedWingLongitudinalSetpoint. |
-| sink_rate_target | `float32` | m/s | | target sinkrate to change altitude. Defaults to FW_T_SINK_MAX if NAN. Not used if height_rate is directly set in FixedWingLongitudinalSetpoint. |
-| speed_weight | `float32` | | [0 : 2] | , 0=pitch controls altitude only, 2=pitch controls airspeed only |
-| enforce_low_height_condition | `bool` | boolean | | if true, the altitude controller is configured with an alternative timeconstant for tighter altitude tracking |
-| disable_underspeed_protection | `bool` | boolean | | if true, underspeed handling is disabled in the altitude controller |
+| timestamp | `uint64` | us | | Time since system start |
+| pitch_min | `float32` | rad | [-pi : pi] | Defaults to FW_P_LIM_MIN if NAN. |
+| pitch_max | `float32` | rad | [-pi : pi] | Defaults to FW_P_LIM_MAX if NAN. |
+| throttle_min | `float32` | norm | [0 : 1] | Defaults to FW_THR_MIN if NAN. |
+| throttle_max | `float32` | norm | [0 : 1] | Defaults to FW_THR_MAX if NAN. |
+| climb_rate_target | `float32` | m/s | | Target climbrate to change altitude. Defaults to FW_T_CLIMB_MAX if NAN. Not used if height_rate is directly set in FixedWingLongitudinalSetpoint. |
+| sink_rate_target | `float32` | m/s | | Target sinkrate to change altitude. Defaults to FW_T_SINK_MAX if NAN. Not used if height_rate is directly set in FixedWingLongitudinalSetpoint. |
+| speed_weight | `float32` | | [0 : 2] | 0=pitch controls altitude only, 2=pitch controls airspeed only |
+| enforce_low_height_condition | `bool` | | | If true, the altitude controller is configured with an alternative timeconstant for tighter altitude tracking |
+| disable_underspeed_protection | `bool` | | | If true, underspeed handling is disabled in the altitude controller |
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| -------------------------------------------------------------------- | -------- | ----- | -- |
-| MESSAGE_VERSION | `uint32` | 0 | |
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------------ | -------- | ----- | -- |
+| MESSAGE_VERSION | `uint32` | 0 | |
## Source Message
@@ -38,22 +41,23 @@ Click here to see original file
```c
# Fixed Wing Longitudinal Control Configuration message
+#
# Used by the fw_lateral_longitudinal_control module and TECS to constrain FixedWingLongitudinalSetpoint messages
# and configure the resultant setpoints.
uint32 MESSAGE_VERSION = 0
-uint64 timestamp # time since system start (microseconds)
+uint64 timestamp # [us] Time since system start
-float32 pitch_min # [rad][@range -pi, pi] defaults to FW_P_LIM_MIN if NAN.
-float32 pitch_max # [rad][@range -pi, pi] defaults to FW_P_LIM_MAX if NAN.
-float32 throttle_min # [norm] [@range 0,1] deaults to FW_THR_MIN if NAN.
-float32 throttle_max # [norm] [@range 0,1] defaults to FW_THR_MAX if NAN.
-float32 climb_rate_target # [m/s] target climbrate to change altitude. Defaults to FW_T_CLIMB_MAX if NAN. Not used if height_rate is directly set in FixedWingLongitudinalSetpoint.
-float32 sink_rate_target # [m/s] target sinkrate to change altitude. Defaults to FW_T_SINK_MAX if NAN. Not used if height_rate is directly set in FixedWingLongitudinalSetpoint.
-float32 speed_weight # [@range 0,2], 0=pitch controls altitude only, 2=pitch controls airspeed only
-bool enforce_low_height_condition # [boolean] if true, the altitude controller is configured with an alternative timeconstant for tighter altitude tracking
-bool disable_underspeed_protection # [boolean] if true, underspeed handling is disabled in the altitude controller
+float32 pitch_min # [rad] [@range -pi, pi] Defaults to FW_P_LIM_MIN if NAN.
+float32 pitch_max # [rad] [@range -pi, pi] Defaults to FW_P_LIM_MAX if NAN.
+float32 throttle_min # [norm] [@range 0,1] Defaults to FW_THR_MIN if NAN.
+float32 throttle_max # [norm] [@range 0,1] Defaults to FW_THR_MAX if NAN.
+float32 climb_rate_target # [m/s] Target climbrate to change altitude. Defaults to FW_T_CLIMB_MAX if NAN. Not used if height_rate is directly set in FixedWingLongitudinalSetpoint.
+float32 sink_rate_target # [m/s] Target sinkrate to change altitude. Defaults to FW_T_SINK_MAX if NAN. Not used if height_rate is directly set in FixedWingLongitudinalSetpoint.
+float32 speed_weight # [-] [@range 0,2] 0=pitch controls altitude only, 2=pitch controls airspeed only
+bool enforce_low_height_condition # If true, the altitude controller is configured with an alternative timeconstant for tighter altitude tracking
+bool disable_underspeed_protection # If true, underspeed handling is disabled in the altitude controller
```
:::
diff --git a/docs/ko/msg_docs/MagWorkerData.md b/docs/ko/msg_docs/MagWorkerData.md
index d064f7b94c..864c6a25fc 100644
--- a/docs/ko/msg_docs/MagWorkerData.md
+++ b/docs/ko/msg_docs/MagWorkerData.md
@@ -4,7 +4,7 @@ pageClass: is-wide-page
# MagWorkerData (UORB message)
-**TOPICS:** mag_workerdata
+**TOPICS:** mag_worker_data
## Fields
@@ -23,9 +23,9 @@ pageClass: is-wide-page
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ------------------------------------------------------ | ------- | ----- | -- |
-| MAX_MAGS | `uint8` | 4 | |
+| 명칭 | 형식 | Value | 설명 |
+| ---------------------------------------------------- | ------- | ----- | -- |
+| MAX_MAGS | `uint8` | 4 | |
## Source Message
diff --git a/docs/ko/msg_docs/MagnetometerBiasEstimate.md b/docs/ko/msg_docs/MagnetometerBiasEstimate.md
index 3b3ff1987c..14fddaece3 100644
--- a/docs/ko/msg_docs/MagnetometerBiasEstimate.md
+++ b/docs/ko/msg_docs/MagnetometerBiasEstimate.md
@@ -4,7 +4,7 @@ pageClass: is-wide-page
# MagnetometerBiasEstimate (UORB message)
-**TOPICS:** magnetometer_biasestimate
+**TOPICS:** magnetometer_bias_estimate
## Fields
diff --git a/docs/ko/msg_docs/ManualControlSetpoint.md b/docs/ko/msg_docs/ManualControlSetpoint.md
index 7cbccf2f40..a3188dfce0 100644
--- a/docs/ko/msg_docs/ManualControlSetpoint.md
+++ b/docs/ko/msg_docs/ManualControlSetpoint.md
@@ -30,17 +30,17 @@ pageClass: is-wide-page
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ------------------------------------------------------------------------------------------- | -------- | ----- | ---------------------------------------------------------------- |
-| MESSAGE_VERSION | `uint32` | 0 | |
-| SOURCE_UNKNOWN | `uint8` | 0 | |
-| SOURCE_RC | `uint8` | 1 | radio control (input_rc) |
-| SOURCE_MAVLINK_0 | `uint8` | 2 | mavlink instance 0 |
-| SOURCE_MAVLINK_1 | `uint8` | 3 | mavlink instance 1 |
-| SOURCE_MAVLINK_2 | `uint8` | 4 | mavlink instance 2 |
-| SOURCE_MAVLINK_3 | `uint8` | 5 | mavlink instance 3 |
-| SOURCE_MAVLINK_4 | `uint8` | 6 | mavlink instance 4 |
-| SOURCE_MAVLINK_5 | `uint8` | 7 | mavlink instance 5 |
+| 명칭 | 형식 | Value | 설명 |
+| ----------------------------------------------------------------------------------------- | -------- | ----- | ---------------------------------------------------------------- |
+| MESSAGE_VERSION | `uint32` | 0 | |
+| SOURCE_UNKNOWN | `uint8` | 0 | |
+| SOURCE_RC | `uint8` | 1 | radio control (input_rc) |
+| SOURCE_MAVLINK_0 | `uint8` | 2 | mavlink instance 0 |
+| SOURCE_MAVLINK_1 | `uint8` | 3 | mavlink instance 1 |
+| SOURCE_MAVLINK_2 | `uint8` | 4 | mavlink instance 2 |
+| SOURCE_MAVLINK_3 | `uint8` | 5 | mavlink instance 3 |
+| SOURCE_MAVLINK_4 | `uint8` | 6 | mavlink instance 4 |
+| SOURCE_MAVLINK_5 | `uint8` | 7 | mavlink instance 5 |
## Source Message
diff --git a/docs/ko/msg_docs/ManualControlSwitches.md b/docs/ko/msg_docs/ManualControlSwitches.md
index e5bbf63d8a..4aee61004a 100644
--- a/docs/ko/msg_docs/ManualControlSwitches.md
+++ b/docs/ko/msg_docs/ManualControlSwitches.md
@@ -4,7 +4,7 @@ pageClass: is-wide-page
# ManualControlSwitches (UORB message)
-**TOPICS:** manual_controlswitches
+**TOPICS:** manual_control_switches
## Fields
@@ -29,20 +29,20 @@ pageClass: is-wide-page
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| --------------------------------------------------------------------------------------------- | ------- | ----- | ---------------------------------------------------- |
-| SWITCH_POS_NONE | `uint8` | 0 | switch is not mapped |
-| SWITCH_POS_ON | `uint8` | 1 | switch activated (value = 1) |
-| SWITCH_POS_MIDDLE | `uint8` | 2 | middle position (value = 0) |
-| SWITCH_POS_OFF | `uint8` | 3 | switch not activated (value = -1) |
-| MODE_SLOT_NONE | `uint8` | 0 | no mode slot assigned |
-| MODE_SLOT_1 | `uint8` | 1 | mode slot 1 selected |
-| MODE_SLOT_2 | `uint8` | 2 | mode slot 2 selected |
-| MODE_SLOT_3 | `uint8` | 3 | mode slot 3 selected |
-| MODE_SLOT_4 | `uint8` | 4 | mode slot 4 selected |
-| MODE_SLOT_5 | `uint8` | 5 | mode slot 5 selected |
-| MODE_SLOT_6 | `uint8` | 6 | mode slot 6 selected |
-| MODE_SLOT_NUM | `uint8` | 6 | number of slots |
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------------------------------------- | ------- | ----- | ---------------------------------------------------- |
+| SWITCH_POS_NONE | `uint8` | 0 | switch is not mapped |
+| SWITCH_POS_ON | `uint8` | 1 | switch activated (value = 1) |
+| SWITCH_POS_MIDDLE | `uint8` | 2 | middle position (value = 0) |
+| SWITCH_POS_OFF | `uint8` | 3 | switch not activated (value = -1) |
+| MODE_SLOT_NONE | `uint8` | 0 | no mode slot assigned |
+| MODE_SLOT_1 | `uint8` | 1 | mode slot 1 selected |
+| MODE_SLOT_2 | `uint8` | 2 | mode slot 2 selected |
+| MODE_SLOT_3 | `uint8` | 3 | mode slot 3 selected |
+| MODE_SLOT_4 | `uint8` | 4 | mode slot 4 selected |
+| MODE_SLOT_5 | `uint8` | 5 | mode slot 5 selected |
+| MODE_SLOT_6 | `uint8` | 6 | mode slot 6 selected |
+| MODE_SLOT_NUM | `uint8` | 6 | number of slots |
## Source Message
diff --git a/docs/ko/msg_docs/MavlinkLog.md b/docs/ko/msg_docs/MavlinkLog.md
index ddc17e1344..8a429f0563 100644
--- a/docs/ko/msg_docs/MavlinkLog.md
+++ b/docs/ko/msg_docs/MavlinkLog.md
@@ -16,9 +16,9 @@ pageClass: is-wide-page
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ------------------------------------------------------------------------------------------- | ------- | ----- | -- |
-| ORB_QUEUE_LENGTH | `uint8` | 8 | |
+| 명칭 | 형식 | Value | 설명 |
+| ----------------------------------------------------------------------------------------- | ------- | ----- | -- |
+| ORB_QUEUE_LENGTH | `uint8` | 8 | |
## Source Message
diff --git a/docs/ko/msg_docs/MavlinkTunnel.md b/docs/ko/msg_docs/MavlinkTunnel.md
index d32551de64..d327070f5f 100644
--- a/docs/ko/msg_docs/MavlinkTunnel.md
+++ b/docs/ko/msg_docs/MavlinkTunnel.md
@@ -21,19 +21,19 @@ MAV_TUNNEL_PAYLOAD_TYPE enum.
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ | ------- | ----- | ---------------------------------------- |
-| MAV_TUNNEL_PAYLOAD_TYPE_UNKNOWN | `uint8` | 0 | Encoding of payload unknown |
-| MAV_TUNNEL_PAYLOAD_TYPE_STORM32_RESERVED0 | `uint8` | 200 | Registered for STorM32 gimbal controller |
-| MAV_TUNNEL_PAYLOAD_TYPE_STORM32_RESERVED1 | `uint8` | 201 | Registered for STorM32 gimbal controller |
-| MAV_TUNNEL_PAYLOAD_TYPE_STORM32_RESERVED2 | `uint8` | 202 | Registered for STorM32 gimbal controller |
-| MAV_TUNNEL_PAYLOAD_TYPE_STORM32_RESERVED3 | `uint8` | 203 | Registered for STorM32 gimbal controller |
-| MAV_TUNNEL_PAYLOAD_TYPE_STORM32_RESERVED4 | `uint8` | 204 | Registered for STorM32 gimbal controller |
-| MAV_TUNNEL_PAYLOAD_TYPE_STORM32_RESERVED5 | `uint8` | 205 | Registered for STorM32 gimbal controller |
-| MAV_TUNNEL_PAYLOAD_TYPE_STORM32_RESERVED6 | `uint8` | 206 | Registered for STorM32 gimbal controller |
-| MAV_TUNNEL_PAYLOAD_TYPE_STORM32_RESERVED7 | `uint8` | 207 | Registered for STorM32 gimbal controller |
-| MAV_TUNNEL_PAYLOAD_TYPE_STORM32_RESERVED8 | `uint8` | 208 | Registered for STorM32 gimbal controller |
-| MAV_TUNNEL_PAYLOAD_TYPE_STORM32_RESERVED9 | `uint8` | 209 | Registered for STorM32 gimbal controller |
+| 명칭 | 형식 | Value | 설명 |
+| ---------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- | ------- | ----- | ---------------------------------------- |
+| MAV_TUNNEL_PAYLOAD_TYPE_UNKNOWN | `uint8` | 0 | Encoding of payload unknown |
+| MAV_TUNNEL_PAYLOAD_TYPE_STORM32_RESERVED0 | `uint8` | 200 | Registered for STorM32 gimbal controller |
+| MAV_TUNNEL_PAYLOAD_TYPE_STORM32_RESERVED1 | `uint8` | 201 | Registered for STorM32 gimbal controller |
+| MAV_TUNNEL_PAYLOAD_TYPE_STORM32_RESERVED2 | `uint8` | 202 | Registered for STorM32 gimbal controller |
+| MAV_TUNNEL_PAYLOAD_TYPE_STORM32_RESERVED3 | `uint8` | 203 | Registered for STorM32 gimbal controller |
+| MAV_TUNNEL_PAYLOAD_TYPE_STORM32_RESERVED4 | `uint8` | 204 | Registered for STorM32 gimbal controller |
+| MAV_TUNNEL_PAYLOAD_TYPE_STORM32_RESERVED5 | `uint8` | 205 | Registered for STorM32 gimbal controller |
+| MAV_TUNNEL_PAYLOAD_TYPE_STORM32_RESERVED6 | `uint8` | 206 | Registered for STorM32 gimbal controller |
+| MAV_TUNNEL_PAYLOAD_TYPE_STORM32_RESERVED7 | `uint8` | 207 | Registered for STorM32 gimbal controller |
+| MAV_TUNNEL_PAYLOAD_TYPE_STORM32_RESERVED8 | `uint8` | 208 | Registered for STorM32 gimbal controller |
+| MAV_TUNNEL_PAYLOAD_TYPE_STORM32_RESERVED9 | `uint8` | 209 | Registered for STorM32 gimbal controller |
## Source Message
diff --git a/docs/ko/msg_docs/MessageFormatRequest.md b/docs/ko/msg_docs/MessageFormatRequest.md
index e79150861c..681b66e3a8 100644
--- a/docs/ko/msg_docs/MessageFormatRequest.md
+++ b/docs/ko/msg_docs/MessageFormatRequest.md
@@ -4,7 +4,7 @@ pageClass: is-wide-page
# MessageFormatRequest (UORB message)
-**TOPICS:** message_formatrequest
+**TOPICS:** message_format_request
## Fields
@@ -16,9 +16,9 @@ pageClass: is-wide-page
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| --------------------------------------------------------------------------------------------------------- | -------- | ----- | --------------------------------------------------------------------------------------------------------------------------------------------------- |
-| LATEST_PROTOCOL_VERSION | `uint16` | 1 | Current version of this protocol. Increase this whenever the MessageFormatRequest or MessageFormatResponse changes. |
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------------------------------------------------- | -------- | ----- | --------------------------------------------------------------------------------------------------------------------------------------------------- |
+| LATEST_PROTOCOL_VERSION | `uint16` | 1 | Current version of this protocol. Increase this whenever the MessageFormatRequest or MessageFormatResponse changes. |
## Source Message
diff --git a/docs/ko/msg_docs/MessageFormatResponse.md b/docs/ko/msg_docs/MessageFormatResponse.md
index dab3670a29..17863ee66f 100644
--- a/docs/ko/msg_docs/MessageFormatResponse.md
+++ b/docs/ko/msg_docs/MessageFormatResponse.md
@@ -4,7 +4,7 @@ pageClass: is-wide-page
# MessageFormatResponse (UORB message)
-**TOPICS:** message_formatresponse
+**TOPICS:** message_format_response
## Fields
diff --git a/docs/ko/msg_docs/ModeCompleted.md b/docs/ko/msg_docs/ModeCompleted.md
index 612c19d953..fc8b13d529 100644
--- a/docs/ko/msg_docs/ModeCompleted.md
+++ b/docs/ko/msg_docs/ModeCompleted.md
@@ -18,11 +18,11 @@ Mode completion result, published by an active mode. The possible values of nav_
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| --------------------------------------------------------------------------------------------------- | -------- | ----- | ---------------------------------------------- |
-| MESSAGE_VERSION | `uint32` | 0 | |
-| RESULT_SUCCESS | `uint8` | 0 | |
-| RESULT_FAILURE_OTHER | `uint8` | 100 | Mode failed (generic error) |
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------------------------------------------- | -------- | ----- | ---------------------------------------------- |
+| MESSAGE_VERSION | `uint32` | 0 | |
+| RESULT_SUCCESS | `uint8` | 0 | |
+| RESULT_FAILURE_OTHER | `uint8` | 100 | Mode failed (generic error) |
## Source Message
diff --git a/docs/ko/msg_docs/NavigatorMissionItem.md b/docs/ko/msg_docs/NavigatorMissionItem.md
index 93e9bd7529..99c3d690c7 100644
--- a/docs/ko/msg_docs/NavigatorMissionItem.md
+++ b/docs/ko/msg_docs/NavigatorMissionItem.md
@@ -4,7 +4,7 @@ pageClass: is-wide-page
# NavigatorMissionItem (UORB message)
-**TOPICS:** navigator_missionitem
+**TOPICS:** navigator_mission_item
## Fields
diff --git a/docs/ko/msg_docs/NavigatorStatus.md b/docs/ko/msg_docs/NavigatorStatus.md
index 88f7cd48de..728abc7e18 100644
--- a/docs/ko/msg_docs/NavigatorStatus.md
+++ b/docs/ko/msg_docs/NavigatorStatus.md
@@ -18,10 +18,10 @@ Current status of a Navigator mode. The possible values of nav_state are defined
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| -------------------------------------------------------------- | ------- | ----- | --------------------------------------------------- |
-| FAILURE_NONE | `uint8` | 0 | |
-| FAILURE_HAGL | `uint8` | 1 | Target altitude exceeds maximum height above ground |
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------ | ------- | ----- | --------------------------------------------------- |
+| FAILURE_NONE | `uint8` | 0 | |
+| FAILURE_HAGL | `uint8` | 1 | Target altitude exceeds maximum height above ground |
## Source Message
diff --git a/docs/ko/msg_docs/ObstacleDistance.md b/docs/ko/msg_docs/ObstacleDistance.md
index af0fa0246a..a1e6dfbd58 100644
--- a/docs/ko/msg_docs/ObstacleDistance.md
+++ b/docs/ko/msg_docs/ObstacleDistance.md
@@ -23,15 +23,15 @@ Obstacle distances in front of the sensor.
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| -------------------------------------------------------------------------------------------------------------------------------------------- | ------- | ----- | -- |
-| MAV_FRAME_GLOBAL | `uint8` | 0 | |
-| MAV_FRAME_LOCAL_NED | `uint8` | 1 | |
-| MAV_FRAME_BODY_FRD | `uint8` | 12 | |
-| MAV_DISTANCE_SENSOR_LASER | `uint8` | 0 | |
-| MAV_DISTANCE_SENSOR_ULTRASOUND | `uint8` | 1 | |
-| MAV_DISTANCE_SENSOR_INFRARED | `uint8` | 2 | |
-| MAV_DISTANCE_SENSOR_RADAR | `uint8` | 3 | |
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------------------------------------------------------------------------------------ | ------- | ----- | -- |
+| MAV_FRAME_GLOBAL | `uint8` | 0 | |
+| MAV_FRAME_LOCAL_NED | `uint8` | 1 | |
+| MAV_FRAME_BODY_FRD | `uint8` | 12 | |
+| MAV_DISTANCE_SENSOR_LASER | `uint8` | 0 | |
+| MAV_DISTANCE_SENSOR_ULTRASOUND | `uint8` | 1 | |
+| MAV_DISTANCE_SENSOR_INFRARED | `uint8` | 2 | |
+| MAV_DISTANCE_SENSOR_RADAR | `uint8` | 3 | |
## Source Message
diff --git a/docs/ko/msg_docs/OffboardControlMode.md b/docs/ko/msg_docs/OffboardControlMode.md
index ebb818ef90..117ff4654b 100644
--- a/docs/ko/msg_docs/OffboardControlMode.md
+++ b/docs/ko/msg_docs/OffboardControlMode.md
@@ -6,7 +6,7 @@ pageClass: is-wide-page
Off-board control mode.
-**TOPICS:** offboard_controlmode
+**TOPICS:** offboard_control_mode
## Fields
diff --git a/docs/ko/msg_docs/OnboardComputerStatus.md b/docs/ko/msg_docs/OnboardComputerStatus.md
index faf2732f7a..5d7b7aeacb 100644
--- a/docs/ko/msg_docs/OnboardComputerStatus.md
+++ b/docs/ko/msg_docs/OnboardComputerStatus.md
@@ -6,7 +6,7 @@ pageClass: is-wide-page
ONBOARD_COMPUTER_STATUS message data.
-**TOPICS:** onboard_computerstatus
+**TOPICS:** onboard_computer_status
## Fields
diff --git a/docs/ko/msg_docs/OpenDroneIdArmStatus.md b/docs/ko/msg_docs/OpenDroneIdArmStatus.md
index 85005cc985..8a0ff3861f 100644
--- a/docs/ko/msg_docs/OpenDroneIdArmStatus.md
+++ b/docs/ko/msg_docs/OpenDroneIdArmStatus.md
@@ -4,7 +4,7 @@ pageClass: is-wide-page
# OpenDroneIdArmStatus (UORB message)
-**TOPICS:** open_droneid_armstatus
+**TOPICS:** open_drone_id_arm_status
## Fields
diff --git a/docs/ko/msg_docs/OpenDroneIdOperatorId.md b/docs/ko/msg_docs/OpenDroneIdOperatorId.md
index e1a879b49e..0058e86f19 100644
--- a/docs/ko/msg_docs/OpenDroneIdOperatorId.md
+++ b/docs/ko/msg_docs/OpenDroneIdOperatorId.md
@@ -4,7 +4,7 @@ pageClass: is-wide-page
# OpenDroneIdOperatorId (UORB message)
-**TOPICS:** open_droneid_operatorid
+**TOPICS:** open_drone_id_operator_id
## Fields
diff --git a/docs/ko/msg_docs/OpenDroneIdSelfId.md b/docs/ko/msg_docs/OpenDroneIdSelfId.md
index 4c20d7a368..0b2d6a9a97 100644
--- a/docs/ko/msg_docs/OpenDroneIdSelfId.md
+++ b/docs/ko/msg_docs/OpenDroneIdSelfId.md
@@ -4,7 +4,7 @@ pageClass: is-wide-page
# OpenDroneIdSelfId (UORB message)
-**TOPICS:** open_droneid_selfid
+**TOPICS:** open_drone_id_self_id
## Fields
diff --git a/docs/ko/msg_docs/OpenDroneIdSystem.md b/docs/ko/msg_docs/OpenDroneIdSystem.md
index 7e92821350..7ddb668dfd 100644
--- a/docs/ko/msg_docs/OpenDroneIdSystem.md
+++ b/docs/ko/msg_docs/OpenDroneIdSystem.md
@@ -4,7 +4,7 @@ pageClass: is-wide-page
# OpenDroneIdSystem (UORB message)
-**TOPICS:** open_droneid_system
+**TOPICS:** open_drone_id_system
## Fields
diff --git a/docs/ko/msg_docs/OrbTestLarge.md b/docs/ko/msg_docs/OrbTestLarge.md
index ad59a33640..78474280d1 100644
--- a/docs/ko/msg_docs/OrbTestLarge.md
+++ b/docs/ko/msg_docs/OrbTestLarge.md
@@ -4,7 +4,7 @@ pageClass: is-wide-page
# OrbTestLarge (UORB message)
-**TOPICS:** orb_testlarge
+**TOPICS:** orb_test_large
## Fields
diff --git a/docs/ko/msg_docs/OrbTestMedium.md b/docs/ko/msg_docs/OrbTestMedium.md
index 8e7aaf27c3..a7dbf4264f 100644
--- a/docs/ko/msg_docs/OrbTestMedium.md
+++ b/docs/ko/msg_docs/OrbTestMedium.md
@@ -16,9 +16,9 @@ pageClass: is-wide-page
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ------------------------------------------------------------------------------------------- | ------- | ----- | -- |
-| ORB_QUEUE_LENGTH | `uint8` | 16 | |
+| 명칭 | 형식 | Value | 설명 |
+| ----------------------------------------------------------------------------------------- | ------- | ----- | -- |
+| ORB_QUEUE_LENGTH | `uint8` | 16 | |
## Source Message
diff --git a/docs/ko/msg_docs/OrbitStatus.md b/docs/ko/msg_docs/OrbitStatus.md
index 4273d7f627..262110a341 100644
--- a/docs/ko/msg_docs/OrbitStatus.md
+++ b/docs/ko/msg_docs/OrbitStatus.md
@@ -22,14 +22,14 @@ ORBIT_YAW_BEHAVIOUR.
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- | ------- | ----- | -- |
-| ORBIT_YAW_BEHAVIOUR_HOLD_FRONT_TO_CIRCLE_CENTER | `uint8` | 0 | |
-| ORBIT_YAW_BEHAVIOUR_HOLD_INITIAL_HEADING | `uint8` | 1 | |
-| ORBIT_YAW_BEHAVIOUR_UNCONTROLLED | `uint8` | 2 | |
-| ORBIT_YAW_BEHAVIOUR_HOLD_FRONT_TANGENT_TO_CIRCLE | `uint8` | 3 | |
-| ORBIT_YAW_BEHAVIOUR_RC_CONTROLLED | `uint8` | 4 | |
-| ORBIT_YAW_BEHAVIOUR_UNCHANGED | `uint8` | 5 | |
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ | ------- | ----- | -- |
+| ORBIT_YAW_BEHAVIOUR_HOLD_FRONT_TO_CIRCLE_CENTER | `uint8` | 0 | |
+| ORBIT_YAW_BEHAVIOUR_HOLD_INITIAL_HEADING | `uint8` | 1 | |
+| ORBIT_YAW_BEHAVIOUR_UNCONTROLLED | `uint8` | 2 | |
+| ORBIT_YAW_BEHAVIOUR_HOLD_FRONT_TANGENT_TO_CIRCLE | `uint8` | 3 | |
+| ORBIT_YAW_BEHAVIOUR_RC_CONTROLLED | `uint8` | 4 | |
+| ORBIT_YAW_BEHAVIOUR_UNCHANGED | `uint8` | 5 | |
## Source Message
diff --git a/docs/ko/msg_docs/ParameterResetRequest.md b/docs/ko/msg_docs/ParameterResetRequest.md
index f945088419..2b531e50c9 100644
--- a/docs/ko/msg_docs/ParameterResetRequest.md
+++ b/docs/ko/msg_docs/ParameterResetRequest.md
@@ -6,7 +6,7 @@ pageClass: is-wide-page
ParameterResetRequest : Used by the primary to reset one or all parameter value(s) on the remote.
-**TOPICS:** parameter_resetrequest
+**TOPICS:** parameter_reset_request
## Fields
@@ -18,9 +18,9 @@ ParameterResetRequest : Used by the primary to reset one or all parameter value(
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ------------------------------------------------------------------------------------------- | ------- | ----- | -- |
-| ORB_QUEUE_LENGTH | `uint8` | 4 | |
+| 명칭 | 형식 | Value | 설명 |
+| ----------------------------------------------------------------------------------------- | ------- | ----- | -- |
+| ORB_QUEUE_LENGTH | `uint8` | 4 | |
## Source Message
diff --git a/docs/ko/msg_docs/ParameterSetUsedRequest.md b/docs/ko/msg_docs/ParameterSetUsedRequest.md
index 1539fa0b2e..5f861b0daa 100644
--- a/docs/ko/msg_docs/ParameterSetUsedRequest.md
+++ b/docs/ko/msg_docs/ParameterSetUsedRequest.md
@@ -6,7 +6,7 @@ pageClass: is-wide-page
ParameterSetUsedRequest : Used by a remote to update the used flag for a parameter on the primary.
-**TOPICS:** parameter_setused_request
+**TOPICS:** parameter_set_used_request
## Fields
@@ -17,9 +17,9 @@ ParameterSetUsedRequest : Used by a remote to update the used flag for a paramet
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ------------------------------------------------------------------------------------------- | ------- | ----- | -- |
-| ORB_QUEUE_LENGTH | `uint8` | 64 | |
+| 명칭 | 형식 | Value | 설명 |
+| ----------------------------------------------------------------------------------------- | ------- | ----- | -- |
+| ORB_QUEUE_LENGTH | `uint8` | 64 | |
## Source Message
diff --git a/docs/ko/msg_docs/ParameterSetValueRequest.md b/docs/ko/msg_docs/ParameterSetValueRequest.md
index 3a405780ef..e2edc67d89 100644
--- a/docs/ko/msg_docs/ParameterSetValueRequest.md
+++ b/docs/ko/msg_docs/ParameterSetValueRequest.md
@@ -19,9 +19,9 @@ ParameterSetValueRequest : Used by a remote or primary to update the value for a
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ------------------------------------------------------------------------------------------- | ------- | ----- | -- |
-| ORB_QUEUE_LENGTH | `uint8` | 32 | |
+| 명칭 | 형식 | Value | 설명 |
+| ----------------------------------------------------------------------------------------- | ------- | ----- | -- |
+| ORB_QUEUE_LENGTH | `uint8` | 32 | |
## Source Message
diff --git a/docs/ko/msg_docs/ParameterSetValueResponse.md b/docs/ko/msg_docs/ParameterSetValueResponse.md
index da1392e540..79bfa010bf 100644
--- a/docs/ko/msg_docs/ParameterSetValueResponse.md
+++ b/docs/ko/msg_docs/ParameterSetValueResponse.md
@@ -18,9 +18,9 @@ ParameterSetValueResponse : Response to a set value request by either primary or
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ------------------------------------------------------------------------------------------- | ------- | ----- | -- |
-| ORB_QUEUE_LENGTH | `uint8` | 4 | |
+| 명칭 | 형식 | Value | 설명 |
+| ----------------------------------------------------------------------------------------- | ------- | ----- | -- |
+| ORB_QUEUE_LENGTH | `uint8` | 4 | |
## Source Message
diff --git a/docs/ko/msg_docs/PositionControllerLandingStatus.md b/docs/ko/msg_docs/PositionControllerLandingStatus.md
index f91a4d7514..88d7bd4f35 100644
--- a/docs/ko/msg_docs/PositionControllerLandingStatus.md
+++ b/docs/ko/msg_docs/PositionControllerLandingStatus.md
@@ -4,7 +4,7 @@ pageClass: is-wide-page
# PositionControllerLandingStatus (UORB message)
-**TOPICS:** position_controllerlanding_status
+**TOPICS:** position_controller_landing_status
## Fields
@@ -17,13 +17,13 @@ pageClass: is-wide-page
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| --------------------------------------------------------------------------------------------------------- | ------- | ----- | ------------------------------------------------------------------------------------------------------------------------------------ |
-| NOT_ABORTED | `uint8` | 0 | |
-| ABORTED_BY_OPERATOR | `uint8` | 1 | |
-| TERRAIN_NOT_FOUND | `uint8` | 2 | FW_LND_ABORT (1 << 0) |
-| TERRAIN_TIMEOUT | `uint8` | 3 | FW_LND_ABORT (1 << 1) |
-| UNKNOWN_ABORT_CRITERION | `uint8` | 4 | |
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------------------------------------------------- | ------- | ----- | ------------------------------------------------------------------------------------------------------------------------------------ |
+| NOT_ABORTED | `uint8` | 0 | |
+| ABORTED_BY_OPERATOR | `uint8` | 1 | |
+| TERRAIN_NOT_FOUND | `uint8` | 2 | FW_LND_ABORT (1 << 0) |
+| TERRAIN_TIMEOUT | `uint8` | 3 | FW_LND_ABORT (1 << 1) |
+| UNKNOWN_ABORT_CRITERION | `uint8` | 4 | |
## Source Message
diff --git a/docs/ko/msg_docs/PositionControllerStatus.md b/docs/ko/msg_docs/PositionControllerStatus.md
index 3b7dd545d9..8ad453a08a 100644
--- a/docs/ko/msg_docs/PositionControllerStatus.md
+++ b/docs/ko/msg_docs/PositionControllerStatus.md
@@ -4,7 +4,7 @@ pageClass: is-wide-page
# PositionControllerStatus (UORB message)
-**TOPICS:** position_controllerstatus
+**TOPICS:** position_controller_status
## Fields
diff --git a/docs/ko/msg_docs/PositionSetpoint.md b/docs/ko/msg_docs/PositionSetpoint.md
index a00b37083c..cfde088fe8 100644
--- a/docs/ko/msg_docs/PositionSetpoint.md
+++ b/docs/ko/msg_docs/PositionSetpoint.md
@@ -35,16 +35,16 @@ this file is only used in the position_setpoint triple as a dependency.
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| --------------------------------------------------------------------------------------------------------- | ------- | ----- | --------------------------------------------------------------------------- |
-| SETPOINT_TYPE_POSITION | `uint8` | 0 | position setpoint |
-| SETPOINT_TYPE_VELOCITY | `uint8` | 1 | velocity setpoint |
-| SETPOINT_TYPE_LOITER | `uint8` | 2 | loiter setpoint |
-| SETPOINT_TYPE_TAKEOFF | `uint8` | 3 | takeoff setpoint |
-| SETPOINT_TYPE_LAND | `uint8` | 4 | land setpoint, altitude must be ignored, descend until landing |
-| SETPOINT_TYPE_IDLE | `uint8` | 5 | do nothing, switch off motors or keep at idle speed (MC) |
-| LOITER_TYPE_ORBIT | `uint8` | 0 | Circular pattern |
-| LOITER_TYPE_FIGUREEIGHT | `uint8` | 1 | Pattern resembling an 8 |
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------------------------------------------------- | ------- | ----- | --------------------------------------------------------------------------- |
+| SETPOINT_TYPE_POSITION | `uint8` | 0 | position setpoint |
+| SETPOINT_TYPE_VELOCITY | `uint8` | 1 | velocity setpoint |
+| SETPOINT_TYPE_LOITER | `uint8` | 2 | loiter setpoint |
+| SETPOINT_TYPE_TAKEOFF | `uint8` | 3 | takeoff setpoint |
+| SETPOINT_TYPE_LAND | `uint8` | 4 | land setpoint, altitude must be ignored, descend until landing |
+| SETPOINT_TYPE_IDLE | `uint8` | 5 | do nothing, switch off motors or keep at idle speed (MC) |
+| LOITER_TYPE_ORBIT | `uint8` | 0 | Circular pattern |
+| LOITER_TYPE_FIGUREEIGHT | `uint8` | 1 | Pattern resembling an 8 |
## Source Message
diff --git a/docs/ko/msg_docs/PositionSetpointTriplet.md b/docs/ko/msg_docs/PositionSetpointTriplet.md
index 52762394aa..4c9b7935d8 100644
--- a/docs/ko/msg_docs/PositionSetpointTriplet.md
+++ b/docs/ko/msg_docs/PositionSetpointTriplet.md
@@ -6,7 +6,7 @@ pageClass: is-wide-page
Global position setpoint triplet in WGS84 coordinates. This are the three next waypoints (or just the next two or one).
-**TOPICS:** position_setpointtriplet
+**TOPICS:** position_setpoint_triplet
## Fields
diff --git a/docs/ko/msg_docs/PowerButtonState.md b/docs/ko/msg_docs/PowerButtonState.md
index a28a40261c..473e9baf4d 100644
--- a/docs/ko/msg_docs/PowerButtonState.md
+++ b/docs/ko/msg_docs/PowerButtonState.md
@@ -6,7 +6,7 @@ pageClass: is-wide-page
power button state notification message.
-**TOPICS:** power_buttonstate
+**TOPICS:** power_button_state
## Fields
@@ -17,12 +17,12 @@ power button state notification message.
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ----------------------------------------------------------------------------------------------------------------------------------------------------------------------- | ------- | ----- | ------------------------------------------------------------------------------------------ |
-| PWR_BUTTON_STATE_IDEL | `uint8` | 0 | Button went up without meeting shutdown button down time (delete event) |
-| PWR_BUTTON_STATE_DOWN | `uint8` | 1 | Button went Down |
-| PWR_BUTTON_STATE_UP | `uint8` | 2 | Button went Up |
-| PWR_BUTTON_STATE_REQUEST_SHUTDOWN | `uint8` | 3 | Button went Up after meeting shutdown button down time |
+| 명칭 | 형식 | Value | 설명 |
+| --------------------------------------------------------------------------------------------------------------------------------------------------------------------- | ------- | ----- | ------------------------------------------------------------------------------------------ |
+| PWR_BUTTON_STATE_IDEL | `uint8` | 0 | Button went up without meeting shutdown button down time (delete event) |
+| PWR_BUTTON_STATE_DOWN | `uint8` | 1 | Button went Down |
+| PWR_BUTTON_STATE_UP | `uint8` | 2 | Button went Up |
+| PWR_BUTTON_STATE_REQUEST_SHUTDOWN | `uint8` | 3 | Button went Up after meeting shutdown button down time |
## Source Message
diff --git a/docs/ko/msg_docs/PurePursuitStatus.md b/docs/ko/msg_docs/PurePursuitStatus.md
index b099125813..efa799de5a 100644
--- a/docs/ko/msg_docs/PurePursuitStatus.md
+++ b/docs/ko/msg_docs/PurePursuitStatus.md
@@ -6,7 +6,7 @@ pageClass: is-wide-page
Pure pursuit status.
