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https://github.com/ArduPilot/ardupilot
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7d6b926749
Use an Euler yaw heading that switches between a 321 and 312 rotation sequence to avoid areas of singularity. Using Euler yaw decouples the observation from the roll and pitch states and prevents magnetic disturbances from affecting roll and pitch via the magnetometer fusion process. |
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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 | ||