mirror of
https://gitee.com/mirrors_PX4/PX4-Autopilot.git
synced 2026-06-28 04:50:35 +08:00
ekf2: split horizontal and vertical origin reset
Allow partial resets (only lat/lon or only altitude)
This commit is contained in:
committed by
Mathieu Bresciani
parent
f3d58cdf10
commit
9169a7c5fc
@@ -261,6 +261,8 @@ public:
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// get the ekf WGS-84 origin position and height and the system time it was last set
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// return true if the origin is valid
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bool getEkfGlobalOrigin(uint64_t &origin_time, double &latitude, double &longitude, float &origin_alt) const;
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bool checkLatLonValidity(double latitude, double longitude, float eph = 0.f);
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bool checkAltitudeValidity(float altitude, float epv = 0.f);
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bool setEkfGlobalOrigin(double latitude, double longitude, float altitude, float eph = 0.f, float epv = 0.f);
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// get the 1-sigma horizontal and vertical position uncertainty of the ekf WGS-84 position
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@@ -765,6 +767,9 @@ private:
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P.slice<S.dof, S.dof>(S.idx, S.idx) = cov;
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}
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bool setLatLonOrigin(double latitude, double longitude, float eph = NAN);
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bool setAltOrigin(float altitude, float epv = NAN);
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// update quaternion states and covariances using an innovation, observation variance and Jacobian vector
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bool fuseYaw(estimator_aid_source1d_s &aid_src_status, const VectorState &H_YAW);
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void computeYawInnovVarAndH(float variance, float &innovation_variance, VectorState &H_YAW) const;
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@@ -72,63 +72,95 @@ bool Ekf::getEkfGlobalOrigin(uint64_t &origin_time, double &latitude, double &lo
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return _NED_origin_initialised;
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}
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bool Ekf::checkLatLonValidity(const double latitude, const double longitude, const float eph)
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{
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const bool lat_valid = (PX4_ISFINITE(latitude) && (abs(latitude) <= 90));
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const bool lon_valid = (PX4_ISFINITE(longitude) && (abs(longitude) <= 180));
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const bool eph_valid = (PX4_ISFINITE(eph) && (eph >= 0.f));
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return (lat_valid && lon_valid && eph_valid);
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}
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bool Ekf::checkAltitudeValidity(const float altitude, const float epv)
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{
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// sanity check valid altitude anywhere between the Mariana Trench and edge of Space
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const bool alt_valid = (PX4_ISFINITE(altitude) && ((altitude > -12'000.f) && (altitude < 100'000.f)));
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const bool epv_valid = (PX4_ISFINITE(epv) && (epv >= 0.f));
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return alt_valid && epv_valid;
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}
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bool Ekf::setEkfGlobalOrigin(const double latitude, const double longitude, const float altitude, const float eph,
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const float epv)
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{
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// sanity check valid latitude/longitude and altitude anywhere between the Mariana Trench and edge of Space
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if (PX4_ISFINITE(latitude) && (abs(latitude) <= 90)
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&& PX4_ISFINITE(longitude) && (abs(longitude) <= 180)
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&& PX4_ISFINITE(altitude) && (altitude > -12'000.f) && (altitude < 100'000.f)
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) {
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bool current_pos_available = false;
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double current_lat = static_cast<double>(NAN);
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double current_lon = static_cast<double>(NAN);
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// if we are already doing aiding, correct for the change in position since the EKF started navigating
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if (_pos_ref.isInitialized() && isHorizontalAidingActive()) {
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_pos_ref.reproject(_state.pos(0), _state.pos(1), current_lat, current_lon);
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current_pos_available = true;
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}
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const float gps_alt_ref_prev = _gps_alt_ref;
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// reinitialize map projection to latitude, longitude, altitude, and reset position
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_pos_ref.initReference(latitude, longitude, _time_delayed_us);
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_gps_alt_ref = altitude;
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_gpos_origin_eph = eph;
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_gpos_origin_epv = epv;
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_NED_origin_initialised = true;
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_earth_rate_NED = calcEarthRateNED(math::radians(static_cast<float>(latitude)));
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if (current_pos_available) {
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// reset horizontal position if we already have a global origin
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Vector2f position = _pos_ref.project(current_lat, current_lon);
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resetHorizontalPositionTo(position);
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}
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if (PX4_ISFINITE(gps_alt_ref_prev) && isVerticalPositionAidingActive()) {
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// determine current z
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const float z_prev = _state.pos(2);
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const float current_alt = -z_prev + gps_alt_ref_prev;
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#if defined(CONFIG_EKF2_GNSS)
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const float gps_hgt_bias = _gps_hgt_b_est.getBias();
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#endif // CONFIG_EKF2_GNSS
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resetVerticalPositionTo(_gps_alt_ref - current_alt);
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ECL_DEBUG("EKF global origin updated, resetting vertical position %.1fm -> %.1fm", (double)z_prev,
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(double)_state.pos(2));
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#if defined(CONFIG_EKF2_GNSS)
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// adjust existing GPS height bias
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_gps_hgt_b_est.setBias(gps_hgt_bias);
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#endif // CONFIG_EKF2_GNSS
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}
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return true;
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if (!setLatLonOrigin(latitude, longitude, eph)) {
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return false;
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}
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return false;
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// altitude is optional
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setAltOrigin(altitude, epv);
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return true;
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}
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bool Ekf::setLatLonOrigin(const double latitude, const double longitude, const float eph)
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{
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if (!checkLatLonValidity(latitude, longitude, eph)) {
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return false;
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}
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bool current_pos_available = false;
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double current_lat = static_cast<double>(NAN);
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double current_lon = static_cast<double>(NAN);
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// if we are already doing aiding, correct for the change in position since the EKF started navigating
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if (_pos_ref.isInitialized() && isHorizontalAidingActive()) {
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_pos_ref.reproject(_state.pos(0), _state.pos(1), current_lat, current_lon);
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current_pos_available = true;
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}
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// reinitialize map projection to latitude, longitude, altitude, and reset position
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_pos_ref.initReference(latitude, longitude, _time_delayed_us);
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_gpos_origin_eph = eph;
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_NED_origin_initialised = true;
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if (current_pos_available) {
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// reset horizontal position if we already have a global origin
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Vector2f position = _pos_ref.project(current_lat, current_lon);
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resetHorizontalPositionTo(position);
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}
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return true;
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}
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bool Ekf::setAltOrigin(const float altitude, const float epv)
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{
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if (!checkAltitudeValidity(altitude, epv)) {
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return false;
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}
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const float gps_alt_ref_prev = _gps_alt_ref;
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_gps_alt_ref = altitude;
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_gpos_origin_epv = epv;
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if (PX4_ISFINITE(gps_alt_ref_prev) && isVerticalPositionAidingActive()) {
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// determine current z
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const float z_prev = _state.pos(2);
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const float current_alt = -z_prev + gps_alt_ref_prev;
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#if defined(CONFIG_EKF2_GNSS)
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const float gps_hgt_bias = _gps_hgt_b_est.getBias();
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#endif // CONFIG_EKF2_GNSS
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resetVerticalPositionTo(_gps_alt_ref - current_alt);
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ECL_DEBUG("EKF global origin updated, resetting vertical position %.1fm -> %.1fm", (double)z_prev,
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(double)_state.pos(2));
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#if defined(CONFIG_EKF2_GNSS)
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// adjust existing GPS height bias
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_gps_hgt_b_est.setBias(gps_hgt_bias);
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#endif // CONFIG_EKF2_GNSS
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}
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return true;
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}
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void Ekf::get_ekf_gpos_accuracy(float *ekf_eph, float *ekf_epv) const
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