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https://github.com/ArduPilot/ardupilot
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165335b9e3
Allow different process noise to be set for body (sensor bias) and earth field states. This allows a stable magnetometer bias estimate to be available at end of flight whilst still allowing for external magnetic anomalies during landing. Adjust default values to give stable mag bias learning and fast learning of external anomalies. |
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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 |