fly316/PX4-Autopilot
7
0
Fork 0
mirror of https://gitee.com/mirrors_PX4/PX4-Autopilot.git synced 2026-10-14 20:33:34 +08:00
Code Issues Packages Projects Releases Wiki Activity

docs(i18n): PX4 guide translations (Crowdin) - zh-CN (#26760)

Browse Source 
Co-authored-by: Crowdin Bot <support+bot@crowdin.com>
This commit is contained in:
PX4 Build Bot
2026-03-19 15:36:32 +11:00
committed by GitHub
co-authored by Crowdin Bot
parent be0ee3d185
commit db1b8d9ce6
16 changed files with 478 additions and 253 deletions
Download Patch File Download Diff File Expand all files Collapse all files
docs/zh/msg_docs/ActuatorMotors.md
+7 -7
View File
@@ -22,11 +22,11 @@ Published by the vehicle's allocation and consumed by the ESC protocol drivers e
## Constants
| 参数名 | 类型 | 值 | 描述 |
| --------------------------------------------------------------------------------------------------------- | -------- | --- | -- |
| <a id="#MESSAGE_VERSION"></a> MESSAGE_VERSION | `uint32` | 0 | |
| <a id="#ACTUATOR_FUNCTION_MOTOR1"></a> ACTUATOR_FUNCTION_MOTOR1 | `uint8` | 101 | |
| <a id="#NUM_CONTROLS"></a> NUM_CONTROLS | `uint8` | 12 | |
| 参数名 | 类型 | 值 | 描述 |
| --------------------------------------------------------------------------------------------------------- | -------- | --- | -------------------------------------------------------------------------------------- |
| <a id="#MESSAGE_VERSION"></a> MESSAGE_VERSION | `uint32` | 0 | |
| <a id="#ACTUATOR_FUNCTION_MOTOR1"></a> ACTUATOR_FUNCTION_MOTOR1 | `uint8` | 101 | output_functions.yaml Motor.start |
| <a id="#NUM_CONTROLS"></a> NUM_CONTROLS | `uint8` | 12 | output_functions.yaml Motor.count |
## Source Message
@@ -48,9 +48,9 @@ uint64 timestamp_sample # [us] Sampling timestamp of the data this control respo
uint16 reversible_flags # [-] Bitset indicating which motors are configured to be reversible
uint8 ACTUATOR_FUNCTION_MOTOR1 = 101
uint8 ACTUATOR_FUNCTION_MOTOR1 = 101 # output_functions.yaml Motor.start
uint8 NUM_CONTROLS = 12
uint8 NUM_CONTROLS = 12 # output_functions.yaml Motor.count
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)
```
docs/zh/msg_docs/EscReport.md
+2 -23
View File
@@ -29,17 +29,7 @@ pageClass: is-wide-page
| 参数名 | 类型 | 值 | 描述 |
| ------------------------------------------------------------------------------------------------------------------------------------------ | ------- | --- | ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ |
| <a id="#ACTUATOR_FUNCTION_MOTOR1"></a> ACTUATOR_FUNCTION_MOTOR1 | `uint8` | 101 | |
| <a id="#ACTUATOR_FUNCTION_MOTOR2"></a> ACTUATOR_FUNCTION_MOTOR2 | `uint8` | 102 | |
| <a id="#ACTUATOR_FUNCTION_MOTOR3"></a> ACTUATOR_FUNCTION_MOTOR3 | `uint8` | 103 | |
| <a id="#ACTUATOR_FUNCTION_MOTOR4"></a> ACTUATOR_FUNCTION_MOTOR4 | `uint8` | 104 | |
| <a id="#ACTUATOR_FUNCTION_MOTOR5"></a> ACTUATOR_FUNCTION_MOTOR5 | `uint8` | 105 | |
| <a id="#ACTUATOR_FUNCTION_MOTOR6"></a> ACTUATOR_FUNCTION_MOTOR6 | `uint8` | 106 | |
| <a id="#ACTUATOR_FUNCTION_MOTOR7"></a> ACTUATOR_FUNCTION_MOTOR7 | `uint8` | 107 | |
| <a id="#ACTUATOR_FUNCTION_MOTOR8"></a> ACTUATOR_FUNCTION_MOTOR8 | `uint8` | 108 | |
