forked from Archive/PX4-Autopilot
EKF: Add reporting of bad accel status
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@ -506,6 +506,7 @@ union ekf_solution_status {
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uint16_t pred_pos_horiz_rel : 1; // 8 - True if the EKF has sufficient data to enter a mode that will provide a (relative) position estimate
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uint16_t pred_pos_horiz_rel : 1; // 8 - True if the EKF has sufficient data to enter a mode that will provide a (relative) position estimate
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uint16_t pred_pos_horiz_abs : 1; // 9 - True if the EKF has sufficient data to enter a mode that will provide a (absolute) position estimate
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uint16_t pred_pos_horiz_abs : 1; // 9 - True if the EKF has sufficient data to enter a mode that will provide a (absolute) position estimate
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uint16_t gps_glitch : 1; // 10 - True if the EKF has detected a GPS glitch
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uint16_t gps_glitch : 1; // 10 - True if the EKF has detected a GPS glitch
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uint16_t accel_error : 1; // 11 - True if the EKF has detected bad accelerometer data
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} flags;
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} flags;
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uint16_t value;
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uint16_t value;
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};
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};
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@ -862,6 +862,7 @@ void Ekf::get_ekf_soln_status(uint16_t *status)
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bool gps_pos_innov_bad = (_vel_pos_test_ratio[3] > 1.0f) || (_vel_pos_test_ratio[4] > 1.0f);
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bool gps_pos_innov_bad = (_vel_pos_test_ratio[3] > 1.0f) || (_vel_pos_test_ratio[4] > 1.0f);
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bool mag_innov_good = (_mag_test_ratio[0] < 1.0f) && (_mag_test_ratio[1] < 1.0f) && (_mag_test_ratio[2] < 1.0f) && (_yaw_test_ratio < 1.0f);
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bool mag_innov_good = (_mag_test_ratio[0] < 1.0f) && (_mag_test_ratio[1] < 1.0f) && (_mag_test_ratio[2] < 1.0f) && (_yaw_test_ratio < 1.0f);
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soln_status.flags.gps_glitch = (gps_vel_innov_bad || gps_pos_innov_bad) && mag_innov_good;
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soln_status.flags.gps_glitch = (gps_vel_innov_bad || gps_pos_innov_bad) && mag_innov_good;
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soln_status.flags.accel_error = _bad_vert_accel_detected;
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*status = soln_status.value;
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*status = soln_status.value;
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}
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}
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