-**TOPICS:** pure_pursuitstatus
+**TOPICS:** pure_pursuit_status
## Fields
diff --git a/docs/ko/msg_docs/QshellReq.md b/docs/ko/msg_docs/QshellReq.md
index 451f900693..63857b04f5 100644
--- a/docs/ko/msg_docs/QshellReq.md
+++ b/docs/ko/msg_docs/QshellReq.md
@@ -17,9 +17,9 @@ pageClass: is-wide-page
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ---------------------------------------------------------- | -------- | ----- | -- |
-| MAX_STRLEN | `uint32` | 100 | |
+| 명칭 | 형식 | Value | 설명 |
+| -------------------------------------------------------- | -------- | ----- | -- |
+| MAX_STRLEN | `uint32` | 100 | |
## Source Message
diff --git a/docs/ko/msg_docs/RaptorInput.md b/docs/ko/msg_docs/RaptorInput.md
index 7089aae299..da312ff72f 100644
--- a/docs/ko/msg_docs/RaptorInput.md
+++ b/docs/ko/msg_docs/RaptorInput.md
@@ -23,10 +23,10 @@ Raptor Input.
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| -------------------------------------------------------------------- | -------- | ----- | ---------------------------------------------------------------- |
-| MESSAGE_VERSION | `uint32` | 0 | |
-| ACTION_DIM | `uint8` | 4 | Policy output dimensionality (for quadrotors) |
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------------ | -------- | ----- | ---------------------------------------------------------------- |
+| MESSAGE_VERSION | `uint32` | 0 | |
+| ACTION_DIM | `uint8` | 4 | Policy output dimensionality (for quadrotors) |
## Source Message
diff --git a/docs/ko/msg_docs/RaptorStatus.md b/docs/ko/msg_docs/RaptorStatus.md
index 0325c004db..e2e3c6f5ca 100644
--- a/docs/ko/msg_docs/RaptorStatus.md
+++ b/docs/ko/msg_docs/RaptorStatus.md
@@ -39,16 +39,16 @@ Raptor Status.
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- | -------- | ----- | --------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- |
-| MESSAGE_VERSION | `uint32` | 0 | |
-| EXIT_REASON_NONE | `uint8` | 0 | No exit reason => Raptor control step was executed (actuator_motors should have been published) |
-| EXIT_REASON_NO_ANGULAR_VELOCITY_UPDATE | `uint8` | 1 | We synchronize the control onto the input observation with the highest update frequency, which is vehicle_angular_velocity. If there was no update, we do not need to execute the policy again |
-| EXIT_REASON_NOT_ALL_OBSERVATIONS_SET | `uint8` | 2 | We can not execute the policy if not all observations are available |
-| EXIT_REASON_ANGULAR_VELOCITY_STALE | `uint8` | 3 | If OBSERVATION_TIMEOUT_ANGULAR_VELOCITY is exceeded, we treat the vehicle_angular_velocity as stale and can not run the policy |
-| EXIT_REASON_LOCAL_POSITION_STALE | `uint8` | 4 | If OBSERVATION_TIMEOUT_LOCAL_POSITION is exceeded, we treat the vehicle_local_position as stale and can not run the policy |
-| EXIT_REASON_ATTITUDE_STALE | `uint8` | 5 | If OBSERVATION_TIMEOUT_ATTITUDE is exceeded, we treat the vehicle_attitude as stale and can not run the policy |
-| EXIT_REASON_EXECUTOR_STATUS_SOURCE_NOT_CONTROL | `uint8` | 6 | The executor that runs the policy can run in oversampling mode, where it decides if the policy should be ran based on the timestamp and not based on fixed synchronization onto the vehicle_angular_velocity. In this case the executor can decide to skip running the policy if the interval is too small, in which case this flag is set. |
+| 명칭 | 형식 | Value | 설명 |
+| ----------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- | -------- | ----- | --------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- |
+| MESSAGE_VERSION | `uint32` | 0 | |
+| EXIT_REASON_NONE | `uint8` | 0 | No exit reason => Raptor control step was executed (actuator_motors should have been published) |
+| EXIT_REASON_NO_ANGULAR_VELOCITY_UPDATE | `uint8` | 1 | We synchronize the control onto the input observation with the highest update frequency, which is vehicle_angular_velocity. If there was no update, we do not need to execute the policy again |
+| EXIT_REASON_NOT_ALL_OBSERVATIONS_SET | `uint8` | 2 | We can not execute the policy if not all observations are available |
+| EXIT_REASON_ANGULAR_VELOCITY_STALE | `uint8` | 3 | If OBSERVATION_TIMEOUT_ANGULAR_VELOCITY is exceeded, we treat the vehicle_angular_velocity as stale and can not run the policy |
+| EXIT_REASON_LOCAL_POSITION_STALE | `uint8` | 4 | If OBSERVATION_TIMEOUT_LOCAL_POSITION is exceeded, we treat the vehicle_local_position as stale and can not run the policy |
+| EXIT_REASON_ATTITUDE_STALE | `uint8` | 5 | If OBSERVATION_TIMEOUT_ATTITUDE is exceeded, we treat the vehicle_attitude as stale and can not run the policy |
+| EXIT_REASON_EXECUTOR_STATUS_SOURCE_NOT_CONTROL | `uint8` | 6 | The executor that runs the policy can run in oversampling mode, where it decides if the policy should be ran based on the timestamp and not based on fixed synchronization onto the vehicle_angular_velocity. In this case the executor can decide to skip running the policy if the interval is too small, in which case this flag is set. |
## Source Message
diff --git a/docs/ko/msg_docs/RateCtrlStatus.md b/docs/ko/msg_docs/RateCtrlStatus.md
index 9b297ca4a0..cb7412deef 100644
--- a/docs/ko/msg_docs/RateCtrlStatus.md
+++ b/docs/ko/msg_docs/RateCtrlStatus.md
@@ -4,7 +4,7 @@ pageClass: is-wide-page
# RateCtrlStatus (UORB message)
-**TOPICS:** rate_ctrlstatus
+**TOPICS:** rate_ctrl_status
## Fields
diff --git a/docs/ko/msg_docs/RcChannels.md b/docs/ko/msg_docs/RcChannels.md
index 90baf9744a..80ed6c9fe6 100644
--- a/docs/ko/msg_docs/RcChannels.md
+++ b/docs/ko/msg_docs/RcChannels.md
@@ -21,39 +21,39 @@ pageClass: is-wide-page
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ------------------------------------------------------------------------------------------------------------------------------------ | ------- | ----- | -- |
-| FUNCTION_THROTTLE | `uint8` | 0 | |
-| FUNCTION_ROLL | `uint8` | 1 | |
-| FUNCTION_PITCH | `uint8` | 2 | |
-| FUNCTION_YAW | `uint8` | 3 | |
-| FUNCTION_RETURN | `uint8` | 4 | |
-| FUNCTION_LOITER | `uint8` | 5 | |
-| FUNCTION_OFFBOARD | `uint8` | 6 | |
-| FUNCTION_FLAPS | `uint8` | 7 | |
-| FUNCTION_AUX_1 | `uint8` | 8 | |
-| FUNCTION_AUX_2 | `uint8` | 9 | |
-| FUNCTION_AUX_3 | `uint8` | 10 | |
-| FUNCTION_AUX_4 | `uint8` | 11 | |
-| FUNCTION_AUX_5 | `uint8` | 12 | |
-| FUNCTION_AUX_6 | `uint8` | 13 | |
-| FUNCTION_PARAM_1 | `uint8` | 14 | |
-| FUNCTION_PARAM_2 | `uint8` | 15 | |
-| FUNCTION_PARAM_3_5 | `uint8` | 16 | |
-| FUNCTION_KILLSWITCH | `uint8` | 17 | |
-| FUNCTION_TRANSITION | `uint8` | 18 | |
-| FUNCTION_GEAR | `uint8` | 19 | |
-| FUNCTION_ARMSWITCH | `uint8` | 20 | |
-| FUNCTION_FLTBTN_SLOT_1 | `uint8` | 21 | |
-| FUNCTION_FLTBTN_SLOT_2 | `uint8` | 22 | |
-| FUNCTION_FLTBTN_SLOT_3 | `uint8` | 23 | |
-| FUNCTION_FLTBTN_SLOT_4 | `uint8` | 24 | |
-| FUNCTION_FLTBTN_SLOT_5 | `uint8` | 25 | |
-| FUNCTION_FLTBTN_SLOT_6 | `uint8` | 26 | |
-| FUNCTION_ENGAGE_MAIN_MOTOR | `uint8` | 27 | |
-| FUNCTION_PAYLOAD_POWER | `uint8` | 28 | |
-| FUNCTION_TERMINATION | `uint8` | 29 | |
-| FUNCTION_FLTBTN_SLOT_COUNT | `uint8` | 6 | |
+| 명칭 | 형식 | Value | 설명 |
+| ---------------------------------------------------------------------------------------------------------------------------------- | ------- | ----- | -- |
+| FUNCTION_THROTTLE | `uint8` | 0 | |
+| FUNCTION_ROLL | `uint8` | 1 | |
+| FUNCTION_PITCH | `uint8` | 2 | |
+| FUNCTION_YAW | `uint8` | 3 | |
+| FUNCTION_RETURN | `uint8` | 4 | |
+| FUNCTION_LOITER | `uint8` | 5 | |
+| FUNCTION_OFFBOARD | `uint8` | 6 | |
+| FUNCTION_FLAPS | `uint8` | 7 | |
+| FUNCTION_AUX_1 | `uint8` | 8 | |
+| FUNCTION_AUX_2 | `uint8` | 9 | |
+| FUNCTION_AUX_3 | `uint8` | 10 | |
+| FUNCTION_AUX_4 | `uint8` | 11 | |
+| FUNCTION_AUX_5 | `uint8` | 12 | |
+| FUNCTION_AUX_6 | `uint8` | 13 | |
+| FUNCTION_PARAM_1 | `uint8` | 14 | |
+| FUNCTION_PARAM_2 | `uint8` | 15 | |
+| FUNCTION_PARAM_3_5 | `uint8` | 16 | |
+| FUNCTION_KILLSWITCH | `uint8` | 17 | |
+| FUNCTION_TRANSITION | `uint8` | 18 | |
+| FUNCTION_GEAR | `uint8` | 19 | |
+| FUNCTION_ARMSWITCH | `uint8` | 20 | |
+| FUNCTION_FLTBTN_SLOT_1 | `uint8` | 21 | |
+| FUNCTION_FLTBTN_SLOT_2 | `uint8` | 22 | |
+| FUNCTION_FLTBTN_SLOT_3 | `uint8` | 23 | |
+| FUNCTION_FLTBTN_SLOT_4 | `uint8` | 24 | |
+| FUNCTION_FLTBTN_SLOT_5 | `uint8` | 25 | |
+| FUNCTION_FLTBTN_SLOT_6 | `uint8` | 26 | |
+| FUNCTION_ENGAGE_MAIN_MOTOR | `uint8` | 27 | |
+| FUNCTION_PAYLOAD_POWER | `uint8` | 28 | |
+| FUNCTION_TERMINATION | `uint8` | 29 | |
+| FUNCTION_FLTBTN_SLOT_COUNT | `uint8` | 6 | |
## Source Message
diff --git a/docs/ko/msg_docs/RcParameterMap.md b/docs/ko/msg_docs/RcParameterMap.md
index 52fbfddb41..80a6e91985 100644
--- a/docs/ko/msg_docs/RcParameterMap.md
+++ b/docs/ko/msg_docs/RcParameterMap.md
@@ -4,7 +4,7 @@ pageClass: is-wide-page
# RcParameterMap (UORB message)
-**TOPICS:** rc_parametermap
+**TOPICS:** rc_parameter_map
## Fields
@@ -21,10 +21,10 @@ pageClass: is-wide-page
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| -------------------------------------------------------------------------------------------------------------------- | ------- | ----- | ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ |
-| RC_PARAM_MAP_NCHAN | `uint8` | 3 | This limit is also hardcoded in the enum RC_CHANNELS_FUNCTION in rc_channels.h |
-| PARAM_ID_LEN | `uint8` | 16 | corresponds to MAVLINK_MSG_PARAM_VALUE_FIELD_PARAM_ID_LEN |
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------------------------------------------------------------ | ------- | ----- | ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ |
+| RC_PARAM_MAP_NCHAN | `uint8` | 3 | This limit is also hardcoded in the enum RC_CHANNELS_FUNCTION in rc_channels.h |
+| PARAM_ID_LEN | `uint8` | 16 | corresponds to MAVLINK_MSG_PARAM_VALUE_FIELD_PARAM_ID_LEN |
## Source Message
diff --git a/docs/ko/msg_docs/RegisterExtComponentReply.md b/docs/ko/msg_docs/RegisterExtComponentReply.md
index 0f210ccbef..18e57aee36 100644
--- a/docs/ko/msg_docs/RegisterExtComponentReply.md
+++ b/docs/ko/msg_docs/RegisterExtComponentReply.md
@@ -4,7 +4,7 @@ pageClass: is-wide-page
# RegisterExtComponentReply (UORB message)
-**TOPICS:** register_extcomponent_reply
+**TOPICS:** register_ext_component_reply
## Fields
@@ -22,10 +22,10 @@ pageClass: is-wide-page
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ------------------------------------------------------------------------------------------- | -------- | ----- | -- |
-| MESSAGE_VERSION | `uint32` | 1 | |
-| ORB_QUEUE_LENGTH | `uint8` | 2 | |
+| 명칭 | 형식 | Value | 설명 |
+| ----------------------------------------------------------------------------------------- | -------- | ----- | -- |
+| MESSAGE_VERSION | `uint32` | 1 | |
+| ORB_QUEUE_LENGTH | `uint8` | 2 | |
## Source Message
diff --git a/docs/ko/msg_docs/RegisterExtComponentReplyV0.md b/docs/ko/msg_docs/RegisterExtComponentReplyV0.md
index 3266cff2ce..2d2c8c5de0 100644
--- a/docs/ko/msg_docs/RegisterExtComponentReplyV0.md
+++ b/docs/ko/msg_docs/RegisterExtComponentReplyV0.md
@@ -4,7 +4,7 @@ pageClass: is-wide-page
# RegisterExtComponentReplyV0 (UORB message)
-**TOPICS:** register_extcomponent_replyv0
+**TOPICS:** register_ext_component_reply_v0
## Fields
@@ -21,10 +21,10 @@ pageClass: is-wide-page
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ------------------------------------------------------------------------------------------- | -------- | ----- | -- |
-| MESSAGE_VERSION | `uint32` | 0 | |
-| ORB_QUEUE_LENGTH | `uint8` | 2 | |
+| 명칭 | 형식 | Value | 설명 |
+| ----------------------------------------------------------------------------------------- | -------- | ----- | -- |
+| MESSAGE_VERSION | `uint32` | 0 | |
+| ORB_QUEUE_LENGTH | `uint8` | 2 | |
## Source Message
diff --git a/docs/ko/msg_docs/RegisterExtComponentRequest.md b/docs/ko/msg_docs/RegisterExtComponentRequest.md
index c373dd7477..a08d1a0663 100644
--- a/docs/ko/msg_docs/RegisterExtComponentRequest.md
+++ b/docs/ko/msg_docs/RegisterExtComponentRequest.md
@@ -6,7 +6,7 @@ pageClass: is-wide-page
Request to register an external component.
-**TOPICS:** register_extcomponent_request
+**TOPICS:** register_ext_component_request
## Fields
@@ -26,11 +26,11 @@ Request to register an external component.
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ----------------------------------------------------------------------------------------------------------------------------------------------------------- | -------- | ----- | ---------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- |
-| MESSAGE_VERSION | `uint32` | 1 | |
-| LATEST_PX4_ROS2_API_VERSION | `uint16` | 1 | API version compatibility. Increase this on a breaking semantic change. Changes to any message field are detected separately and do not require an API version change. |
-| ORB_QUEUE_LENGTH | `uint8` | 2 | |
+| 명칭 | 형식 | Value | 설명 |
+| --------------------------------------------------------------------------------------------------------------------------------------------------------- | -------- | ----- | ---------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- |
+| MESSAGE_VERSION | `uint32` | 1 | |
+| LATEST_PX4_ROS2_API_VERSION | `uint16` | 1 | API version compatibility. Increase this on a breaking semantic change. Changes to any message field are detected separately and do not require an API version change. |
+| ORB_QUEUE_LENGTH | `uint8` | 2 | |
## Source Message
diff --git a/docs/ko/msg_docs/RegisterExtComponentRequestV0.md b/docs/ko/msg_docs/RegisterExtComponentRequestV0.md
index ce3700a623..58aa143a68 100644
--- a/docs/ko/msg_docs/RegisterExtComponentRequestV0.md
+++ b/docs/ko/msg_docs/RegisterExtComponentRequestV0.md
@@ -6,7 +6,7 @@ pageClass: is-wide-page
Request to register an external component.
-**TOPICS:** register_extcomponent_requestv0
+**TOPICS:** register_ext_component_request_v0
## Fields
@@ -25,11 +25,11 @@ Request to register an external component.
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ----------------------------------------------------------------------------------------------------------------------------------------------------------- | -------- | ----- | ---------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- |
-| MESSAGE_VERSION | `uint32` | 0 | |
-| LATEST_PX4_ROS2_API_VERSION | `uint16` | 1 | API version compatibility. Increase this on a breaking semantic change. Changes to any message field are detected separately and do not require an API version change. |
-| ORB_QUEUE_LENGTH | `uint8` | 2 | |
+| 명칭 | 형식 | Value | 설명 |
+| --------------------------------------------------------------------------------------------------------------------------------------------------------- | -------- | ----- | ---------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- |
+| MESSAGE_VERSION | `uint32` | 0 | |
+| LATEST_PX4_ROS2_API_VERSION | `uint16` | 1 | API version compatibility. Increase this on a breaking semantic change. Changes to any message field are detected separately and do not require an API version change. |
+| ORB_QUEUE_LENGTH | `uint8` | 2 | |
## Source Message
diff --git a/docs/ko/msg_docs/RoverAttitudeSetpoint.md b/docs/ko/msg_docs/RoverAttitudeSetpoint.md
index 2d6d3c390f..29e99ecc47 100644
--- a/docs/ko/msg_docs/RoverAttitudeSetpoint.md
+++ b/docs/ko/msg_docs/RoverAttitudeSetpoint.md
@@ -6,7 +6,7 @@ pageClass: is-wide-page
Rover Attitude Setpoint.
-**TOPICS:** rover_attitudesetpoint
+**TOPICS:** rover_attitude_setpoint
## Fields
diff --git a/docs/ko/msg_docs/RoverAttitudeStatus.md b/docs/ko/msg_docs/RoverAttitudeStatus.md
index 416d52ec34..aa28a5663a 100644
--- a/docs/ko/msg_docs/RoverAttitudeStatus.md
+++ b/docs/ko/msg_docs/RoverAttitudeStatus.md
@@ -6,7 +6,7 @@ pageClass: is-wide-page
Rover Attitude Status.
-**TOPICS:** rover_attitudestatus
+**TOPICS:** rover_attitude_status
## Fields
diff --git a/docs/ko/msg_docs/RoverPositionSetpoint.md b/docs/ko/msg_docs/RoverPositionSetpoint.md
index 7371a64cc6..8467d51e56 100644
--- a/docs/ko/msg_docs/RoverPositionSetpoint.md
+++ b/docs/ko/msg_docs/RoverPositionSetpoint.md
@@ -6,7 +6,7 @@ pageClass: is-wide-page
Rover Position Setpoint.
-**TOPICS:** rover_positionsetpoint
+**TOPICS:** rover_position_setpoint
## Fields
diff --git a/docs/ko/msg_docs/RoverRateSetpoint.md b/docs/ko/msg_docs/RoverRateSetpoint.md
index 35029e72d3..ff8e3d2d09 100644
--- a/docs/ko/msg_docs/RoverRateSetpoint.md
+++ b/docs/ko/msg_docs/RoverRateSetpoint.md
@@ -6,7 +6,7 @@ pageClass: is-wide-page
Rover Rate setpoint.
-**TOPICS:** rover_ratesetpoint
+**TOPICS:** rover_rate_setpoint
## Fields
diff --git a/docs/ko/msg_docs/RoverRateStatus.md b/docs/ko/msg_docs/RoverRateStatus.md
index 3bd0642d4f..39b608963c 100644
--- a/docs/ko/msg_docs/RoverRateStatus.md
+++ b/docs/ko/msg_docs/RoverRateStatus.md
@@ -6,7 +6,7 @@ pageClass: is-wide-page
Rover Rate Status.
-**TOPICS:** rover_ratestatus
+**TOPICS:** rover_rate_status
## Fields
diff --git a/docs/ko/msg_docs/RoverSpeedSetpoint.md b/docs/ko/msg_docs/RoverSpeedSetpoint.md
index 3c87dda1fe..dfb97f7440 100644
--- a/docs/ko/msg_docs/RoverSpeedSetpoint.md
+++ b/docs/ko/msg_docs/RoverSpeedSetpoint.md
@@ -6,7 +6,7 @@ pageClass: is-wide-page
Rover Speed Setpoint.
-**TOPICS:** rover_speedsetpoint
+**TOPICS:** rover_speed_setpoint
## Fields
diff --git a/docs/ko/msg_docs/RoverSpeedStatus.md b/docs/ko/msg_docs/RoverSpeedStatus.md
index 161c20da43..49e3107e06 100644
--- a/docs/ko/msg_docs/RoverSpeedStatus.md
+++ b/docs/ko/msg_docs/RoverSpeedStatus.md
@@ -6,7 +6,7 @@ pageClass: is-wide-page
Rover Velocity Status.
-**TOPICS:** rover_speedstatus
+**TOPICS:** rover_speed_status
## Fields
diff --git a/docs/ko/msg_docs/RoverSteeringSetpoint.md b/docs/ko/msg_docs/RoverSteeringSetpoint.md
index fb18a4dd08..afe9294e61 100644
--- a/docs/ko/msg_docs/RoverSteeringSetpoint.md
+++ b/docs/ko/msg_docs/RoverSteeringSetpoint.md
@@ -6,7 +6,7 @@ pageClass: is-wide-page
Rover Steering setpoint.
-**TOPICS:** rover_steeringsetpoint
+**TOPICS:** rover_steering_setpoint
## Fields
diff --git a/docs/ko/msg_docs/RoverThrottleSetpoint.md b/docs/ko/msg_docs/RoverThrottleSetpoint.md
index d05660b098..052eadcbc1 100644
--- a/docs/ko/msg_docs/RoverThrottleSetpoint.md
+++ b/docs/ko/msg_docs/RoverThrottleSetpoint.md
@@ -6,7 +6,7 @@ pageClass: is-wide-page
Rover Throttle setpoint.
-**TOPICS:** rover_throttlesetpoint
+**TOPICS:** rover_throttle_setpoint
## Fields
diff --git a/docs/ko/msg_docs/RtlStatus.md b/docs/ko/msg_docs/RtlStatus.md
index b2937a5a61..77a19112a2 100644
--- a/docs/ko/msg_docs/RtlStatus.md
+++ b/docs/ko/msg_docs/RtlStatus.md
@@ -19,13 +19,13 @@ pageClass: is-wide-page
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ | ------- | ----- | ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- |
-| RTL_STATUS_TYPE_NONE | `uint8` | 0 | pending if evaluation can't pe performed currently e.g. when it is still loading the safe points |
-| RTL_STATUS_TYPE_DIRECT_SAFE_POINT | `uint8` | 1 | chosen to directly go to a safe point or home position |
-| RTL_STATUS_TYPE_DIRECT_MISSION_LAND | `uint8` | 2 | going straight to the beginning of the mission landing |
-| RTL_STATUS_TYPE_FOLLOW_MISSION | `uint8` | 3 | Following the mission from start index to mission landing. Start index is current WP if in Mission mode, and closest WP otherwise. |
-| RTL_STATUS_TYPE_FOLLOW_MISSION_REVERSE | `uint8` | 4 | Following the mission in reverse from start index to the beginning of the mission. Start index is previous WP if in Mission mode, and closest WP otherwise. |
+| 명칭 | 형식 | Value | 설명 |
+| ---------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- | ------- | ----- | ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- |
+| RTL_STATUS_TYPE_NONE | `uint8` | 0 | pending if evaluation can't pe performed currently e.g. when it is still loading the safe points |
+| RTL_STATUS_TYPE_DIRECT_SAFE_POINT | `uint8` | 1 | chosen to directly go to a safe point or home position |
+| RTL_STATUS_TYPE_DIRECT_MISSION_LAND | `uint8` | 2 | going straight to the beginning of the mission landing |
+| RTL_STATUS_TYPE_FOLLOW_MISSION | `uint8` | 3 | Following the mission from start index to mission landing. Start index is current WP if in Mission mode, and closest WP otherwise. |
+| RTL_STATUS_TYPE_FOLLOW_MISSION_REVERSE | `uint8` | 4 | Following the mission in reverse from start index to the beginning of the mission. Start index is previous WP if in Mission mode, and closest WP otherwise. |
## Source Message
diff --git a/docs/ko/msg_docs/RtlTimeEstimate.md b/docs/ko/msg_docs/RtlTimeEstimate.md
index 640008a18e..f71a30f333 100644
--- a/docs/ko/msg_docs/RtlTimeEstimate.md
+++ b/docs/ko/msg_docs/RtlTimeEstimate.md
@@ -4,7 +4,7 @@ pageClass: is-wide-page
# RtlTimeEstimate (UORB message)
-**TOPICS:** rtl_timeestimate
+**TOPICS:** rtl_time_estimate
## Fields
diff --git a/docs/ko/msg_docs/SatelliteInfo.md b/docs/ko/msg_docs/SatelliteInfo.md
index 244068aee3..0f889eac3b 100644
--- a/docs/ko/msg_docs/SatelliteInfo.md
+++ b/docs/ko/msg_docs/SatelliteInfo.md
@@ -21,9 +21,9 @@ pageClass: is-wide-page
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ------------------------------------------------------------------------------------------------------------------------------ | ------- | ----- | -- |
-| SAT_INFO_MAX_SATELLITES | `uint8` | 40 | |
+| 명칭 | 형식 | Value | 설명 |
+| ---------------------------------------------------------------------------------------------------------------------------- | ------- | ----- | -- |
+| SAT_INFO_MAX_SATELLITES | `uint8` | 40 | |
## Source Message
diff --git a/docs/ko/msg_docs/SensorAccel.md b/docs/ko/msg_docs/SensorAccel.md
index e73dd5b593..fa8ce793fa 100644
--- a/docs/ko/msg_docs/SensorAccel.md
+++ b/docs/ko/msg_docs/SensorAccel.md
@@ -23,9 +23,9 @@ pageClass: is-wide-page
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ------------------------------------------------------------------------------------------- | ------- | ----- | -- |
-| ORB_QUEUE_LENGTH | `uint8` | 8 | |
+| 명칭 | 형식 | Value | 설명 |
+| ----------------------------------------------------------------------------------------- | ------- | ----- | -- |
+| ORB_QUEUE_LENGTH | `uint8` | 8 | |
## Source Message
diff --git a/docs/ko/msg_docs/SensorAccelFifo.md b/docs/ko/msg_docs/SensorAccelFifo.md
index 210582255b..37066f8488 100644
--- a/docs/ko/msg_docs/SensorAccelFifo.md
+++ b/docs/ko/msg_docs/SensorAccelFifo.md
@@ -4,7 +4,7 @@ pageClass: is-wide-page
# SensorAccelFifo (UORB message)
-**TOPICS:** sensor_accelfifo
+**TOPICS:** sensor_accel_fifo
## Fields
diff --git a/docs/ko/msg_docs/SensorBaro.md b/docs/ko/msg_docs/SensorBaro.md
index 5ab06a270a..16ca8c4ffd 100644
--- a/docs/ko/msg_docs/SensorBaro.md
+++ b/docs/ko/msg_docs/SensorBaro.md
@@ -24,9 +24,9 @@ The information is published in the `SCALED_PRESSURE_n` MAVLink messages (along
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ------------------------------------------------------------------------------------------- | ------- | ----- | -- |
-| ORB_QUEUE_LENGTH | `uint8` | 4 | |
+| 명칭 | 형식 | Value | 설명 |
+| ----------------------------------------------------------------------------------------- | ------- | ----- | -- |
+| ORB_QUEUE_LENGTH | `uint8` | 4 | |
## Source Message
diff --git a/docs/ko/msg_docs/SensorCombined.md b/docs/ko/msg_docs/SensorCombined.md
index bcadd24a73..8c243c1cb3 100644
--- a/docs/ko/msg_docs/SensorCombined.md
+++ b/docs/ko/msg_docs/SensorCombined.md
@@ -25,12 +25,12 @@ Sensor readings in SI-unit form. These fields are scaled and offset-compensated
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| --------------------------------------------------------------------------------------------------------------- | ------- | ---------- | ----------------------------------------------------------------------------------------------------------------------------------------- |
-| RELATIVE_TIMESTAMP_INVALID | `int32` | 2147483647 | (0x7fffffff) If one of the relative timestamps is set to this value, it means the associated sensor values are invalid |
-| CLIPPING_X | `uint8` | 1 | |
-| CLIPPING_Y | `uint8` | 2 | |
-| CLIPPING_Z | `uint8` | 4 | |
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------------------------------------------------------- | ------- | ---------- | ----------------------------------------------------------------------------------------------------------------------------------------- |
+| RELATIVE_TIMESTAMP_INVALID | `int32` | 2147483647 | (0x7fffffff) If one of the relative timestamps is set to this value, it means the associated sensor values are invalid |
+| CLIPPING_X | `uint8` | 1 | |
+| CLIPPING_Y | `uint8` | 2 | |
+| CLIPPING_Z | `uint8` | 4 | |
## Source Message
diff --git a/docs/ko/msg_docs/SensorGnssRelative.md b/docs/ko/msg_docs/SensorGnssRelative.md
index 0fea3a7b92..1d7f9d42a4 100644
--- a/docs/ko/msg_docs/SensorGnssRelative.md
+++ b/docs/ko/msg_docs/SensorGnssRelative.md
@@ -6,7 +6,7 @@ pageClass: is-wide-page
GNSS relative positioning information in NED frame. The NED frame is defined as the local topological system at the reference station.
-**TOPICS:** sensor_gnssrelative
+**TOPICS:** sensor_gnss_relative
## Fields
diff --git a/docs/ko/msg_docs/SensorGnssStatus.md b/docs/ko/msg_docs/SensorGnssStatus.md
index a0392d9293..bf273d74e9 100644
--- a/docs/ko/msg_docs/SensorGnssStatus.md
+++ b/docs/ko/msg_docs/SensorGnssStatus.md
@@ -6,7 +6,7 @@ pageClass: is-wide-page
Gnss quality indicators.
-**TOPICS:** sensor_gnssstatus
+**TOPICS:** sensor_gnss_status
## Fields
diff --git a/docs/ko/msg_docs/SensorGps.md b/docs/ko/msg_docs/SensorGps.md
index 895a60e8f0..4c30353dbf 100644
--- a/docs/ko/msg_docs/SensorGps.md
+++ b/docs/ko/msg_docs/SensorGps.md
@@ -52,39 +52,39 @@ GPS position in WGS84 coordinates. the field 'timestamp' is for the position & v
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ------------------------------------------------------------------------------------------------------------------------------------------------------------------- | -------- | ----- | ---------------------------------------------------------- |
-| FIX_TYPE_NONE | `uint8` | 1 | Value 0 is also valid to represent no fix. |
-| FIX_TYPE_2D | `uint8` | 2 | |
-| FIX_TYPE_3D | `uint8` | 3 | |
-| FIX_TYPE_RTCM_CODE_DIFFERENTIAL | `uint8` | 4 | |
-| FIX_TYPE_RTK_FLOAT | `uint8` | 5 | |
-| FIX_TYPE_RTK_FIXED | `uint8` | 6 | |
-| FIX_TYPE_EXTRAPOLATED | `uint8` | 8 | |
-| JAMMING_STATE_UNKNOWN | `uint8` | 0 | default |
-| JAMMING_STATE_OK | `uint8` | 1 | |
-| JAMMING_STATE_MITIGATED | `uint8` | 2 | |
-| JAMMING_STATE_DETECTED | `uint8` | 3 | |
-| SPOOFING_STATE_UNKNOWN | `uint8` | 0 | default |
-| SPOOFING_STATE_OK | `uint8` | 1 | |
-| SPOOFING_STATE_MITIGATED | `uint8` | 2 | |
-| SPOOFING_STATE_DETECTED | `uint8` | 3 | |
-| AUTHENTICATION_STATE_UNKNOWN | `uint8` | 0 | default |
-| AUTHENTICATION_STATE_INITIALIZING | `uint8` | 1 | |
-| AUTHENTICATION_STATE_ERROR | `uint8` | 2 | |
-| AUTHENTICATION_STATE_OK | `uint8` | 3 | |
-| AUTHENTICATION_STATE_DISABLED | `uint8` | 4 | |
-| SYSTEM_ERROR_OK | `uint32` | 0 | default |
-| SYSTEM_ERROR_INCOMING_CORRECTIONS | `uint32` | 1 | |
-| SYSTEM_ERROR_CONFIGURATION | `uint32` | 2 | |
-| SYSTEM_ERROR_SOFTWARE | `uint32` | 4 | |
-| SYSTEM_ERROR_ANTENNA | `uint32` | 8 | |
-| SYSTEM_ERROR_EVENT_CONGESTION | `uint32` | 16 | |
-| SYSTEM_ERROR_CPU_OVERLOAD | `uint32` | 32 | |
-| SYSTEM_ERROR_OUTPUT_CONGESTION | `uint32` | 64 | |
-| RTCM_MSG_USED_UNKNOWN | `uint8` | 0 | |
-| RTCM_MSG_USED_NOT_USED | `uint8` | 1 | |
-| RTCM_MSG_USED_USED | `uint8` | 2 | |
+| 명칭 | 형식 | Value | 설명 |
+| ----------------------------------------------------------------------------------------------------------------------------------------------------------------- | -------- | ----- | ---------------------------------------------------------- |
+| FIX_TYPE_NONE | `uint8` | 1 | Value 0 is also valid to represent no fix. |
+| FIX_TYPE_2D | `uint8` | 2 | |
+| FIX_TYPE_3D | `uint8` | 3 | |
+| FIX_TYPE_RTCM_CODE_DIFFERENTIAL | `uint8` | 4 | |
+| FIX_TYPE_RTK_FLOAT | `uint8` | 5 | |
+| FIX_TYPE_RTK_FIXED | `uint8` | 6 | |
+| FIX_TYPE_EXTRAPOLATED | `uint8` | 8 | |
+| JAMMING_STATE_UNKNOWN | `uint8` | 0 | default |
+| JAMMING_STATE_OK | `uint8` | 1 | |
+| JAMMING_STATE_MITIGATED | `uint8` | 2 | |
+| JAMMING_STATE_DETECTED | `uint8` | 3 | |
+| SPOOFING_STATE_UNKNOWN | `uint8` | 0 | default |
+| SPOOFING_STATE_OK | `uint8` | 1 | |
+| SPOOFING_STATE_MITIGATED | `uint8` | 2 | |
+| SPOOFING_STATE_DETECTED | `uint8` | 3 | |
+| AUTHENTICATION_STATE_UNKNOWN | `uint8` | 0 | default |
+| AUTHENTICATION_STATE_INITIALIZING | `uint8` | 1 | |
+| AUTHENTICATION_STATE_ERROR | `uint8` | 2 | |
+| AUTHENTICATION_STATE_OK | `uint8` | 3 | |
+| AUTHENTICATION_STATE_DISABLED | `uint8` | 4 | |
+| SYSTEM_ERROR_OK | `uint32` | 0 | default |
+| SYSTEM_ERROR_INCOMING_CORRECTIONS | `uint32` | 1 | |
+| SYSTEM_ERROR_CONFIGURATION | `uint32` | 2 | |
+| SYSTEM_ERROR_SOFTWARE | `uint32` | 4 | |
+| SYSTEM_ERROR_ANTENNA | `uint32` | 8 | |
+| SYSTEM_ERROR_EVENT_CONGESTION | `uint32` | 16 | |
+| SYSTEM_ERROR_CPU_OVERLOAD | `uint32` | 32 | |
+| SYSTEM_ERROR_OUTPUT_CONGESTION | `uint32` | 64 | |
+| RTCM_MSG_USED_UNKNOWN | `uint8` | 0 | |
+| RTCM_MSG_USED_NOT_USED | `uint8` | 1 | |
+| RTCM_MSG_USED_USED | `uint8` | 2 | |
## Source Message
diff --git a/docs/ko/msg_docs/SensorGyro.md b/docs/ko/msg_docs/SensorGyro.md
index 71eb80d0c5..6dc85207fc 100644
--- a/docs/ko/msg_docs/SensorGyro.md
+++ b/docs/ko/msg_docs/SensorGyro.md
@@ -23,9 +23,9 @@ pageClass: is-wide-page
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ------------------------------------------------------------------------------------------- | ------- | ----- | -- |
-| ORB_QUEUE_LENGTH | `uint8` | 8 | |
+| 명칭 | 형식 | Value | 설명 |
+| ----------------------------------------------------------------------------------------- | ------- | ----- | -- |
+| ORB_QUEUE_LENGTH | `uint8` | 8 | |
## Source Message
diff --git a/docs/ko/msg_docs/SensorGyroFft.md b/docs/ko/msg_docs/SensorGyroFft.md
index db7dd2359d..a1b4edddb3 100644
--- a/docs/ko/msg_docs/SensorGyroFft.md
+++ b/docs/ko/msg_docs/SensorGyroFft.md
@@ -4,7 +4,7 @@ pageClass: is-wide-page
# SensorGyroFft (UORB message)
-**TOPICS:** sensor_gyrofft
+**TOPICS:** sensor_gyro_fft
## Fields
diff --git a/docs/ko/msg_docs/SensorGyroFifo.md b/docs/ko/msg_docs/SensorGyroFifo.md
index 9309924553..1494c0d382 100644
--- a/docs/ko/msg_docs/SensorGyroFifo.md
+++ b/docs/ko/msg_docs/SensorGyroFifo.md
@@ -4,7 +4,7 @@ pageClass: is-wide-page
# SensorGyroFifo (UORB message)
-**TOPICS:** sensor_gyrofifo
+**TOPICS:** sensor_gyro_fifo
## Fields
@@ -22,9 +22,9 @@ pageClass: is-wide-page
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ------------------------------------------------------------------------------------------- | ------- | ----- | -- |
-| ORB_QUEUE_LENGTH | `uint8` | 4 | |
+| 명칭 | 형식 | Value | 설명 |
+| ----------------------------------------------------------------------------------------- | ------- | ----- | -- |
+| ORB_QUEUE_LENGTH | `uint8` | 4 | |
## Source Message
diff --git a/docs/ko/msg_docs/SensorMag.md b/docs/ko/msg_docs/SensorMag.md
index 98b4a1d1fd..19779e15cd 100644
--- a/docs/ko/msg_docs/SensorMag.md
+++ b/docs/ko/msg_docs/SensorMag.md
@@ -21,9 +21,9 @@ pageClass: is-wide-page
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ------------------------------------------------------------------------------------------- | ------- | ----- | -- |
-| ORB_QUEUE_LENGTH | `uint8` | 4 | |
+| 명칭 | 형식 | Value | 설명 |
+| ----------------------------------------------------------------------------------------- | ------- | ----- | -- |
+| ORB_QUEUE_LENGTH | `uint8` | 4 | |
## Source Message
diff --git a/docs/ko/msg_docs/SensorOpticalFlow.md b/docs/ko/msg_docs/SensorOpticalFlow.md
index 1b6e407e1c..79a5a1b372 100644
--- a/docs/ko/msg_docs/SensorOpticalFlow.md
+++ b/docs/ko/msg_docs/SensorOpticalFlow.md
@@ -4,7 +4,7 @@ pageClass: is-wide-page
# SensorOpticalFlow (UORB message)
-**TOPICS:** sensor_opticalflow
+**TOPICS:** sensor_optical_flow
## Fields
@@ -28,12 +28,12 @@ pageClass: is-wide-page
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ------------------------------------------------------------------------------------------------- | ------- | ----- | -- |
-| MODE_UNKNOWN | `uint8` | 0 | |
-| MODE_BRIGHT | `uint8` | 1 | |
-| MODE_LOWLIGHT | `uint8` | 2 | |
-| MODE_SUPER_LOWLIGHT | `uint8` | 3 | |
+| 명칭 | 형식 | Value | 설명 |
+| ----------------------------------------------------------------------------------------------- | ------- | ----- | -- |
+| MODE_UNKNOWN | `uint8` | 0 | |
+| MODE_BRIGHT | `uint8` | 1 | |
+| MODE_LOWLIGHT | `uint8` | 2 | |
+| MODE_SUPER_LOWLIGHT | `uint8` | 3 | |
## Source Message
diff --git a/docs/ko/msg_docs/SensorPreflightMag.md b/docs/ko/msg_docs/SensorPreflightMag.md
index 2f47320d2a..e4f218590c 100644
--- a/docs/ko/msg_docs/SensorPreflightMag.md
+++ b/docs/ko/msg_docs/SensorPreflightMag.md
@@ -6,7 +6,7 @@ pageClass: is-wide-page
Pre-flight sensor check metrics. The topic will not be updated when the vehicle is armed.
