forked from Archive/PX4-Autopilot
Merge pull request #92 from priseborough/pr-ekf2HgtResetFix
EKF: Fix vulnerability in height reset
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commit
64e95910c4
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@ -184,9 +184,7 @@ void Ekf::controlFusionModes()
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_control_status.flags.rng_hgt = false;
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// adjust the height offset so we can use the GPS
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_hgt_sensor_offset = _state.pos(2) + gps_init.hgt - _gps_alt_ref;
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if (!baro_hgt_available) {
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printf("EKF baro hgt timeout - switching to gps\n");
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}
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printf("EKF baro hgt timeout - switching to gps\n");
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}
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}
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@ -87,11 +87,15 @@ bool Ekf::resetPosition()
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// Reset height state using the last height measurement
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void Ekf::resetHeight()
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{
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// Get the most recent GPS data
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gpsSample gps_newest = _gps_buffer.get_newest();
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if (_control_status.flags.rng_hgt) {
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rangeSample range_newest = _range_buffer.get_newest();
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if (_time_last_imu - range_newest.time_us < 2 * RNG_MAX_INTERVAL) {
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_state.pos(2) = _hgt_sensor_offset - range_newest.rng;
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P[8][8] = sq(_params.range_noise);
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} else {
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// TODO: reset to last known range based estimate
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@ -107,6 +111,7 @@ void Ekf::resetHeight()
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if (_time_last_imu - baro_newest.time_us < 2 * BARO_MAX_INTERVAL) {
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_state.pos(2) = _hgt_sensor_offset - baro_newest.hgt + _baro_hgt_offset;
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P[8][8] = sq(_params.baro_noise);
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} else {
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// TODO: reset to last known baro based estimate
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@ -114,11 +119,9 @@ void Ekf::resetHeight()
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} else if (_control_status.flags.gps_hgt) {
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// initialize vertical position and velocity with newest gps measurement
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gpsSample gps_newest = _gps_buffer.get_newest();
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if (_time_last_imu - gps_newest.time_us < 2 * GPS_MAX_INTERVAL) {
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_state.pos(2) = _hgt_sensor_offset - gps_newest.hgt + _gps_alt_ref;
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_state.vel(2) = gps_newest.vel(2);
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P[8][8] = sq(gps_newest.hacc);
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} else {
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// TODO: reset to last known gps based estimate
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@ -129,6 +132,15 @@ void Ekf::resetHeight()
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_baro_hgt_offset = baro_newest.hgt + _state.pos(2);
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}
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// If we are using GPS, then use it to reset the vertical velocity
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if (_control_status.flags.gps && (_time_last_imu - gps_newest.time_us < 2 * GPS_MAX_INTERVAL)) {
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_state.vel(2) = gps_newest.vel(2);
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P[5][5] = sq(1.5f * gps_newest.sacc);
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} else {
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P[5][5] = fminf(sq(_state.vel(2)),1000.0f);
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_state.vel(2) = 0.0f;
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}
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}
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// Reset heading and magnetic field states
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