mirror of https://github.com/ArduPilot/ardupilot
AP_AHRS: fixed earth frame accel for EKF3 with significant trim
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@ -591,7 +591,7 @@ void AP_AHRS::update_EKF3(void)
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// use the primary IMU for accel earth frame
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// use the primary IMU for accel earth frame
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Vector3f accel = _ins.get_accel(primary_accel);
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Vector3f accel = _ins.get_accel(primary_accel);
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accel -= abias;
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accel -= abias;
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_accel_ef = _dcm_matrix * accel;
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_accel_ef = _dcm_matrix * get_rotation_autopilot_body_to_vehicle_body() * accel;
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nav_filter_status filt_state;
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nav_filter_status filt_state;
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EKF3.getFilterStatus(filt_state);
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EKF3.getFilterStatus(filt_state);
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