mirror of https://github.com/ArduPilot/ardupilot
8f27297896
When using GPS for yaw correction we need to apply the x and y omegaI corrections from the _omega_I_sum in the period before we get to the minimum ground speed for GPS yaw correction. Otherwise we get a large sudden omega_I change on takeoff. |
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examples | ||
AP_AHRS.h | ||
AP_AHRS_DCM.cpp | ||
AP_AHRS_DCM.h | ||
AP_AHRS_HIL.cpp | ||
AP_AHRS_HIL.h | ||
AP_AHRS_Quaternion.cpp | ||
AP_AHRS_Quaternion.h |