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Fix magnetometer typo

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This commit is contained in:
Hamish Willee
2023-01-30 10:24:16 +01:00
committed by Silvan Fuhrer
parent 8da993c30e
commit f25abbc80a
8 changed files with 12 additions and 12 deletions
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msg/EstimatorEventFlags.msg
+2 -2
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@@ -31,7 +31,7 @@ bool height_sensor_timeout # 4 - true when the height sensor has n
bool stopping_navigation # 5 - true when the filter has insufficient data to estimate velocity and position and is falling back to an attitude, height and height rate mode of operation
bool invalid_accel_bias_cov_reset # 6 - true when the filter has detected bad acceerometer bias state esitmstes and has reset the corresponding covariance matrix elements
bool bad_yaw_using_gps_course # 7 - true when the filter has detected an invalid yaw estimate and has reset the yaw angle to the GPS ground course
bool stopping_mag_use # 8 - true when the filter has detected bad magnetometer data and is stopping further use of the magnetomer data
bool stopping_mag_use # 8 - true when the filter has detected bad magnetometer data and is stopping further use of the magnetometer data
bool vision_data_stopped # 9 - true when the vision system data has stopped for a significant time period
bool emergency_yaw_reset_mag_stopped # 10 - true when the filter has detected bad magnetometer data, has reset the yaw to anothter source of data and has stopped further use of the magnetomer data
bool emergency_yaw_reset_mag_stopped # 10 - true when the filter has detected bad magnetometer data, has reset the yaw to anothter source of data and has stopped further use of the magnetometer data
bool emergency_yaw_reset_gps_yaw_stopped # 11 - true when the filter has detected bad GNSS yaw data, has reset the yaw to anothter source of data and has stopped further use of the GNSS yaw data
msg/EstimatorStatus.msg
+1 -1
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@@ -35,7 +35,7 @@ uint8 CS_EV_HGT = 14 # 14 - true when height data from external vision measurem
uint8 CS_BETA = 15 # 15 - true when synthetic sideslip measurements are being fused
uint8 CS_MAG_FIELD = 16 # 16 - true when only the magnetic field states are updated by the magnetometer
uint8 CS_FIXED_WING = 17 # 17 - true when thought to be operating as a fixed wing vehicle with constrained sideslip
uint8 CS_MAG_FAULT = 18 # 18 - true when the magnetomer has been declared faulty and is no longer being used
uint8 CS_MAG_FAULT = 18 # 18 - true when the magnetometer has been declared faulty and is no longer being used
uint8 CS_ASPD = 19 # 19 - true when airspeed measurements are being fused
uint8 CS_GND_EFFECT = 20 # 20 - true when when protection from ground effect induced static pressure rise is active
uint8 CS_RNG_STUCK = 21 # 21 - true when a stuck range finder sensor has been detected