6b04a81b8d
Fixes bugs that prevented planes being able to reset yaw to GPS to recovery from takeoff with a bad magnetoemter. 1) If the velocity innovation check had not failed by the time the in-air transition occurred, then the yaw reset would not be performed 2) The velocity states were not being reset 3) The non fly-forward vehicle (copter) reset could occur first and effectively lock out the fly-forward vehicle (plane) yaw check. |
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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 | ||