-**TOPICS:** sensor_preflightmag
+**TOPICS:** sensor_preflight_mag
## Fields
diff --git a/docs/ko/msg_docs/SensorsStatusImu.md b/docs/ko/msg_docs/SensorsStatusImu.md
index cd716510f9..51a393aa53 100644
--- a/docs/ko/msg_docs/SensorsStatusImu.md
+++ b/docs/ko/msg_docs/SensorsStatusImu.md
@@ -6,7 +6,7 @@ pageClass: is-wide-page
Sensor check metrics. This will be zero for a sensor that's primary or unpopulated.
-**TOPICS:** sensors_statusimu
+**TOPICS:** sensors_status_imu
## Fields
diff --git a/docs/ko/msg_docs/SystemPower.md b/docs/ko/msg_docs/SystemPower.md
index fae286bc67..83efd7eda8 100644
--- a/docs/ko/msg_docs/SystemPower.md
+++ b/docs/ko/msg_docs/SystemPower.md
@@ -27,16 +27,16 @@ pageClass: is-wide-page
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ------------------------------------------------------------------------------------------------- | ------- | ----- | -- |
-| BRICK1_VALID_SHIFTS | `uint8` | 0 | |
-| BRICK1_VALID_MASK | `uint8` | 1 | |
-| BRICK2_VALID_SHIFTS | `uint8` | 1 | |
-| BRICK2_VALID_MASK | `uint8` | 2 | |
-| BRICK3_VALID_SHIFTS | `uint8` | 2 | |
-| BRICK3_VALID_MASK | `uint8` | 4 | |
-| BRICK4_VALID_SHIFTS | `uint8` | 3 | |
-| BRICK4_VALID_MASK | `uint8` | 8 | |
+| 명칭 | 형식 | Value | 설명 |
+| ----------------------------------------------------------------------------------------------- | ------- | ----- | -- |
+| BRICK1_VALID_SHIFTS | `uint8` | 0 | |
+| BRICK1_VALID_MASK | `uint8` | 1 | |
+| BRICK2_VALID_SHIFTS | `uint8` | 1 | |
+| BRICK2_VALID_MASK | `uint8` | 2 | |
+| BRICK3_VALID_SHIFTS | `uint8` | 2 | |
+| BRICK3_VALID_MASK | `uint8` | 4 | |
+| BRICK4_VALID_SHIFTS | `uint8` | 3 | |
+| BRICK4_VALID_MASK | `uint8` | 8 | |
## Source Message
diff --git a/docs/ko/msg_docs/TakeoffStatus.md b/docs/ko/msg_docs/TakeoffStatus.md
index 4797f9e947..030ebe66bb 100644
--- a/docs/ko/msg_docs/TakeoffStatus.md
+++ b/docs/ko/msg_docs/TakeoffStatus.md
@@ -18,14 +18,14 @@ Status of the takeoff state machine currently just available for multicopters.
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ------------------------------------------------------------------------------------------------------------------------------------------------------------------- | ------- | ----- | -- |
-| TAKEOFF_STATE_UNINITIALIZED | `uint8` | 0 | |
-| TAKEOFF_STATE_DISARMED | `uint8` | 1 | |
-| TAKEOFF_STATE_SPOOLUP | `uint8` | 2 | |
-| TAKEOFF_STATE_READY_FOR_TAKEOFF | `uint8` | 3 | |
-| TAKEOFF_STATE_RAMPUP | `uint8` | 4 | |
-| TAKEOFF_STATE_FLIGHT | `uint8` | 5 | |
+| 명칭 | 형식 | Value | 설명 |
+| ----------------------------------------------------------------------------------------------------------------------------------------------------------------- | ------- | ----- | -- |
+| TAKEOFF_STATE_UNINITIALIZED | `uint8` | 0 | |
+| TAKEOFF_STATE_DISARMED | `uint8` | 1 | |
+| TAKEOFF_STATE_SPOOLUP | `uint8` | 2 | |
+| TAKEOFF_STATE_READY_FOR_TAKEOFF | `uint8` | 3 | |
+| TAKEOFF_STATE_RAMPUP | `uint8` | 4 | |
+| TAKEOFF_STATE_FLIGHT | `uint8` | 5 | |
## Source Message
diff --git a/docs/ko/msg_docs/TaskStackInfo.md b/docs/ko/msg_docs/TaskStackInfo.md
index b876ff4a7d..89f61d0213 100644
--- a/docs/ko/msg_docs/TaskStackInfo.md
+++ b/docs/ko/msg_docs/TaskStackInfo.md
@@ -6,7 +6,7 @@ pageClass: is-wide-page
stack information for a single running process.
-**TOPICS:** task_stackinfo
+**TOPICS:** task_stack_info
## Fields
@@ -18,9 +18,9 @@ stack information for a single running process.
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ------------------------------------------------------------------------------------------- | ------- | ----- | -- |
-| ORB_QUEUE_LENGTH | `uint8` | 2 | |
+| 명칭 | 형식 | Value | 설명 |
+| ----------------------------------------------------------------------------------------- | ------- | ----- | -- |
+| ORB_QUEUE_LENGTH | `uint8` | 2 | |
## Source Message
diff --git a/docs/ko/msg_docs/TelemetryStatus.md b/docs/ko/msg_docs/TelemetryStatus.md
index 0061ddec9a..c94308039f 100644
--- a/docs/ko/msg_docs/TelemetryStatus.md
+++ b/docs/ko/msg_docs/TelemetryStatus.md
@@ -36,6 +36,7 @@ pageClass: is-wide-page
| heartbeat_type_onboard_controller | `bool` | | | MAV_TYPE_ONBOARD_CONTROLLER |
| heartbeat_type_gimbal | `bool` | | | MAV_TYPE_GIMBAL |
| heartbeat_type_adsb | `bool` | | | MAV_TYPE_ADSB |
+| heartbeat_type_flarm | `bool` | | | MAV_TYPE_FLARM |
| heartbeat_type_camera | `bool` | | | MAV_TYPE_CAMERA |
| heartbeat_type_parachute | `bool` | | | MAV_TYPE_PARACHUTE |
| heartbeat_type_open_drone_id | `bool` | | | MAV_TYPE_ODID |
@@ -51,14 +52,14 @@ pageClass: is-wide-page
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ---------------------------------------------------------------------------------------------------------------------------------- | -------- | ------- | ------------------------------------------------------------------ |
-| LINK_TYPE_GENERIC | `uint8` | 0 | |
-| LINK_TYPE_UBIQUITY_BULLET | `uint8` | 1 | |
-| LINK_TYPE_WIRE | `uint8` | 2 | |
-| LINK_TYPE_USB | `uint8` | 3 | |
-| LINK_TYPE_IRIDIUM | `uint8` | 4 | |
-| HEARTBEAT_TIMEOUT_US | `uint64` | 2500000 | Heartbeat timeout (tolerate missing 1 + jitter) |
+| 명칭 | 형식 | Value | 설명 |
+| -------------------------------------------------------------------------------------------------------------------------------- | -------- | ------- | ------------------------------------------------------------------ |
+| LINK_TYPE_GENERIC | `uint8` | 0 | |
+| LINK_TYPE_UBIQUITY_BULLET | `uint8` | 1 | |
+| LINK_TYPE_WIRE | `uint8` | 2 | |
+| LINK_TYPE_USB | `uint8` | 3 | |
+| LINK_TYPE_IRIDIUM | `uint8` | 4 | |
+| HEARTBEAT_TIMEOUT_US | `uint64` | 2500000 | Heartbeat timeout (tolerate missing 1 + jitter) |
## Source Message
@@ -113,6 +114,7 @@ bool heartbeat_type_gcs # MAV_TYPE_GCS
bool heartbeat_type_onboard_controller # MAV_TYPE_ONBOARD_CONTROLLER
bool heartbeat_type_gimbal # MAV_TYPE_GIMBAL
bool heartbeat_type_adsb # MAV_TYPE_ADSB
+bool heartbeat_type_flarm # MAV_TYPE_FLARM
bool heartbeat_type_camera # MAV_TYPE_CAMERA
bool heartbeat_type_parachute # MAV_TYPE_PARACHUTE
bool heartbeat_type_open_drone_id # MAV_TYPE_ODID
diff --git a/docs/ko/msg_docs/TiltrotorExtraControls.md b/docs/ko/msg_docs/TiltrotorExtraControls.md
index 8a081e8243..1384289bc1 100644
--- a/docs/ko/msg_docs/TiltrotorExtraControls.md
+++ b/docs/ko/msg_docs/TiltrotorExtraControls.md
@@ -4,7 +4,7 @@ pageClass: is-wide-page
# TiltrotorExtraControls (UORB message)
-**TOPICS:** tiltrotor_extracontrols
+**TOPICS:** tiltrotor_extra_controls
## Fields
diff --git a/docs/ko/msg_docs/TimesyncStatus.md b/docs/ko/msg_docs/TimesyncStatus.md
index 0893914b5d..719de90220 100644
--- a/docs/ko/msg_docs/TimesyncStatus.md
+++ b/docs/ko/msg_docs/TimesyncStatus.md
@@ -19,11 +19,11 @@ pageClass: is-wide-page
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| --------------------------------------------------------------------------------------------------------- | ------- | ----- | -- |
-| SOURCE_PROTOCOL_UNKNOWN | `uint8` | 0 | |
-| SOURCE_PROTOCOL_MAVLINK | `uint8` | 1 | |
-| SOURCE_PROTOCOL_DDS | `uint8` | 2 | |
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------------------------------------------------- | ------- | ----- | -- |
+| SOURCE_PROTOCOL_UNKNOWN | `uint8` | 0 | |
+| SOURCE_PROTOCOL_MAVLINK | `uint8` | 1 | |
+| SOURCE_PROTOCOL_DDS | `uint8` | 2 | |
## Source Message
diff --git a/docs/ko/msg_docs/TrajectorySetpoint.md b/docs/ko/msg_docs/TrajectorySetpoint.md
index 78afc474ec..5765eec965 100644
--- a/docs/ko/msg_docs/TrajectorySetpoint.md
+++ b/docs/ko/msg_docs/TrajectorySetpoint.md
@@ -22,9 +22,9 @@ Trajectory setpoint in NED frame. Input to PID position controller. Needs to be
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| -------------------------------------------------------------------- | -------- | ----- | -- |
-| MESSAGE_VERSION | `uint32` | 0 | |
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------------ | -------- | ----- | -- |
+| MESSAGE_VERSION | `uint32` | 0 | |
## Source Message
diff --git a/docs/ko/msg_docs/TransponderReport.md b/docs/ko/msg_docs/TransponderReport.md
index a501f648a3..b759ee2d8c 100644
--- a/docs/ko/msg_docs/TransponderReport.md
+++ b/docs/ko/msg_docs/TransponderReport.md
@@ -28,37 +28,37 @@ pageClass: is-wide-page
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ | -------- | ----- | -- |
-| PX4_ADSB_FLAGS_VALID_COORDS | `uint16` | 1 | |
-| PX4_ADSB_FLAGS_VALID_ALTITUDE | `uint16` | 2 | |
-| PX4_ADSB_FLAGS_VALID_HEADING | `uint16` | 4 | |
-| PX4_ADSB_FLAGS_VALID_VELOCITY | `uint16` | 8 | |
-| PX4_ADSB_FLAGS_VALID_CALLSIGN | `uint16` | 16 | |
-| PX4_ADSB_FLAGS_VALID_SQUAWK | `uint16` | 32 | |
-| PX4_ADSB_FLAGS_RETRANSLATE | `uint16` | 256 | |
-| ADSB_EMITTER_TYPE_NO_INFO | `uint16` | 0 | |
-| ADSB_EMITTER_TYPE_LIGHT | `uint16` | 1 | |
-| ADSB_EMITTER_TYPE_SMALL | `uint16` | 2 | |
-| ADSB_EMITTER_TYPE_LARGE | `uint16` | 3 | |
-| ADSB_EMITTER_TYPE_HIGH_VORTEX_LARGE | `uint16` | 4 | |
-| ADSB_EMITTER_TYPE_HEAVY | `uint16` | 5 | |
-| ADSB_EMITTER_TYPE_HIGHLY_MANUV | `uint16` | 6 | |
-| ADSB_EMITTER_TYPE_ROTOCRAFT | `uint16` | 7 | |
-| ADSB_EMITTER_TYPE_UNASSIGNED | `uint16` | 8 | |
-| ADSB_EMITTER_TYPE_GLIDER | `uint16` | 9 | |
-| ADSB_EMITTER_TYPE_LIGHTER_AIR | `uint16` | 10 | |
-| ADSB_EMITTER_TYPE_PARACHUTE | `uint16` | 11 | |
-| ADSB_EMITTER_TYPE_ULTRA_LIGHT | `uint16` | 12 | |
-| ADSB_EMITTER_TYPE_UNASSIGNED2 | `uint16` | 13 | |
-| ADSB_EMITTER_TYPE_UAV | `uint16` | 14 | |
-| ADSB_EMITTER_TYPE_SPACE | `uint16` | 15 | |
-| ADSB_EMITTER_TYPE_UNASSGINED3 | `uint16` | 16 | |
-| ADSB_EMITTER_TYPE_EMERGENCY_SURFACE | `uint16` | 17 | |
-| ADSB_EMITTER_TYPE_SERVICE_SURFACE | `uint16` | 18 | |
-| ADSB_EMITTER_TYPE_POINT_OBSTACLE | `uint16` | 19 | |
-| ADSB_EMITTER_TYPE_ENUM_END | `uint16` | 20 | |
-| ORB_QUEUE_LENGTH | `uint8` | 16 | |
+| 명칭 | 형식 | Value | 설명 |
+| ---------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- | -------- | ----- | -- |
+| PX4_ADSB_FLAGS_VALID_COORDS | `uint16` | 1 | |
+| PX4_ADSB_FLAGS_VALID_ALTITUDE | `uint16` | 2 | |
+| PX4_ADSB_FLAGS_VALID_HEADING | `uint16` | 4 | |
+| PX4_ADSB_FLAGS_VALID_VELOCITY | `uint16` | 8 | |
+| PX4_ADSB_FLAGS_VALID_CALLSIGN | `uint16` | 16 | |
+| PX4_ADSB_FLAGS_VALID_SQUAWK | `uint16` | 32 | |
+| PX4_ADSB_FLAGS_RETRANSLATE | `uint16` | 256 | |
+| ADSB_EMITTER_TYPE_NO_INFO | `uint16` | 0 | |
+| ADSB_EMITTER_TYPE_LIGHT | `uint16` | 1 | |
+| ADSB_EMITTER_TYPE_SMALL | `uint16` | 2 | |
+| ADSB_EMITTER_TYPE_LARGE | `uint16` | 3 | |
+| ADSB_EMITTER_TYPE_HIGH_VORTEX_LARGE | `uint16` | 4 | |
+| ADSB_EMITTER_TYPE_HEAVY | `uint16` | 5 | |
+| ADSB_EMITTER_TYPE_HIGHLY_MANUV | `uint16` | 6 | |
+| ADSB_EMITTER_TYPE_ROTOCRAFT | `uint16` | 7 | |
+| ADSB_EMITTER_TYPE_UNASSIGNED | `uint16` | 8 | |
+| ADSB_EMITTER_TYPE_GLIDER | `uint16` | 9 | |
+| ADSB_EMITTER_TYPE_LIGHTER_AIR | `uint16` | 10 | |
+| ADSB_EMITTER_TYPE_PARACHUTE | `uint16` | 11 | |
+| ADSB_EMITTER_TYPE_ULTRA_LIGHT | `uint16` | 12 | |
+| ADSB_EMITTER_TYPE_UNASSIGNED2 | `uint16` | 13 | |
+| ADSB_EMITTER_TYPE_UAV | `uint16` | 14 | |
+| ADSB_EMITTER_TYPE_SPACE | `uint16` | 15 | |
+| ADSB_EMITTER_TYPE_UNASSGINED3 | `uint16` | 16 | |
+| ADSB_EMITTER_TYPE_EMERGENCY_SURFACE | `uint16` | 17 | |
+| ADSB_EMITTER_TYPE_SERVICE_SURFACE | `uint16` | 18 | |
+| ADSB_EMITTER_TYPE_POINT_OBSTACLE | `uint16` | 19 | |
+| ADSB_EMITTER_TYPE_ENUM_END | `uint16` | 20 | |
+| ORB_QUEUE_LENGTH | `uint8` | 16 | |
## Source Message
diff --git a/docs/ko/msg_docs/TuneControl.md b/docs/ko/msg_docs/TuneControl.md
index 5e1da3cd11..6ac453e9c4 100644
--- a/docs/ko/msg_docs/TuneControl.md
+++ b/docs/ko/msg_docs/TuneControl.md
@@ -22,33 +22,33 @@ This message is used to control the tunes, when the tune_id is set to CUSTOM. th
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ------------------------------------------------------------------------------------------------------------------------------------------------------------- | ------- | ----- | -- |
-| TUNE_ID_STOP | `uint8` | 0 | |
-| TUNE_ID_STARTUP | `uint8` | 1 | |
-| TUNE_ID_ERROR | `uint8` | 2 | |
-| TUNE_ID_NOTIFY_POSITIVE | `uint8` | 3 | |
-| TUNE_ID_NOTIFY_NEUTRAL | `uint8` | 4 | |
-| TUNE_ID_NOTIFY_NEGATIVE | `uint8` | 5 | |
-| TUNE_ID_ARMING_WARNING | `uint8` | 6 | |
-| TUNE_ID_BATTERY_WARNING_SLOW | `uint8` | 7 | |
-| TUNE_ID_BATTERY_WARNING_FAST | `uint8` | 8 | |
-| TUNE_ID_GPS_WARNING | `uint8` | 9 | |
-| TUNE_ID_ARMING_FAILURE | `uint8` | 10 | |
-| TUNE_ID_PARACHUTE_RELEASE | `uint8` | 11 | |
-| TUNE_ID_SINGLE_BEEP | `uint8` | 12 | |
-| TUNE_ID_HOME_SET | `uint8` | 13 | |
-| TUNE_ID_SD_INIT | `uint8` | 14 | |
-| TUNE_ID_SD_ERROR | `uint8` | 15 | |
-| TUNE_ID_PROG_PX4IO | `uint8` | 16 | |
-| TUNE_ID_PROG_PX4IO_OK | `uint8` | 17 | |
-| TUNE_ID_PROG_PX4IO_ERR | `uint8` | 18 | |
-| TUNE_ID_POWER_OFF | `uint8` | 19 | |
-| NUMBER_OF_TUNES | `uint8` | 20 | |
-| VOLUME_LEVEL_MIN | `uint8` | 0 | |
-| VOLUME_LEVEL_DEFAULT | `uint8` | 20 | |
-| VOLUME_LEVEL_MAX | `uint8` | 100 | |
-| ORB_QUEUE_LENGTH | `uint8` | 4 | |
+| 명칭 | 형식 | Value | 설명 |
+| ----------------------------------------------------------------------------------------------------------------------------------------------------------- | ------- | ----- | -- |
+| TUNE_ID_STOP | `uint8` | 0 | |
+| TUNE_ID_STARTUP | `uint8` | 1 | |
+| TUNE_ID_ERROR | `uint8` | 2 | |
+| TUNE_ID_NOTIFY_POSITIVE | `uint8` | 3 | |
+| TUNE_ID_NOTIFY_NEUTRAL | `uint8` | 4 | |
+| TUNE_ID_NOTIFY_NEGATIVE | `uint8` | 5 | |
+| TUNE_ID_ARMING_WARNING | `uint8` | 6 | |
+| TUNE_ID_BATTERY_WARNING_SLOW | `uint8` | 7 | |
+| TUNE_ID_BATTERY_WARNING_FAST | `uint8` | 8 | |
+| TUNE_ID_GPS_WARNING | `uint8` | 9 | |
+| TUNE_ID_ARMING_FAILURE | `uint8` | 10 | |
+| TUNE_ID_PARACHUTE_RELEASE | `uint8` | 11 | |
+| TUNE_ID_SINGLE_BEEP | `uint8` | 12 | |
+| TUNE_ID_HOME_SET | `uint8` | 13 | |
+| TUNE_ID_SD_INIT | `uint8` | 14 | |
+| TUNE_ID_SD_ERROR | `uint8` | 15 | |
+| TUNE_ID_PROG_PX4IO | `uint8` | 16 | |
+| TUNE_ID_PROG_PX4IO_OK | `uint8` | 17 | |
+| TUNE_ID_PROG_PX4IO_ERR | `uint8` | 18 | |
+| TUNE_ID_POWER_OFF | `uint8` | 19 | |
+| NUMBER_OF_TUNES | `uint8` | 20 | |
+| VOLUME_LEVEL_MIN | `uint8` | 0 | |
+| VOLUME_LEVEL_DEFAULT | `uint8` | 20 | |
+| VOLUME_LEVEL_MAX | `uint8` | 100 | |
+| ORB_QUEUE_LENGTH | `uint8` | 4 | |
## Source Message
diff --git a/docs/ko/msg_docs/UavcanParameterRequest.md b/docs/ko/msg_docs/UavcanParameterRequest.md
index d2cb0f7771..0e3250cd3b 100644
--- a/docs/ko/msg_docs/UavcanParameterRequest.md
+++ b/docs/ko/msg_docs/UavcanParameterRequest.md
@@ -6,7 +6,7 @@ pageClass: is-wide-page
UAVCAN-MAVLink parameter bridge request type.
-**TOPICS:** uavcan_parameterrequest
+**TOPICS:** uavcan_parameter_request
## Fields
@@ -23,16 +23,16 @@ UAVCAN-MAVLink parameter bridge request type.
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ------------------------------------------------------------------------------------------------------------------------------------------------------------------- | ------- | ----- | ------------------------------------------------------------------------------------------------------------------------------------------ |
-| MESSAGE_TYPE_PARAM_REQUEST_READ | `uint8` | 20 | MAVLINK_MSG_ID_PARAM_REQUEST_READ |
-| MESSAGE_TYPE_PARAM_REQUEST_LIST | `uint8` | 21 | MAVLINK_MSG_ID_PARAM_REQUEST_LIST |
-| MESSAGE_TYPE_PARAM_SET | `uint8` | 23 | MAVLINK_MSG_ID_PARAM_SET |
-| NODE_ID_ALL | `uint8` | 0 | MAV_COMP_ID_ALL |
-| PARAM_TYPE_UINT8 | `uint8` | 1 | MAV_PARAM_TYPE_UINT8 |
-| PARAM_TYPE_INT64 | `uint8` | 8 | MAV_PARAM_TYPE_INT64 |
-| PARAM_TYPE_REAL32 | `uint8` | 9 | MAV_PARAM_TYPE_REAL32 |
-| ORB_QUEUE_LENGTH | `uint8` | 4 | |
+| 명칭 | 형식 | Value | 설명 |
+| ----------------------------------------------------------------------------------------------------------------------------------------------------------------- | ------- | ----- | ------------------------------------------------------------------------------------------------------------------------------------------ |
+| MESSAGE_TYPE_PARAM_REQUEST_READ | `uint8` | 20 | MAVLINK_MSG_ID_PARAM_REQUEST_READ |
+| MESSAGE_TYPE_PARAM_REQUEST_LIST | `uint8` | 21 | MAVLINK_MSG_ID_PARAM_REQUEST_LIST |
+| MESSAGE_TYPE_PARAM_SET | `uint8` | 23 | MAVLINK_MSG_ID_PARAM_SET |
+| NODE_ID_ALL | `uint8` | 0 | MAV_COMP_ID_ALL |
+| PARAM_TYPE_UINT8 | `uint8` | 1 | MAV_PARAM_TYPE_UINT8 |
+| PARAM_TYPE_INT64 | `uint8` | 8 | MAV_PARAM_TYPE_INT64 |
+| PARAM_TYPE_REAL32 | `uint8` | 9 | MAV_PARAM_TYPE_REAL32 |
+| ORB_QUEUE_LENGTH | `uint8` | 4 | |
## Source Message
diff --git a/docs/ko/msg_docs/UavcanParameterValue.md b/docs/ko/msg_docs/UavcanParameterValue.md
index 606f06bbad..d7efeb7811 100644
--- a/docs/ko/msg_docs/UavcanParameterValue.md
+++ b/docs/ko/msg_docs/UavcanParameterValue.md
@@ -6,7 +6,7 @@ pageClass: is-wide-page
UAVCAN-MAVLink parameter bridge response type.
-**TOPICS:** uavcan_parametervalue
+**TOPICS:** uavcan_parameter_value
## Fields
diff --git a/docs/ko/msg_docs/UlogStream.md b/docs/ko/msg_docs/UlogStream.md
index 2025b806f0..eb8b8ec85e 100644
--- a/docs/ko/msg_docs/UlogStream.md
+++ b/docs/ko/msg_docs/UlogStream.md
@@ -21,10 +21,10 @@ Message to stream ULog data from the logger. Corresponds to the LOGGING_DATA. ma
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ------------------------------------------------------------------------------------------- | ------- | ----- | ------------------------------------------------------------------------------------ |
-| FLAGS_NEED_ACK | `uint8` | 1 | if set, this message requires to be acked. |
-| ORB_QUEUE_LENGTH | `uint8` | 16 | TODO: we might be able to reduce this if mavlink polled on the topic |
+| 명칭 | 형식 | Value | 설명 |
+| ----------------------------------------------------------------------------------------- | ------- | ----- | ------------------------------------------------------------------------------------ |
+| FLAGS_NEED_ACK | `uint8` | 1 | if set, this message requires to be acked. |
+| ORB_QUEUE_LENGTH | `uint8` | 16 | TODO: we might be able to reduce this if mavlink polled on the topic |
## Source Message
diff --git a/docs/ko/msg_docs/UlogStreamAck.md b/docs/ko/msg_docs/UlogStreamAck.md
index 67fa1eed8a..1d7838b21d 100644
--- a/docs/ko/msg_docs/UlogStreamAck.md
+++ b/docs/ko/msg_docs/UlogStreamAck.md
@@ -6,7 +6,7 @@ pageClass: is-wide-page
Ack a previously sent ulog_stream message that had. the NEED_ACK flag set.
-**TOPICS:** ulog_streamack
+**TOPICS:** ulog_stream_ack
## Fields
@@ -17,10 +17,10 @@ Ack a previously sent ulog_stream message that had. the NEED_ACK flag set.
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ------------------------------------------------------------------------------------- | ------- | ----- | ------------------------------------------------------------------------------------------------------------------------ |
-| ACK_TIMEOUT | `int32` | 50 | timeout waiting for an ack until we retry to send the message [ms] |
-| ACK_MAX_TRIES | `int32` | 50 | maximum amount of tries to (re-)send a message, each time waiting ACK_TIMEOUT ms |
+| 명칭 | 형식 | Value | 설명 |
+| ----------------------------------------------------------------------------------- | ------- | ----- | ------------------------------------------------------------------------------------------------------------------------ |
+| ACK_TIMEOUT | `int32` | 50 | timeout waiting for an ack until we retry to send the message [ms] |
+| ACK_MAX_TRIES | `int32` | 50 | maximum amount of tries to (re-)send a message, each time waiting ACK_TIMEOUT ms |
## Source Message
diff --git a/docs/ko/msg_docs/UnregisterExtComponent.md b/docs/ko/msg_docs/UnregisterExtComponent.md
index 67f2a7e058..eddc1058c1 100644
--- a/docs/ko/msg_docs/UnregisterExtComponent.md
+++ b/docs/ko/msg_docs/UnregisterExtComponent.md
@@ -4,7 +4,7 @@ pageClass: is-wide-page
# UnregisterExtComponent (UORB message)
-**TOPICS:** unregister_extcomponent
+**TOPICS:** unregister_ext_component
## Fields
@@ -18,9 +18,9 @@ pageClass: is-wide-page
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| -------------------------------------------------------------------- | -------- | ----- | -- |
-| MESSAGE_VERSION | `uint32` | 0 | |
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------------ | -------- | ----- | -- |
+| MESSAGE_VERSION | `uint32` | 0 | |
## Source Message
diff --git a/docs/ko/msg_docs/VehicleAirData.md b/docs/ko/msg_docs/VehicleAirData.md
index cc1ceb71e1..ec964acd4c 100644
--- a/docs/ko/msg_docs/VehicleAirData.md
+++ b/docs/ko/msg_docs/VehicleAirData.md
@@ -9,7 +9,7 @@ Vehicle air data.
Data from the currently selected barometer (plus ambient temperature from the source specified in temperature_source).
Includes calculated data such as barometric altitude and air density.
-**TOPICS:** vehicle_airdata
+**TOPICS:** vehicle_air_data
## Fields
diff --git a/docs/ko/msg_docs/VehicleAngularAccelerationSetpoint.md b/docs/ko/msg_docs/VehicleAngularAccelerationSetpoint.md
index 4989f5d30b..cd2bc7bedd 100644
--- a/docs/ko/msg_docs/VehicleAngularAccelerationSetpoint.md
+++ b/docs/ko/msg_docs/VehicleAngularAccelerationSetpoint.md
@@ -4,7 +4,7 @@ pageClass: is-wide-page
# VehicleAngularAccelerationSetpoint (UORB message)
-**TOPICS:** vehicle_angularacceleration_setpoint
+**TOPICS:** vehicle_angular_acceleration_setpoint
## Fields
diff --git a/docs/ko/msg_docs/VehicleAngularVelocity.md b/docs/ko/msg_docs/VehicleAngularVelocity.md
index b12ac9e5a6..1b2552bedf 100644
--- a/docs/ko/msg_docs/VehicleAngularVelocity.md
+++ b/docs/ko/msg_docs/VehicleAngularVelocity.md
@@ -17,9 +17,9 @@ pageClass: is-wide-page
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| -------------------------------------------------------------------- | -------- | ----- | -- |
-| MESSAGE_VERSION | `uint32` | 0 | |
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------------ | -------- | ----- | -- |
+| MESSAGE_VERSION | `uint32` | 0 | |
## Source Message
diff --git a/docs/ko/msg_docs/VehicleAttitude.md b/docs/ko/msg_docs/VehicleAttitude.md
index f3c3cc59c0..59c6ed443d 100644
--- a/docs/ko/msg_docs/VehicleAttitude.md
+++ b/docs/ko/msg_docs/VehicleAttitude.md
@@ -20,9 +20,9 @@ This is similar to the mavlink message ATTITUDE_QUATERNION, but for onboard use.
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| -------------------------------------------------------------------- | -------- | ----- | -- |
-| MESSAGE_VERSION | `uint32` | 0 | |
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------------ | -------- | ----- | -- |
+| MESSAGE_VERSION | `uint32` | 0 | |
## Source Message
diff --git a/docs/ko/msg_docs/VehicleAttitudeSetpoint.md b/docs/ko/msg_docs/VehicleAttitudeSetpoint.md
index 27ab886978..96c48ee7eb 100644
--- a/docs/ko/msg_docs/VehicleAttitudeSetpoint.md
+++ b/docs/ko/msg_docs/VehicleAttitudeSetpoint.md
@@ -17,9 +17,9 @@ pageClass: is-wide-page
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| -------------------------------------------------------------------- | -------- | ----- | -- |
-| MESSAGE_VERSION | `uint32` | 1 | |
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------------ | -------- | ----- | -- |
+| MESSAGE_VERSION | `uint32` | 1 | |
## Source Message
diff --git a/docs/ko/msg_docs/VehicleAttitudeSetpointV0.md b/docs/ko/msg_docs/VehicleAttitudeSetpointV0.md
index 1d1ed1de3f..756358d9ae 100644
--- a/docs/ko/msg_docs/VehicleAttitudeSetpointV0.md
+++ b/docs/ko/msg_docs/VehicleAttitudeSetpointV0.md
@@ -19,9 +19,9 @@ pageClass: is-wide-page
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| -------------------------------------------------------------------- | -------- | ----- | -- |
-| MESSAGE_VERSION | `uint32` | 0 | |
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------------ | -------- | ----- | -- |
+| MESSAGE_VERSION | `uint32` | 0 | |
## Source Message
diff --git a/docs/ko/msg_docs/VehicleCommand.md b/docs/ko/msg_docs/VehicleCommand.md
index 88a1068ee2..858bb56c5b 100644
--- a/docs/ko/msg_docs/VehicleCommand.md
+++ b/docs/ko/msg_docs/VehicleCommand.md
@@ -1490,34 +1490,34 @@ Change mode by specifying nav_state directly.
### ORBIT_YAW_BEHAVIOUR {#ORBIT_YAW_BEHAVIOUR}
-| 명칭 | 형식 | Value | 설명 |
-| -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- | ------- | ----- | -- |
-| ORBIT_YAW_BEHAVIOUR_HOLD_FRONT_TO_CIRCLE_CENTER | `uint8` | 0 | |
-| ORBIT_YAW_BEHAVIOUR_HOLD_INITIAL_HEADING | `uint8` | 1 | |
-| ORBIT_YAW_BEHAVIOUR_UNCONTROLLED | `uint8` | 2 | |
-| ORBIT_YAW_BEHAVIOUR_HOLD_FRONT_TANGENT_TO_CIRCLE | `uint8` | 3 | |
-| ORBIT_YAW_BEHAVIOUR_RC_CONTROLLED | `uint8` | 4 | |
-| ORBIT_YAW_BEHAVIOUR_UNCHANGED | `uint8` | 5 | |
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ | ------- | ----- | -- |
+| ORBIT_YAW_BEHAVIOUR_HOLD_FRONT_TO_CIRCLE_CENTER | `uint8` | 0 | |
+| ORBIT_YAW_BEHAVIOUR_HOLD_INITIAL_HEADING | `uint8` | 1 | |
+| ORBIT_YAW_BEHAVIOUR_UNCONTROLLED | `uint8` | 2 | |
+| ORBIT_YAW_BEHAVIOUR_HOLD_FRONT_TANGENT_TO_CIRCLE | `uint8` | 3 | |
+| ORBIT_YAW_BEHAVIOUR_RC_CONTROLLED | `uint8` | 4 | |
+| ORBIT_YAW_BEHAVIOUR_UNCHANGED | `uint8` | 5 | |
### VEHICLE_ROI {#VEHICLE_ROI}
-| 명칭 | 형식 | Value | 설명 |
-| ------------------------------------------------------------------------------------------------------------------------ | ------- | ----- | -------------------------------------------- |
-| VEHICLE_ROI_NONE | `uint8` | 0 | No region of interest. |
-| VEHICLE_ROI_WPNEXT | `uint8` | 1 | Point toward next MISSION. |
-| VEHICLE_ROI_WPINDEX | `uint8` | 2 | Point toward given MISSION. |
-| VEHICLE_ROI_LOCATION | `uint8` | 3 | Point toward fixed location. |
-| VEHICLE_ROI_TARGET | `uint8` | 4 | Point toward target. |
-| VEHICLE_ROI_ENUM_END | `uint8` | 5 | |
+| 명칭 | 형식 | Value | 설명 |
+| ---------------------------------------------------------------------------------------------------------------------- | ------- | ----- | -------------------------------------------- |
+| VEHICLE_ROI_NONE | `uint8` | 0 | No region of interest. |
+| VEHICLE_ROI_WPNEXT | `uint8` | 1 | Point toward next MISSION. |
+| VEHICLE_ROI_WPINDEX | `uint8` | 2 | Point toward given MISSION. |
+| VEHICLE_ROI_LOCATION | `uint8` | 3 | Point toward fixed location. |
+| VEHICLE_ROI_TARGET | `uint8` | 4 | Point toward target. |
+| VEHICLE_ROI_ENUM_END | `uint8` | 5 | |
### SPEED_TYPE {#SPEED_TYPE}
-| 명칭 | 형식 | Value | 설명 |
-| -------------------------------------------------------------------------------------------------------------------------------- | ------- | ----- | -- |
-| SPEED_TYPE_AIRSPEED | `uint8` | 0 | |
-| SPEED_TYPE_GROUNDSPEED | `uint8` | 1 | |
-| SPEED_TYPE_CLIMB_SPEED | `uint8` | 2 | |
-| SPEED_TYPE_DESCEND_SPEED | `uint8` | 3 | |
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------------------------------------------------------------------------ | ------- | ----- | -- |
+| SPEED_TYPE_AIRSPEED | `uint8` | 0 | |
+| SPEED_TYPE_GROUNDSPEED | `uint8` | 1 | |
+| SPEED_TYPE_CLIMB_SPEED | `uint8` | 2 | |
+| SPEED_TYPE_DESCEND_SPEED | `uint8` | 3 | |
### MAV_MOUNT_MODE {#MAV_MOUNT_MODE}
@@ -1526,50 +1526,50 @@ Change mode by specifying nav_state directly.