| <a id="#ACTUATOR_FUNCTION_MOTOR9"></a> ACTUATOR_FUNCTION_MOTOR9 | `uint8` | 109 | |
| <a id="#ACTUATOR_FUNCTION_MOTOR10"></a> ACTUATOR_FUNCTION_MOTOR10 | `uint8` | 110 | |
| <a id="#ACTUATOR_FUNCTION_MOTOR11"></a> ACTUATOR_FUNCTION_MOTOR11 | `uint8` | 111 | |
| <a id="#ACTUATOR_FUNCTION_MOTOR12"></a> ACTUATOR_FUNCTION_MOTOR12 | `uint8` | 112 | |
| <a id="#ACTUATOR_FUNCTION_MOTOR_MAX"></a> ACTUATOR_FUNCTION_MOTOR_MAX | `uint8` | 112 | output_functions.yaml Motor.start + Motor.count - 1 |
| <a id="#FAILURE_OVER_CURRENT"></a> FAILURE_OVER_CURRENT | `uint8` | 0 | (1 << 0) |
| <a id="#FAILURE_OVER_VOLTAGE"></a> FAILURE_OVER_VOLTAGE | `uint8` | 1 | (1 << 1) |
| <a id="#FAILURE_MOTOR_OVER_TEMPERATURE"></a> FAILURE_MOTOR_OVER_TEMPERATURE | `uint8` | 2 | (1 << 2) |
@@ -73,19 +63,8 @@ uint8 esc_cmdcount # Counter of number of commands
uint8 esc_state # State of ESC - depend on Vendor
uint8 actuator_function # actuator output function (one of Motor1...MotorN)
uint8 ACTUATOR_FUNCTION_MOTOR1 = 101
uint8 ACTUATOR_FUNCTION_MOTOR2 = 102
uint8 ACTUATOR_FUNCTION_MOTOR3 = 103
uint8 ACTUATOR_FUNCTION_MOTOR4 = 104
uint8 ACTUATOR_FUNCTION_MOTOR5 = 105
uint8 ACTUATOR_FUNCTION_MOTOR6 = 106
uint8 ACTUATOR_FUNCTION_MOTOR7 = 107
uint8 ACTUATOR_FUNCTION_MOTOR8 = 108
uint8 ACTUATOR_FUNCTION_MOTOR9 = 109
uint8 ACTUATOR_FUNCTION_MOTOR10 = 110
uint8 ACTUATOR_FUNCTION_MOTOR11 = 111
uint8 ACTUATOR_FUNCTION_MOTOR12 = 112
uint8 ACTUATOR_FUNCTION_MOTOR_MAX = 112 # output_functions.yaml Motor.start + Motor.count - 1
uint16 failures # Bitmask to indicate the internal ESC faults
int8 esc_power # Applied power 0-100 in % (negative values reserved)
docs/zh/msg_docs/EstimatorStatusFlags.md
+4
View File
@@ -61,6 +61,8 @@ pageClass: is-wide-page
| cs_gnss_fault | `bool` | | | 45 - true if GNSS true if GNSS measurements (lat, lon, vel) have been declared faulty |
| cs_yaw_manual | `bool` | | | 46 - true if yaw has been set manually |
| cs_gnss_hgt_fault | `bool` | | | 47 - true if GNSS true if GNSS measurements (alt) have been declared faulty |
| cs_in_transition | `bool` | | | 48 - true if the vehicle is in vtol transition |
| cs_heading_observable | `bool` | | | 49 - true when heading is observable |
| fault_status_changes | `uint32` | | | number of filter fault status (fs) changes |
| fs_bad_mag_x | `bool` | | | 0 - true if the fusion of the magnetometer X-axis has encountered a numerical error |
| fs_bad_mag_y | `bool` | | | 1 - true if the fusion of the magnetometer Y-axis has encountered a numerical error |
@@ -136,6 +138,8 @@ bool cs_gnss_vel # 44 - true if GNSS velocity measurement fusion
bool cs_gnss_fault # 45 - true if GNSS true if GNSS measurements (lat, lon, vel) have been declared faulty
bool cs_yaw_manual # 46 - true if yaw has been set manually
bool cs_gnss_hgt_fault # 47 - true if GNSS true if GNSS measurements (alt) have been declared faulty
bool cs_in_transition # 48 - true if the vehicle is in vtol transition
bool cs_heading_observable # 49 - true when heading is observable
# fault status
uint32 fault_status_changes # number of filter fault status (fs) changes