mirror of https://github.com/ArduPilot/ardupilot
aa14de9d39
Vibration in the 400Hz delta angles could cause the angular rate condition check for in-flight magnetic field alignment to fail. The symptons were failure to start magnetic field learning as expected when EK2_MAG_CAL=3 was set. |
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| .. | ||
| AP_NavEKF2.cpp | ||
| AP_NavEKF2.h | ||
| AP_NavEKF2_AirDataFusion.cpp | ||
| AP_NavEKF2_Control.cpp | ||
| AP_NavEKF2_MagFusion.cpp | ||
| AP_NavEKF2_Measurements.cpp | ||
| AP_NavEKF2_OptFlowFusion.cpp | ||
| AP_NavEKF2_Outputs.cpp | ||
| AP_NavEKF2_PosVelFusion.cpp | ||
| AP_NavEKF2_VehicleStatus.cpp | ||
| AP_NavEKF2_core.cpp | ||
| AP_NavEKF2_core.h | ||
| AP_NavEKF_GyroBias.cpp | ||