mirror of https://github.com/ArduPilot/ardupilot
9b37c29efa
This removes errors in the in-flight reset of the earth field states by: 1) Using a state vector and magnetometer measurement from the same time coordinate 2) Not using the AHRS trim offsets in the calculation |
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.. | ||
Models | ||
AP_NavEKF.cpp | ||
AP_NavEKF.h | ||
AP_Nav_Common.h | ||
AP_SmallEKF.cpp | ||
AP_SmallEKF.h |