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ----------------------------------------------------------------------------------------------------------------------------------------------------------------------------- | -------- | ----- | ------------------------------------------------------------------------------------------------------------------------------------------------------------------ |
-| MESSAGE_VERSION | `uint32` | 0 | |
-| PREFLIGHT_CALIBRATION_TEMPERATURE_CALIBRATION | `uint16` | 3 | Param value for VEHICLE_CMD_PREFLIGHT_CALIBRATION to start temperature calibration. |
-| VEHICLE_MOUNT_MODE_RETRACT | `uint8` | 0 | Load and keep safe position (Roll,Pitch,Yaw) from permanent memory and stop stabilization. |
-| VEHICLE_MOUNT_MODE_NEUTRAL | `uint8` | 1 | Load and keep neutral position (Roll,Pitch,Yaw) from permanent memory. |
-| VEHICLE_MOUNT_MODE_MAVLINK_TARGETING | `uint8` | 2 | Load neutral position and start MAVLink Roll,Pitch,Yaw control with stabilization. |
-| VEHICLE_MOUNT_MODE_RC_TARGETING | `uint8` | 3 | Load neutral position and start RC Roll,Pitch,Yaw control with stabilization. |
-| VEHICLE_MOUNT_MODE_GPS_POINT | `uint8` | 4 | Load neutral position and start to point to Lat,Lon,Alt. |
-| VEHICLE_MOUNT_MODE_ENUM_END | `uint8` | 5 | |
-| PARACHUTE_ACTION_DISABLE | `uint8` | 0 | |
-| PARACHUTE_ACTION_ENABLE | `uint8` | 1 | |
-| PARACHUTE_ACTION_RELEASE | `uint8` | 2 | |
-| FAILURE_UNIT_SENSOR_GYRO | `uint8` | 0 | |
-| FAILURE_UNIT_SENSOR_ACCEL | `uint8` | 1 | |
-| FAILURE_UNIT_SENSOR_MAG | `uint8` | 2 | |
-| FAILURE_UNIT_SENSOR_BARO | `uint8` | 3 | |
-| FAILURE_UNIT_SENSOR_GPS | `uint8` | 4 | |
-| FAILURE_UNIT_SENSOR_OPTICAL_FLOW | `uint8` | 5 | |
-| FAILURE_UNIT_SENSOR_VIO | `uint8` | 6 | |
-| FAILURE_UNIT_SENSOR_DISTANCE_SENSOR | `uint8` | 7 | |
-| FAILURE_UNIT_SENSOR_AIRSPEED | `uint8` | 8 | |
-| FAILURE_UNIT_SYSTEM_BATTERY | `uint8` | 100 | |
-| FAILURE_UNIT_SYSTEM_MOTOR | `uint8` | 101 | |
-| FAILURE_UNIT_SYSTEM_SERVO | `uint8` | 102 | |
-| FAILURE_UNIT_SYSTEM_AVOIDANCE | `uint8` | 103 | |
-| FAILURE_UNIT_SYSTEM_RC_SIGNAL | `uint8` | 104 | |
-| FAILURE_UNIT_SYSTEM_MAVLINK_SIGNAL | `uint8` | 105 | |
-| FAILURE_TYPE_OK | `uint8` | 0 | |
-| FAILURE_TYPE_OFF | `uint8` | 1 | |
-| FAILURE_TYPE_STUCK | `uint8` | 2 | |
-| FAILURE_TYPE_GARBAGE | `uint8` | 3 | |
-| FAILURE_TYPE_WRONG | `uint8` | 4 | |
-| FAILURE_TYPE_SLOW | `uint8` | 5 | |
-| FAILURE_TYPE_DELAYED | `uint8` | 6 | |
-| FAILURE_TYPE_INTERMITTENT | `uint8` | 7 | |
-| ARMING_ACTION_DISARM | `int8` | 0 | |
-| ARMING_ACTION_ARM | `int8` | 1 | |
-| GRIPPER_ACTION_RELEASE | `uint8` | 0 | |
-| GRIPPER_ACTION_GRAB | `uint8` | 1 | |
-| SAFETY_OFF | `uint8` | 0 | |
-| SAFETY_ON | `uint8` | 1 | |
-| ORB_QUEUE_LENGTH | `uint8` | 8 | |
-| COMPONENT_MODE_EXECUTOR_START | `uint16` | 1000 | |
+| 명칭 | 형식 | Value | 설명 |
+| --------------------------------------------------------------------------------------------------------------------------------------------------------------------------- | -------- | ----- | ------------------------------------------------------------------------------------------------------------------------------------------------------------------ |
+| MESSAGE_VERSION | `uint32` | 0 | |
+| PREFLIGHT_CALIBRATION_TEMPERATURE_CALIBRATION | `uint16` | 3 | Param value for VEHICLE_CMD_PREFLIGHT_CALIBRATION to start temperature calibration. |
+| VEHICLE_MOUNT_MODE_RETRACT | `uint8` | 0 | Load and keep safe position (Roll,Pitch,Yaw) from permanent memory and stop stabilization. |
+| VEHICLE_MOUNT_MODE_NEUTRAL | `uint8` | 1 | Load and keep neutral position (Roll,Pitch,Yaw) from permanent memory. |
+| VEHICLE_MOUNT_MODE_MAVLINK_TARGETING | `uint8` | 2 | Load neutral position and start MAVLink Roll,Pitch,Yaw control with stabilization. |
+| VEHICLE_MOUNT_MODE_RC_TARGETING | `uint8` | 3 | Load neutral position and start RC Roll,Pitch,Yaw control with stabilization. |
+| VEHICLE_MOUNT_MODE_GPS_POINT | `uint8` | 4 | Load neutral position and start to point to Lat,Lon,Alt. |
+| VEHICLE_MOUNT_MODE_ENUM_END | `uint8` | 5 | |
+| PARACHUTE_ACTION_DISABLE | `uint8` | 0 | |
+| PARACHUTE_ACTION_ENABLE | `uint8` | 1 | |
+| PARACHUTE_ACTION_RELEASE | `uint8` | 2 | |
+| FAILURE_UNIT_SENSOR_GYRO | `uint8` | 0 | |
+| FAILURE_UNIT_SENSOR_ACCEL | `uint8` | 1 | |
+| FAILURE_UNIT_SENSOR_MAG | `uint8` | 2 | |
+| FAILURE_UNIT_SENSOR_BARO | `uint8` | 3 | |
+| FAILURE_UNIT_SENSOR_GPS | `uint8` | 4 | |
+| FAILURE_UNIT_SENSOR_OPTICAL_FLOW | `uint8` | 5 | |
+| FAILURE_UNIT_SENSOR_VIO | `uint8` | 6 | |
+| FAILURE_UNIT_SENSOR_DISTANCE_SENSOR | `uint8` | 7 | |
+| FAILURE_UNIT_SENSOR_AIRSPEED | `uint8` | 8 | |
+| FAILURE_UNIT_SYSTEM_BATTERY | `uint8` | 100 | |
+| FAILURE_UNIT_SYSTEM_MOTOR | `uint8` | 101 | |
+| FAILURE_UNIT_SYSTEM_SERVO | `uint8` | 102 | |
+| FAILURE_UNIT_SYSTEM_AVOIDANCE | `uint8` | 103 | |
+| FAILURE_UNIT_SYSTEM_RC_SIGNAL | `uint8` | 104 | |
+| FAILURE_UNIT_SYSTEM_MAVLINK_SIGNAL | `uint8` | 105 | |
+| FAILURE_TYPE_OK | `uint8` | 0 | |
+| FAILURE_TYPE_OFF | `uint8` | 1 | |
+| FAILURE_TYPE_STUCK | `uint8` | 2 | |
+| FAILURE_TYPE_GARBAGE | `uint8` | 3 | |
+| FAILURE_TYPE_WRONG | `uint8` | 4 | |
+| FAILURE_TYPE_SLOW | `uint8` | 5 | |
+| FAILURE_TYPE_DELAYED | `uint8` | 6 | |
+| FAILURE_TYPE_INTERMITTENT | `uint8` | 7 | |
+| ARMING_ACTION_DISARM | `int8` | 0 | |
+| ARMING_ACTION_ARM | `int8` | 1 | |
+| GRIPPER_ACTION_RELEASE | `uint8` | 0 | |
+| GRIPPER_ACTION_GRAB | `uint8` | 1 | |
+| SAFETY_OFF | `uint8` | 0 | |
+| SAFETY_ON | `uint8` | 1 | |
+| ORB_QUEUE_LENGTH | `uint8` | 8 | |
+| COMPONENT_MODE_EXECUTOR_START | `uint16` | 1000 | |
## Source Message
diff --git a/docs/ko/msg_docs/VehicleCommandAck.md b/docs/ko/msg_docs/VehicleCommandAck.md
index 1573f3a243..509f1a0097 100644
--- a/docs/ko/msg_docs/VehicleCommandAck.md
+++ b/docs/ko/msg_docs/VehicleCommandAck.md
@@ -4,42 +4,55 @@ pageClass: is-wide-page
# VehicleCommandAck (UORB message)
-Vehicle Command Ackonwledgement uORB message. Used for acknowledging the vehicle command being received. Follows the MAVLink COMMAND_ACK message definition.
+Vehicle Command Acknowledgement uORB message.
-**TOPICS:** vehicle_commandack
+Used for acknowledging the vehicle command being received.
+Follows the MAVLink COMMAND_ACK message definition
+
+**TOPICS:** vehicle_command_ack
## Fields
-| 명칭 | 형식 | Unit [Frame] | Range/Enum | 설명 |
-| ------------------------------------- | -------- | ---------------------------------------------------------------- | ---------- | ----------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- |
-| timestamp | `uint64` | | | time since system start (microseconds) |
-| command | `uint32` | | | Command that is being acknowledged |
-| result | `uint8` | | | Command result |
-| result_param1 | `uint8` | | | Also used as progress[%], it can be set with the reason why the command was denied, or the progress percentage when result is MAV_RESULT_IN_PROGRESS |
-| result_param2 | `int32` | | | Additional parameter of the result, example: which parameter of MAV_CMD_NAV_WAYPOINT caused it to be denied. |
-| target_system | `uint8` | | | |
-| target_component | `uint16` | | | Target component / mode executor |
-| from_external | `bool` | | | Indicates if the command came from an external source |
+| 명칭 | 형식 | Unit [Frame] | Range/Enum | 설명 |
+| ------------------------------------- | -------- | ------------------------------------------------------------------------------------------ | ----------------------------------------------------------------------------------- | ----------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- |
+| timestamp | `uint64` | us | | time since system start |
+| command | `uint32` | | | Command that is being acknowledged |
+| result | `uint8` | | [VEHICLE_CMD_RESULT](#VEHICLE_CMD_RESULT) | Command result |
+| result_param1 | `uint8` | | | Can be set with the reason why the command was denied, or the progress percentage when result is MAV_RESULT_IN_PROGRESS (%) |
+| result_param2 | `int32` | enum ARM_AUTH_DENIED_REASON | | Additional parameter of the result, example: which parameter of MAV_CMD_NAV_WAYPOINT caused it to be denied, or what ARM_AUTH_DENIED_REASON |
+| target_system | `uint8` | | | Target system |
+| target_component | `uint16` | | | Target component / mode executor |
+| from_external | `bool` | | | Indicates if the command came from an external source |
+
+## Enums
+
+### VEHICLE_CMD_RESULT {#VEHICLE_CMD_RESULT}
+
+| 명칭 | 형식 | Value | 설명 |
+| -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- | ------- | ----- | ------------------------------------------------------------------------- |
+| VEHICLE_CMD_RESULT_ACCEPTED | `uint8` | 0 | Command ACCEPTED and EXECUTED |
+| VEHICLE_CMD_RESULT_TEMPORARILY_REJECTED | `uint8` | 1 | Command TEMPORARY REJECTED/DENIED |
+| VEHICLE_CMD_RESULT_DENIED | `uint8` | 2 | Command PERMANENTLY DENIED |
+| VEHICLE_CMD_RESULT_UNSUPPORTED | `uint8` | 3 | Command UNKNOWN/UNSUPPORTED |
+| VEHICLE_CMD_RESULT_FAILED | `uint8` | 4 | Command executed, but failed |
+| VEHICLE_CMD_RESULT_IN_PROGRESS | `uint8` | 5 | Command being executed |
+| VEHICLE_CMD_RESULT_CANCELLED | `uint8` | 6 | Command Canceled |
+| VEHICLE_CMD_RESULT_COMMAND_LONG_ONLY | `uint8` | 7 | Command is only accepted when sent as a COMMAND_LONG |
+| VEHICLE_CMD_RESULT_COMMAND_INT_ONLY | `uint8` | 8 | Command is only accepted when sent as a COMMAND_INT |
+| VEHICLE_CMD_RESULT_UNSUPPORTED_MAV_FRAME | `uint8` | 9 | Command does not support specified frame |
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| --------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- | -------- | ----- | --------------------------------- |
-| MESSAGE_VERSION | `uint32` | 0 | |
-| VEHICLE_CMD_RESULT_ACCEPTED | `uint8` | 0 | Command ACCEPTED and EXECUTED |
-| VEHICLE_CMD_RESULT_TEMPORARILY_REJECTED | `uint8` | 1 | Command TEMPORARY REJECTED/DENIED |
-| VEHICLE_CMD_RESULT_DENIED | `uint8` | 2 | Command PERMANENTLY DENIED |
-| VEHICLE_CMD_RESULT_UNSUPPORTED | `uint8` | 3 | Command UNKNOWN/UNSUPPORTED |
-| VEHICLE_CMD_RESULT_FAILED | `uint8` | 4 | Command executed, but failed |
-| VEHICLE_CMD_RESULT_IN_PROGRESS | `uint8` | 5 | Command being executed |
-| VEHICLE_CMD_RESULT_CANCELLED | `uint8` | 6 | Command Canceled |
-| ARM_AUTH_DENIED_REASON_GENERIC | `uint16` | 0 | |
-| ARM_AUTH_DENIED_REASON_NONE | `uint16` | 1 | |
-| ARM_AUTH_DENIED_REASON_INVALID_WAYPOINT | `uint16` | 2 | |
-| ARM_AUTH_DENIED_REASON_TIMEOUT | `uint16` | 3 | |
-| ARM_AUTH_DENIED_REASON_AIRSPACE_IN_USE | `uint16` | 4 | |
-| ARM_AUTH_DENIED_REASON_BAD_WEATHER | `uint16` | 5 | |
-| ORB_QUEUE_LENGTH | `uint8` | 8 | |
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- | -------- | ----- | -- |
+| MESSAGE_VERSION | `uint32` | 1 | |
+| ORB_QUEUE_LENGTH | `uint8` | 8 | |
+| ARM_AUTH_DENIED_REASON_GENERIC | `uint16` | 0 | |
+| ARM_AUTH_DENIED_REASON_NONE | `uint16` | 1 | |
+| ARM_AUTH_DENIED_REASON_INVALID_WAYPOINT | `uint16` | 2 | |
+| ARM_AUTH_DENIED_REASON_TIMEOUT | `uint16` | 3 | |
+| ARM_AUTH_DENIED_REASON_AIRSPACE_IN_USE | `uint16` | 4 | |
+| ARM_AUTH_DENIED_REASON_BAD_WEATHER | `uint16` | 5 | |
## Source Message
@@ -49,23 +62,35 @@ Vehicle Command Ackonwledgement uORB message. Used for acknowledging the vehicle
Click here to see original file
```c
-# Vehicle Command Ackonwledgement uORB message.
+# Vehicle Command Acknowledgement uORB message.
+#
# Used for acknowledging the vehicle command being received.
# Follows the MAVLink COMMAND_ACK message definition
-uint32 MESSAGE_VERSION = 0
+uint32 MESSAGE_VERSION = 1
-uint64 timestamp # time since system start (microseconds)
+uint64 timestamp # [us] time since system start
-# Result cases. This follows the MAVLink MAV_RESULT enum definition
-uint8 VEHICLE_CMD_RESULT_ACCEPTED = 0 # Command ACCEPTED and EXECUTED |
-uint8 VEHICLE_CMD_RESULT_TEMPORARILY_REJECTED = 1 # Command TEMPORARY REJECTED/DENIED |
-uint8 VEHICLE_CMD_RESULT_DENIED = 2 # Command PERMANENTLY DENIED |
-uint8 VEHICLE_CMD_RESULT_UNSUPPORTED = 3 # Command UNKNOWN/UNSUPPORTED |
-uint8 VEHICLE_CMD_RESULT_FAILED = 4 # Command executed, but failed |
-uint8 VEHICLE_CMD_RESULT_IN_PROGRESS = 5 # Command being executed |
-uint8 VEHICLE_CMD_RESULT_CANCELLED = 6 # Command Canceled
+uint8 ORB_QUEUE_LENGTH = 8
+uint32 command # [-] Command that is being acknowledged
+
+uint8 result # [@enum VEHICLE_CMD_RESULT] Command result
+# VEHICLE_CMD_RESULT Result cases. Follows the MAVLink MAV_RESULT enum definition
+uint8 VEHICLE_CMD_RESULT_ACCEPTED = 0 # Command ACCEPTED and EXECUTED
+uint8 VEHICLE_CMD_RESULT_TEMPORARILY_REJECTED = 1 # Command TEMPORARY REJECTED/DENIED
+uint8 VEHICLE_CMD_RESULT_DENIED = 2 # Command PERMANENTLY DENIED
+uint8 VEHICLE_CMD_RESULT_UNSUPPORTED = 3 # Command UNKNOWN/UNSUPPORTED
+uint8 VEHICLE_CMD_RESULT_FAILED = 4 # Command executed, but failed
+uint8 VEHICLE_CMD_RESULT_IN_PROGRESS = 5 # Command being executed
+uint8 VEHICLE_CMD_RESULT_CANCELLED = 6 # Command Canceled
+uint8 VEHICLE_CMD_RESULT_COMMAND_LONG_ONLY = 7 # Command is only accepted when sent as a COMMAND_LONG
+uint8 VEHICLE_CMD_RESULT_COMMAND_INT_ONLY = 8 # Command is only accepted when sent as a COMMAND_INT
+uint8 VEHICLE_CMD_RESULT_UNSUPPORTED_MAV_FRAME = 9 # Command does not support specified frame
+
+uint8 result_param1 # [-] Can be set with the reason why the command was denied, or the progress percentage when result is MAV_RESULT_IN_PROGRESS (%)
+
+int32 result_param2 # [enum ARM_AUTH_DENIED_REASON] Additional parameter of the result, example: which parameter of MAV_CMD_NAV_WAYPOINT caused it to be denied, or what ARM_AUTH_DENIED_REASON
# Arming denied specific cases
uint16 ARM_AUTH_DENIED_REASON_GENERIC = 0
uint16 ARM_AUTH_DENIED_REASON_NONE = 1
@@ -74,16 +99,10 @@ uint16 ARM_AUTH_DENIED_REASON_TIMEOUT = 3
uint16 ARM_AUTH_DENIED_REASON_AIRSPACE_IN_USE = 4
uint16 ARM_AUTH_DENIED_REASON_BAD_WEATHER = 5
-uint8 ORB_QUEUE_LENGTH = 8
+uint8 target_system # [-] Target system
+uint16 target_component # Target component / mode executor
-uint32 command # Command that is being acknowledged
-uint8 result # Command result
-uint8 result_param1 # Also used as progress[%], it can be set with the reason why the command was denied, or the progress percentage when result is MAV_RESULT_IN_PROGRESS
-int32 result_param2 # Additional parameter of the result, example: which parameter of MAV_CMD_NAV_WAYPOINT caused it to be denied.
-uint8 target_system
-uint16 target_component # Target component / mode executor
-
-bool from_external # Indicates if the command came from an external source
+bool from_external # Indicates if the command came from an external source
```
:::
diff --git a/docs/ko/msg_docs/VehicleCommandAckV0.md b/docs/ko/msg_docs/VehicleCommandAckV0.md
new file mode 100644
index 0000000000..298c20f5ed
--- /dev/null
+++ b/docs/ko/msg_docs/VehicleCommandAckV0.md
@@ -0,0 +1,89 @@
+---
+pageClass: is-wide-page
+---
+
+# VehicleCommandAckV0 (UORB message)
+
+Vehicle Command Ackonwledgement uORB message. Used for acknowledging the vehicle command being received. Follows the MAVLink COMMAND_ACK message definition.
+
+**TOPICS:** vehicle_command_ack_v0
+
+## Fields
+
+| 명칭 | 형식 | Unit [Frame] | Range/Enum | 설명 |
+| ------------------------------------- | -------- | ---------------------------------------------------------------- | ---------- | ----------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- |
+| timestamp | `uint64` | | | time since system start (microseconds) |
+| command | `uint32` | | | Command that is being acknowledged |
+| result | `uint8` | | | Command result |
+| result_param1 | `uint8` | | | Also used as progress[%], it can be set with the reason why the command was denied, or the progress percentage when result is MAV_RESULT_IN_PROGRESS |
+| result_param2 | `int32` | | | Additional parameter of the result, example: which parameter of MAV_CMD_NAV_WAYPOINT caused it to be denied. |
+| target_system | `uint8` | | | |
+| target_component | `uint16` | | | Target component / mode executor |
+| from_external | `bool` | | | Indicates if the command came from an external source |
+
+## Constants
+
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- | -------- | ----- | --------------------------------- |
+| MESSAGE_VERSION | `uint32` | 0 | |
+| VEHICLE_CMD_RESULT_ACCEPTED | `uint8` | 0 | Command ACCEPTED and EXECUTED |
+| VEHICLE_CMD_RESULT_TEMPORARILY_REJECTED | `uint8` | 1 | Command TEMPORARY REJECTED/DENIED |
+| VEHICLE_CMD_RESULT_DENIED | `uint8` | 2 | Command PERMANENTLY DENIED |
+| VEHICLE_CMD_RESULT_UNSUPPORTED | `uint8` | 3 | Command UNKNOWN/UNSUPPORTED |
+| VEHICLE_CMD_RESULT_FAILED | `uint8` | 4 | Command executed, but failed |
+| VEHICLE_CMD_RESULT_IN_PROGRESS | `uint8` | 5 | Command being executed |
+| VEHICLE_CMD_RESULT_CANCELLED | `uint8` | 6 | Command Canceled |
+| ARM_AUTH_DENIED_REASON_GENERIC | `uint16` | 0 | |
+| ARM_AUTH_DENIED_REASON_NONE | `uint16` | 1 | |
+| ARM_AUTH_DENIED_REASON_INVALID_WAYPOINT | `uint16` | 2 | |
+| ARM_AUTH_DENIED_REASON_TIMEOUT | `uint16` | 3 | |
+| ARM_AUTH_DENIED_REASON_AIRSPACE_IN_USE | `uint16` | 4 | |
+| ARM_AUTH_DENIED_REASON_BAD_WEATHER | `uint16` | 5 | |
+| ORB_QUEUE_LENGTH | `uint8` | 8 | |
+
+## Source Message
+
+[Source file (GitHub)](https://github.com/PX4/PX4-Autopilot/blob/main/msg/px4_msgs_old/msg/VehicleCommandAckV0.msg)
+
+:::details
+Click here to see original file
+
+```c
+# Vehicle Command Ackonwledgement uORB message.
+# Used for acknowledging the vehicle command being received.
+# Follows the MAVLink COMMAND_ACK message definition
+
+uint32 MESSAGE_VERSION = 0
+
+uint64 timestamp # time since system start (microseconds)
+
+# Result cases. This follows the MAVLink MAV_RESULT enum definition
+uint8 VEHICLE_CMD_RESULT_ACCEPTED = 0 # Command ACCEPTED and EXECUTED |
+uint8 VEHICLE_CMD_RESULT_TEMPORARILY_REJECTED = 1 # Command TEMPORARY REJECTED/DENIED |
+uint8 VEHICLE_CMD_RESULT_DENIED = 2 # Command PERMANENTLY DENIED |
+uint8 VEHICLE_CMD_RESULT_UNSUPPORTED = 3 # Command UNKNOWN/UNSUPPORTED |
+uint8 VEHICLE_CMD_RESULT_FAILED = 4 # Command executed, but failed |
+uint8 VEHICLE_CMD_RESULT_IN_PROGRESS = 5 # Command being executed |
+uint8 VEHICLE_CMD_RESULT_CANCELLED = 6 # Command Canceled
+
+# Arming denied specific cases
+uint16 ARM_AUTH_DENIED_REASON_GENERIC = 0
+uint16 ARM_AUTH_DENIED_REASON_NONE = 1
+uint16 ARM_AUTH_DENIED_REASON_INVALID_WAYPOINT = 2
+uint16 ARM_AUTH_DENIED_REASON_TIMEOUT = 3
+uint16 ARM_AUTH_DENIED_REASON_AIRSPACE_IN_USE = 4
+uint16 ARM_AUTH_DENIED_REASON_BAD_WEATHER = 5
+
+uint8 ORB_QUEUE_LENGTH = 8
+
+uint32 command # Command that is being acknowledged
+uint8 result # Command result
+uint8 result_param1 # Also used as progress[%], it can be set with the reason why the command was denied, or the progress percentage when result is MAV_RESULT_IN_PROGRESS
+int32 result_param2 # Additional parameter of the result, example: which parameter of MAV_CMD_NAV_WAYPOINT caused it to be denied.
+uint8 target_system
+uint16 target_component # Target component / mode executor
+
+bool from_external # Indicates if the command came from an external source
+```
+
+:::
diff --git a/docs/ko/msg_docs/VehicleControlMode.md b/docs/ko/msg_docs/VehicleControlMode.md
index 63d54865b1..9cdc1bc6ca 100644
--- a/docs/ko/msg_docs/VehicleControlMode.md
+++ b/docs/ko/msg_docs/VehicleControlMode.md
@@ -29,9 +29,9 @@ pageClass: is-wide-page
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| -------------------------------------------------------------------- | -------- | ----- | -- |
-| MESSAGE_VERSION | `uint32` | 0 | |
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------------ | -------- | ----- | -- |
+| MESSAGE_VERSION | `uint32` | 0 | |
## Source Message
diff --git a/docs/ko/msg_docs/VehicleGlobalPosition.md b/docs/ko/msg_docs/VehicleGlobalPosition.md
index 7e3fcd4f4a..595141025c 100644
--- a/docs/ko/msg_docs/VehicleGlobalPosition.md
+++ b/docs/ko/msg_docs/VehicleGlobalPosition.md
@@ -6,7 +6,7 @@ pageClass: is-wide-page
Fused global position in WGS84. This struct contains global position estimation. It is not the raw GPS. measurement (@see vehicle_gps_position). This topic is usually published by the position. estimator, which will take more sources of information into account than just GPS,. e.g. control inputs of the vehicle in a Kalman-filter implementation.
-**TOPICS:** vehicle_global_position vehicle_global_position_groundtruth external_ins_global_position estimator_global_position aux_global_position
+**TOPICS:** vehicle_global_position vehicle_global_position_groundtruth external_ins_global_position estimator_global_position
## Fields
@@ -33,9 +33,9 @@ Fused global position in WGS84. This struct contains global position estimation.
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| -------------------------------------------------------------------- | -------- | ----- | -- |
-| MESSAGE_VERSION | `uint32` | 0 | |
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------------ | -------- | ----- | -- |
+| MESSAGE_VERSION | `uint32` | 0 | |
## Source Message
@@ -81,7 +81,6 @@ bool dead_reckoning # True if this position is estimated through dead-reckoning
# TOPICS vehicle_global_position vehicle_global_position_groundtruth external_ins_global_position
# TOPICS estimator_global_position
-# TOPICS aux_global_position
```
:::
diff --git a/docs/ko/msg_docs/VehicleGlobalPositionV0.md b/docs/ko/msg_docs/VehicleGlobalPositionV0.md
new file mode 100644
index 0000000000..f27a0c8b4b
--- /dev/null
+++ b/docs/ko/msg_docs/VehicleGlobalPositionV0.md
@@ -0,0 +1,86 @@
+---
+pageClass: is-wide-page
+---
+
+# VehicleGlobalPositionV0 (UORB message)
+
+Fused global position in WGS84. This struct contains global position estimation. It is not the raw GPS. measurement (@see vehicle_gps_position). This topic is usually published by the position. estimator, which will take more sources of information into account than just GPS,. e.g. control inputs of the vehicle in a Kalman-filter implementation.
+
+**TOPICS:** vehicle_global_position vehicle_global_position_groundtruth external_ins_global_position estimator_global_position
+
+## Fields
+
+| 명칭 | 형식 | Unit [Frame] | Range/Enum | 설명 |
+| ------------------------------------------------------------------------------------ | --------- | ---------------------------------------------------------------- | ---------- | ---------------------------------------------------------------------------- |
+| timestamp | `uint64` | | | time since system start (microseconds) |
+| timestamp_sample | `uint64` | | | the timestamp of the raw data (microseconds) |
+| lat | `float64` | | | Latitude, (degrees) |
+| lon | `float64` | | | Longitude, (degrees) |
+| alt | `float32` | | | Altitude AMSL, (meters) |
+| alt_ellipsoid | `float32` | | | Altitude above ellipsoid, (meters) |
+| lat_lon_valid | `bool` | | | |
+| alt_valid | `bool` | | | |
+| delta_alt | `float32` | | | Reset delta for altitude |
+| delta_terrain | `float32` | | | Reset delta for terrain |
+| lat_lon_reset_counter | `uint8` | | | Counter for reset events on horizontal position coordinates |
+| alt_reset_counter | `uint8` | | | Counter for reset events on altitude |
+| terrain_reset_counter | `uint8` | | | Counter for reset events on terrain |
+| eph | `float32` | | | Standard deviation of horizontal position error, (metres) |
+| epv | `float32` | | | Standard deviation of vertical position error, (metres) |
+| terrain_alt | `float32` | | | Terrain altitude WGS84, (metres) |
+| terrain_alt_valid | `bool` | | | Terrain altitude estimate is valid |
+| dead_reckoning | `bool` | | | True if this position is estimated through dead-reckoning |
+
+## Constants
+
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------------ | -------- | ----- | -- |
+| MESSAGE_VERSION | `uint32` | 0 | |
+
+## Source Message
+
+[Source file (GitHub)](https://github.com/PX4/PX4-Autopilot/blob/main/msg/px4_msgs_old/msg/VehicleGlobalPositionV0.msg)
+
+:::details
+Click here to see original file
+
+```c
+# Fused global position in WGS84.
+# This struct contains global position estimation. It is not the raw GPS
+# measurement (@see vehicle_gps_position). This topic is usually published by the position
+# estimator, which will take more sources of information into account than just GPS,
+# e.g. control inputs of the vehicle in a Kalman-filter implementation.
+#
+
+uint32 MESSAGE_VERSION = 0
+
+uint64 timestamp # time since system start (microseconds)
+uint64 timestamp_sample # the timestamp of the raw data (microseconds)
+
+float64 lat # Latitude, (degrees)
+float64 lon # Longitude, (degrees)
+float32 alt # Altitude AMSL, (meters)
+float32 alt_ellipsoid # Altitude above ellipsoid, (meters)
+
+bool lat_lon_valid
+bool alt_valid
+
+float32 delta_alt # Reset delta for altitude
+float32 delta_terrain # Reset delta for terrain
+uint8 lat_lon_reset_counter # Counter for reset events on horizontal position coordinates
+uint8 alt_reset_counter # Counter for reset events on altitude
+uint8 terrain_reset_counter # Counter for reset events on terrain
+
+float32 eph # Standard deviation of horizontal position error, (metres)
+float32 epv # Standard deviation of vertical position error, (metres)
+
+float32 terrain_alt # Terrain altitude WGS84, (metres)
+bool terrain_alt_valid # Terrain altitude estimate is valid
+
+bool dead_reckoning # True if this position is estimated through dead-reckoning
+
+# TOPICS vehicle_global_position vehicle_global_position_groundtruth external_ins_global_position
+# TOPICS estimator_global_position
+```
+
+:::
diff --git a/docs/ko/msg_docs/VehicleImu.md b/docs/ko/msg_docs/VehicleImu.md
index 74520f4fa4..f29254ab4e 100644
--- a/docs/ko/msg_docs/VehicleImu.md
+++ b/docs/ko/msg_docs/VehicleImu.md
@@ -27,11 +27,11 @@ IMU readings in SI-unit form.
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ---------------------------------------------------------- | ------- | ----- | -- |
-| CLIPPING_X | `uint8` | 1 | |
-| CLIPPING_Y | `uint8` | 2 | |
-| CLIPPING_Z | `uint8` | 4 | |
+| 명칭 | 형식 | Value | 설명 |
+| -------------------------------------------------------- | ------- | ----- | -- |
+| CLIPPING_X | `uint8` | 1 | |
+| CLIPPING_Y | `uint8` | 2 | |
+| CLIPPING_Z | `uint8` | 4 | |
## Source Message
diff --git a/docs/ko/msg_docs/VehicleImuStatus.md b/docs/ko/msg_docs/VehicleImuStatus.md
index 7cf1612c42..1acea3a534 100644
--- a/docs/ko/msg_docs/VehicleImuStatus.md
+++ b/docs/ko/msg_docs/VehicleImuStatus.md
@@ -4,7 +4,7 @@ pageClass: is-wide-page
# VehicleImuStatus (UORB message)
-**TOPICS:** vehicle_imustatus
+**TOPICS:** vehicle_imu_status
## Fields
diff --git a/docs/ko/msg_docs/VehicleLandDetected.md b/docs/ko/msg_docs/VehicleLandDetected.md
index b7a3cbd68e..888be3ceb0 100644
--- a/docs/ko/msg_docs/VehicleLandDetected.md
+++ b/docs/ko/msg_docs/VehicleLandDetected.md
@@ -4,7 +4,7 @@ pageClass: is-wide-page
# VehicleLandDetected (UORB message)
-**TOPICS:** vehicle_landdetected
+**TOPICS:** vehicle_land_detected
## Fields
@@ -26,9 +26,9 @@ pageClass: is-wide-page
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| -------------------------------------------------------------------- | -------- | ----- | -- |
-| MESSAGE_VERSION | `uint32` | 0 | |
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------------ | -------- | ----- | -- |
+| MESSAGE_VERSION | `uint32` | 0 | |
## Source Message
diff --git a/docs/ko/msg_docs/VehicleLocalPosition.md b/docs/ko/msg_docs/VehicleLocalPosition.md
index c2d2a179c0..c134a4eaa4 100644
--- a/docs/ko/msg_docs/VehicleLocalPosition.md
+++ b/docs/ko/msg_docs/VehicleLocalPosition.md
@@ -68,12 +68,12 @@ Fused local position in NED. The coordinate system origin is the vehicle positio
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| -------------------------------------------------------------------------------------------------------------------------------- | -------- | ----- | ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ |
-| MESSAGE_VERSION | `uint32` | 1 | |
-| DIST_BOTTOM_SENSOR_NONE | `uint8` | 0 | |
-| DIST_BOTTOM_SENSOR_RANGE | `uint8` | 1 | (1 << 0) a range sensor is used to estimate dist_bottom field |
-| DIST_BOTTOM_SENSOR_FLOW | `uint8` | 2 | (1 << 1) a flow sensor is used to estimate dist_bottom field (mostly fixed-wing use case) |
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------------------------------------------------------------------------ | -------- | ----- | ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ |
+| MESSAGE_VERSION | `uint32` | 1 | |
+| DIST_BOTTOM_SENSOR_NONE | `uint8` | 0 | |
+| DIST_BOTTOM_SENSOR_RANGE | `uint8` | 1 | (1 << 0) a range sensor is used to estimate dist_bottom field |
+| DIST_BOTTOM_SENSOR_FLOW | `uint8` | 2 | (1 << 1) a flow sensor is used to estimate dist_bottom field (mostly fixed-wing use case) |
## Source Message
diff --git a/docs/ko/msg_docs/VehicleLocalPositionSetpoint.md b/docs/ko/msg_docs/VehicleLocalPositionSetpoint.md
index a6015eae16..6455819fdd 100644
--- a/docs/ko/msg_docs/VehicleLocalPositionSetpoint.md
+++ b/docs/ko/msg_docs/VehicleLocalPositionSetpoint.md
@@ -6,7 +6,7 @@ pageClass: is-wide-page
Local position setpoint in NED frame. Telemetry of PID position controller to monitor tracking. NaN means the state was not controlled.
