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Now that we are using a consistent 50Hz minimum update rate for the covariance prediction we do not need a different initial gyro bias uncertainty for plane and copter to maintain filter stability margins. The default value of 0.1 rad/s was too high and gave excessive settling time of the filter attitude after startup. The initial attitude uncertainty has been increased to allow for some movement during startup. |
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.. | ||
Models | ||
AP_Nav_Common.h | ||
AP_NavEKF.cpp | ||
AP_NavEKF.h | ||
AP_SmallEKF.cpp | ||
AP_SmallEKF.h |