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EKF: Use fixed wing status flag in MAG_FUSE_TYPE_AUTOFW logic
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-4
@@ -165,12 +165,11 @@ void Ekf::fuseMag()
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/*
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When flying as a fixed wing aircraft, a misaligned magnetometer can cause an error in pitch/roll and accel bias estimates.
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When MAG_FUSE_TYPE_AUTOFW is selected and the vehicle is flying as a fixed wing as detected by the use of wind estimation
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and current airspeed estimates, then magnetometer fusion is only allowed to access the magnetic field states.
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When MAG_FUSE_TYPE_AUTOFW is selected and the vehicle is flying as a fixed wing, then magnetometer fusion is only allowed
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to access the magnetic field states.
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*/
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_control_status.flags.update_mag_states_only = (_params.mag_fusion_type == MAG_FUSE_TYPE_AUTOFW)
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&& _control_status.flags.wind
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&& (_time_last_imu - _time_last_airspeed < 1E7);
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&& _control_status.flags.fixed_wing;
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// update the states and covariance using sequential fusion of the magnetometer components
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for (uint8_t index = 0; index <= 2; index++) {
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