-**TOPICS:** vehicle_localposition_setpoint
+**TOPICS:** vehicle_local_position_setpoint
## Fields
diff --git a/docs/ko/msg_docs/VehicleLocalPositionV0.md b/docs/ko/msg_docs/VehicleLocalPositionV0.md
index f76947c7dd..422846c926 100644
--- a/docs/ko/msg_docs/VehicleLocalPositionV0.md
+++ b/docs/ko/msg_docs/VehicleLocalPositionV0.md
@@ -67,12 +67,12 @@ Fused local position in NED. The coordinate system origin is the vehicle positio
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| -------------------------------------------------------------------------------------------------------------------------------- | -------- | ----- | ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ |
-| MESSAGE_VERSION | `uint32` | 0 | |
-| DIST_BOTTOM_SENSOR_NONE | `uint8` | 0 | |
-| DIST_BOTTOM_SENSOR_RANGE | `uint8` | 1 | (1 << 0) a range sensor is used to estimate dist_bottom field |
-| DIST_BOTTOM_SENSOR_FLOW | `uint8` | 2 | (1 << 1) a flow sensor is used to estimate dist_bottom field (mostly fixed-wing use case) |
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------------------------------------------------------------------------ | -------- | ----- | ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ |
+| MESSAGE_VERSION | `uint32` | 0 | |
+| DIST_BOTTOM_SENSOR_NONE | `uint8` | 0 | |
+| DIST_BOTTOM_SENSOR_RANGE | `uint8` | 1 | (1 << 0) a range sensor is used to estimate dist_bottom field |
+| DIST_BOTTOM_SENSOR_FLOW | `uint8` | 2 | (1 << 1) a flow sensor is used to estimate dist_bottom field (mostly fixed-wing use case) |
## Source Message
diff --git a/docs/ko/msg_docs/VehicleOdometry.md b/docs/ko/msg_docs/VehicleOdometry.md
index 30159d40ef..4b658fb27f 100644
--- a/docs/ko/msg_docs/VehicleOdometry.md
+++ b/docs/ko/msg_docs/VehicleOdometry.md
@@ -32,26 +32,26 @@ Fits ROS REP 147 for aerial vehicles
### POSE_FRAME {#POSE_FRAME}
-| 명칭 | 형식 | Value | 설명 |
-| ----------------------------------------------------------------------------------------------- | ------- | ----- | ---------------------------------------------------------------------------------------------------------------------------------------------------------------- |
-| POSE_FRAME_UNKNOWN | `uint8` | 0 | Unknown frame |
-| POSE_FRAME_NED | `uint8` | 1 | North-East-Down (NED) navigation frame. Aligned with True North. |
-| POSE_FRAME_FRD | `uint8` | 2 | Forward-Right-Down (FRD) frame. Constant arbitrary heading offset from True North. Z is down. |
+| 명칭 | 형식 | Value | 설명 |
+| --------------------------------------------------------------------------------------------- | ------- | ----- | ---------------------------------------------------------------------------------------------------------------------------------------------------------------- |
+| POSE_FRAME_UNKNOWN | `uint8` | 0 | Unknown frame |
+| POSE_FRAME_NED | `uint8` | 1 | North-East-Down (NED) navigation frame. Aligned with True North. |
+| POSE_FRAME_FRD | `uint8` | 2 | Forward-Right-Down (FRD) frame. Constant arbitrary heading offset from True North. Z is down. |
### VELOCITY_FRAME {#VELOCITY_FRAME}
-| 명칭 | 형식 | Value | 설명 |
-| ------------------------------------------------------------------------------------------------------------------------------ | ------- | ----- | ------------------------------------------------------------------------------------------------------------------------------------------------------- |
-| VELOCITY_FRAME_UNKNOWN | `uint8` | 0 | Unknown frame |
-| VELOCITY_FRAME_NED | `uint8` | 1 | NED navigation frame at current position. |
-| VELOCITY_FRAME_FRD | `uint8` | 2 | FRD navigation frame at current position. Constant arbitrary heading offset from True North. Z is down. |
-| VELOCITY_FRAME_BODY_FRD | `uint8` | 3 | FRD body-fixed frame |
+| 명칭 | 형식 | Value | 설명 |
+| ---------------------------------------------------------------------------------------------------------------------------- | ------- | ----- | ------------------------------------------------------------------------------------------------------------------------------------------------------- |
+| VELOCITY_FRAME_UNKNOWN | `uint8` | 0 | Unknown frame |
+| VELOCITY_FRAME_NED | `uint8` | 1 | NED navigation frame at current position. |
+| VELOCITY_FRAME_FRD | `uint8` | 2 | FRD navigation frame at current position. Constant arbitrary heading offset from True North. Z is down. |
+| VELOCITY_FRAME_BODY_FRD | `uint8` | 3 | FRD body-fixed frame |
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| -------------------------------------------------------------------- | -------- | ----- | -- |
-| MESSAGE_VERSION | `uint32` | 0 | |
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------------ | -------- | ----- | -- |
+| MESSAGE_VERSION | `uint32` | 0 | |
## Source Message
diff --git a/docs/ko/msg_docs/VehicleOpticalFlow.md b/docs/ko/msg_docs/VehicleOpticalFlow.md
index 848458e9b6..ce756250a8 100644
--- a/docs/ko/msg_docs/VehicleOpticalFlow.md
+++ b/docs/ko/msg_docs/VehicleOpticalFlow.md
@@ -6,7 +6,7 @@ pageClass: is-wide-page
Optical flow in XYZ body frame in SI units.
-**TOPICS:** vehicle_opticalflow
+**TOPICS:** vehicle_optical_flow
## Fields
diff --git a/docs/ko/msg_docs/VehicleRatesSetpoint.md b/docs/ko/msg_docs/VehicleRatesSetpoint.md
index 9ddb01c33a..9d41d8c560 100644
--- a/docs/ko/msg_docs/VehicleRatesSetpoint.md
+++ b/docs/ko/msg_docs/VehicleRatesSetpoint.md
@@ -4,7 +4,7 @@ pageClass: is-wide-page
# VehicleRatesSetpoint (UORB message)
-**TOPICS:** vehicle_ratessetpoint
+**TOPICS:** vehicle_rates_setpoint
## Fields
@@ -19,9 +19,9 @@ pageClass: is-wide-page
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| -------------------------------------------------------------------- | -------- | ----- | -- |
-| MESSAGE_VERSION | `uint32` | 0 | |
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------------ | -------- | ----- | -- |
+| MESSAGE_VERSION | `uint32` | 0 | |
## Source Message
diff --git a/docs/ko/msg_docs/VehicleRoi.md b/docs/ko/msg_docs/VehicleRoi.md
index f54ffc2be4..3b0c15c68c 100644
--- a/docs/ko/msg_docs/VehicleRoi.md
+++ b/docs/ko/msg_docs/VehicleRoi.md
@@ -23,14 +23,14 @@ Vehicle Region Of Interest (ROI).
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ----------------------------------------------------------------------------------- | ------- | ----- | ---------------------------------------------- |
-| ROI_NONE | `uint8` | 0 | No region of interest |
-| ROI_WPNEXT | `uint8` | 1 | Point toward next MISSION with optional offset |
-| ROI_WPINDEX | `uint8` | 2 | Point toward given MISSION |
-| ROI_LOCATION | `uint8` | 3 | Point toward fixed location |
-| ROI_TARGET | `uint8` | 4 | Point toward target |
-| ROI_ENUM_END | `uint8` | 5 | |
+| 명칭 | 형식 | Value | 설명 |
+| --------------------------------------------------------------------------------- | ------- | ----- | ---------------------------------------------- |
+| ROI_NONE | `uint8` | 0 | No region of interest |
+| ROI_WPNEXT | `uint8` | 1 | Point toward next MISSION with optional offset |
+| ROI_WPINDEX | `uint8` | 2 | Point toward given MISSION |
+| ROI_LOCATION | `uint8` | 3 | Point toward fixed location |
+| ROI_TARGET | `uint8` | 4 | Point toward target |
+| ROI_ENUM_END | `uint8` | 5 | |
## Source Message
diff --git a/docs/ko/msg_docs/VehicleStatus.md b/docs/ko/msg_docs/VehicleStatus.md
index d7663812c3..5051665bcd 100644
--- a/docs/ko/msg_docs/VehicleStatus.md
+++ b/docs/ko/msg_docs/VehicleStatus.md
@@ -22,6 +22,7 @@ Encodes the system state of the vehicle published by commander.
| nav_state_user_intention | `uint8` | | | Mode that the user selected (might be different from nav_state in a failsafe situation) |
| nav_state | `uint8` | | | Currently active mode |
| executor_in_charge | `uint8` | | | Current mode executor in charge (0=Autopilot) |
+| nav_state_display | `uint8` | | | User-visible nav state sent via MAVLink (executor state if active, otherwise nav_state) |
| valid_nav_states_mask | `uint32` | | | Bitmask for all valid nav_state values |
| can_set_nav_states_mask | `uint32` | | | Bitmask for all modes that a user can select |
| failure_detector_status | `uint16` | | | |
@@ -48,77 +49,78 @@ Encodes the system state of the vehicle published by commander.
| open_drone_id_system_healthy | `bool` | | | |
| parachute_system_present | `bool` | | | |
| parachute_system_healthy | `bool` | | | |
+| traffic_avoidance_system_present | `bool` | | | |
| rc_calibration_in_progress | `bool` | | | |
| calibration_enabled | `bool` | | | |
| pre_flight_checks_pass | `bool` | | | true if all checks necessary to arm pass |
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ----------------------------------------------------------------------------------------------------------------------------------------------------------------------------- | -------- | ----- | ----------------------------------------------------------------------------- |
-| MESSAGE_VERSION | `uint32` | 1 | |
-| ARMING_STATE_DISARMED | `uint8` | 1 | |
-| ARMING_STATE_ARMED | `uint8` | 2 | |
-| ARM_DISARM_REASON_STICK_GESTURE | `uint8` | 1 | |
-| ARM_DISARM_REASON_RC_SWITCH | `uint8` | 2 | |
-| ARM_DISARM_REASON_COMMAND_INTERNAL | `uint8` | 3 | |
-| ARM_DISARM_REASON_COMMAND_EXTERNAL | `uint8` | 4 | |
-| ARM_DISARM_REASON_MISSION_START | `uint8` | 5 | |
-| ARM_DISARM_REASON_LANDING | `uint8` | 6 | |
-| ARM_DISARM_REASON_PREFLIGHT_INACTION | `uint8` | 7 | |
-| ARM_DISARM_REASON_KILL_SWITCH | `uint8` | 8 | |
-| ARM_DISARM_REASON_RC_BUTTON | `uint8` | 13 | |
-| ARM_DISARM_REASON_FAILSAFE | `uint8` | 14 | |
-| NAVIGATION_STATE_MANUAL | `uint8` | 0 | Manual mode |
-| NAVIGATION_STATE_ALTCTL | `uint8` | 1 | Altitude control mode |
-| NAVIGATION_STATE_POSCTL | `uint8` | 2 | Position control mode |
-| NAVIGATION_STATE_AUTO_MISSION | `uint8` | 3 | Auto mission mode |
-| NAVIGATION_STATE_AUTO_LOITER | `uint8` | 4 | Auto loiter mode |
-| NAVIGATION_STATE_AUTO_RTL | `uint8` | 5 | Auto return to launch mode |
-| NAVIGATION_STATE_POSITION_SLOW | `uint8` | 6 | |
-| NAVIGATION_STATE_FREE5 | `uint8` | 7 | |
-| NAVIGATION_STATE_ALTITUDE_CRUISE | `uint8` | 8 | Altitude with Cruise mode |
-| NAVIGATION_STATE_FREE3 | `uint8` | 9 | |
-| NAVIGATION_STATE_ACRO | `uint8` | 10 | Acro mode |
-| NAVIGATION_STATE_FREE2 | `uint8` | 11 | |
-| NAVIGATION_STATE_DESCEND | `uint8` | 12 | Descend mode (no position control) |
-| NAVIGATION_STATE_TERMINATION | `uint8` | 13 | Termination mode |
-| NAVIGATION_STATE_OFFBOARD | `uint8` | 14 | |
-| NAVIGATION_STATE_STAB | `uint8` | 15 | Stabilized mode |
-| NAVIGATION_STATE_FREE1 | `uint8` | 16 | |
-| NAVIGATION_STATE_AUTO_TAKEOFF | `uint8` | 17 | Takeoff |
-| NAVIGATION_STATE_AUTO_LAND | `uint8` | 18 | Land |
-| NAVIGATION_STATE_AUTO_FOLLOW_TARGET | `uint8` | 19 | Auto Follow |
-| NAVIGATION_STATE_AUTO_PRECLAND | `uint8` | 20 | Precision land with landing target |
-| NAVIGATION_STATE_ORBIT | `uint8` | 21 | Orbit in a circle |
-| NAVIGATION_STATE_AUTO_VTOL_TAKEOFF | `uint8` | 22 | Takeoff, transition, establish loiter |
-| NAVIGATION_STATE_EXTERNAL1 | `uint8` | 23 | |
-| NAVIGATION_STATE_EXTERNAL2 | `uint8` | 24 | |
-| NAVIGATION_STATE_EXTERNAL3 | `uint8` | 25 | |
-| NAVIGATION_STATE_EXTERNAL4 | `uint8` | 26 | |
-| NAVIGATION_STATE_EXTERNAL5 | `uint8` | 27 | |
-| NAVIGATION_STATE_EXTERNAL6 | `uint8` | 28 | |
-| NAVIGATION_STATE_EXTERNAL7 | `uint8` | 29 | |
-| NAVIGATION_STATE_EXTERNAL8 | `uint8` | 30 | |
-| NAVIGATION_STATE_MAX | `uint8` | 31 | |
-| FAILURE_NONE | `uint16` | 0 | |
-| FAILURE_ROLL | `uint16` | 1 | (1 << 0) |
-| FAILURE_PITCH | `uint16` | 2 | (1 << 1) |
-| FAILURE_ALT | `uint16` | 4 | (1 << 2) |
-| FAILURE_EXT | `uint16` | 8 | (1 << 3) |
-| FAILURE_ARM_ESC | `uint16` | 16 | (1 << 4) |
-| FAILURE_BATTERY | `uint16` | 32 | (1 << 5) |
-| FAILURE_IMBALANCED_PROP | `uint16` | 64 | (1 << 6) |
-| FAILURE_MOTOR | `uint16` | 128 | (1 << 7) |
-| HIL_STATE_OFF | `uint8` | 0 | |
-| HIL_STATE_ON | `uint8` | 1 | |
-| VEHICLE_TYPE_UNSPECIFIED | `uint8` | 0 | |
-| VEHICLE_TYPE_ROTARY_WING | `uint8` | 1 | |
-| VEHICLE_TYPE_FIXED_WING | `uint8` | 2 | |
-| VEHICLE_TYPE_ROVER | `uint8` | 3 | |
-| FAILSAFE_DEFER_STATE_DISABLED | `uint8` | 0 | |
-| FAILSAFE_DEFER_STATE_ENABLED | `uint8` | 1 | |
-| FAILSAFE_DEFER_STATE_WOULD_FAILSAFE | `uint8` | 2 | Failsafes deferred, but would trigger a failsafe |
+| 명칭 | 형식 | Value | 설명 |
+| --------------------------------------------------------------------------------------------------------------------------------------------------------------------------- | -------- | ----- | ----------------------------------------------------------------------------- |
+| MESSAGE_VERSION | `uint32` | 2 | |
+| ARMING_STATE_DISARMED | `uint8` | 1 | |
+| ARMING_STATE_ARMED | `uint8` | 2 | |
+| ARM_DISARM_REASON_STICK_GESTURE | `uint8` | 1 | |
+| ARM_DISARM_REASON_RC_SWITCH | `uint8` | 2 | |
+| ARM_DISARM_REASON_COMMAND_INTERNAL | `uint8` | 3 | |
+| ARM_DISARM_REASON_COMMAND_EXTERNAL | `uint8` | 4 | |
+| ARM_DISARM_REASON_MISSION_START | `uint8` | 5 | |
+| ARM_DISARM_REASON_LANDING | `uint8` | 6 | |
+| ARM_DISARM_REASON_PREFLIGHT_INACTION | `uint8` | 7 | |
+| ARM_DISARM_REASON_KILL_SWITCH | `uint8` | 8 | |
+| ARM_DISARM_REASON_RC_BUTTON | `uint8` | 13 | |
+| ARM_DISARM_REASON_FAILSAFE | `uint8` | 14 | |
+| NAVIGATION_STATE_MANUAL | `uint8` | 0 | Manual mode |
+| NAVIGATION_STATE_ALTCTL | `uint8` | 1 | Altitude control mode |
+| NAVIGATION_STATE_POSCTL | `uint8` | 2 | Position control mode |
+| NAVIGATION_STATE_AUTO_MISSION | `uint8` | 3 | Auto mission mode |
+| NAVIGATION_STATE_AUTO_LOITER | `uint8` | 4 | Auto loiter mode |
+| NAVIGATION_STATE_AUTO_RTL | `uint8` | 5 | Auto return to launch mode |
+| NAVIGATION_STATE_POSITION_SLOW | `uint8` | 6 | |
+| NAVIGATION_STATE_FREE5 | `uint8` | 7 | |
+| NAVIGATION_STATE_ALTITUDE_CRUISE | `uint8` | 8 | Altitude with Cruise mode |
+| NAVIGATION_STATE_FREE3 | `uint8` | 9 | |
+| NAVIGATION_STATE_ACRO | `uint8` | 10 | Acro mode |
+| NAVIGATION_STATE_FREE2 | `uint8` | 11 | |
+| NAVIGATION_STATE_DESCEND | `uint8` | 12 | Descend mode (no position control) |
+| NAVIGATION_STATE_TERMINATION | `uint8` | 13 | Termination mode |
+| NAVIGATION_STATE_OFFBOARD | `uint8` | 14 | |
+| NAVIGATION_STATE_STAB | `uint8` | 15 | Stabilized mode |
+| NAVIGATION_STATE_FREE1 | `uint8` | 16 | |
+| NAVIGATION_STATE_AUTO_TAKEOFF | `uint8` | 17 | Takeoff |
+| NAVIGATION_STATE_AUTO_LAND | `uint8` | 18 | Land |
+| NAVIGATION_STATE_AUTO_FOLLOW_TARGET | `uint8` | 19 | Auto Follow |
+| NAVIGATION_STATE_AUTO_PRECLAND | `uint8` | 20 | Precision land with landing target |
+| NAVIGATION_STATE_ORBIT | `uint8` | 21 | Orbit in a circle |
+| NAVIGATION_STATE_AUTO_VTOL_TAKEOFF | `uint8` | 22 | Takeoff, transition, establish loiter |
+| NAVIGATION_STATE_EXTERNAL1 | `uint8` | 23 | |
+| NAVIGATION_STATE_EXTERNAL2 | `uint8` | 24 | |
+| NAVIGATION_STATE_EXTERNAL3 | `uint8` | 25 | |
+| NAVIGATION_STATE_EXTERNAL4 | `uint8` | 26 | |
+| NAVIGATION_STATE_EXTERNAL5 | `uint8` | 27 | |
+| NAVIGATION_STATE_EXTERNAL6 | `uint8` | 28 | |
+| NAVIGATION_STATE_EXTERNAL7 | `uint8` | 29 | |
+| NAVIGATION_STATE_EXTERNAL8 | `uint8` | 30 | |
+| NAVIGATION_STATE_MAX | `uint8` | 31 | |
+| FAILURE_NONE | `uint16` | 0 | |
+| FAILURE_ROLL | `uint16` | 1 | (1 << 0) |
+| FAILURE_PITCH | `uint16` | 2 | (1 << 1) |
+| FAILURE_ALT | `uint16` | 4 | (1 << 2) |
+| FAILURE_EXT | `uint16` | 8 | (1 << 3) |
+| FAILURE_ARM_ESC | `uint16` | 16 | (1 << 4) |
+| FAILURE_BATTERY | `uint16` | 32 | (1 << 5) |
+| FAILURE_IMBALANCED_PROP | `uint16` | 64 | (1 << 6) |
+| FAILURE_MOTOR | `uint16` | 128 | (1 << 7) |
+| HIL_STATE_OFF | `uint8` | 0 | |
+| HIL_STATE_ON | `uint8` | 1 | |
+| VEHICLE_TYPE_UNSPECIFIED | `uint8` | 0 | |
+| VEHICLE_TYPE_ROTARY_WING | `uint8` | 1 | |
+| VEHICLE_TYPE_FIXED_WING | `uint8` | 2 | |
+| VEHICLE_TYPE_ROVER | `uint8` | 3 | |
+| FAILSAFE_DEFER_STATE_DISABLED | `uint8` | 0 | |
+| FAILSAFE_DEFER_STATE_ENABLED | `uint8` | 1 | |
+| FAILSAFE_DEFER_STATE_WOULD_FAILSAFE | `uint8` | 2 | Failsafes deferred, but would trigger a failsafe |
## Source Message
@@ -130,7 +132,7 @@ Click here to see original file
```c
# Encodes the system state of the vehicle published by commander
-uint32 MESSAGE_VERSION = 1
+uint32 MESSAGE_VERSION = 2
uint64 timestamp # time since system start (microseconds)
@@ -193,6 +195,7 @@ uint8 NAVIGATION_STATE_EXTERNAL8 = 30
uint8 NAVIGATION_STATE_MAX = 31
uint8 executor_in_charge # Current mode executor in charge (0=Autopilot)
+uint8 nav_state_display # User-visible nav state sent via MAVLink (executor state if active, otherwise nav_state)
uint32 valid_nav_states_mask # Bitmask for all valid nav_state values
uint32 can_set_nav_states_mask # Bitmask for all modes that a user can select
@@ -256,6 +259,8 @@ bool open_drone_id_system_healthy
bool parachute_system_present
bool parachute_system_healthy
+bool traffic_avoidance_system_present
+
bool rc_calibration_in_progress
bool calibration_enabled
diff --git a/docs/ko/msg_docs/VehicleStatusV0.md b/docs/ko/msg_docs/VehicleStatusV0.md
index c3d872ff41..b1fba4c292 100644
--- a/docs/ko/msg_docs/VehicleStatusV0.md
+++ b/docs/ko/msg_docs/VehicleStatusV0.md
@@ -6,7 +6,7 @@ pageClass: is-wide-page
Encodes the system state of the vehicle published by commander.
-**TOPICS:** vehicle_statusv0
+**TOPICS:** vehicle_status_v0
## Fields
@@ -56,76 +56,76 @@ Encodes the system state of the vehicle published by commander.
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- | -------- | ----- | ----------------------------------------------------------------------------- |
-| MESSAGE_VERSION | `uint32` | 0 | |
-| ARMING_STATE_DISARMED | `uint8` | 1 | |
-| ARMING_STATE_ARMED | `uint8` | 2 | |
-| ARM_DISARM_REASON_TRANSITION_TO_STANDBY | `uint8` | 0 | |
-| ARM_DISARM_REASON_STICK_GESTURE | `uint8` | 1 | |
-| ARM_DISARM_REASON_RC_SWITCH | `uint8` | 2 | |
-| ARM_DISARM_REASON_COMMAND_INTERNAL | `uint8` | 3 | |
-| ARM_DISARM_REASON_COMMAND_EXTERNAL | `uint8` | 4 | |
-| ARM_DISARM_REASON_MISSION_START | `uint8` | 5 | |
-| ARM_DISARM_REASON_SAFETY_BUTTON | `uint8` | 6 | |
-| ARM_DISARM_REASON_AUTO_DISARM_LAND | `uint8` | 7 | |
-| ARM_DISARM_REASON_AUTO_DISARM_PREFLIGHT | `uint8` | 8 | |
-| ARM_DISARM_REASON_KILL_SWITCH | `uint8` | 9 | |
-| ARM_DISARM_REASON_LOCKDOWN | `uint8` | 10 | |
-| ARM_DISARM_REASON_FAILURE_DETECTOR | `uint8` | 11 | |
-| ARM_DISARM_REASON_SHUTDOWN | `uint8` | 12 | |
-| ARM_DISARM_REASON_UNIT_TEST | `uint8` | 13 | |
-| NAVIGATION_STATE_MANUAL | `uint8` | 0 | Manual mode |
-| NAVIGATION_STATE_ALTCTL | `uint8` | 1 | Altitude control mode |
-| NAVIGATION_STATE_POSCTL | `uint8` | 2 | Position control mode |
-| NAVIGATION_STATE_AUTO_MISSION | `uint8` | 3 | Auto mission mode |
-| NAVIGATION_STATE_AUTO_LOITER | `uint8` | 4 | Auto loiter mode |
-| NAVIGATION_STATE_AUTO_RTL | `uint8` | 5 | Auto return to launch mode |
-| NAVIGATION_STATE_POSITION_SLOW | `uint8` | 6 | |
-| NAVIGATION_STATE_FREE5 | `uint8` | 7 | |
-| NAVIGATION_STATE_FREE4 | `uint8` | 8 | |
-| NAVIGATION_STATE_FREE3 | `uint8` | 9 | |
-| NAVIGATION_STATE_ACRO | `uint8` | 10 | Acro mode |
-| NAVIGATION_STATE_FREE2 | `uint8` | 11 | |
-| NAVIGATION_STATE_DESCEND | `uint8` | 12 | Descend mode (no position control) |
-| NAVIGATION_STATE_TERMINATION | `uint8` | 13 | Termination mode |
-| NAVIGATION_STATE_OFFBOARD | `uint8` | 14 | |
-| NAVIGATION_STATE_STAB | `uint8` | 15 | Stabilized mode |
-| NAVIGATION_STATE_FREE1 | `uint8` | 16 | |
-| NAVIGATION_STATE_AUTO_TAKEOFF | `uint8` | 17 | Takeoff |
-| NAVIGATION_STATE_AUTO_LAND | `uint8` | 18 | Land |
-| NAVIGATION_STATE_AUTO_FOLLOW_TARGET | `uint8` | 19 | Auto Follow |
-| NAVIGATION_STATE_AUTO_PRECLAND | `uint8` | 20 | Precision land with landing target |
-| NAVIGATION_STATE_ORBIT | `uint8` | 21 | Orbit in a circle |
-| NAVIGATION_STATE_AUTO_VTOL_TAKEOFF | `uint8` | 22 | Takeoff, transition, establish loiter |
-| NAVIGATION_STATE_EXTERNAL1 | `uint8` | 23 | |
-| NAVIGATION_STATE_EXTERNAL2 | `uint8` | 24 | |
-| NAVIGATION_STATE_EXTERNAL3 | `uint8` | 25 | |
-| NAVIGATION_STATE_EXTERNAL4 | `uint8` | 26 | |
-| NAVIGATION_STATE_EXTERNAL5 | `uint8` | 27 | |
-| NAVIGATION_STATE_EXTERNAL6 | `uint8` | 28 | |
-| NAVIGATION_STATE_EXTERNAL7 | `uint8` | 29 | |
-| NAVIGATION_STATE_EXTERNAL8 | `uint8` | 30 | |
-| NAVIGATION_STATE_MAX | `uint8` | 31 | |
-| FAILURE_NONE | `uint16` | 0 | |
-| FAILURE_ROLL | `uint16` | 1 | (1 << 0) |
-| FAILURE_PITCH | `uint16` | 2 | (1 << 1) |
-| FAILURE_ALT | `uint16` | 4 | (1 << 2) |
-| FAILURE_EXT | `uint16` | 8 | (1 << 3) |
-| FAILURE_ARM_ESC | `uint16` | 16 | (1 << 4) |
-| FAILURE_BATTERY | `uint16` | 32 | (1 << 5) |
-| FAILURE_IMBALANCED_PROP | `uint16` | 64 | (1 << 6) |
-| FAILURE_MOTOR | `uint16` | 128 | (1 << 7) |
-| HIL_STATE_OFF | `uint8` | 0 | |
-| HIL_STATE_ON | `uint8` | 1 | |
-| VEHICLE_TYPE_UNKNOWN | `uint8` | 0 | |
-| VEHICLE_TYPE_ROTARY_WING | `uint8` | 1 | |
-| VEHICLE_TYPE_FIXED_WING | `uint8` | 2 | |
-| VEHICLE_TYPE_ROVER | `uint8` | 3 | |
-| VEHICLE_TYPE_AIRSHIP | `uint8` | 4 | |
-| FAILSAFE_DEFER_STATE_DISABLED | `uint8` | 0 | |
-| FAILSAFE_DEFER_STATE_ENABLED | `uint8` | 1 | |
-| FAILSAFE_DEFER_STATE_WOULD_FAILSAFE | `uint8` | 2 | Failsafes deferred, but would trigger a failsafe |
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ | -------- | ----- | ----------------------------------------------------------------------------- |
+| MESSAGE_VERSION | `uint32` | 0 | |
+| ARMING_STATE_DISARMED | `uint8` | 1 | |
+| ARMING_STATE_ARMED | `uint8` | 2 | |
+| ARM_DISARM_REASON_TRANSITION_TO_STANDBY | `uint8` | 0 | |
+| ARM_DISARM_REASON_STICK_GESTURE | `uint8` | 1 | |
+| ARM_DISARM_REASON_RC_SWITCH | `uint8` | 2 | |
+| ARM_DISARM_REASON_COMMAND_INTERNAL | `uint8` | 3 | |
+| ARM_DISARM_REASON_COMMAND_EXTERNAL | `uint8` | 4 | |
+| ARM_DISARM_REASON_MISSION_START | `uint8` | 5 | |
+| ARM_DISARM_REASON_SAFETY_BUTTON | `uint8` | 6 | |
+| ARM_DISARM_REASON_AUTO_DISARM_LAND | `uint8` | 7 | |
+| ARM_DISARM_REASON_AUTO_DISARM_PREFLIGHT | `uint8` | 8 | |
+| ARM_DISARM_REASON_KILL_SWITCH | `uint8` | 9 | |
+| ARM_DISARM_REASON_LOCKDOWN | `uint8` | 10 | |
+| ARM_DISARM_REASON_FAILURE_DETECTOR | `uint8` | 11 | |
+| ARM_DISARM_REASON_SHUTDOWN | `uint8` | 12 | |
+| ARM_DISARM_REASON_UNIT_TEST | `uint8` | 13 | |
+| NAVIGATION_STATE_MANUAL | `uint8` | 0 | Manual mode |
+| NAVIGATION_STATE_ALTCTL | `uint8` | 1 | Altitude control mode |
+| NAVIGATION_STATE_POSCTL | `uint8` | 2 | Position control mode |
+| NAVIGATION_STATE_AUTO_MISSION | `uint8` | 3 | Auto mission mode |
+| NAVIGATION_STATE_AUTO_LOITER | `uint8` | 4 | Auto loiter mode |
+| NAVIGATION_STATE_AUTO_RTL | `uint8` | 5 | Auto return to launch mode |
+| NAVIGATION_STATE_POSITION_SLOW | `uint8` | 6 | |
+| NAVIGATION_STATE_FREE5 | `uint8` | 7 | |
+| NAVIGATION_STATE_FREE4 | `uint8` | 8 | |
+| NAVIGATION_STATE_FREE3 | `uint8` | 9 | |
+| NAVIGATION_STATE_ACRO | `uint8` | 10 | Acro mode |
+| NAVIGATION_STATE_FREE2 | `uint8` | 11 | |
+| NAVIGATION_STATE_DESCEND | `uint8` | 12 | Descend mode (no position control) |
+| NAVIGATION_STATE_TERMINATION | `uint8` | 13 | Termination mode |
+| NAVIGATION_STATE_OFFBOARD | `uint8` | 14 | |
+| NAVIGATION_STATE_STAB | `uint8` | 15 | Stabilized mode |
+| NAVIGATION_STATE_FREE1 | `uint8` | 16 | |
+| NAVIGATION_STATE_AUTO_TAKEOFF | `uint8` | 17 | Takeoff |
+| NAVIGATION_STATE_AUTO_LAND | `uint8` | 18 | Land |
+| NAVIGATION_STATE_AUTO_FOLLOW_TARGET | `uint8` | 19 | Auto Follow |
+| NAVIGATION_STATE_AUTO_PRECLAND | `uint8` | 20 | Precision land with landing target |
+| NAVIGATION_STATE_ORBIT | `uint8` | 21 | Orbit in a circle |
+| NAVIGATION_STATE_AUTO_VTOL_TAKEOFF | `uint8` | 22 | Takeoff, transition, establish loiter |
+| NAVIGATION_STATE_EXTERNAL1 | `uint8` | 23 | |
+| NAVIGATION_STATE_EXTERNAL2 | `uint8` | 24 | |
+| NAVIGATION_STATE_EXTERNAL3 | `uint8` | 25 | |
+| NAVIGATION_STATE_EXTERNAL4 | `uint8` | 26 | |
+| NAVIGATION_STATE_EXTERNAL5 | `uint8` | 27 | |
+| NAVIGATION_STATE_EXTERNAL6 | `uint8` | 28 | |
+| NAVIGATION_STATE_EXTERNAL7 | `uint8` | 29 | |
+| NAVIGATION_STATE_EXTERNAL8 | `uint8` | 30 | |
+| NAVIGATION_STATE_MAX | `uint8` | 31 | |
+| FAILURE_NONE | `uint16` | 0 | |
+| FAILURE_ROLL | `uint16` | 1 | (1 << 0) |
+| FAILURE_PITCH | `uint16` | 2 | (1 << 1) |
+| FAILURE_ALT | `uint16` | 4 | (1 << 2) |
+| FAILURE_EXT | `uint16` | 8 | (1 << 3) |
+| FAILURE_ARM_ESC | `uint16` | 16 | (1 << 4) |
+| FAILURE_BATTERY | `uint16` | 32 | (1 << 5) |
+| FAILURE_IMBALANCED_PROP | `uint16` | 64 | (1 << 6) |
+| FAILURE_MOTOR | `uint16` | 128 | (1 << 7) |
+| HIL_STATE_OFF | `uint8` | 0 | |
+| HIL_STATE_ON | `uint8` | 1 | |
+| VEHICLE_TYPE_UNKNOWN | `uint8` | 0 | |
+| VEHICLE_TYPE_ROTARY_WING | `uint8` | 1 | |
+| VEHICLE_TYPE_FIXED_WING | `uint8` | 2 | |
+| VEHICLE_TYPE_ROVER | `uint8` | 3 | |
+| VEHICLE_TYPE_AIRSHIP | `uint8` | 4 | |
+| FAILSAFE_DEFER_STATE_DISABLED | `uint8` | 0 | |
+| FAILSAFE_DEFER_STATE_ENABLED | `uint8` | 1 | |
+| FAILSAFE_DEFER_STATE_WOULD_FAILSAFE | `uint8` | 2 | Failsafes deferred, but would trigger a failsafe |
## Source Message
diff --git a/docs/ko/msg_docs/VehicleStatusV1.md b/docs/ko/msg_docs/VehicleStatusV1.md
new file mode 100644
index 0000000000..c9d37c611e
--- /dev/null
+++ b/docs/ko/msg_docs/VehicleStatusV1.md
@@ -0,0 +1,287 @@
+---
+pageClass: is-wide-page
+---
+
+# VehicleStatusV1 (UORB message)
+
+Encodes the system state of the vehicle published by commander.
