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When changing the vehicle yaw angle, the correlation between the attitude errors and errors in other states is invalid so the corresponding co-variance terms need to be zeroed. This needs to be done in more than one place. |
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.. | ||
AP_NavEKF2_AirDataFusion.cpp | ||
AP_NavEKF2_Buffer.h | ||
AP_NavEKF2_Control.cpp | ||
AP_NavEKF2_core.cpp | ||
AP_NavEKF2_core.h | ||
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.cpp | ||
AP_NavEKF2.h | ||
AP_NavEKF_GyroBias.cpp |