mirror of
https://gitee.com/mirrors_PX4/PX4-Autopilot.git
synced 2026-10-27 07:13:35 +08:00
docs: auto-sync metadata [skip ci]
Co-Authored-By: PX4 BuildBot <bot@px4.io>
This commit is contained in:
@@ -22729,82 +22729,6 @@ Yaw rate proportional gain.
|
||||
|
||||
## Failure Detector
|
||||
|
||||
### FD_ACT_EN (`INT32`) {#FD_ACT_EN}
|
||||
|
||||
Enable Actuator Failure check.
|
||||
|
||||
If enabled, failure detector will verify that for motors, a minimum amount of ESC current per throttle
|
||||
level is being consumed.
|
||||
Otherwise this indicates an motor failure.
|
||||
|
||||
| Reboot | minValue | maxValue | increment | default | unit |
|
||||
| ------- | -------- | -------- | --------- | ------------ | ---- |
|
||||
| ✓ | | | | Disabled (0) | |
|
||||
|
||||
### FD_ACT_HIGH_OFF (`FLOAT`) {#FD_ACT_HIGH_OFF}
|
||||
|
||||
Overcurrent motor failure limit offset.
|
||||
|
||||
threshold = FD_ACT_MOT_C2T \* thrust + FD_ACT_HIGH_OFF
|
||||
|
||||
| Reboot | minValue | maxValue | increment | default | unit |
|
||||
| ------ | -------- | -------- | --------- | ------- | ---- |
|
||||
| | 0 | 30 | 1 | 10. | A |
|
||||
|
||||
### FD_ACT_LOW_OFF (`FLOAT`) {#FD_ACT_LOW_OFF}
|
||||
|
||||
Undercurrent motor failure limit offset.
|
||||
|
||||
threshold = FD_ACT_MOT_C2T \* thrust - FD_ACT_LOW_OFF
|
||||
|
||||
| Reboot | minValue | maxValue | increment | default | unit |
|
||||
| ------ | -------- | -------- | --------- | ------- | ---- |
|
||||
| | 0 | 30 | 1 | 10. | A |
|
||||
|
||||
### FD_ACT_MOT_C2T (`FLOAT`) {#FD_ACT_MOT_C2T}
|
||||
|
||||
Motor Failure Current/Throttle Scale.
|
||||
|
||||
Determines the slope between expected steady state current and linearized, normalized thrust command.
|
||||
E.g. FD_ACT_MOT_C2T A represents the expected steady state current at 100%.
|
||||
FD_ACT_LOW_OFF and FD_ACT_HIGH_OFF offset the threshold from that slope.
|
||||
|
||||
| Reboot | minValue | maxValue | increment | default | unit |
|
||||
| ------ | -------- | -------- | --------- | ------- | ---- |
|
||||
| | 0.0 | 50.0 | 1 | 35. | A/% |
|
||||
|
||||
### FD_ACT_MOT_THR (`FLOAT`) {#FD_ACT_MOT_THR}
|
||||
|
||||
Motor Failure Thrust Threshold.
|
||||
|
||||
Failure detection per motor only triggers above this thrust value.
|
||||
Set to 1 to disable the detection.
|
||||
|
||||
| Reboot | minValue | maxValue | increment | default | unit |
|
||||
| ------ | -------- | -------- | --------- | ------- | ---- |
|
||||
| | 0.0 | 1.0 | 0.01 | 0.2 | norm |
|
||||
|
||||
### FD_ACT_MOT_TOUT (`INT32`) {#FD_ACT_MOT_TOUT}
|
||||
|
||||
Motor Failure Hysteresis Time.
|
||||
|
||||
Motor failure only triggers after current thresholds are exceeded for this time.
|
||||
|
||||
| Reboot | minValue | maxValue | increment | default | unit |
|
||||
| ------ | -------- | -------- | --------- | ------- | ---- |
|
||||
| | 10 | 10000 | 100 | 1000 | ms |
|
||||
|
||||
### FD_ESCS_EN (`INT32`) {#FD_ESCS_EN}
|
||||
|
||||
Enable checks on ESCs that report their arming state.