+
+**TOPICS:** vehicle_status_v1
+
+## Fields
+
+| 명칭 | 형식 | Unit [Frame] | Range/Enum | 설명 |
+| ---------------------------------------------------------------------------------------------------------------- | -------- | ---------------------------------------------------------------- | --------------------------------------------------------------------------------------- | ---------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- |
+| timestamp | `uint64` | us | | Time since system start |
+| armed_time | `uint64` | us | | Arming timestamp |
+| takeoff_time | `uint64` | us | | Takeoff timestamp |
+| arming_state | `uint8` | | | |
+| latest_arming_reason | `uint8` | | | |
+| latest_disarming_reason | `uint8` | | | |
+| nav_state_timestamp | `uint64` | | | Time when current nav_state activated |
+| nav_state_user_intention | `uint8` | | | Mode that the user selected (might be different from nav_state in a failsafe situation) |
+| nav_state | `uint8` | | [NAVIGATION_STATE](#NAVIGATION_STATE) | Currently active mode |
+| executor_in_charge | `uint8` | | | Current mode executor in charge (0=Autopilot) |
+| valid_nav_states_mask | `uint32` | | | Bitmask for all valid nav_state values |
+| can_set_nav_states_mask | `uint32` | | | Bitmask for all modes that a user can select |
+| failure_detector_status | `uint16` | | [FAILURE](#FAILURE) | |
+| hil_state | `uint8` | enum HIL_STATE | | |
+| vehicle_type | `uint8` | | [VEHICLE_TYPE](#VEHICLE_TYPE) | |
+| failsafe | `bool` | | | true if system is in failsafe state (e.g.:RTL, Hover, Terminate, ...) |
+| failsafe_and_user_took_over | `bool` | | | true if system is in failsafe state but the user took over control |
+| failsafe_defer_state | `uint8` | | [FAILSAFE_DEFER_STATE](#FAILSAFE_DEFER_STATE) | |
+| gcs_connection_lost | `bool` | | | datalink to GCS lost |
+| gcs_connection_lost_counter | `uint8` | | | counts unique GCS connection lost events |
+| high_latency_data_link_lost | `bool` | | | Set to true if the high latency data link (eg. RockBlock Iridium 9603 telemetry module) is lost |
+| is_vtol | `bool` | | | True if the system is VTOL capable |
+| is_vtol_tailsitter | `bool` | | | True if the system performs a 90° pitch down rotation during transition from MC to FW |
+| in_transition_mode | `bool` | | | True if VTOL is doing a transition |
+| in_transition_to_fw | `bool` | | | True if VTOL is doing a transition from MC to FW |
+| system_type | `uint8` | | | system type, contains mavlink MAV_TYPE |
+| system_id | `uint8` | | | system id, contains MAVLink's system ID field |
+| component_id | `uint8` | | | subsystem / component id, contains MAVLink's component ID field |
+| safety_button_available | `bool` | | | Set to true if a safety button is connected |
+| safety_off | `bool` | | | Set to true if safety is off |
+| power_input_valid | `bool` | | | Set if input power is valid |
+| usb_connected | `bool` | | | Set to true (never cleared) once telemetry received from usb link |
+| open_drone_id_system_present | `bool` | | | |
+| open_drone_id_system_healthy | `bool` | | | |
+| parachute_system_present | `bool` | | | |
+| parachute_system_healthy | `bool` | | | |
+| rc_calibration_in_progress | `bool` | | | |
+| calibration_enabled | `bool` | | | |
+| pre_flight_checks_pass | `bool` | | | true if all checks necessary to arm pass |
+
+## Enums
+
+### NAVIGATION_STATE {#NAVIGATION_STATE}
+
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------------------------------------------------------------------------------------------------------------------- | ------- | ----- | ----------------------------------------------------- |
+| NAVIGATION_STATE_MANUAL | `uint8` | 0 | Manual mode |
+| NAVIGATION_STATE_ALTCTL | `uint8` | 1 | Altitude control mode |
+| NAVIGATION_STATE_POSCTL | `uint8` | 2 | Position control mode |
+| NAVIGATION_STATE_AUTO_MISSION | `uint8` | 3 | Auto mission mode |
+| NAVIGATION_STATE_AUTO_LOITER | `uint8` | 4 | Auto loiter mode |
+| NAVIGATION_STATE_AUTO_RTL | `uint8` | 5 | Auto return to launch mode |
+| NAVIGATION_STATE_POSITION_SLOW | `uint8` | 6 | |
+| NAVIGATION_STATE_FREE5 | `uint8` | 7 | |
+| NAVIGATION_STATE_ALTITUDE_CRUISE | `uint8` | 8 | Altitude with Cruise mode |
+| NAVIGATION_STATE_FREE3 | `uint8` | 9 | |
+| NAVIGATION_STATE_ACRO | `uint8` | 10 | Acro mode |
+| NAVIGATION_STATE_FREE2 | `uint8` | 11 | |
+| NAVIGATION_STATE_DESCEND | `uint8` | 12 | Descend mode (no position control) |
+| NAVIGATION_STATE_TERMINATION | `uint8` | 13 | Termination mode |
+| NAVIGATION_STATE_OFFBOARD | `uint8` | 14 | |
+| NAVIGATION_STATE_STAB | `uint8` | 15 | Stabilized mode |
+| NAVIGATION_STATE_FREE1 | `uint8` | 16 | |
+| NAVIGATION_STATE_AUTO_TAKEOFF | `uint8` | 17 | Takeoff |
+| NAVIGATION_STATE_AUTO_LAND | `uint8` | 18 | Land |
+| NAVIGATION_STATE_AUTO_FOLLOW_TARGET | `uint8` | 19 | Auto Follow |
+| NAVIGATION_STATE_AUTO_PRECLAND | `uint8` | 20 | Precision land with landing target |
+| NAVIGATION_STATE_ORBIT | `uint8` | 21 | Orbit in a circle |
+| NAVIGATION_STATE_AUTO_VTOL_TAKEOFF | `uint8` | 22 | Takeoff, transition, establish loiter |
+| NAVIGATION_STATE_EXTERNAL1 | `uint8` | 23 | |
+| NAVIGATION_STATE_EXTERNAL2 | `uint8` | 24 | |
+| NAVIGATION_STATE_EXTERNAL3 | `uint8` | 25 | |
+| NAVIGATION_STATE_EXTERNAL4 | `uint8` | 26 | |
+| NAVIGATION_STATE_EXTERNAL5 | `uint8` | 27 | |
+| NAVIGATION_STATE_EXTERNAL6 | `uint8` | 28 | |
+| NAVIGATION_STATE_EXTERNAL7 | `uint8` | 29 | |
+| NAVIGATION_STATE_EXTERNAL8 | `uint8` | 30 | |
+| NAVIGATION_STATE_MAX | `uint8` | 31 | |
+
+### FAILURE {#FAILURE}
+
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------------------------------------------------- | -------- | ----- | ----------------------------------------------------------------------------- |
+| FAILURE_NONE | `uint16` | 0 | |
+| FAILURE_ROLL | `uint16` | 1 | (1 << 0) |
+| FAILURE_PITCH | `uint16` | 2 | (1 << 1) |
+| FAILURE_ALT | `uint16` | 4 | (1 << 2) |
+| FAILURE_EXT | `uint16` | 8 | (1 << 3) |
+| FAILURE_ARM_ESC | `uint16` | 16 | (1 << 4) |
+| FAILURE_BATTERY | `uint16` | 32 | (1 << 5) |
+| FAILURE_IMBALANCED_PROP | `uint16` | 64 | (1 << 6) |
+| FAILURE_MOTOR | `uint16` | 128 | (1 << 7) |
+
+### VEHICLE_TYPE {#VEHICLE_TYPE}
+
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------------------------------------------------------------------------ | ------- | ----- | -- |
+| VEHICLE_TYPE_UNSPECIFIED | `uint8` | 0 | |
+| VEHICLE_TYPE_ROTARY_WING | `uint8` | 1 | |
+| VEHICLE_TYPE_FIXED_WING | `uint8` | 2 | |
+| VEHICLE_TYPE_ROVER | `uint8` | 3 | |
+
+### FAILSAFE_DEFER_STATE {#FAILSAFE_DEFER_STATE}
+
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------------------------------------------------------------------------------------------------------------------- | ------- | ----- | ------------------------------------------------ |
+| FAILSAFE_DEFER_STATE_DISABLED | `uint8` | 0 | |
+| FAILSAFE_DEFER_STATE_ENABLED | `uint8` | 1 | |
+| FAILSAFE_DEFER_STATE_WOULD_FAILSAFE | `uint8` | 2 | Failsafes deferred, but would trigger a failsafe |
+
+## Constants
+
+| 명칭 | 형식 | Value | 설명 |
+| --------------------------------------------------------------------------------------------------------------------------------------------------------------------------- | -------- | ----- | -- |
+| MESSAGE_VERSION | `uint32` | 1 | |
+| ARMING_STATE_DISARMED | `uint8` | 1 | |
+| ARMING_STATE_ARMED | `uint8` | 2 | |
+| ARM_DISARM_REASON_STICK_GESTURE | `uint8` | 1 | |
+| ARM_DISARM_REASON_RC_SWITCH | `uint8` | 2 | |
+| ARM_DISARM_REASON_COMMAND_INTERNAL | `uint8` | 3 | |
+| ARM_DISARM_REASON_COMMAND_EXTERNAL | `uint8` | 4 | |
+| ARM_DISARM_REASON_MISSION_START | `uint8` | 5 | |
+| ARM_DISARM_REASON_LANDING | `uint8` | 6 | |
+| ARM_DISARM_REASON_PREFLIGHT_INACTION | `uint8` | 7 | |
+| ARM_DISARM_REASON_KILL_SWITCH | `uint8` | 8 | |
+| ARM_DISARM_REASON_RC_BUTTON | `uint8` | 13 | |
+| ARM_DISARM_REASON_FAILSAFE | `uint8` | 14 | |
+| HIL_STATE_OFF | `uint8` | 0 | |
+| HIL_STATE_ON | `uint8` | 1 | |
+
+## Source Message
+
+[Source file (GitHub)](https://github.com/PX4/PX4-Autopilot/blob/main/msg/px4_msgs_old/msg/VehicleStatusV1.msg)
+
+:::details
+Click here to see original file
+
+```c
+# Encodes the system state of the vehicle published by commander
+
+uint32 MESSAGE_VERSION = 1
+
+uint64 timestamp # [us] Time since system start
+
+uint64 armed_time # [us] Arming timestamp
+uint64 takeoff_time # [us] Takeoff timestamp
+
+uint8 arming_state
+uint8 ARMING_STATE_DISARMED = 1
+uint8 ARMING_STATE_ARMED = 2
+
+uint8 latest_arming_reason
+uint8 latest_disarming_reason
+uint8 ARM_DISARM_REASON_STICK_GESTURE = 1
+uint8 ARM_DISARM_REASON_RC_SWITCH = 2
+uint8 ARM_DISARM_REASON_COMMAND_INTERNAL = 3
+uint8 ARM_DISARM_REASON_COMMAND_EXTERNAL = 4
+uint8 ARM_DISARM_REASON_MISSION_START = 5
+uint8 ARM_DISARM_REASON_LANDING = 6
+uint8 ARM_DISARM_REASON_PREFLIGHT_INACTION = 7
+uint8 ARM_DISARM_REASON_KILL_SWITCH = 8
+uint8 ARM_DISARM_REASON_RC_BUTTON = 13
+uint8 ARM_DISARM_REASON_FAILSAFE = 14
+
+uint64 nav_state_timestamp # Time when current nav_state activated
+
+uint8 nav_state_user_intention # Mode that the user selected (might be different from nav_state in a failsafe situation)
+
+uint8 nav_state # [@enum NAVIGATION_STATE] Currently active mode
+uint8 NAVIGATION_STATE_MANUAL = 0 # Manual mode
+uint8 NAVIGATION_STATE_ALTCTL = 1 # Altitude control mode
+uint8 NAVIGATION_STATE_POSCTL = 2 # Position control mode
+uint8 NAVIGATION_STATE_AUTO_MISSION = 3 # Auto mission mode
+uint8 NAVIGATION_STATE_AUTO_LOITER = 4 # Auto loiter mode
+uint8 NAVIGATION_STATE_AUTO_RTL = 5 # Auto return to launch mode
+uint8 NAVIGATION_STATE_POSITION_SLOW = 6
+uint8 NAVIGATION_STATE_FREE5 = 7
+uint8 NAVIGATION_STATE_ALTITUDE_CRUISE = 8 # Altitude with Cruise mode
+uint8 NAVIGATION_STATE_FREE3 = 9
+uint8 NAVIGATION_STATE_ACRO = 10 # Acro mode
+uint8 NAVIGATION_STATE_FREE2 = 11
+uint8 NAVIGATION_STATE_DESCEND = 12 # Descend mode (no position control)
+uint8 NAVIGATION_STATE_TERMINATION = 13 # Termination mode
+uint8 NAVIGATION_STATE_OFFBOARD = 14
+uint8 NAVIGATION_STATE_STAB = 15 # Stabilized mode
+uint8 NAVIGATION_STATE_FREE1 = 16
+uint8 NAVIGATION_STATE_AUTO_TAKEOFF = 17 # Takeoff
+uint8 NAVIGATION_STATE_AUTO_LAND = 18 # Land
+uint8 NAVIGATION_STATE_AUTO_FOLLOW_TARGET = 19 # Auto Follow
+uint8 NAVIGATION_STATE_AUTO_PRECLAND = 20 # Precision land with landing target
+uint8 NAVIGATION_STATE_ORBIT = 21 # Orbit in a circle
+uint8 NAVIGATION_STATE_AUTO_VTOL_TAKEOFF = 22 # Takeoff, transition, establish loiter
+uint8 NAVIGATION_STATE_EXTERNAL1 = 23
+uint8 NAVIGATION_STATE_EXTERNAL2 = 24
+uint8 NAVIGATION_STATE_EXTERNAL3 = 25
+uint8 NAVIGATION_STATE_EXTERNAL4 = 26
+uint8 NAVIGATION_STATE_EXTERNAL5 = 27
+uint8 NAVIGATION_STATE_EXTERNAL6 = 28
+uint8 NAVIGATION_STATE_EXTERNAL7 = 29
+uint8 NAVIGATION_STATE_EXTERNAL8 = 30
+uint8 NAVIGATION_STATE_MAX = 31
+
+uint8 executor_in_charge # [-] Current mode executor in charge (0=Autopilot)
+
+uint32 valid_nav_states_mask # [-] Bitmask for all valid nav_state values
+uint32 can_set_nav_states_mask # [-] Bitmask for all modes that a user can select
+
+# Bitmask of detected failures
+uint16 failure_detector_status # [@enum FAILURE]
+uint16 FAILURE_NONE = 0
+uint16 FAILURE_ROLL = 1 # (1 << 0)
+uint16 FAILURE_PITCH = 2 # (1 << 1)
+uint16 FAILURE_ALT = 4 # (1 << 2)
+uint16 FAILURE_EXT = 8 # (1 << 3)
+uint16 FAILURE_ARM_ESC = 16 # (1 << 4)
+uint16 FAILURE_BATTERY = 32 # (1 << 5)
+uint16 FAILURE_IMBALANCED_PROP = 64 # (1 << 6)
+uint16 FAILURE_MOTOR = 128 # (1 << 7)
+
+uint8 hil_state # [enum HIL_STATE]
+uint8 HIL_STATE_OFF = 0
+uint8 HIL_STATE_ON = 1
+
+# Current vehicle locomotion method. A vehicle can have different methods (e.g. VTOL transitions from RW to FW method)
+uint8 vehicle_type # [@enum VEHICLE_TYPE]
+uint8 VEHICLE_TYPE_UNSPECIFIED = 0
+uint8 VEHICLE_TYPE_ROTARY_WING = 1
+uint8 VEHICLE_TYPE_FIXED_WING = 2
+uint8 VEHICLE_TYPE_ROVER = 3
+
+uint8 FAILSAFE_DEFER_STATE_DISABLED = 0
+uint8 FAILSAFE_DEFER_STATE_ENABLED = 1
+uint8 FAILSAFE_DEFER_STATE_WOULD_FAILSAFE = 2 # Failsafes deferred, but would trigger a failsafe
+
+bool failsafe # true if system is in failsafe state (e.g.:RTL, Hover, Terminate, ...)
+bool failsafe_and_user_took_over # true if system is in failsafe state but the user took over control
+uint8 failsafe_defer_state # [@enum FAILSAFE_DEFER_STATE]
+
+# Link loss
+bool gcs_connection_lost # datalink to GCS lost
+uint8 gcs_connection_lost_counter # counts unique GCS connection lost events
+bool high_latency_data_link_lost # Set to true if the high latency data link (eg. RockBlock Iridium 9603 telemetry module) is lost
+
+# VTOL flags
+bool is_vtol # True if the system is VTOL capable
+bool is_vtol_tailsitter # True if the system performs a 90° pitch down rotation during transition from MC to FW
+bool in_transition_mode # True if VTOL is doing a transition
+bool in_transition_to_fw # True if VTOL is doing a transition from MC to FW
+
+# MAVLink identification
+uint8 system_type # system type, contains mavlink MAV_TYPE
+uint8 system_id # system id, contains MAVLink's system ID field
+uint8 component_id # subsystem / component id, contains MAVLink's component ID field
+
+bool safety_button_available # Set to true if a safety button is connected
+bool safety_off # Set to true if safety is off
+
+bool power_input_valid # Set if input power is valid
+bool usb_connected # Set to true (never cleared) once telemetry received from usb link
+
+bool open_drone_id_system_present
+bool open_drone_id_system_healthy
+
+bool parachute_system_present
+bool parachute_system_healthy
+
+bool rc_calibration_in_progress
+bool calibration_enabled
+
+bool pre_flight_checks_pass # true if all checks necessary to arm pass
+```
+
+:::
diff --git a/docs/ko/msg_docs/VtolVehicleStatus.md b/docs/ko/msg_docs/VtolVehicleStatus.md
index b725e0ccdd..bc09d11ed2 100644
--- a/docs/ko/msg_docs/VtolVehicleStatus.md
+++ b/docs/ko/msg_docs/VtolVehicleStatus.md
@@ -6,7 +6,7 @@ pageClass: is-wide-page
VEHICLE_VTOL_STATE, should match 1:1 MAVLinks's MAV_VTOL_STATE.
-**TOPICS:** vtol_vehiclestatus
+**TOPICS:** vtol_vehicle_status
## Fields
@@ -18,14 +18,14 @@ VEHICLE_VTOL_STATE, should match 1:1 MAVLinks's MAV_VTOL_STATE.
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ | -------- | ----- | -- |
-| MESSAGE_VERSION | `uint32` | 0 | |
-| VEHICLE_VTOL_STATE_UNDEFINED | `uint8` | 0 | |
-| VEHICLE_VTOL_STATE_TRANSITION_TO_FW | `uint8` | 1 | |
-| VEHICLE_VTOL_STATE_TRANSITION_TO_MC | `uint8` | 2 | |
-| VEHICLE_VTOL_STATE_MC | `uint8` | 3 | |
-| VEHICLE_VTOL_STATE_FW | `uint8` | 4 | |
+| 명칭 | 형식 | Value | 설명 |
+| ---------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- | -------- | ----- | -- |
+| MESSAGE_VERSION | `uint32` | 0 | |
+| VEHICLE_VTOL_STATE_UNDEFINED | `uint8` | 0 | |
+| VEHICLE_VTOL_STATE_TRANSITION_TO_FW | `uint8` | 1 | |
+| VEHICLE_VTOL_STATE_TRANSITION_TO_MC | `uint8` | 2 | |
+| VEHICLE_VTOL_STATE_MC | `uint8` | 3 | |
+| VEHICLE_VTOL_STATE_FW | `uint8` | 4 | |
## Source Message
diff --git a/docs/ko/msg_docs/Vtx.md b/docs/ko/msg_docs/Vtx.md
index 2ab56882dd..d9511574b7 100644
--- a/docs/ko/msg_docs/Vtx.md
+++ b/docs/ko/msg_docs/Vtx.md
@@ -24,20 +24,20 @@ pageClass: is-wide-page
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| ------------------------------------------------------------------------------------------------------------------------------------------------------- | ------- | ----- | ----------------------------------------- |
-| BAND_NAME_LENGTH | `uint8` | 12 | |
-| POWER_LABEL_LENGTH | `uint8` | 4 | |
-| PROTOCOL_NONE | `uint8` | 0 | No protocol is detected, usually an error |
-| PROTOCOL_SMART_AUDIO_V1 | `uint8` | 10 | |
-| PROTOCOL_SMART_AUDIO_V2 | `uint8` | 20 | |
-| PROTOCOL_SMART_AUDIO_V2_1 | `uint8` | 21 | |
-| PROTOCOL_TRAMP | `uint8` | 100 | |
-| DEVICE_UNKNOWN | `uint8` | 0 | |
-| DEVICE_PEAK_THOR_T67 | `uint8` | 20 | |
-| DEVICE_RUSH_MAX_SOLO | `uint8` | 40 | |
-| MODE_NORMAL | `uint8` | 0 | |
-| MODE_PIT | `uint8` | 1 | |
+| 명칭 | 형식 | Value | 설명 |
+| ----------------------------------------------------------------------------------------------------------------------------------------------------- | ------- | ----- | ----------------------------------------- |
+| BAND_NAME_LENGTH | `uint8` | 12 | |
+| POWER_LABEL_LENGTH | `uint8` | 4 | |
+| PROTOCOL_NONE | `uint8` | 0 | No protocol is detected, usually an error |
+| PROTOCOL_SMART_AUDIO_V1 | `uint8` | 10 | |
+| PROTOCOL_SMART_AUDIO_V2 | `uint8` | 20 | |
+| PROTOCOL_SMART_AUDIO_V2_1 | `uint8` | 21 | |
+| PROTOCOL_TRAMP | `uint8` | 100 | |
+| DEVICE_UNKNOWN | `uint8` | 0 | |
+| DEVICE_PEAK_THOR_T67 | `uint8` | 20 | |
+| DEVICE_RUSH_MAX_SOLO | `uint8` | 40 | |
+| MODE_NORMAL | `uint8` | 0 | |
+| MODE_PIT | `uint8` | 1 | |
## Source Message
diff --git a/docs/ko/msg_docs/Wind.md b/docs/ko/msg_docs/Wind.md
index 30f6c498e4..1dccdcddc5 100644
--- a/docs/ko/msg_docs/Wind.md
+++ b/docs/ko/msg_docs/Wind.md
@@ -28,9 +28,9 @@ Published by the navigation filter (EKF2) for use by other flight modules and li
## Constants
-| 명칭 | 형식 | Value | 설명 |
-| -------------------------------------------------------------------- | -------- | ----- | -- |
-| MESSAGE_VERSION | `uint32` | 0 | |
+| 명칭 | 형식 | Value | 설명 |
+| ------------------------------------------------------------------ | -------- | ----- | -- |
+| MESSAGE_VERSION | `uint32` | 0 | |
## Source Message
diff --git a/docs/ko/msg_docs/YawEstimatorStatus.md b/docs/ko/msg_docs/YawEstimatorStatus.md
index 3bd44fc563..392f045576 100644
--- a/docs/ko/msg_docs/YawEstimatorStatus.md
+++ b/docs/ko/msg_docs/YawEstimatorStatus.md
@@ -4,7 +4,7 @@ pageClass: is-wide-page
# YawEstimatorStatus (UORB message)
-**TOPICS:** yaw_estimatorstatus
+**TOPICS:** yaw_estimator_status
## Fields
diff --git a/docs/ko/msg_docs/index.md b/docs/ko/msg_docs/index.md
index 603270ff7a..3912b8abca 100644
--- a/docs/ko/msg_docs/index.md
+++ b/docs/ko/msg_docs/index.md
@@ -18,15 +18,16 @@ Graphs showing how these are used [can be found here](../middleware/uorb_graph.m
- [AirspeedValidated](AirspeedValidated.md) — Validated airspeed.
- [ArmingCheckReply](ArmingCheckReply.md) — Arming check reply.
- [ArmingCheckRequest](ArmingCheckRequest.md) — Arming check request.
+- [AuxGlobalPosition](AuxGlobalPosition.md) — Auxiliary global position.
- [BatteryStatus](BatteryStatus.md) — Battery status.
- [ConfigOverrides](ConfigOverrides.md) — Configurable overrides by (external) modes or mode executors.
- [Event](Event.md) — Events interface.
-- [FixedWingLateralSetpoint](FixedWingLateralSetpoint.md) — Fixed Wing Lateral Setpoint message. Used by the fw_lateral_longitudinal_control module. At least one of course, airspeed_direction, or lateral_acceleration must be finite.
-- [FixedWingLongitudinalSetpoint](FixedWingLongitudinalSetpoint.md) — Fixed Wing Longitudinal Setpoint message. Used by the fw_lateral_longitudinal_control module. If pitch_direct and throttle_direct are not both finite, then the controller relies on altitude/height_rate and equivalent_airspeed to control vertical motion. If both altitude and height_rate are NAN, the controller maintains the current altitude.
-- [GotoSetpoint](GotoSetpoint.md) — Position and (optional) heading setpoints with corresponding speed constraints. Setpoints are intended as inputs to position and heading smoothers, respectively. Setpoints do not need to be kinematically consistent. Optional heading setpoints may be specified as controlled by the respective flag. Unset optional setpoints are not controlled. Unset optional constraints default to vehicle specifications.
+- [FixedWingLateralSetpoint](FixedWingLateralSetpoint.md) — Fixed Wing Lateral Setpoint message.
+- [FixedWingLongitudinalSetpoint](FixedWingLongitudinalSetpoint.md) — Fixed Wing Longitudinal Setpoint message.
+- [GotoSetpoint](GotoSetpoint.md) — Position and (optional) heading setpoints with corresponding speed constraints.
- [HomePosition](HomePosition.md) — GPS home position in WGS84 coordinates.
-- [LateralControlConfiguration](LateralControlConfiguration.md) — Fixed Wing Lateral Control Configuration message. Used by the fw_lateral_longitudinal_control module to constrain FixedWingLateralSetpoint messages.
-- [LongitudinalControlConfiguration](LongitudinalControlConfiguration.md) — Fixed Wing Longitudinal Control Configuration message. Used by the fw_lateral_longitudinal_control module and TECS to constrain FixedWingLongitudinalSetpoint messages. and configure the resultant setpoints.
+- [LateralControlConfiguration](LateralControlConfiguration.md) — Fixed Wing Lateral Control Configuration message.
+- [LongitudinalControlConfiguration](LongitudinalControlConfiguration.md) — Fixed Wing Longitudinal Control Configuration message.
- [ManualControlSetpoint](ManualControlSetpoint.md)
- [ModeCompleted](ModeCompleted.md) — Mode completion result, published by an active mode. The possible values of nav_state are defined in the VehicleStatus msg. Note that this is not always published (e.g. when a user switches modes or on. failsafe activation).
- [RaptorInput](RaptorInput.md) — Raptor Input.
@@ -39,7 +40,7 @@ Graphs showing how these are used [can be found here](../middleware/uorb_graph.m
- [VehicleAttitude](VehicleAttitude.md) — This is similar to the mavlink message ATTITUDE_QUATERNION, but for onboard use. The quaternion uses the Hamilton convention, and the order is q(w, x, y, z).
- [VehicleAttitudeSetpoint](VehicleAttitudeSetpoint.md)
- [VehicleCommand](VehicleCommand.md) — Vehicle Command uORB message. Used for commanding a mission / action / etc. Follows the MAVLink COMMAND_INT / COMMAND_LONG definition.
-- [VehicleCommandAck](VehicleCommandAck.md) — Vehicle Command Ackonwledgement uORB message. Used for acknowledging the vehicle command being received. Follows the MAVLink COMMAND_ACK message definition.
+- [VehicleCommandAck](VehicleCommandAck.md) — Vehicle Command Acknowledgement uORB message.
- [VehicleControlMode](VehicleControlMode.md)
- [VehicleGlobalPosition](VehicleGlobalPosition.md) — Fused global position in WGS84. This struct contains global position estimation. It is not the raw GPS. measurement (@see vehicle_gps_position). This topic is usually published by the position. estimator, which will take more sources of information into account than just GPS,. e.g. control inputs of the vehicle in a Kalman-filter implementation.
- [VehicleLandDetected](VehicleLandDetected.md)
@@ -267,5 +268,8 @@ Graphs showing how these are used [can be found here](../middleware/uorb_graph.m
- [RegisterExtComponentReplyV0](RegisterExtComponentReplyV0.md)
- [RegisterExtComponentRequestV0](RegisterExtComponentRequestV0.md) — Request to register an external component.
- [VehicleAttitudeSetpointV0](VehicleAttitudeSetpointV0.md)
+- [VehicleCommandAckV0](VehicleCommandAckV0.md) — Vehicle Command Ackonwledgement uORB message. Used for acknowledging the vehicle command being received. Follows the MAVLink COMMAND_ACK message definition.
+- [VehicleGlobalPositionV0](VehicleGlobalPositionV0.md) — Fused global position in WGS84. This struct contains global position estimation. It is not the raw GPS. measurement (@see vehicle_gps_position). This topic is usually published by the position. estimator, which will take more sources of information into account than just GPS,. e.g. control inputs of the vehicle in a Kalman-filter implementation.
- [VehicleLocalPositionV0](VehicleLocalPositionV0.md) — Fused local position in NED. The coordinate system origin is the vehicle position at the time when the EKF2-module was started.
- [VehicleStatusV0](VehicleStatusV0.md) — Encodes the system state of the vehicle published by commander.
+- [VehicleStatusV1](VehicleStatusV1.md) — Encodes the system state of the vehicle published by commander.
diff --git a/docs/ko/neural_networks/mc_neural_network_control.md b/docs/ko/neural_networks/mc_neural_network_control.md
index ba696594a3..e7ad40119e 100644
--- a/docs/ko/neural_networks/mc_neural_network_control.md
+++ b/docs/ko/neural_networks/mc_neural_network_control.md
@@ -17,7 +17,7 @@ Note that after training the network you will need to update and rebuild PX4.
TLFM is a mature inference library intended for use on embedded devices.
It has support for several architectures, so there is a high likelihood that you can build it for the board you want to use.
-If not, there are other possible NN frameworks, such as [Eigen](https://eigen.tuxfamily.org/index.php?title=Main_Page) and [Executorch](https://pytorch.org/executorch-overview).
+If not, there are other possible NN frameworks, such as [Eigen](https://eigen.tuxfamily.org/index.php?title=Main_Page) and [Executorch](https://docs.pytorch.org/executorch/stable/intro-overview.html).
This document explains how you can include the module in your PX4 build, and provides a broad overview of how it works.
The other documents in the section provide more information about the integration, allowing you to replace the NN with a version trained on different data, or even to replace the TLFM library altogether.
diff --git a/docs/ko/neural_networks/nn_module_utilities.md b/docs/ko/neural_networks/nn_module_utilities.md
index 5b21cb6817..d559d46d07 100644
--- a/docs/ko/neural_networks/nn_module_utilities.md
+++ b/docs/ko/neural_networks/nn_module_utilities.md
@@ -41,7 +41,7 @@ This only works for some flight controllers, so you might have to use an RC cont
This specifies what you want to create, you can read more about this in the [Control Interface](../ros2/px4_ros2_control_interface.md).
In this case we register an arming check and a mode.
2. Wait for a [RegisterExtComponentReply](../msg_docs/RegisterExtComponentReply.md).
- This will give feedback on wether the mode registration was successful, and what the mode and arming check id is for the new mode.
+ This will give feedback on whether the mode registration was successful, and what the mode and arming check id is for the new mode.
3. [Optional] With the mode id, publish a [VehicleControlMode](../msg_docs/VehicleControlMode.md) message on the `config_control_setpoints` topic.
Here you can configure what other modules run in parallel.
The example controller replaces everything, so it turns off allocation.
@@ -71,7 +71,7 @@ For these messages to be saved in your logs you need to include `debug` in the [
The module has two includes for measuring the inference times.
The first one is a driver that works on the actual flight controller units, but a second one, `chrono`, is loaded for SITL testing.
-Which timing library is included and used is based on wether PX4 is built with NUTTX or not.
+Which timing library is included and used is based on whether PX4 is built with NUTTX or not.
## Changing the setpoint
diff --git a/docs/ko/neural_networks/raptor.md b/docs/ko/neural_networks/raptor.md
index 4a7685e1c1..c30ceb1b38 100644
--- a/docs/ko/neural_networks/raptor.md
+++ b/docs/ko/neural_networks/raptor.md
@@ -1,6 +1,6 @@
# RAPTOR: A Neural Network Module for Adaptive Quadrotor Control
-/out` to `fmu/out/`, and [Adusting the QoS settings](../ros2/user_guide.md#ros-2-subscriber-qos-settings).
+Modifying topic names to match the new naming pattern, which changed from `fmu//out` to `fmu/out/`, and [Adjusting the QoS settings](../ros2/user_guide.md#ros-2-subscriber-qos-settings).
For more information see [Fast-RTPS to uXRCE-DDS Migration Guidelines](../middleware/uxrce_dds.md#fast-rtps-to-uxrce-dds-migration-guidelines)
@@ -102,7 +102,7 @@ For more information see [Fast-RTPS to uXRCE-DDS Migration Guidelines](../middle
- Failsafe state machine rewrite and [web simulation](../config/safety_simulation.md)
- Improved preflight failure check reporting (requires QGC [v4.2.0](https://github.com/mavlink/qgroundcontrol/releases/tag/v4.2.0) or later): [PX4-Autopilot#20030](https://github.com/PX4/PX4-Autopilot/pull/20030) and [qgroundcontrol#10362](https://github.com/mavlink/qgroundcontrol/pull/10362)
-- [Package delivery in mission](../advanced/package_delivery.md): For package delivery applications, inital support for payload delivery in mission for gripper actuator was added
+- [Package delivery in mission](../advanced/package_delivery.md): For package delivery applications, initial support for payload delivery in mission for gripper actuator was added
- Manual control setpoint message redefinition: `manual_control_setpoint.x`, `y`, `z`, `w` -> `roll`, `pitch`, `yaw`, `throttle`; `throttle scale [0,1] -> [-1,1]` - [PX4-Autopilot#15949](https://github.com/PX4/PX4-Autopilot/pull/15949)
- Default motor PWM configuration - [PX4-Autopilot#21800](https://github.com/PX4/PX4-Autopilot/pull/21800)
- Fix PWM/Oneshot calibration - [PX4-Autopilot#21726](https://github.com/PX4/PX4-Autopilot/pull/21726)
@@ -135,7 +135,7 @@ For more information see [Fast-RTPS to uXRCE-DDS Migration Guidelines](../middle
- [Gazebo-classic] Addition of Omnicopter model: A fully actuated omnidirectional vehicle model has been added to Gazebo SITL - https://github.com/PX4/PX4-SITL_gazebo-classic/pull/866
- [Gazebo-classic] Addition of Advanced liftdrag plugin: Advanced liftdrag plugin that models nonlinear aerodynamics based on AVL - [PX4-SITL_gazebo-classic#901](https://github.com/PX4/PX4-SITL_gazebo-classic/pull/901)
- [Gazebo-classic] Addition of Safe landing world: Addition of safe landing world, for testing safe landing - [PX4-SITL_gazebo-classic#93](https://github.com/PX4/PX4-SITL_gazebo-classic/pull/93)
-- [Gazebo-classic] Depricated Ubuntu Bionic reated tests: Removed testing due to EOL of Ubuntu Bionic - [PX4-SITL_gazebo-classic#974](https://github.com/PX4/PX4-SITL_gazebo-classic/pull/974)
+- [Gazebo-classic] Deprecated Ubuntu Bionic reated tests: Removed testing due to EOL of Ubuntu Bionic - [PX4-SITL_gazebo-classic#974](https://github.com/PX4/PX4-SITL_gazebo-classic/pull/974)
- [SIH] Standalone sensor simulations in tree: Ability to simulate sensors in tree that was part of SIH is now a stand alone sensor module. Sensors include magnetometer, GPS, Barometer, Airspeed - [PX4-Autopilot#20137](https://github.com/PX4/PX4-Autopilot/pull/20137), https://github.com/PX4/PX4-Autopilot/tree/main/src/modules/simulation/sensor_airspeed_sim
- [SIH] Failure injection for battery simulation - https://github.com/PX4/PX4-Autopilot/commit/ebc1d7544e8146788c9e7cf5e8b64f60199240e4
diff --git a/docs/ko/releases/1.15.md b/docs/ko/releases/1.15.md
index cc03b8a837..ec3f473e96 100644
--- a/docs/ko/releases/1.15.md
+++ b/docs/ko/releases/1.15.md
@@ -79,7 +79,7 @@ Please continue reading for [upgrade instructions](#upgrade-guide).
- Correct way of describing the quaternion uncertainty using Lie group theory
- Use Joseph stabilized covariance update algorithm for better covariance stability and allow use of "consider states" (inactive states with non-zero variance) ([PX4-Autopilot#22770](https://github.com/PX4/PX4-Autopilot/pull/22770))
- Covariance prediction, measurement jacobians, state struct and covariance index auto-generated using SymForce
-- Manual position update throught MAVLink (`MAV_CMD_EXTERNAL_POSITION_ESTIMATE`)
+- Manual position update through MAVLink (`MAV_CMD_EXTERNAL_POSITION_ESTIMATE`)
- Add Auxiliary Global Position (AGP) fusion (for e.g.: external map matching vision algorithm)
**Mag:**
diff --git a/docs/ko/releases/1.16.md b/docs/ko/releases/1.16.md
index 27124c57fb..f72e2cfe70 100644
--- a/docs/ko/releases/1.16.md
+++ b/docs/ko/releases/1.16.md
@@ -57,7 +57,7 @@ Please continue reading for [upgrade instructions](#upgrade-guide).
- [Voltage-based estimation with load compensation](../config/battery.md#voltage-based-estimation-with-load-compensation) now uses a real-time estimate of the internal resistance of the battery to compensate voltage drops under load (with increased current), providing a better capacity estimate than with the raw measured voltage.
- Thrust-based load compensation has been removed (along with the `BATn_V_LOAD_DROP` parameters, where `n` is the battery number).
-- The [Position (GNSS) loss failsafe](../config/safety.md#position-gnss-loss-failsafe) configurable delay (`COM_POS_FS_DELAY`) has been removed.
+- The [Position (GNSS) loss failsafe](../config/safety.md#position-loss-failsafe) configurable delay (`COM_POS_FS_DELAY`) has been removed.
The failsafe will now trigger 1 second after position has been lost. ([PX4-Autopilot#24063](https://github.com/PX4/PX4-Autopilot/pull/24063)).
- [Log Encryption](../dev_log/log_encryption.md) now generates an encrypted log that contains the public-key-encrypted symmetric key that can be used to decrypt it, instead of putting the key into a separate file.
@@ -160,7 +160,7 @@ Please continue reading for [upgrade instructions](#upgrade-guide).
- mavlink_ftp: handle relative paths correctly. ([PX4-Autopilot#22980](https://github.com/PX4/PX4-Autopilot/pull/22980))
- Parameter to always start mavlink stream via USB. ([PX4-Autopilot#22234](https://github.com/PX4/PX4-Autopilot/pull/22234))
- Refactor: MAVLink message handling in one function, reference instead of pointer to main instance ([PX4-Autopilo#23219](https://github.com/PX4/PX4-Autopilot/pull/22234))
-- mavlink log handler rewrite for improved effeciency ([PX4-Autopilo#23219](https://github.com/PX4/PX4-Autopilot/pull/22234))
+- mavlink log handler rewrite for improved efficiency ([PX4-Autopilo#23219](https://github.com/PX4/PX4-Autopilot/pull/22234))
### Multi-Rotor
diff --git a/docs/ko/releases/1.17.md b/docs/ko/releases/1.17.md
index 4d757780d5..d8a9c85165 100644
--- a/docs/ko/releases/1.17.md
+++ b/docs/ko/releases/1.17.md
@@ -9,11 +9,11 @@ const { site } = useData();
-This contains changes to PX4 planned for PX4 v1.17 (since the last major release [PX v1.16](../releases/1.16.md)).
+This contains changes in PX4 v1.17 (since the last major release [PX v1.16](../releases/1.16.md)).
:::warning
PX4 v1.17 is in alpha/beta testing.
@@ -57,7 +57,7 @@ Please continue reading for [upgrade instructions](#upgrade-guide).
-->
--
// Template function to get the message version suffix
-// The correct message version is directly inferred from the message defintion
+// The correct message version is directly inferred from the message definition
template
std::string getMessageNameVersion() {
if (T::MESSAGE_VERSION == 0) return "";
diff --git a/docs/ko/ros2/px4_ros2_navigation_interface.md b/docs/ko/ros2/px4_ros2_navigation_interface.md
index fd625d7331..e490a4fa8d 100644
--- a/docs/ko/ros2/px4_ros2_navigation_interface.md
+++ b/docs/ko/ros2/px4_ros2_navigation_interface.md
@@ -104,7 +104,7 @@ The following steps are required to get started:
To send a position measurement, you populate the position struct with the values you have measured.
Then call the interface's update function with that struct as the argument.
-For a basic example of how to use this interface, check out the [examples](https://github.com/Auterion/px4-ros2-interface-lib/tree/main/examples/cpp/navigation) in the `Auterion/px4-ros2-interface-lib` repository, such as [examples/cpp/navigation/local_navigation](https://github.com/Auterion/px4-ros2-interface-lib/blob/main/examples/cpp/navigation/local_navigation/include/local_navigation.hpp) or [examples/cpp/navigation/global_navigation](https://github.com/Auterion/px4-ros2-interface-lib/blob/main/examples/cpp/navigation/local_navigation/include/global_navigation.hpp).
+For a basic example of how to use this interface, check out the [examples](https://github.com/Auterion/px4-ros2-interface-lib/tree/main/examples/cpp/navigation) in the `Auterion/px4-ros2-interface-lib` repository, such as [examples/cpp/navigation/local_navigation](https://github.com/Auterion/px4-ros2-interface-lib/blob/main/examples/cpp/navigation/local_navigation/include/local_navigation.hpp) or [examples/cpp/navigation/global_navigation](https://github.com/Auterion/px4-ros2-interface-lib/blob/main/examples/cpp/navigation/global_navigation/include/global_navigation.hpp).
### Local Position Updates
@@ -223,7 +223,7 @@ private:
### Global Position Updates
-First ensure that the PX4 parameter [`EKF2_AGP_CTRL`](../advanced_config/parameter_reference.md#EKF2_AGP_CTRL) is properly configured to fuse external global measurements, by setting the appropriate bits to `true`:
+First ensure that the PX4 [`EKF2_AGP_CTRLn`](../advanced_config/parameter_reference.md#EKF2_AGP0_CTRL) parameters are properly configured to fuse external global measurements, by setting the appropriate bits to `true`:
- `0`: Horizontal position data
- `1`: Vertical position data
diff --git a/docs/ko/ros2/user_guide.md b/docs/ko/ros2/user_guide.md
index 64e10d82e8..e8024ac876 100644
--- a/docs/ko/ros2/user_guide.md
+++ b/docs/ko/ros2/user_guide.md
@@ -9,7 +9,7 @@ From PX4 v1.14, ROS 2 uses [uXRCE-DDS](../middleware/uxrce_dds.md) middleware, r
The [migration guide](../middleware/uxrce_dds.md#fast-rtps-to-uxrce-dds-migration-guidelines) explains what you need to do in order to migrate ROS 2 apps from PX4 v1.13 to PX4 v1.14.
-If you're still working on PX4 v1.13, please follow the instructions in the [PX4 v1.13 Docs](https://docs.px4.io/v1.13/en/ros/ros2_comm.html).
+If you're still working on PX4 v1.13, please follow the instructions in the [PX4 v1.13 Docs](https://docs.px4.io/v1.13/en/ros/ros2_comm).
@@ -137,7 +137,7 @@ To install ROS 2 and its dependencies:
2. Some Python dependencies must also be installed (using **`pip`** or **`apt`**):
```sh
- pip install --user -U empy==3.3.4 pyros-genmsg setuptools
+ pip install --user -U empty==3.3.4 pyros-genmsg setuptools
```
### Setup Micro XRCE-DDS Agent & Client
diff --git a/docs/ko/sensor/airspeed.md b/docs/ko/sensor/airspeed.md
index 01be3aaff2..ad2ddd6b42 100644
--- a/docs/ko/sensor/airspeed.md
+++ b/docs/ko/sensor/airspeed.md
@@ -11,8 +11,8 @@ For fixed-wing flight it is the airspeed that guarantees lift — not ground spe
권장 디지털 속도 센서는 다음과 같습니다.
