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https://github.com/ArduPilot/ardupilot
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287ebe8e6a
Sensor bias corrections were being applied to the incoming IMU data using the wrong delta time. This was what was driving the different tuning between plane and copter for gyro bias process noise so the same gyro bias process noise default tuning value can now be used for all platform types. Sensor bias corrections were being applied a a second time to the output observer inertial data. |
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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 | ||