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https://github.com/ArduPilot/ardupilot
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a8983d075f
The setting of the EKF origin and the entry into GPS aiding mode have been separated to make the logic clear. The order of operations has been changed to ensure that when a reset to GPS is performed, a valid GPS measurement is available in the buffer Declaration of GPS availability is not made unless the GPS data has been entered into the buffer |
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| .. | ||
| AP_NavEKF2_AirDataFusion.cpp | ||
| 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 | ||