- Based on [Pitot tube](https://en.wikipedia.org/wiki/Pitot_tube)
- - I2C MEAS Spec series (e.g. [MS4525DO](https://www.te.com/usa-en/product-CAT-BLPS0002.html), [MS5525](https://www.te.com/usa-en/product-CAT-BLPS0003.html))
- - [mRo I2C Airspeed Sensor JST-GH MS4525DO](https://store.3dr.com/mro-i2c-airspeed-sensor-jst-gh-ms4525do/) (3DR store)
+ - I2C MEAS Spec series (e.g. [MS4525DO](https://www.te.com/en/product-20003581-00.html), [MS5525](https://www.te.com/usa-en/product-CAT-BLPS0003.html))
+ - [mRo I2C Airspeed Sensor JST-GH MS4525DO](https://store.3dr.com/airspeed-sensor-jst-gh-ms4525do/) (3DR store)
- [Digital Differential Airspeed Sensor Kit - MS4525DO](https://store-drotek.com/793-digital-differential-airspeed-sensor-kit-.html) (Drotek).
- [Holybro Digital Air Speed Sensor - MS4525DO](https://holybro.com/collections/sensors/products/digital-air-speed-sensor-ms4525do)
- [Holybro Digital Air Speed Sensor - MS5525DSO](https://holybro.com/collections/sensors/products/digital-air-speed-sensor-ms5525dso)
diff --git a/docs/ko/sensor/airspeed_tfslot.md b/docs/ko/sensor/airspeed_tfslot.md
index 79fe759421..ef34468786 100644
--- a/docs/ko/sensor/airspeed_tfslot.md
+++ b/docs/ko/sensor/airspeed_tfslot.md
@@ -5,7 +5,7 @@
[TFSLOT](https://github.com/ThunderFly-aerospace/TFSLOT01) is an airspeed sensor based on venturi effects.
-In the basic configuration, the TFSLOT is equipped with the [TFASPDIMU02](https://github.com/ThunderFly-aerospace/TFASPDIMU02) sensor board, which contains a differential pressure sensor ([Sensirion SDP3x series](https://sensirion.com/products/catalog/?filter_series=d1816d53-f5c8-47e3-ab47-818c3fd54259)) and a 9-axis motion tracking sensor ([ICM-20948](https://invensense.tdk.com/products/motion-tracking/9-axis/icm-20948/)).
+In the basic configuration, the TFSLOT is equipped with the [TFASPDIMU02](https://github.com/ThunderFly-aerospace/TFASPDIMU02) sensor board, which contains a differential pressure sensor ([Sensirion SDP3x series](https://sensirion.com/products/catalog?filter_series=d1816d53-f5c8-47e3-ab47-818c3fd54259)) and a 9-axis motion tracking sensor ([ICM-20948](https://invensense.tdk.com/products/motion-tracking/9-axis/icm-20948/)).
The IMU unit can be used as an external compass.
- This design brings several advantages when used on small-scale and slow-flying UAVs.
diff --git a/docs/ko/sensor/grf_lidar.md b/docs/ko/sensor/grf_lidar.md
new file mode 100644
index 0000000000..1403a37277
--- /dev/null
+++ b/docs/ko/sensor/grf_lidar.md
@@ -0,0 +1,69 @@
+# Lightware GRF250/GRF500 Gimbal Lidar
+
+LightWare [GRF250](https://lightwarelidar.com/shop/grf-250/) and [GRF500](https://lightwarelidar.com/shop/grf-500/) are small and light Lidar modules with a range of 250m and 500m, respectively.
+
+
+
+:::info
+The Lidar driver is not included in the default build of PX4.
+You will need to [create and use a custom build](#add-the-driver-to-the-px4-build).
+:::
+
+## 구매처
+
+Order these modules from:
+
+- [GRF250](https://lightwarelidar.com/shop/grf-250/)
+- [GRF500](https://lightwarelidar.com/shop/grf-500/)
+
+## 하드웨어 설정
+
+The rangefinder can be connected to any unused serial port, such as `TELEM2`.
+[Parameter Configuration](#parameter-configuration) explains how to configure the port to use and the other properties of the rangefinder.
+
+## PX4 Setup
+
+### Add the Driver to the PX4 Build
+
+The [lightware_grf_serial](../modules/modules_driver_distance_sensor.md#lightware-grf-serial) driver for this Lidar is not included in PX4 firmware by default.
+In order to use these modules you will first need to update the firmware configuration to add the driver, and then build the firmware.
+
+1. Update the firmware configuration. You can use either of the following options:
+ - Menuconfig:
+ 1. Install and open [menuconfig](../hardware/porting_guide_config.md#px4-menuconfig-setup)
+ 2. In [menuconfig](../hardware/porting_guide_config.md#px4-menuconfig-setup), navigate to **Drivers > Distance sensors**
+ 3. Select/Enable `lightware_grf_serial`
+ 4. Save the configuration
+
+ - Manually update `default.px4` to include the configuration key:
+ 1. Open the `default.px4board` config file that corresponds to the board you want to build for.
+ For example, to add the driver to `fmu-v6x` boards you would update [/boards/px4/fmu-v6x/default.px4board ](https://github.com/PX4/PX4-Autopilot/blob/main/boards/px4/fmu-v6x/default.px4board)
+ 2. Add the following line and save the file:
+
+ ```txt
+ CONFIG_DRIVERS_DISTANCE_SENSOR_LIGHTWARE_GRF_SERIAL=y
+ ```
+
+2. [Build PX4](../dev_setup/building_px4.md) for your flight controller target and upload the new firmware.
+
+### Parameter Configuration
+
+You will need to configure PX4 to indicate the serial port to which the sensor is connected (as per [Serial Port Configuration](../peripherals/serial_configuration.md)) and also the orientation and other properties of the sensor.
+
+The [parameters to change](../advanced_config/parameters.md) are listed in the table.
+
+| 매개변수 | 설명 |
+| ----------------------------------------------------------------------------------------------------------------------------------------------------------------------- | ------------------------------------------------------------------ |
+| [SENS_EN_GRF_CFG](../advanced_config/parameter_reference.md#SENS_EN_GRF_CFG) | Set to the serial port the sensor is connected to. |
+| [GRF_RATE_CFG](../advanced_config/parameter_reference.md#GRF_RATE_CFG) | Set the update rate. |
+| [GRF_SENS_MODEL](../advanced_config/parameter_reference.md#GRF_SENS_MODEL) | Set the sensor model to use. |
+
+## 시험
+
+You can confirm that the sensor is correctly configured by connecting QGroundControl, and observing that [DISTANCE_SENSOR](https://mavlink.io/en/messages/common.html#DISTANCE_SENSOR) is present in the [MAVLink Inspector](https://docs.qgroundcontrol.com/master/en/qgc-user-guide/analyze_view/mavlink_inspector.html).
+
+Moving the sensor around at various distances from a surface will have the `current_distance` value change.
+
+## 문제 해결
+
+If you are having problems with connecting to the sensor you may need to unassign a the default serial port. [Unassign Default Serial Port](../peripherals/serial_configuration.md)
diff --git a/docs/ko/sensor/inertial_navigation_systems.md b/docs/ko/sensor/inertial_navigation_systems.md
index 8a2ec11989..5d9b087cf3 100644
--- a/docs/ko/sensor/inertial_navigation_systems.md
+++ b/docs/ko/sensor/inertial_navigation_systems.md
@@ -49,5 +49,4 @@ Essentially it is an AHRS that also includes position/velocity estimation.
## 추가 정보
-- [What is an Inertial Navigation System?](https://www.vectornav.com/resources/inertial-navigation-articles/what-is-an-ins) (VectorNav)
- [Inertial Navigation Primer](https://www.vectornav.com/resources/inertial-navigation-primer) (VectorNav)
diff --git a/docs/ko/sensor/inertiallabs.md b/docs/ko/sensor/inertiallabs.md
index b748a2fee3..2dee4e3aa2 100644
--- a/docs/ko/sensor/inertiallabs.md
+++ b/docs/ko/sensor/inertiallabs.md
@@ -21,8 +21,8 @@ The mode is configurable using a parameter.
[Get technical support or send requests to sales team](https://inertiallabs.com/inertial-labs-inc/contact-inertial-labs-team/).
Recommended sensors:
-- [INS-U GNSS/INS](https://inertiallabs.com/ins-u-datasheet): Recommended for fixed-wing systems without hovering, where static heading is not necessary.
-- [INS-DU DUAL GNSS/INS](https://inertiallabs.com/ins-du-datasheet): Recommended for multicopter systems where hovering and low dynamics requires the use of static heading.
+- [INS-U GNSS/INS](https://inertiallabs.com/wp-content/uploads/2026/01/INS-U_INS-U-OEM_Datasheet_REV2.18_JAN2026.pdf): Recommended for fixed-wing systems without hovering, where static heading is not necessary.
+- [INS-DU DUAL GNSS/INS](https://inertiallabs.com/wp-content/uploads/2025/12/INS-DU_INS-DU-OEM_Datasheet_REV1.00_DEC2025.pdf): Recommended for multicopter systems where hovering and low dynamics requires the use of static heading.
## 하드웨어 설정
diff --git a/docs/ko/sensor/lidar_lite.md b/docs/ko/sensor/lidar_lite.md
index d3f8683f64..98a8548842 100644
--- a/docs/ko/sensor/lidar_lite.md
+++ b/docs/ko/sensor/lidar_lite.md
@@ -6,7 +6,7 @@ LIDAR-Lite는 드론, 로봇 또는 무인 차량용 소형 고성능 광학 원
## 구매처
-- [LIDAR-Lite v3](https://buy.garmin.com/en-AU/AU/p/557294) (5cm - 40m)
+- [LIDAR-Lite v3](https://www.garmin.com/en-AU/p/557294/) (5cm - 40m)
## 핀배열
diff --git a/docs/ko/sensor/microstrain.md b/docs/ko/sensor/microstrain.md
index 0c5bf0061d..0f14391f52 100644
--- a/docs/ko/sensor/microstrain.md
+++ b/docs/ko/sensor/microstrain.md
@@ -7,10 +7,10 @@ Widely used across industries like aerospace, robotics, industrial automation, a
The driver currently supports the following hardware:
-- [`MicroStrain CV7-AR`](https://www.hbkworld.com/en/products/transducers/inertial-sensors/vertical-reference-units--vru-/3dm-cv7-ar): Inertial Measurement Unit (IMU) and Vertical Reference Unit (VRU)
-- [`MicroStrain CV7-AHRS`](https://www.hbkworld.com/en/products/transducers/inertial-sensors/attitude-and-heading-reference-systems--ahrs-/3dm-cv7-ahrs): Inertial Measurement Unit (IMU) and Attitude Heading Reference System (AHRS)
-- [`MicroStrain CV7-INS`](https://www.hbkworld.com/en/products/transducers/inertial-sensors/inertial-navigation-systems--ins-/3dm-cv7-ins): Inertial Measurement Unit (IMU) and Inertial Navigation System (INS).
-- [`MicroStrain CV7-GNSS/INS`](https://www.hbkworld.com/en/products/transducers/inertial-sensors/inertial-navigation-systems--ins-/3dm-cv7-gnss-ins): Inertial Measurement Unit (IMU) and Inertial Navigation System (INS) combined with dual multiband (GNSS) receivers.
+- [`MicroStrain CV7-AR`](https://www.hbkworld.com/en/products/transducers/inertial-sensors/vertical-reference/3dm-cv7-ar): Inertial Measurement Unit (IMU) and Vertical Reference Unit (VRU)
+- [`MicroStrain CV7-AHRS`](https://www.hbkworld.com/en/products/transducers/inertial-sensors/attitude-and-heading/3dm-cv7-ahrs): Inertial Measurement Unit (IMU) and Attitude Heading Reference System (AHRS)
+- [`MicroStrain CV7-INS`](https://www.hbkworld.com/en/products/transducers/inertial-sensors/navigation/3dm-cv7-ins): Inertial Measurement Unit (IMU) and Inertial Navigation System (INS).
+- [`MicroStrain CV7-GNSS/INS`](https://www.hbkworld.com/en/products/transducers/inertial-sensors/navigation/3dm-cv7-gnss-ins): Inertial Measurement Unit (IMU) and Inertial Navigation System (INS) combined with dual multiband (GNSS) receivers.
PX4 can use these sensors to provide raw IMU data for EKF2 or to replace EKF2 as an external INS.
For more information, including user manuals and datasheets, please refer to the sensors product page.
@@ -18,7 +18,7 @@ For more information, including user manuals and datasheets, please refer to the
## 구매처
MicroStrain sensors can be purchased through HBK's official [MicroStrain product page](https://www.hbkworld.com/en/products/transducers/inertial-sensors) or through authorized distributors globally.
-For large orders, custom requirements, or technical inquiries, reach out directly to [sales](https://www.hbkworld.com/en/contact-us/contact-sales-microstrain)
+For large orders, custom requirements, or technical inquiries, reach out directly to [sales](https://www.hbkworld.com/en/contact-us)
## 하드웨어 설정
diff --git a/docs/ko/sensor/optical_flow.md b/docs/ko/sensor/optical_flow.md
index 779386fe14..eb14c0e902 100644
--- a/docs/ko/sensor/optical_flow.md
+++ b/docs/ko/sensor/optical_flow.md
@@ -71,7 +71,7 @@ Bitcraze, Tindie, Hex, Thone 및 Alientek의 일부 제품을 포함하여 여
### 기타 카메라 / 센서
카메라 통합 보드를 사용할 수 있습니다.
-For this the [Optical Flow repo](https://github.com/PX4/OpticalFlow) can be used (see also [snap_cam](https://github.com/PX4/snap_cam)).
+For this the [Optical Flow repo](https://github.com/PX4/PX4-OpticalFlow) can be used (see also [snap_cam](https://github.com/PX4/snap_cam)).
## 거리 측정기
diff --git a/docs/ko/sensor/px4flow.md b/docs/ko/sensor/px4flow.md
index d0d5104758..83edc7f785 100644
--- a/docs/ko/sensor/px4flow.md
+++ b/docs/ko/sensor/px4flow.md
@@ -5,4 +5,4 @@
PX4 does not support the PX4Flow [optical flow](../sensor/optical_flow.md) sensor from PX4 v1.13 (it doesn't work with current firmware).
PX4 may work with older PX4Flow firmware.
-Documentation has been removed (if needed, see [Legacy Docs for PX4Flow in v1.13](https://docs.px4.io/v1.13/en/sensor/px4flow.html)).
+Documentation has been removed (if needed, see [Legacy Docs for PX4Flow in v1.13](https://docs.px4.io/v1.13/en/sensor/px4flow)).
diff --git a/docs/ko/sensor/rangefinders.md b/docs/ko/sensor/rangefinders.md
index 067cc0431e..3bfacd53ba 100644
--- a/docs/ko/sensor/rangefinders.md
+++ b/docs/ko/sensor/rangefinders.md
@@ -93,7 +93,7 @@ It has a sensor range from (5cm - 40m) and can be connected to either PWM or I2C
### MaxBotix I2CXL-MaxSonar-EZ
-The MaxBotix [I2CXL-MaxSonar-EZ](https://www.maxbotix.com/product-category/i2cxl-maxsonar-ez-products) range has a number of relatively short-ranged sonar based rangefinders that are suitable for assisted takeoff/landing and collision avoidance.
+The MaxBotix [I2CXL-MaxSonar-EZ](https://maxbotix.com/collections/i2cxl-maxsonar-ez-products) range has a number of relatively short-ranged sonar based rangefinders that are suitable for assisted takeoff/landing and collision avoidance.
These can be connected using an I2C port.
The rangefinders are enabled using the parameter [SENS_EN_MB12XX](../advanced_config/parameter_reference.md#SENS_EN_MB12XX).
@@ -163,7 +163,7 @@ Features:
- [VL53L1CBV0FY-1](https://www.st.com/resource/en/datasheet/vl53l1.pdf) sensor
- Input voltage sensor
-- CAN connectors: 2 [UCANPHY Micro (JST-GH 4)](https://raccoonlabdev.github.io/docs/guide/wires/).
+- CAN connectors: 2 [UCANPHY Micro (JST-GH 4)](https://docs.raccoonlab.co/guide/wires/).
## Configuration/Setup {#configuration}
diff --git a/docs/ko/sensor/sbgecom.md b/docs/ko/sensor/sbgecom.md
index c9f0777c00..2cb5ba4cdb 100644
--- a/docs/ko/sensor/sbgecom.md
+++ b/docs/ko/sensor/sbgecom.md
@@ -2,7 +2,7 @@
[SBG-Systems](https://www.sbg-systems.com/) designs, manufactures, and support an extensive range of state-of-the-art inertial sensors such as Inertial Measurement Units (IMU), Attitude and Heading Reference Systems (AHRS), Inertial Navigation Systems with embedded GNSS (INS/GNSS), and so on.
-PX4 supports [all SBG Systems products](https://www.sbg-systems.com/products/) and can use these as an [external INS](../sensor/inertial_navigation_systems.md) (bypassing/replacing the EKF2 estimator), or as a source of raw sensor data provided to the navigation estimator.
+PX4 supports [all SBG Systems products](https://www.sbg-systems.com/) and can use these as an [external INS](../sensor/inertial_navigation_systems.md) (bypassing/replacing the EKF2 estimator), or as a source of raw sensor data provided to the navigation estimator.
@@ -17,7 +17,7 @@ SBG Systems products provide a range of benefits to PX4 users and can be integra
The sbgECom PX4 driver is streamlined to provide a simple plug-and-play architecture, removing engineering obstacles and allowing the acceleration of the design, development, and launch of platforms to keep pace with the rapid rate of innovation.
-The driver supports [all SBG Systems products](https://www.sbg-systems.com/products/).
+The driver supports [all SBG Systems products](https://www.sbg-systems.com/).
In particular the following systems are recommended:
- **Pulse:** Recommended for fixed-wing systems without hovering, where static heading is not necessary.
@@ -151,5 +151,5 @@ Published topics can be viewed using the `listener` command.
## Hardware Specifications
-- [Product Briefs](https://www.sbg-systems.com/products/)
+- [Product Briefs](https://www.sbg-systems.com/)
- [Datasheets](https://www.sbg-systems.com/contact/#products)
diff --git a/docs/ko/sensor/sf45_rotating_lidar.md b/docs/ko/sensor/sf45_rotating_lidar.md
index e7583c2d3b..fe1f50fee8 100644
--- a/docs/ko/sensor/sf45_rotating_lidar.md
+++ b/docs/ko/sensor/sf45_rotating_lidar.md
@@ -12,7 +12,7 @@ You will need to [create and use a custom build](#add-the-driver-to-the-px4-buil
## LightWare Studio Setup
-In the [LightWare Studio](https://www.lightwarelidar.com/resources-software) app set following values:
+In the [LightWare Studio](https://lightwarelidar.com/resources-software/) app set following values:
| 매개변수 | 설명 |
| --------- | ------ |
diff --git a/docs/ko/sensor/sfxx_lidar.md b/docs/ko/sensor/sfxx_lidar.md
index 30daec9f04..b3920cde7d 100644
--- a/docs/ko/sensor/sfxx_lidar.md
+++ b/docs/ko/sensor/sfxx_lidar.md
@@ -9,14 +9,14 @@ LightWare는 UAV에 장착에 적합한 경량의 범용 레이저 고도계( "
아래의 모델들은 PX4에서 지원되며, I2C 또는 직렬 버스에 연결할 수 있습니다 (아래 표는 각 모델에 사용할 수 있는 버스를 나타냄).
-| 모델 | 범위 (m) | 버스 | 설명 |
-| ------------------------------------------------------- | ------------------------- | ------------ | ------------------------------------------------------------------------------------------------------------- |
-| [SF11/C](https://lightwarelidar.com/shop/sf11-c-100-m/) | 100 | 직렬 또는 I2C 버스 | |
-| [LW20/C](https://lightware.co.za/products/lw20-c-100-m) | 100 | I2C 버스 | 감지 및 회피 애플리케이션을 위한 서보가 있는 방수 (IP67) |
-| [SF30/D](https://lightwarelidar.com/shop/sf30-d-200-m/) | 200 | I2C 버스 | Waterproofed (IP67) |
-| [SF45/B](../sensor/sf45_rotating_lidar.md) | 50 | 직렬 | Rotary Lidar (Used for [Collision Prevention](../computer_vision/collision_prevention.md)) |
-| [GRF250](https://lightwarelidar.com/shop/grf-250/) | 250 | I2C | Gimbal Range Finder |
-| [GRF500](https://lightwarelidar.com/shop/grf-500/) | 500 | I2C | Gimbal Range Finder |
+| 모델 | 범위 (m) | 버스 | 설명 |
+| ---------------------------------------------------------- | ------------------------- | ------------ | ------------------------------------------------------------------------------------------------------------- |
+| [SF11/C](https://lightwarelidar.com/shop/sf11-c-100-m/) | 100 | 직렬 또는 I2C 버스 | |
+| [LW20/C](https://lightwarelidar.com/products/lw20-c-100-m) | 100 | I2C 버스 | 감지 및 회피 애플리케이션을 위한 서보가 있는 방수 (IP67) |
+| [SF30/D](https://lightwarelidar.com/shop/sf30-d-200-m/) | 200 | I2C 버스 | Waterproofed (IP67) |
+| [SF45/B](../sensor/sf45_rotating_lidar.md) | 50 | 직렬 | Rotary Lidar (Used for [Collision Prevention](../computer_vision/collision_prevention.md)) |
+| [GRF250](../sensor/grf_lidar.md) | 250 | 직렬 또는 I2C 버스 | Gimbal Range Finder |
+| [GRF500](../sensor/grf_lidar.md) | 500 | 직렬 또는 I2C 버스 | Gimbal Range Finder |
:::details
Discontinued
diff --git a/docs/ko/sensor/teraranger.md b/docs/ko/sensor/teraranger.md
index 2350e6af46..6681cdc7a3 100644
--- a/docs/ko/sensor/teraranger.md
+++ b/docs/ko/sensor/teraranger.md
@@ -1,12 +1,17 @@
-# TeraRanger 거리계
+# TeraRanger Rangefinders (Discontinued)
+
+:::warning
+TeraRanger Evo sensors were discontinued by Terabee in May 2024.
+Limited stock may still be available from third-party resellers such as [Tribotix](https://tribotix.com/product/teraranger-evo-60m/).
+:::
TeraRanger는 적외선 ToF(Time-of-Flight) 기반의 다양한 경량 거리측정 센서입니다.
They are typically faster and have greater range than sonar, and smaller and lighter than laser-based systems.
PX4는 아래 장치들을 지원합니다.
-- [TeraRanger Evo 60m](https://www.terabee.com/shop/lidar-tof-range-finders/teraranger-evo-60m/) (0.5 – 60 m)
-- [TeraRanger Evo 600Hz](https://www.terabee.com/shop/lidar-tof-range-finders/teraranger-evo-600hz/) (0.75 - 8 m)
+- [TeraRanger Evo 60m](https://tribotix.com/product/teraranger-evo-60m/) (0.5 – 60 m)
+- [TeraRanger Evo 600Hz](https://tribotix.com/product/teraranger-evo-600hz/) (0.75 - 8 m)
:::info
PX4 also supports _TeraRanger One_ (I2C adapter required).
diff --git a/docs/ko/sensor/thunderfly_tachometer.md b/docs/ko/sensor/thunderfly_tachometer.md
index 412422f979..c9a68b9525 100644
--- a/docs/ko/sensor/thunderfly_tachometer.md
+++ b/docs/ko/sensor/thunderfly_tachometer.md
@@ -31,7 +31,7 @@ TFRPM01A 전자 장치에는 프로브가 연결 여부를 표시하는 LED가
홀 효과 센서 (자기 적으로 작동)는 먼지, 먼지 및 물이 감지된 로터에 접촉할 수있는 열악한 환경에 이상적입니다.
다양한 홀 효과 센서가 시판중입니다.
-For example, a [55100 Miniature Flange Mounting Proximity Sensor](https://m.littelfuse.com/media?resourcetype=datasheets&itemid=6d69d457-770e-46ba-9998-012c5e0aedd7&filename=littelfuse-hall-effect-sensors-55100-datasheet) is a good choice.
+For example, a [55100 Miniature Flange Mounting Proximity Sensor](https://www.littelfuse.com/assetdocs/littelfuse-hall-effect-sensors-55100-datasheet?assetguid=6d69d457-770e-46ba-9998-012c5e0aedd7) is a good choice.
@@ -90,7 +90,7 @@ pcf8583 status
```
드라이버가 실행중인 경우 I²C 포트가 실행중인 인스턴스의 다른 기본 매개변수와 함께 인쇄됩니다.
-드라이버가 실행 중이 아니면, 위에서 설명한 절차를 사용하여 시작할 수 있습니다.
+If the driver is not running it can be started using theprocedure described above.
The [listener](../modules/modules_command.md#listener) command allows you to monitor RPM UORB messages from the running driver.
diff --git a/docs/ko/sensor/vectornav.md b/docs/ko/sensor/vectornav.md
index e38e66dca5..41f983dd72 100644
--- a/docs/ko/sensor/vectornav.md
+++ b/docs/ko/sensor/vectornav.md
@@ -42,7 +42,7 @@ This can be changed to any rigid rotation using the VectorNav Reference Frame Ro
If using a GNSS-enabled product, the GNSS antenna must be mounted rigidly with respect to the inertial sensor and with an unobstructed sky view. If using a dual-GNSS-enabled product (VN-3X0), the secondary antenna must be mounted rigidly with respect to the primary antenna and the inertial sensor with an unobstructed sky view.
-For more mounting requirements and recommendations, see the relevant [Quick Start Guide](https://www.vectornav.com/resources/quick-start-guides).
+For more mounting requirements and recommendations, see the relevant [Quick Start Guide](https://www.vectornav.com/resources/technical-documentation/quick-start-guides).
## 펌웨어 설정
@@ -82,7 +82,7 @@ IMU data should be published at 800Hz (400Hz if using VN-300).
## VectorNav Configuration
-Definitions for all commands and registers referenced in this section can be found in the respective [VectorNav ICD](https://www.vectornav.com/resources/interface-control-documents).
+Definitions for all commands and registers referenced in this section can be found in the respective [VectorNav ICD](https://www.vectornav.com/resources/technical-documentation/interface-control-documents).
Upon initialization, PX4 configures the VectorNav unit as follows:
@@ -137,5 +137,5 @@ Published topics can be viewed using the `listener` command.
## Hardware Specifications
-- [Product Briefs](https://www.vectornav.com/resources/product-briefs)
-- [Datasheets](https://www.vectornav.com/resources/datasheets)
+- [Product Briefs](https://www.vectornav.com/resources/product-information/product-briefs)
+- [Datasheets](https://www.vectornav.com/resources/technical-documentation/datasheets)
diff --git a/docs/ko/sensor_bus/translator_tfi2cadt.md b/docs/ko/sensor_bus/translator_tfi2cadt.md
index 664b3797db..c8341c07d4 100644
--- a/docs/ko/sensor_bus/translator_tfi2cadt.md
+++ b/docs/ko/sensor_bus/translator_tfi2cadt.md
@@ -13,7 +13,7 @@ The module contains two pairs of connectors, each pair responsible for different
:::info
[TFI2CADT01](https://github.com/ThunderFly-aerospace/TFI2CADT01) is designed as open-source hardware with GPLv3 license.
-It is commercially available from [ThunderFly](https://www.thunderfly.cz/) company or from [Tindie eshop](https://www.tindie.com/products/26353/).
+It is commercially available from [ThunderFly](https://www.thunderfly.cz/) company or from [Tindie eshop](https://www.tindie.com/products/thunderfly/tfi2cadt01-pixhawk-i2c-address-translator/).
:::
## Address Translation Method
@@ -30,7 +30,7 @@ If you need your own value for address translation, changing the configuration r
The tachometer sensor [TFRPM01](../sensor/thunderfly_tachometer.md) can be set to two different addresses using a solder jumper.
If the autopilot has three buses, only 6 sensors can be connected and no bus remains free (2 available addresses \* 3 I2C ports).
In some multicopters or VTOL solutions, there is a need to measure the RPM of 8 or more elements.
-The [TFI2CADT01](https://www.tindie.com/products/26353/) is highly recommended in this case.
+The [TFI2CADT01](https://www.tindie.com/products/thunderfly/tfi2cadt01-pixhawk-i2c-address-translator/) is highly recommended in this case.
diff --git a/docs/ko/sim_gazebo_classic/index.md b/docs/ko/sim_gazebo_classic/index.md
index 7b95cd2961..ad927b521d 100644
--- a/docs/ko/sim_gazebo_classic/index.md
+++ b/docs/ko/sim_gazebo_classic/index.md
@@ -347,7 +347,7 @@ The video below shows that the location of the environment is aligned with the w
For extended development sessions it might be more convenient to start Gazebo Classic and PX4 separately or even from within an IDE.
-In addition to the existing cmake targets that run `sitl_run.sh` with parameters for px4 to load the correct model it creates a launcher targets named `px4_` that is a thin wrapper around original sitl px4 app.
+In addition to the existing cmake targets that run `sitl_run.sh` with parameters for PX4 to load the correct model it creates a launcher targets named `px4_` that is a thin wrapper around original sitl PX4 app.
This thin wrapper simply embeds app arguments like current working directories and the path to the model file.
To start Gazebo Classic and PX4 separately:
@@ -368,7 +368,7 @@ To start Gazebo Classic and PX4 separately:
- Start the debug session directly from IDE
-This approach significantly reduces the debug cycle time because simulator is always running in background and you only re-run the px4 process which is very light.
+This approach significantly reduces the debug cycle time because simulator is always running in background and you only re-run the PX4 process which is very light.
## Simulated Survey Camera
diff --git a/docs/ko/sim_gazebo_gz/gazebo_models.md b/docs/ko/sim_gazebo_gz/gazebo_models.md
index 880a74758e..f594c1cb3e 100644
--- a/docs/ko/sim_gazebo_gz/gazebo_models.md
+++ b/docs/ko/sim_gazebo_gz/gazebo_models.md
@@ -45,7 +45,7 @@ You can connect a PX4-enabled vehicle to an instance of _gz-server_ using severa
You can then drag and drop any PX4 model into your simulation.
::: info
- These models are taken from an web-server called [Gazebo Fuel](https://app.gazebosim.org/dashboard), which essentially acts as an online database for all types of models and worlds that can be launched in Gazebo.
+ These models are taken from an web-server called [Gazebo Fuel](https://app.gazebosim.org/PX4), which essentially acts as an online database for all types of models and worlds that can be launched in Gazebo.
:::
diff --git a/docs/ko/sim_gazebo_gz/index.md b/docs/ko/sim_gazebo_gz/index.md
index e46d72b927..606b40e082 100644
--- a/docs/ko/sim_gazebo_gz/index.md
+++ b/docs/ko/sim_gazebo_gz/index.md
@@ -5,7 +5,7 @@ Gazebo was previously known as "Gazebo Ignition" (while _Gazebo Classic_ was pre
See the [official blog post](https://www.openrobotics.org/blog/2022/4/6/a-new-era-for-gazebo) for more information.
:::
-[Gazebo](https://gazebosim.org/home) is an open source robotics simulator.
+[Gazebo](https://gazebosim.org/docs/latest/getstarted/) is an open source robotics simulator.
It supersedes the older [Gazebo Classic](../sim_gazebo_classic/index.md) simulator, and is the only supported version of Gazebo for Ubuntu 22.04 and onwards.
**Supported Vehicles:** Quadrotor, Plane, VTOL, Rover
@@ -303,7 +303,7 @@ where `ARGS` is a list of environment variables including:
- `PX4_GZ_FOLLOW_OFFSET_X`, `PX4_GZ_FOLLOW_OFFSET_Y`, `PX4_GZ_FOLLOW_OFFSET_Z`:
Set the relative offset of the follow camera to the vehicle.
-The PX4 Gazebo worlds and and models databases [can be found on GitHub here](https://github.com/PX4/PX4-gazebo-models).
+The PX4 Gazebo worlds and models databases [can be found on GitHub here](https://github.com/PX4/PX4-gazebo-models).
:::info
`gz_env.sh.in` is compiled and made available in `$PX4_DIR/build/px4_sitl_default/rootfs/gz_env.sh`
diff --git a/docs/ko/sim_gazebo_gz/tools_avl_automation.md b/docs/ko/sim_gazebo_gz/tools_avl_automation.md
index d25780226b..a3eb392fa2 100644
--- a/docs/ko/sim_gazebo_gz/tools_avl_automation.md
+++ b/docs/ko/sim_gazebo_gz/tools_avl_automation.md
@@ -121,7 +121,7 @@ From the stability derivatives log file, the following advanced lift drag plugin
| CYa | CYa | dCy/da (sideforce slope wrt alpha) |
| Cla | Cell | dCl/da (roll moment slope wrt alpha) |
| Cma | Cema | dCm/da (pitching moment slope wrt aLpha - before stall) |
-| Cna | Cena | dCn/da (yaw moment slope wrt alpha) |
+| Can | Cena | dCn/da (yaw moment slope wrt alpha) |
| CLb | CLb | dCL/dbeta (lift coefficient slope wrt beta) |
| CYb | CYb | dCY/dbeta (side force slope wrt beta) |
| Clb | Cell | dCl/dbeta (roll moment slope wrt beta) |
diff --git a/docs/ko/sim_gazebo_gz/vehicles.md b/docs/ko/sim_gazebo_gz/vehicles.md
index 6c93b94d49..a05193bf5e 100644
--- a/docs/ko/sim_gazebo_gz/vehicles.md
+++ b/docs/ko/sim_gazebo_gz/vehicles.md
@@ -8,7 +8,7 @@ Supported vehicle types include: mutirotor, VTOL, Plane, Rover.
:::warning
See [Gazebo Classic Vehicles](../sim_gazebo_classic/vehicles.md) for vehicles that work with the older [Gazebo "Classic" simulation](../sim_gazebo_classic/index.md).
-Note that vehicle models are not interchangable between the two versions of the simulator: the vehicles on this page only work with (new) [Gazebo](../sim_gazebo_gz/index.md).
+Note that vehicle models are not interchangeable between the two versions of the simulator: the vehicles on this page only work with (new) [Gazebo](../sim_gazebo_gz/index.md).
:::
## 멀티콥터
diff --git a/docs/ko/sim_gazebo_gz/worlds.md b/docs/ko/sim_gazebo_gz/worlds.md
index 31e026fabe..2fa1f5b063 100644
--- a/docs/ko/sim_gazebo_gz/worlds.md
+++ b/docs/ko/sim_gazebo_gz/worlds.md
@@ -104,4 +104,4 @@ The PX4 toolchain will automatically spawn a world that has the same name as the
The model specific worlds are:
-- [Aruco world](#aruco): Default world with an [ArUco marker](https://docs.opencv.org/4.x/d5/dae/tutorial_aruco_detection.html) that can be used with with [x500_mono_cam_down](../sim_gazebo_gz/vehicles.md#x500-quadrotor-with-monocular-camera-down-facing) for testing [precision landing](../advanced_features/precland.md).
+- [Aruco world](#aruco): Default world with an [ArUco marker](https://docs.opencv.org/4.x/d5/dae/tutorial_aruco_detection.html) that can be used with [x500_mono_cam_down](../sim_gazebo_gz/vehicles.md#x500-quadrotor-with-monocular-camera-down-facing) for testing [precision landing](../advanced_features/precland.md).
diff --git a/docs/ko/sim_jmavsim/index.md b/docs/ko/sim_jmavsim/index.md
index 5e1a543f4c..56e8de7ca3 100644
--- a/docs/ko/sim_jmavsim/index.md
+++ b/docs/ko/sim_jmavsim/index.md
@@ -310,7 +310,7 @@ sudo gedit /etc/java-8-openjdk/accessibility.properties
and comment out the line indicated below:
```sh
-#assistive_technologies=org.GNOME.Acessibility.AtkWrapper
+#assistive_technologies=org.GNOME.Accessibility.AtkWrapper
```
For more info, check [this GitHub issue](https://github.com/PX4/PX4-Autopilot/issues/9557).
diff --git a/docs/ko/sim_sih/index.md b/docs/ko/sim_sih/index.md
index 413302da84..743ecddb28 100644
--- a/docs/ko/sim_sih/index.md
+++ b/docs/ko/sim_sih/index.md
@@ -121,7 +121,7 @@ CONFIG_MODULES_SIMULATION_SENSOR_MAG_SIM=y
:::
-As an alterative to updating configuration files manually, you can use the following command to launch a GUI configuration tool, and interactively enable the required modules at the path: **modules > Simulation > simulator_sih**.
+As an alternative to updating configuration files manually, you can use the following command to launch a GUI configuration tool, and interactively enable the required modules at the path: **modules > Simulation > simulator_sih**.
For example, to update the fmu-v6x configuration you would use:
```sh
@@ -130,7 +130,7 @@ make px4_fmu-v6x boardconfig
After uploading, check that the required modules are present.
-:::note
+:::info
To use rover in SIH you must use the [rover build](../config_rover/index.md#flashing-the-rover-build) or add the rover modules to your board configuration.
:::
@@ -326,7 +326,7 @@ For SIH as SITL (no FC):
- `param set-default SENS_EN_MAGSIM 1`
- `param set-default SENS_EN_ARSPDSIM 1` (if it is a fixed-wing or VTOL airframe with airspeed sensor)
-For specific examples see the `_sihsim_` airframes in [ROMFS/px4fmu_common/init.d-posix/airframes](https://github.com/PX4/PX4-Autopilot/blob/main/ROMFS/px4fmu_common/init.d-posix/airframes/) (SIH as SITL) and [ROMFS/px4fmu_common/init.d/airframes](https://github.com/PX4/PX4-Autopilot/tree/main/ROMFS/px4fmu_common/init.d/airframes) (SIH on FC).
+For specific examples see the `_sihsim_` airframes in [ROMFS/px4fmu_common/init.d-posix/airframes](https://github.com/PX4/PX4-Autopilot/tree/main/ROMFS/px4fmu_common/init.d-posix/airframes) (SIH as SITL) and [ROMFS/px4fmu_common/init.d/airframes](https://github.com/PX4/PX4-Autopilot/tree/main/ROMFS/px4fmu_common/init.d/airframes) (SIH on FC).
## Controlling Actuators in SIH
diff --git a/docs/ko/simulation/hitl.md b/docs/ko/simulation/hitl.md
index 286cc56354..7debb43b95 100644
--- a/docs/ko/simulation/hitl.md
+++ b/docs/ko/simulation/hitl.md
@@ -104,18 +104,18 @@ make px4_fmu-v6x boardconfig
2. Select a [compatible airframe](#compatible_airframe) you want to test.
Then click **Apply and Restart** on top-right of the _Airframe Setup_ page.
-3. 필요한 경우 RC 또는 조이스틱을 보정합니다.
+3. Calibrate your [Manual Controller](../config/manual_control.md) (RC or Joystick), if needed.
4. UDP를 설정합니다.
1. Under the _General_ tab of the settings menu, uncheck all _AutoConnect_ boxes except for **UDP**.
-5. (선택 사항) 조이스틱과 안정장치를 설정합니다.
- Set the following [parameters](../advanced_config/parameters.md) in order to use a joystick instead of an RC remote control transmitter:
+5. (Optional) Configure your manual controller priority and failsafe:
- - [COM_RC_IN_MODE](../advanced_config/parameter_reference.md#COM_RC_IN_MODE) to "Joystick/No RC Checks". 이것은 조이스틱 입력을 허용하고, RC 입력을 비활성화합니다.
