mirror of
https://github.com/ArduPilot/ardupilot
synced 2025-01-04 15:08:28 -04:00
6f04fae4a0
this allows for a magnetometer to be used as a fallback yaw source in flight when using an external yaw source such as a GPS. The magnetometer bias is learned while the GPS yaw is available and fallback is only done if the mag yaw and GPS yaw are consistent when fallback is enabled This also learns the Z gyro bias until first yaw alignment when MAG_CAL is EXTERNAL_YAW_FALLBACK. This prevents large gyro bias building while waiting for GPS lock |
||
|---|---|---|
| .. | ||
| AP_NavEKF3_AirDataFusion.cpp | ||
| AP_NavEKF3_Buffer.h | ||
| AP_NavEKF3_Control.cpp | ||
| AP_NavEKF3_core.cpp | ||
| AP_NavEKF3_core.h | ||
| AP_NavEKF3_GyroBias.cpp | ||
| AP_NavEKF3_Logging.cpp | ||
| AP_NavEKF3_MagFusion.cpp | ||
| AP_NavEKF3_Measurements.cpp | ||
| AP_NavEKF3_OptFlowFusion.cpp | ||
| AP_NavEKF3_Outputs.cpp | ||
| AP_NavEKF3_PosVelFusion.cpp | ||
| AP_NavEKF3_RngBcnFusion.cpp | ||
| AP_NavEKF3_VehicleStatus.cpp | ||
| AP_NavEKF3.cpp | ||
| AP_NavEKF3.h | ||