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ekf2: fully disable yaw estimator EKFGSF_yaw with CONFIG_EKF2_GNSS (#22233)
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@@ -1028,56 +1028,6 @@ void Ekf::resetQuatStateYaw(float yaw, float yaw_variance)
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_time_last_heading_fuse = _time_delayed_us;
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}
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#if defined(CONFIG_EKF2_GNSS)
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bool Ekf::resetYawToEKFGSF()
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{
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if (!isYawEmergencyEstimateAvailable()) {
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return false;
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}
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// don't allow reset if there's just been a yaw reset
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const bool yaw_alignment_changed = (_control_status_prev.flags.yaw_align != _control_status.flags.yaw_align);
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const bool quat_reset = (_state_reset_status.reset_count.quat != _state_reset_count_prev.quat);
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if (yaw_alignment_changed || quat_reset) {
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return false;
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}
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ECL_INFO("yaw estimator reset heading %.3f -> %.3f rad",
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(double)getEulerYaw(_R_to_earth), (double)_yawEstimator.getYaw());
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resetQuatStateYaw(_yawEstimator.getYaw(), _yawEstimator.getYawVar());
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_control_status.flags.yaw_align = true;
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_information_events.flags.yaw_aligned_to_imu_gps = true;
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return true;
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}
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#endif // CONFIG_EKF2_GNSS
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bool Ekf::isYawEmergencyEstimateAvailable() const
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{
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#if defined(CONFIG_EKF2_GNSS)
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// don't allow reet using the EKF-GSF estimate until the filter has started fusing velocity
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// data and the yaw estimate has converged
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if (!_yawEstimator.isActive()) {
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return false;
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}
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return _yawEstimator.getYawVar() < sq(_params.EKFGSF_yaw_err_max);
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#else
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return false;
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#endif
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}
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#if defined(CONFIG_EKF2_GNSS)
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bool Ekf::getDataEKFGSF(float *yaw_composite, float *yaw_variance, float yaw[N_MODELS_EKFGSF],
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float innov_VN[N_MODELS_EKFGSF], float innov_VE[N_MODELS_EKFGSF], float weight[N_MODELS_EKFGSF])
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{
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return _yawEstimator.getLogData(yaw_composite, yaw_variance, yaw, innov_VN, innov_VE, weight);
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}
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#endif // CONFIG_EKF2_GNSS
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#if defined(CONFIG_EKF2_WIND)
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void Ekf::resetWind()
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{
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