|
||||
|
||||
If enabled, failure detector will verify that all the ESCs have successfully armed when the vehicle has transitioned to the armed state.
|
||||
Timeout for receiving an acknowledgement from the ESCs is 0.3s, if no feedback is received the failure detector will auto disarm the vehicle.
|
||||
|
||||
| Reboot | minValue | maxValue | increment | default | unit |
|
||||
| ------ | -------- | -------- | --------- | ----------- | ---- |
|
||||
| | | | | Enabled (1) | |
|
||||
|
||||
### FD_EXT_ATS_EN (`INT32`) {#FD_EXT_ATS_EN}
|
||||
|
||||
Enable PWM input on for engaging failsafe from an external automatic trigger system (ATS).
|
||||
@@ -28378,6 +28302,63 @@ needs to be changed to match a custom setting
|
||||
| ------- | -------- | -------- | --------- | ------- | ---- |
|
||||
| ✓ | | | | 0 | |
|
||||
|
||||
## Motor Failure
|
||||
|
||||
### FD_ACT_EN (`INT32`) {#FD_ACT_EN}
|
||||
|
||||
Enable Actuator Failure check.
|
||||
|
||||
If enabled, the HealthAndArmingChecks will verify that for motors, a minimum amount of ESC current per throttle
|
||||
level is being consumed.
|
||||
Otherwise this indicates an motor failure.
|
||||
This check only works for ESCs that report current consumption.
|
||||
|
||||
| Reboot | minValue | maxValue | increment | default | unit |
|
||||
| ------ | -------- | -------- | --------- | ------------ | ---- |
|
||||
| | | | | Disabled (0) | |
|
||||
|
||||
### MOTFAIL_C2T (`FLOAT`) {#MOTFAIL_C2T}
|
||||
|
||||
Motor Failure Current/Throttle Scale.
|
||||
|
||||
Determines the slope between expected steady state current and linearized, normalized thrust command.
|
||||
E.g. FD_ACT_MOT_C2T A represents the expected steady state current at 100%.
|
||||
FD_ACT_LOW_OFF and FD_ACT_HIGH_OFF offset the threshold from that slope.
|
||||
|
||||
| Reboot | minValue | maxValue | increment | default | unit |
|
||||
| ------ | -------- | -------- | --------- | ------- | ---- |
|
||||
| | 0.0 | 50.0 | 1 | 35. | A/% |
|
||||
|
||||
### MOTFAIL_HIGH_OFF (`FLOAT`) {#MOTFAIL_HIGH_OFF}
|
||||
|
||||
Overcurrent motor failure limit offset.
|
||||
|
||||
threshold = FD_ACT_MOT_C2T \* thrust + FD_ACT_HIGH_OFF
|
||||
|
||||
| Reboot | minValue | maxValue | increment | default | unit |
|
||||
| ------ | -------- | -------- | --------- | ------- | ---- |
|
||||
| | 0 | 30 | 1 | 10. | A |
|
||||
|
||||
### MOTFAIL_LOW_OFF (`FLOAT`) {#MOTFAIL_LOW_OFF}
|
||||
|
||||
Undercurrent motor failure limit offset.
|
||||
|
||||
threshold = FD_ACT_MOT_C2T \* thrust - FD_ACT_LOW_OFF
|
||||
|
||||
| Reboot | minValue | maxValue | increment | default | unit |
|
||||
| ------ | -------- | -------- | --------- | ------- | ---- |
|
||||
| | 0 | 30 | 1 | 10. | A |
|
||||
|
||||
### MOTFAIL_TIME (`FLOAT`) {#MOTFAIL_TIME}
|
||||
|
||||
Motor Failure Hysteresis Time.
|
||||
|
||||
Motor failure only triggers after current thresholds are exceeded for this time.
|
||||
|
||||
| Reboot | minValue | maxValue | increment | default | unit |
|
||||
| ------ | -------- | -------- | --------- | ------- | ---- |
|
||||
| | 0.01 | 10 | 1 | 1. | s |
|
||||
|
||||
## Mount
|
||||
|
||||
### MNT_DO_STAB (`INT32`) {#MNT_DO_STAB}
|
||||
|
||||
Reference in New Issue
Block a user