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https://github.com/ArduPilot/ardupilot
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5058405f8c
Inhibiting gyro bias estimation during the initial tilt alignment speeds alignment. The calculation of the maxmum state index required has been modified so that it can handle all combinations of inhibited states. Limiting the maximum state index accessed by all EKF operations result in significant processing reductions when higher index states are not being used. |
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| .. | ||
| AP_NavEKF3_AirDataFusion.cpp | ||
| AP_NavEKF3_Buffer.h | ||
| AP_NavEKF3_Control.cpp | ||
| AP_NavEKF3_core.cpp | ||
| AP_NavEKF3_core.h | ||
| AP_NavEKF3_GyroBias.cpp | ||
| AP_NavEKF3_MagFusion.cpp | ||
| AP_NavEKF3_Measurements.cpp | ||
| AP_NavEKF3_OptFlowFusion.cpp | ||
| AP_NavEKF3_Outputs.cpp | ||
| AP_NavEKF3_PosVelFusion.cpp | ||
| AP_NavEKF3_RngBcnFusion.cpp | ||
| AP_NavEKF3_VehicleStatus.cpp | ||
| AP_NavEKF3.cpp | ||
| AP_NavEKF3.h | ||