mirror of
https://gitee.com/mirrors_PX4/PX4-Autopilot.git
synced 2026-10-20 07:03:33 +08:00
New Crowdin translations - ko (#25780)
Co-authored-by: Crowdin Bot <support+bot@crowdin.com>
This commit is contained in:
co-authored by
Crowdin Bot
parent
0d0bfc1937
commit
ead1cf00ff
@@ -276,12 +276,12 @@ The relevant parameters are listed in the table below.
|
||||
|
||||
## 고장 감지기
|
||||
|
||||
고장 감지기를 사용하여 차량의 예기치 않게 전복되거나 외부의 고장 감지 시스템에 따른 보호 조치를 할 수 있습니다.
|
||||
The failure detector allows a vehicle to take protective actions if it unexpectedly flips, detects a motor failure, or if it is notified by an external failure detection system.
|
||||
|
||||
During **flight**, the failure detector can be used to trigger [flight termination](../advanced_config/flight_termination.md) if failure conditions are met, which may then launch a [parachute](../peripherals/parachute.md) or perform some other action.
|
||||
|
||||
:::info
|
||||
Failure detection during flight is deactivated by default (enable by setting the parameter: [CBRK_FLIGHTTERM=0](#CBRK_FLIGHTTERM)).
|
||||
Acting on a detected failure during flight is deactivated by default (enable by setting the parameter: [CBRK_FLIGHTTERM=0](#CBRK_FLIGHTTERM)).
|
||||
:::
|
||||
|
||||
During **takeoff** the failure detector [attitude trigger](#attitude-trigger) invokes the [disarm action](#act_disarm) if the vehicle flips (disarm kills the motors but, unlike flight termination, will not launch a parachute or perform other failure actions).
|
||||
@@ -303,6 +303,26 @@ The failure detector is active in all vehicle types and modes, except for those
|
||||
| <a id="FD_FAIL_P_TTRI"></a>[FD_FAIL_P_TTRI](../advanced_config/parameter_reference.md#FD_FAIL_P_TTRI) | Time to exceed [FD_FAIL_P](#FD_FAIL_P) for failure detection (default 0.3s). |
|
||||
| <a id="FD_FAIL_R_TTRI"></a>[FD_FAIL_R_TTRI](../advanced_config/parameter_reference.md#FD_FAIL_R_TTRI) | Time to exceed [FD_FAIL_R](#FD_FAIL_R) for failure detection (default 0.3s). |
|
||||
|
||||
### Motor Failure Trigger
|
||||
|
||||
The failure detector can be configured to detect a motor failure while armed (and trigger an associated action) in the following conditions:
|
||||
|
||||
- A 300 ms timeout occurs in telemetry from an ESC that was previously available.
|
||||
- The input current in the telemetry of an ESC which was previously positive gets too low for more than [`FD_ACT_MOT_TOUT`](FD_ACT_MOT_TOUT) ms.
|
||||
The "too low" condition is defined by:
|
||||
|
||||
```text
|
||||
{esc current} < {parameter FD_ACT_MOT_C2T} * {motor command between 0 and 1}
|
||||
```
|
||||
|
||||
| 매개변수 | 설명 |
|
||||
| ----------------------------------------------------------------------------------------------------------------------------------------------------------------------- | --------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- |
|
||||
| <a id="FD_ACT_EN"></a>[FD_ACT_EN](../advanced_config/parameter_reference.md#FD_ACT_EN) | Enable/disable the motor failure trigger completely. |
|
||||
| <a id="FD_ACT_MOT_THR"></a>[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. |
|
||||
| <a id="FD_ACT_MOT_C2T"></a>[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. |
|
||||
| <a id="FD_ACT_MOT_TOUT"></a>[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. |
|
||||
| <a id="CA_FAILURE_MODE"></a>[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)
|
||||
|
||||
The [failure detector](#failure-detector), if [enabled](#CBRK_FLIGHTTERM), can also be triggered by an external ATS system.
|
||||
|
||||
Reference in New Issue
Block a user