- - [NAV_RCL_ACT](../advanced_config/parameter_reference.md#NAV_RCL_ACT) to "Disabled". 무선 제어로 HITL을 실행하지 않으면, RC 안전장치가 간섭하지 않습니다.
+ - [Enable a mode in `COM_RC_IN_MODE` that enables and prioritises the controllers you want to use](../config/manual_control.md#px4-configuration).
+ The default `RC or MAVLink keep first` should work if you plan to only have a Joystick (no RC).
+ - You can set [NAV_RCL_ACT](../advanced_config/parameter_reference.md#NAV_RCL_ACT) to disable manual control loss failsafe while flying in a simulation.
:::tip
The _QGroundControl User Guide_ also has instructions on [Joystick](https://docs.qgroundcontrol.com/master/en/qgc-user-guide/setup_view/joystick.html) and [Virtual Joystick](https://docs.qgroundcontrol.com/master/en/qgc-user-guide/settings_view/virtual_joystick.html) setup.
@@ -137,7 +137,7 @@ Make sure _QGroundControl_ is not running!
1. Build PX4 with [Gazebo Classic](../sim_gazebo_classic/index.md) (in order to build the Gazebo Classic plugins).
```sh
- cd
+ cd
DONT_RUN=1 make px4_sitl_default gazebo-classic
```
diff --git a/docs/ko/simulation/index.md b/docs/ko/simulation/index.md
index aee31288f8..a52c31c9aa 100644
--- a/docs/ko/simulation/index.md
+++ b/docs/ko/simulation/index.md
@@ -67,7 +67,7 @@ A SITL build of PX4 uses [SimulatorMavlink.cpp](https://github.com/PX4/PX4-Autop
-PX4 directly uses the [Gazebo API](https://gazebosim.org/docs) to interface with [Gazebo](../sim_gazebo_gz/index.md) and MAVlink is not required.
+PX4 directly uses the [Gazebo API](https://gazebosim.org/docs/) to interface with [Gazebo](../sim_gazebo_gz/index.md) and MAVlink is not required.
## 기본 PX4 MAVLink UDP 포트
@@ -213,7 +213,7 @@ For setup information see the _QGroundControl User Guide_:
PX4 supports capture of both still images and video from within the [Gazebo Classic](../sim_gazebo_classic/index.md) simulated environment.
This can be enabled/set up as described in [Gazebo Glassic > Video Streaming](../sim_gazebo_classic/index.md#video-streaming).
-The simulated camera is a gazebo classic plugin that implements the [MAVLink Camera Protocol](https://mavlink.io/en/protocol/camera.html) .
+The simulated camera is a gazebo classic plugin that implements the [MAVLink Camera Protocol](https://mavlink.io/en/services/camera.html) .
PX4 connects/integrates with this camera in _exactly the same way_ as it would with any other MAVLink camera:
1. [TRIG_INTERFACE](../advanced_config/parameter_reference.md#TRIG_INTERFACE) must be set to `3` to configure the camera trigger driver for use with a MAVLink camera
diff --git a/docs/ko/smart_batteries/index.md b/docs/ko/smart_batteries/index.md
index c4199f989a..af525e39ed 100644
--- a/docs/ko/smart_batteries/index.md
+++ b/docs/ko/smart_batteries/index.md
@@ -1,7 +1,7 @@
# 스마트 배터리
스마트 배터리는 자동조종장치가 "둔감한" 배터리에 대해 추정할 수 있는 것보다 배터리 상태에 대한 더 정확한(그리고 종종 더 자세한) 정보를 제공합니다.
-이를 통하여 보다 안정적인 비행 계획 실패 조건 알림이 가능합니다.
+This allows for more reliable flight planning notification of failure conditions.
정보에는 남은 충전량, 비우기 시간 (예상), 셀 전압 (최대/최소 정격, 현재 전압 등), 온도, 전류, 오류 정보, 배터리 공급 업체, 화학 물질 등이 포함될 수 있습니다.
PX4는 (최소한) 다음과 같은 스마트 배터리를 지원합니다.
diff --git a/docs/ko/smart_batteries/rotoye_batmon.md b/docs/ko/smart_batteries/rotoye_batmon.md
index b4ba96fd30..1c4cae6737 100644
--- a/docs/ko/smart_batteries/rotoye_batmon.md
+++ b/docs/ko/smart_batteries/rotoye_batmon.md
@@ -1,6 +1,6 @@
# Rotoye Batmon
-[Rotoye Batmon](https://rotoye.com/batmon/) is a kit for adding smart battery functionality to off-the-shelf Lithium-Ion and LiPo batteries.
+[Rotoye Batmon](https://shop.rotoye.com/batmon/) is a kit for adding smart battery functionality to off-the-shelf Lithium-Ion and LiPo batteries.
독립형 장치로 또는 공장에서 조립된 스마트 배터리의 일부로 구입할 수 있습니다.
@@ -9,7 +9,7 @@
## 구매처
-[Rotoye Store](https://rotoye.com/batmon/): Batmon kits, custom smart-batteries, and accessories
+[Rotoye Store](https://shop.rotoye.com/batmon/): Batmon kits, custom smart-batteries, and accessories
## Wiring/Connections
@@ -50,7 +50,3 @@ In _QGroundControl_:
batt_smbus start -X -b 1 -a 11 # External bus 1, address 0x0b
batt_smbus start -X -b 1 -a 12 # External bus 1, address 0x0c
```
-
-## 추가 정보
-
-[Quick Start Guide](https://rotoye.com/batmon-tutorial/) (Rotoye)
diff --git a/docs/ko/software_update/stm32_bootloader.md b/docs/ko/software_update/stm32_bootloader.md
index f366dc337f..7e7d28308a 100644
--- a/docs/ko/software_update/stm32_bootloader.md
+++ b/docs/ko/software_update/stm32_bootloader.md
@@ -62,7 +62,7 @@ arm-none-eabi-gdb
### J-Link
-These instructions are for the [J-Link GDB server](https://www.segger.com/jlink-gdb-server.html).
+These instructions are for the [J-Link GDB server](https://www.segger.com/products/debug-probes/j-link/tools/j-link-gdb-server/about-j-link-gdb-server/).
#### 준비 사항
diff --git a/docs/ko/telemetry/cuav_p8_radio.md b/docs/ko/telemetry/cuav_p8_radio.md
index 9297ef41e6..4e643e064e 100644
--- a/docs/ko/telemetry/cuav_p8_radio.md
+++ b/docs/ko/telemetry/cuav_p8_radio.md
@@ -19,7 +19,7 @@ It supports multiple modes such as point-to-point, point-to-multipoint, and rela
## 구매처
-- [CUAV store](https://www.cuav.net/en/p8-2/)
+- [CUAV store](https://www.cuav.net/en/p8-en/)
- [CUAV alibaba](https://www.alibaba.com/product-detail/Free-shipping-CUAV-UAV-P8-Radio_1600324379418.html?spm=a2747.manage.0.0.2dca71d2bY4B0M)
## PX4 설정
@@ -61,6 +61,6 @@ CUAV P8 Radio does not support power supply from the flight controller, it needs
## More information
-[P8 manual](http://manual.cuav.net/data-transmission/p8-radio/p8-user-manual-en.pdf)
+[P8 manual](https://manual.cuav.net/data-transmission/p8-radio/p8_user_manual_cn.pdf)
[CUAV P8 Radio](https://doc.cuav.net/data-transmission/p8-radio/en/) (Official Guide)
diff --git a/docs/ko/telemetry/jfi_telemetry.md b/docs/ko/telemetry/jfi_telemetry.md
index 4f7847e4a8..3742e8dcb2 100644
--- a/docs/ko/telemetry/jfi_telemetry.md
+++ b/docs/ko/telemetry/jfi_telemetry.md
@@ -94,7 +94,7 @@ If you want to change the baud rate:
### One-to-many (1:N) Setups
For one-to-many (1:N) setups a higher baud rate is _highly recommended_ to ensure stable data reception.
-All J.Fi devices should be set to the same baud rate (although communication may work even when when devices use different baud rates).
+All J.Fi devices should be set to the same baud rate (although communication may work even when devices use different baud rates).
This should be changed in both PX4 and the J.Fi modules as explained in the previous section.
You will also need to make sure that all vehicles on the MAVLink network are assigned a unique **System ID** ([MAV_SYS_ID](../advanced_config/parameter_reference.md#MAV_SYS_ID)).
diff --git a/docs/ko/test_and_ci/integration_testing_mavsdk.md b/docs/ko/test_and_ci/integration_testing_mavsdk.md
index 4b0211c9cf..e79003604c 100644
--- a/docs/ko/test_and_ci/integration_testing_mavsdk.md
+++ b/docs/ko/test_and_ci/integration_testing_mavsdk.md
@@ -7,7 +7,7 @@ PX4 can be tested end to end to using integration tests based on [MAVSDK](https:
아래 지침은 로컬에서 테스트를 설정하고 진행하는 방법을 설명합니다.
-:::note
+:::info
This is the recommended integration test framework for PX4.
:::
diff --git a/docs/ko/test_and_ci/integration_testing_ros1_mavros.md b/docs/ko/test_and_ci/integration_testing_ros1_mavros.md
index 02882687a5..491e733cad 100644
--- a/docs/ko/test_and_ci/integration_testing_ros1_mavros.md
+++ b/docs/ko/test_and_ci/integration_testing_ros1_mavros.md
@@ -9,7 +9,7 @@ It should be used only for new test cases that _require_ ROS 1.
[MAVSDK Integration Testing](../test_and_ci/integration_testing_mavsdk.md) is preferred when writing new tests.
:::
-:::note
+:::info
All PX4 integration tests are executed automatically by our [Continuous Integration](../test_and_ci/continous_integration.md) system.
:::
diff --git a/docs/ko/test_and_ci/test_flights.md b/docs/ko/test_and_ci/test_flights.md
index b0c65c3a6d..e262af5797 100644
--- a/docs/ko/test_and_ci/test_flights.md
+++ b/docs/ko/test_and_ci/test_flights.md
@@ -7,7 +7,7 @@ const { site } = useData();
diff --git a/docs/ko/test_and_ci/unit_tests.md b/docs/ko/test_and_ci/unit_tests.md
index 77a39b777b..247befa9c7 100644
--- a/docs/ko/test_and_ci/unit_tests.md
+++ b/docs/ko/test_and_ci/unit_tests.md
@@ -141,7 +141,7 @@ It can be run directly in a debugger, however be careful to only run one test pe
}
```
- `OPTION` can be `OPT_NOALLTEST`,`OPT_NOJIGTEST` or `0` and is considered if within px4 shell one of the two commands are called:
+ `OPTION` can be `OPT_NOALLTEST`,`OPT_NOJIGTEST` or `0` and is considered if within PX4 shell one of the two commands are called:
```sh
pxh> tests all
diff --git a/docs/ko/test_cards/mc_02_full_autonomous.md b/docs/ko/test_cards/mc_02_full_autonomous.md
index 2752d9bb70..6e26b53ec9 100644
--- a/docs/ko/test_cards/mc_02_full_autonomous.md
+++ b/docs/ko/test_cards/mc_02_full_autonomous.md
@@ -54,7 +54,7 @@ Plan a mission on the ground. Ensure the mission has
- 추력을 올릴 때 서서히 이륙한다
- 첫 시도시 임무 내용이 올라가야 함
- 자동 모드 인가시 기체는 자동으로 이륙해야 함
-- Vehicle shoud adjust height to RTL altitude before returning home
+- Vehicle should adjust height to RTL altitude before returning home
- 지면에 착륙시, 콥터가 지면에서 튀면 안됨
@@ -8,7 +8,7 @@ The [CUAV C-RTK GPS receiver](https://www.cuav.net/en/c_rtk_9ps/) is an [RTK GPS
## 구매처
- [cuav taobao](https://item.taobao.com/item.htm?id=565380634341&spm=2014.21600712.0.0)
-- [cuav aliexpress](https://www.aliexpress.com/store/product/CUAV-NEW-Flight-Controller-GPS-C-RTK-differential-positioning-navigation-module-GPS-for-PIX4-Pixhawk-pixhack/3257035_32853894248.html?spm=2114.12010608.0.0.75592fadQKPPEn)
+- [cuav aliexpress](https://www.aliexpress.com/item/32853894248.html?spm=2114.12010608.0.0.75592fadQKPPEn)
## 설정
@@ -16,7 +16,7 @@ RTK setup and use on PX4 via _QGroundControl_ is largely plug and play \(see [RT
## 배선
-C-RTK GPS comes with a cable that terminates in a 6-pin connector and 4-pin connector that are compatible with [Pixhack v3](https://doc.cuav.net/flight-controller/pixhack/en/quick-start-pixhack-v3x.html#gps--compass).
+C-RTK GPS comes with a cable that terminates in a 6-pin connector and 4-pin connector that are compatible with [Pixhack v3](../flight_controller/pixhack_v3.md).
6핀 커넥터는 RTK GPS 용 인터페이스를 제공하며 비행 콘트롤러의 GPS 포트에 연결하여야합니다.
4핀 커넥터는 두 번째 GPS로 사용하기 위한 (옵션) m8n (표준) GPS 인터페이스입니다.
diff --git a/docs/ko/gps_compass/rtk_gps_cuav_c-rtk2.md b/docs/ko/gps_compass/rtk_gps_cuav_c-rtk2.md
index 6aea7d8563..14269d956a 100644
--- a/docs/ko/gps_compass/rtk_gps_cuav_c-rtk2.md
+++ b/docs/ko/gps_compass/rtk_gps_cuav_c-rtk2.md
@@ -1,6 +1,6 @@
# CUAV C-RTK2 GNSS Module (RTK/PPK)
-The [CUAV C-RTK2 receiver](https://www.cuav.net/en/c_rtk_9ps/) is a high-performance PPK/RTK positioning module created by CUAV for professional applications such as drone aerial surveying and mapping.
+The [CUAV C-RTK2 receiver](https://www.cuav.net/en/c-rtk-9ps-en/) is a high-performance PPK/RTK positioning module created by CUAV for professional applications such as drone aerial surveying and mapping.
It has a high-precision IMU and positioning module, and can reduce the number of required [control points](https://www.youtube.com/watch?v=3k7v5aXyuKQ) by more than to 80%.
In addition to surveying/mapping, it is suitable for many other use-cases, including: agricultural plant protection and drone swarms.
@@ -10,7 +10,7 @@ In addition to surveying/mapping, it is suitable for many other use-cases, inclu
- High-performance H7 processor
- High precision industrial grade IMU
-- Support RTK and save RAW raw data (PPK) at the same time
+- Support RTK and save raw data (PPK) at the same time
- Multi-satellite and multi-frequency receivers
- UAVCAN/Dronecan protocol
- Support hotshoe and shutter trigger
@@ -18,7 +18,7 @@ In addition to surveying/mapping, it is suitable for many other use-cases, inclu
## 구매처
-- [CUAV Store](https://store.cuav.net/shop/c-rtk-2/)
+- [CUAV Store](https://store.cuav.net/?route=product%2Fproduct&product_id=159)
- [CUAV aliexpress](https://pt.aliexpress.com/item/1005003754165772.html?spm=a2g0o.store_pc_groupList.8148356.13.2f893550i0NE4o)
# 요약
diff --git a/docs/ko/gps_compass/rtk_gps_datagnss_nano_hrtk.md b/docs/ko/gps_compass/rtk_gps_datagnss_nano_hrtk.md
index 4db5b0567e..29845a96b9 100644
--- a/docs/ko/gps_compass/rtk_gps_datagnss_nano_hrtk.md
+++ b/docs/ko/gps_compass/rtk_gps_datagnss_nano_hrtk.md
@@ -90,7 +90,7 @@ Note that for the base we recommend the [NANO RTK Receiver](https://www.datagnss
-See to [How to setup Base station](https://wiki.datagnss.com/index.php/GEM1305-autopilot#Base_station_setup) for information on how to configure the module for use as a base station (not including step 6 and later, for which you would QGroundControl instead of Mission Planner).
+See to [How to setup Base station](https://docs.datagnss.com/#Base_station_setup) for information on how to configure the module for use as a base station (not including step 6 and later, for which you would QGroundControl instead of Mission Planner).
### Rover Setup (PX4)
@@ -111,13 +111,12 @@ GPS and RTK configuration on PX4 via _QGroundControl_ is plug and play (see [RTK
## Resources
-- [NANO RTK Receiver 2D drawing file](https://wiki.datagnss.com/images/3/31/EVK-DG-1206_V.2.0.pdf)
- [NANO HRTK Receiver Wiki](https://docs.datagnss.com/gnss/rtk_receiver/NANO/nano-helix-rtk/) (DATAGNSS WiKi)
- [HED-10L Heading RTK Receiver](https://docs.datagnss.com/gnss/rtk_receiver/HED-10L/)
## More information
-- [NANO RTK Receiver](https://docs.datagnss.com/gnss/rtk_receiver/NANO/nano-rtk-receiver)
+- [NANO RTK Receiver](https://docs.datagnss.com/gnss/rtk_receiver/NANO/nano-rtk-receiver/)
- [HELIX Antenna for RTK](https://www.datagnss.com/collections/rtk-antenna/products/smart-helix-antenna)
- [RTK Antenna AGR6302G](https://www.datagnss.com/collections/rtk-antenna/products/antenna-agr6302g)
- [AT400 RTK Antenna](https://www.datagnss.com/collections/rtk-antenna/products/at400-multi-band-antenna-for-rtk)
diff --git a/docs/ko/gps_compass/rtk_gps_drotek_xl.md b/docs/ko/gps_compass/rtk_gps_drotek_xl.md
index 7b032cad86..b67ca1c93e 100644
--- a/docs/ko/gps_compass/rtk_gps_drotek_xl.md
+++ b/docs/ko/gps_compass/rtk_gps_drotek_xl.md
@@ -2,7 +2,7 @@
:::info
This module appears to have been discontinued, and is no longer on the Drotek site (September 2023).
-The last documentation was in [PX4 v1.13 here](https://docs.px4.io/v1.13/en/gps_compass/rtk_gps_drotek_xl.html)
+The last documentation was in [PX4 v1.13 here](https://docs.px4.io/v1.13/en/gps_compass/rtk_gps_drotek_xl)
:::
diff --git a/docs/ko/gps_compass/rtk_gps_gem1305.md b/docs/ko/gps_compass/rtk_gps_gem1305.md
index a10248fed2..05589e0039 100644
--- a/docs/ko/gps_compass/rtk_gps_gem1305.md
+++ b/docs/ko/gps_compass/rtk_gps_gem1305.md
@@ -77,7 +77,7 @@ The 1.25mm pitch 6P connector (from left: PIN1 to PIN6) supports UART for GNSS a
## 하드웨어 설정
RTK requires a base RTK module attached to the ground station, and a rover RTK module on the vehicle.
-The data from the base needs to be transmitted to the drone via telemetry radio and inputed into the RTK receiver on the rover.
+The data from the base needs to be transmitted to the drone via telemetry radio and inputted into the RTK receiver on the rover.
@@ -93,7 +93,7 @@ Note that for the base we recommend the [NANO RTK Receiver](https://www.datagnss
-See to [How to setup Base station](https://wiki.datagnss.com/index.php/GEM1305-autopilot#Base_station_setup) for information on how to configure the module for use as a base station (not including step 6 and later, for which you would QGroundControl instead of Mission Planner).
+See to [How to setup Base station](https://docs.datagnss.com/#Base_station_setup) for information on how to configure the module for use as a base station (not including step 6 and later, for which you would QGroundControl instead of Mission Planner).
### Rover Setup (PX4)
@@ -115,14 +115,13 @@ GPS and RTK configuration on PX4 via _QGroundControl_ is plug and play (see [RTK
## Resources
-- [NANO RTK Receiver 2D drawing file](https://wiki.datagnss.com/images/3/31/EVK-DG-1206_V.2.0.pdf)
- [GEM1305 Wiki](https://docs.datagnss.com/gnss/rtk_receiver/GEM1305/) (DATAGNSS WiKi)
- [HED-10L Heading RTK Receiver](https://docs.datagnss.com/gnss/rtk_receiver/HED-10L/)
- [NANO HRTK Receiver](https://docs.datagnss.com/gnss/rtk_receiver/NANO/nano-helix-rtk/)
## More information
-- [NANO RTK Receiver](https://www.datagnss.com/collections/evk/products/tau951m-1312-tiny-evk)
+- [NANO RTK Receiver](https://www.datagnss.com/products/nano-rtk-receiver)
- [HELIX Antenna for RTK](https://www.datagnss.com/collections/rtk-antenna/products/smart-helix-antenna)
- [RTK Antenna AGR6302G](https://www.datagnss.com/collections/rtk-antenna/products/antenna-agr6302g)
- [AT400 RTK Antenna](https://www.datagnss.com/collections/rtk-antenna/products/at400-multi-band-antenna-for-rtk)
diff --git a/docs/ko/gps_compass/rtk_gps_hex_hereplus.md b/docs/ko/gps_compass/rtk_gps_hex_hereplus.md
index af20afe92a..0f01c3f646 100644
--- a/docs/ko/gps_compass/rtk_gps_hex_hereplus.md
+++ b/docs/ko/gps_compass/rtk_gps_hex_hereplus.md
@@ -5,7 +5,7 @@
:::info
This GPS is no longer available for purchase but is still compatible with PX4.
-Usage documentation can be found in [PX4v1.11 docs](https://docs.px4.io/v1.11/en/gps_compass/rtk_gps_hex_hereplus.html)
+Usage documentation can be found in [PX4v1.11 docs](https://docs.px4.io/v1.11/en/gps_compass/rtk_gps_hex_hereplus)
:::
The **Here+ RTK GPS receiver** is a small, light and energy efficient [RTK GPS module](../gps_compass/rtk_gps.md), based on the u-blox M8P. RTK를 사용하면 PX4는 일반 GPS에서 제공하는 것 보다 훨씬 더 정확한 센티미터 수준의 정확도로 위치를 파악할 수 있습니다.
diff --git a/docs/ko/gps_compass/rtk_gps_holybro_h-rtk-f9p.md b/docs/ko/gps_compass/rtk_gps_holybro_h-rtk-f9p.md
index aa56937f56..8044dcd28d 100644
--- a/docs/ko/gps_compass/rtk_gps_holybro_h-rtk-f9p.md
+++ b/docs/ko/gps_compass/rtk_gps_holybro_h-rtk-f9p.md
@@ -19,7 +19,7 @@ Using RTK allows PX4 to get its position with centimetre-level accuracy, which i
## 구매처
- [H-RTK F9P (Holybro Website)](https://holybro.com/products/h-rtk-f9p-gnss-series)
-- [H-RTK Accessories (Holybro Website)](https://holybro.com/collections/h-rtk-gps)
+- [H-RTK Accessories (Holybro Website)](https://holybro.com/collections/gps)
## 설정
@@ -50,6 +50,6 @@ The cables/connectors may need to be modified in order to connect to other fligh
## GPS 소품
-[H-RTK Mount (Holybro Website)](https://holybro.com/products/vertical-mount-for-h-rtk-helical)
+[H-RTK Mount (Holybro Website)](https://holybro.com/collections/gps-accessories/products/vertical-mount-for-h-rtk-helical)
diff --git a/docs/ko/gps_compass/rtk_gps_holybro_h-rtk-m8p.md b/docs/ko/gps_compass/rtk_gps_holybro_h-rtk-m8p.md
index 7a62557d76..d2f983c492 100644
--- a/docs/ko/gps_compass/rtk_gps_holybro_h-rtk-m8p.md
+++ b/docs/ko/gps_compass/rtk_gps_holybro_h-rtk-m8p.md
@@ -2,9 +2,10 @@
:::warning
This GNSS has been discontinued, and is no longer commercially available.
+Replaced by [Holybro H-RTK F9P GNSS](../gps_compass/rtk_gps_holybro_h-rtk-f9p.md).
:::
-The [Holybro H-RTK M8P GNSS](https://holybro.com/collections/standard-h-rtk-series/products/h-rtk-m8p-gnss-series) is an [RTK GNSS module](../gps_compass/rtk_gps.md) series for the mass market.
+The _Holybro H-RTK M8P GNSS_ is an [RTK GNSS module](../gps_compass/rtk_gps.md) series for the mass market.
This family is similar to the [H-RTK M9P](../gps_compass/rtk_gps_holybro_h-rtk-f9p.md) series but uses the smaller, lighter, and less expensive M8P u-blox RTK GNSS module (which still provides far superior position resolution than previous generations\_.
Holybro H-RTK M8P에는 세 가지 모델이 있으며, 각각 다른 요구 사항을 충족하기 위해 서로 다른 안테나 디자인을 사용합니다.
@@ -16,7 +17,7 @@ RTK를 사용하면 PX4는 일반 GPS에서 제공하는 것 보다 훨씬 더
## 구매처
-- [H-RTK M8P (GPS RTK Mounts)](https://holybro.com/products/vertical-mount-for-h-rtk-helical)
+- Discontinued.
## 설정
@@ -30,9 +31,7 @@ All H-RTK GNSS models come with a GH 10-pin connector/cable that is compatible w
The cables/connectors may need to be modified in order to connect to other flight controller boards (see [pin map](#pin_map)below).
:::
-
-
-## 핀 맵
+## Pin Map {#pin_map}
diff --git a/docs/ko/gps_compass/rtk_gps_holybro_unicore_um982.md b/docs/ko/gps_compass/rtk_gps_holybro_unicore_um982.md
index 69d2c0de92..af8d6e1264 100644
--- a/docs/ko/gps_compass/rtk_gps_holybro_unicore_um982.md
+++ b/docs/ko/gps_compass/rtk_gps_holybro_unicore_um982.md
@@ -1,10 +1,10 @@
# Holybro H-RTK Unicore UM982 GPS
-The [Holybro H-RTK Unicore UM982 GPS](https://holybro.com/products/h-rtk-um982) is an multi-band high-precision [RTK GNSS System](../gps_compass/rtk_gps.md) launched by Holybro.
+The [Holybro H-RTK Unicore UM982 GPS](https://holybro.com/products/h-rtk-unicore-um982) is an multi-band high-precision [RTK GNSS System](../gps_compass/rtk_gps.md) launched by Holybro.
-This module is based on the [Unicore UM982 Chip](https://en.unicorecomm.com/products/detail/24), which supports RTK positioning and dual-antenna heading calculation.
+This module is based on the [Unicore UM982 Chip](https://en.unicore.com/products/dual-antenna-gnss-um982/), which supports RTK positioning and dual-antenna heading calculation.
This means that it can generate a moving baseline headline/yaw determinations for autopilots with just one GPS module and dual antennas - a magnetometer is not needed.
Unlike when using a module such as the U-blox F9P, where you would need [two U-blox F9P modules to compute a heading angle](../gps_compass/u-blox_f9p_heading.md), with the Unicore UM982 GPS, you only need one GPS module!
@@ -20,7 +20,7 @@ Additional technical information can be found at [Holybro Technical Documentatio
## 구매처
-- [Holybro Website](https://holybro.com/products/h-rtk-um982)
+- [Holybro Website](https://holybro.com/products/h-rtk-unicore-um982)
## 배선
diff --git a/docs/ko/gps_compass/rtk_gps_locosys_r1.md b/docs/ko/gps_compass/rtk_gps_locosys_r1.md
index 0e608794ce..06025daca0 100644
--- a/docs/ko/gps_compass/rtk_gps_locosys_r1.md
+++ b/docs/ko/gps_compass/rtk_gps_locosys_r1.md
@@ -26,7 +26,7 @@ For an equivalent GPS module with a compass try: [LOCOSYS Hawk R2](../gps_compas
- Fast TTFF at low signal level
- Free hybrid ephemeris prediction to achieve faster cold start
- Default 5Hz, up to 10 Hz update rate (SBAS support 5Hz only).
-- Build-in super capacitor to reserve system data for rapid satellite acquisition
+- Built-in super capacitor to reserve system data for rapid satellite acquisition
diff --git a/docs/ko/gps_compass/rtk_gps_locosys_r2.md b/docs/ko/gps_compass/rtk_gps_locosys_r2.md
index d2c9f493f0..534b964f34 100644
--- a/docs/ko/gps_compass/rtk_gps_locosys_r2.md
+++ b/docs/ko/gps_compass/rtk_gps_locosys_r2.md
@@ -22,8 +22,8 @@ The fast time-to-first-fix, RTK convergence, superior sensitivity, low power con
- Fast TTFF at low signal level
- Free hybrid ephemeris prediction to achieve faster cold start
- Default 5Hz, up to 10 Hz update rate (SBAS support 5Hz only)
-- Build-in super capacitor to reserve system data for rapid satellite acquisition
-- Build-in 3 axis compass function
+- Built-in super capacitor to reserve system data for rapid satellite acquisition
+- Built-in 3 axis compass function
- Three LED indicator for Power, PPS and Data transmit
diff --git a/docs/ko/gps_compass/septentrio.md b/docs/ko/gps_compass/septentrio.md
index 2160154b9e..eb31f237cd 100644
--- a/docs/ko/gps_compass/septentrio.md
+++ b/docs/ko/gps_compass/septentrio.md
@@ -10,7 +10,7 @@ Certain receivers are recommended for autopilot applications because of their ph
Dual-antenna, ultra-low-power GNSS rover receiver with support for heading.
-- [AsteRx-m3 Pro+](https://www.septentrio.com/en/products/gps/gnss-boards/asterx-m3-pro-plus)
+- [AsteRx-m3 Pro+](https://www.septentrio.com/en/products/gnss-receivers/gnss-boards/asterx-m3-pro-plus)
Dual-antenna, ultra-low-power versatile GNSS rover and base receiver with support for heading.
@@ -19,7 +19,7 @@ Certain receivers are recommended for autopilot applications because of their ph
Single-antenna evaluation kit with support for L5 frequency band, based on the mosaic-X5 GNSS
receiver module.
-- [mosaic-go heading](https://www.septentrio.com/en/products/gps/gnss-receiver-modules/mosaic-h-evaluation-kit)
+- [mosaic-go heading](https://www.septentrio.com/en/products/gnss-receivers/gnss-receiver-modules/mosaic-h-evaluation-kit)
Dual-antenna evaluation kit with support for heading, based on the mosaic-H GNSS receiver module.
diff --git a/docs/ko/gps_compass/septentrio_mosaic-go.md b/docs/ko/gps_compass/septentrio_mosaic-go.md
index 87dcc69e74..5e7fcd0772 100644
--- a/docs/ko/gps_compass/septentrio_mosaic-go.md
+++ b/docs/ko/gps_compass/septentrio_mosaic-go.md
@@ -2,8 +2,8 @@
The Septentrio mosaic-go receivers are evaluation kits for their mosaic-X5 and mosaic-H receiver modules.
Because of their small size and low weight, they are ideal for autopilot applications.
-The available variants are the [mosaic-go](https://www.septentrio.com/en/products/gps/gnss-receiver-modules/mosaic-go-evaluation-kit)
-and [mosaic-go heading](https://www.septentrio.com/en/products/gps/gnss-receiver-modules/mosaic-h-evaluation-kit).
+The available variants are the [mosaic-go](https://www.septentrio.com/en/products/gnss-receivers/gnss-receiver-modules/mosaic-go-evaluation-kit)
+and [mosaic-go heading](https://www.septentrio.com/en/products/gnss-receivers/gnss-receiver-modules/mosaic-h-evaluation-kit).
@@ -108,7 +108,7 @@ To enable multi-antenna attitude determination, follow the following procedure:
These can be compensated for with the heading parameters provided by the Septentrio driver in PX4.
:::info
-For optimal heading results, the two antennas should be seperated by at least 30cm / 11.8 in (ideally 50cm / 19.7in or more).
+For optimal heading results, the two antennas should be separated by at least 30cm / 11.8 in (ideally 50cm / 19.7in or more).
For additional configuration of the dual antenna setup, please refer to our [Knowledge Base](https://support.septentrio.com/l/858493/2022-04-19/xgrqd) or the [hardware manual](https://web.septentrio.com/l/858493/2022-04-19/xgrql).
:::
diff --git a/docs/ko/gps_compass/u-blox_f9p_heading.md b/docs/ko/gps_compass/u-blox_f9p_heading.md
index b7f672d078..e0640b3111 100644
--- a/docs/ko/gps_compass/u-blox_f9p_heading.md
+++ b/docs/ko/gps_compass/u-blox_f9p_heading.md
@@ -10,7 +10,7 @@ This feature works on F9P devices that support CAN or expose the GPS UART2 port.
The following devices are supported:
- [ARK RTK GPS](https://arkelectron.com/product/ark-rtk-gps/) (arkelectron.com)
-- [SparkFun GPS-RTK2 Board - ZED-F9P](https://www.sparkfun.com/products/15136) (www.sparkfun.com)
+- [SparkFun GPS-RTK2 Board - ZED-F9P](https://www.sparkfun.com/sparkfun-gps-rtk2-board-zed-f9p-qwiic-gps-15136.html) (www.sparkfun.com)
- [SIRIUS RTK GNSS ROVER (F9P)](https://store-drotek.com/911-sirius-rtk-gnss-rover-f9p.html) (store-drotek.com)
- [mRo u-blox ZED-F9 RTK L1/L2 GPS](https://store.mrobotics.io/product-p/m10020d.htm) (store.mrobotics.io)
- [Holybro H-RTK F9P Helical or Base](https://holybro.com/products/h-rtk-f9p-gnss-series) (Holybro Store)
diff --git a/docs/ko/hardware/board_support_guide.md b/docs/ko/hardware/board_support_guide.md
index ad5dec6778..63183773a5 100644
--- a/docs/ko/hardware/board_support_guide.md
+++ b/docs/ko/hardware/board_support_guide.md
@@ -57,7 +57,7 @@ PX4는 일반적으로 상업적으로 사용 가능한 보드만 지원하므
### VER and REV ID (Hardware Revision and Version Sensing) {#ver_rev_id}
FMUv5 이상에는 전기 감지 메커니즘이 있습니다.
-선택적 구성 데이터와 결합된 이 감지는 필수 장치 및 전원 공급 장치 구성과 관련하여 하드웨어 구성을 정의합니다. Manufacturers must obtain the VER and REV ID from PX4 board maintainers by issuing a PR to ammend the [DS-018 Pixhawk standard](https://github.com/pixhawk/Pixhawk-Standards) for board versions and revisions.
+선택적 구성 데이터와 결합된 이 감지는 필수 장치 및 전원 공급 장치 구성과 관련하여 하드웨어 구성을 정의합니다. Manufacturers must obtain the VER and REV ID from PX4 board maintainers by issuing a PR to amend the [DS-018 Pixhawk standard](https://github.com/pixhawk/Pixhawk-Standards) for board versions and revisions.
Because these boards are 100% compliant with the Pixhawk standard, the values assigned for VER and REV ID are the defaults for that FMU Version.
@@ -97,7 +97,7 @@ _New_ experimental boards are allocated [VER and REV IDs](#ver_rev_id) based on
이 범주에는 PX4 프로젝트 또는 제조업체에서 지원하지 않고 "실험적" 지원에 해당하지 않는 모든 보드가 포함됩니다.
- 보드는 우리가 이미 지원하는 것과 문서상 어느 정도 호환되며 "실험적"으로 올리려면, 최소한의 노력이 필요하지만 개발 팀이나 제조업체 모두 현재 이를 추구하지 않습니다.
-- Manufacturer/Owner of hardware violates our [Code of Conduct](https://discuss.px4.io/t/code-of-conduct/13655)
+- Manufacturer/Owner of hardware violates our [Code of Conduct](https://discuss.px4.io/t/px4-community-code-of-conduct/13655)
- 라이선스 제한으로 인해 보드 지원을 추가하는 데 필요한 도구/libs/drivers/etc가 호환되지 않는 것으로 간주되는 비공개 소스
- 보드가 일반 요구 사항에 명시된 최소 요구 사항을 충족하지 않습니다.
diff --git a/docs/ko/hardware/drone_parts.md b/docs/ko/hardware/drone_parts.md
index fe395f1b44..94c826c1ad 100644
--- a/docs/ko/hardware/drone_parts.md
+++ b/docs/ko/hardware/drone_parts.md
@@ -1,4 +1,4 @@
-# Hardware Hardware Selection & Setup
+# Hardware Selection & Setup
PX4 완제품 기체와 자체 제작 드론의 부품들에 대하여 설명합니다.
diff --git a/docs/ko/index.md b/docs/ko/index.md
index 339b6ecf6c..bc3b4a558c 100644
--- a/docs/ko/index.md
+++ b/docs/ko/index.md
@@ -5,7 +5,7 @@ const { site } = useData();
# PX4 Autopilot 사용자 안내서
-[](https://github.com/PX4/PX4-Autopilot/releases) [](https://discuss.px4.io//) [](https://discord.gg/dronecode)
+[](https://github.com/PX4/PX4-Autopilot/releases) [](https://discuss.px4.io//) [](https://discord.com/invite/dronecode)
PX4 is an open-source autopilot for drones and autonomous vehicles. It runs on multirotors, fixed-wing, VTOL, helicopters, rovers, and more. This guide covers everything from assembly and configuration to flight operations and development.
@@ -49,7 +49,7 @@ Read [Operations](config/operations.md) to understand safety features and failsa
## 지원
-Get help on the [discussion forums](https://discuss.px4.io/) or [Discord](https://discord.gg/dronecode). See the [Support](contribute/support.md) page for diagnosing problems, reporting bugs, and joining the [weekly dev call](contribute/dev_call.md).
+Get help on the [discussion forums](https://discuss.px4.io/) or [Discord](https://discord.com/invite/dronecode). See the [Support](contribute/support.md) page for diagnosing problems, reporting bugs, and joining the [weekly dev call](contribute/dev_call.md).
## 기여
@@ -94,9 +94,9 @@ The calendar default timezone is Central European Time (CET).
## 운영 방법
-The PX4 Autopilot project is hosted by the [Dronecode Foundation](https://www.dronecode.org/), a [Linux Foundation](https://www.linuxfoundation.org/) Collaborative Project. Dronecode holds all PX4 trademarks and serves as the project's legal guardian, ensuring vendor-neutral stewardship. No single company owns the name or controls the roadmap. The source code is licensed under the [BSD 3-Clause](https://opensource.org/license/BSD-3-Clause) license, so you are free to use, modify, and distribute it in your own projects.
+The PX4 Autopilot project is hosted by the [Dronecode Foundation](https://dronecode.org/), a [Linux Foundation](https://www.linuxfoundation.org/) Collaborative Project. Dronecode holds all PX4 trademarks and serves as the project's legal guardian, ensuring vendor-neutral stewardship. No single company owns the name or controls the roadmap. The source code is licensed under the [BSD 3-Clause](https://opensource.org/license/BSD-3-Clause) license, so you are free to use, modify, and distribute it in your own projects.
-
+
-
This page is on a release branch, and hence probably out of date. See the latest version.
+This page is on a release branch, and hence probably out of date. See the latest version.
-
This page is on a release branch, and hence probably out of date. See the latest version.
+This page is on a release branch, and hence probably out of date. See the latest version.
-
This page may be out out of date. See the latest version.
+This page may be out of date. See the latest version.