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https://gitee.com/mirrors_PX4/PX4-Autopilot.git
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95300d5637
- refactor all EKF backend output predictor pieces into new OutputPredictor class - output states are now calculated immediately with new high rate IMU rather than after EKF update - IMU delayed sample is passed as around as control data to avoid storing an extra copy and make the requirement clear
182 lines
6.6 KiB
C++
182 lines
6.6 KiB
C++
/****************************************************************************
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*
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* Copyright (c) 2022 PX4 Development Team. All rights reserved.
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*
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* Redistribution and use in source and binary forms, with or without
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* modification, are permitted provided that the following conditions
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* are met:
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*
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* 1. Redistributions of source code must retain the above copyright
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* notice, this list of conditions and the following disclaimer.
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* 2. Redistributions in binary form must reproduce the above copyright
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* notice, this list of conditions and the following disclaimer in
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* the documentation and/or other materials provided with the
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* distribution.
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* 3. Neither the name PX4 nor the names of its contributors may be
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* used to endorse or promote products derived from this software
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* without specific prior written permission.
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*
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* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
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* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
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* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
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* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
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* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
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* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
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* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
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* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
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* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
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* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
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* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
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* POSSIBILITY OF SUCH DAMAGE.
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*
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****************************************************************************/
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/**
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* @file gnss_height_control.cpp
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* Control functions for ekf GNSS height fusion
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*/
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#include "ekf.h"
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void Ekf::controlGnssHeightFusion(const gpsSample &gps_sample)
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{
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static constexpr const char *HGT_SRC_NAME = "GNSS";
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auto &aid_src = _aid_src_gnss_hgt;
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HeightBiasEstimator &bias_est = _gps_hgt_b_est;
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bias_est.predict(_dt_ekf_avg);
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if (_gps_data_ready) {
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// relax the upper observation noise limit which prevents bad GPS perturbing the position estimate
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float noise = math::max(gps_sample.vacc, 1.5f * _params.gps_pos_noise); // use 1.5 as a typical ratio of vacc/hacc
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if (!isOnlyActiveSourceOfVerticalPositionAiding(_control_status.flags.gps_hgt)) {
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// if we are not using another source of aiding, then we are reliant on the GPS
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// observations to constrain attitude errors and must limit the observation noise value.
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if (noise > _params.pos_noaid_noise) {
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noise = _params.pos_noaid_noise;
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}
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}
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const float measurement = gps_sample.hgt - getEkfGlobalOriginAltitude();
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const float measurement_var = sq(noise);
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const float innov_gate = math::max(_params.gps_pos_innov_gate, 1.f);
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const bool measurement_valid = PX4_ISFINITE(measurement) && PX4_ISFINITE(measurement_var);
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// GNSS position, vertical position GNSS measurement has opposite sign to earth z axis
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updateVerticalPositionAidSrcStatus(gps_sample.time_us,
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-(measurement - bias_est.getBias()),
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measurement_var + bias_est.getBiasVar(),
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innov_gate,
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aid_src);
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const bool gps_checks_passing = isTimedOut(_last_gps_fail_us, (uint64_t)5e6);
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const bool gps_checks_failing = isTimedOut(_last_gps_pass_us, (uint64_t)5e6);
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// update the bias estimator before updating the main filter but after
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// using its current state to compute the vertical position innovation
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if (measurement_valid && gps_checks_passing && !gps_checks_failing) {
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bias_est.setMaxStateNoise(sqrtf(measurement_var));
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bias_est.setProcessNoiseSpectralDensity(_params.gps_hgt_bias_nsd);
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bias_est.fuseBias(measurement - (-_state.pos(2)), measurement_var + P(9, 9));
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}
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// determine if we should use height aiding
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const bool continuing_conditions_passing = (_params.gnss_ctrl & GnssCtrl::VPOS)
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&& measurement_valid
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&& _NED_origin_initialised
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&& _gps_checks_passed;
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const bool starting_conditions_passing = continuing_conditions_passing
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&& isNewestSampleRecent(_time_last_gps_buffer_push, 2 * GNSS_MAX_INTERVAL)
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&& _gps_checks_passed
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&& gps_checks_passing
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&& !gps_checks_failing;
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if (_control_status.flags.gps_hgt) {
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aid_src.fusion_enabled = true;
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if (continuing_conditions_passing) {
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fuseVerticalPosition(aid_src);
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const bool is_fusion_failing = isTimedOut(aid_src.time_last_fuse, _params.hgt_fusion_timeout_max);
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if (isHeightResetRequired()) {
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// All height sources are failing
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ECL_WARN("%s height fusion reset required, all height sources failing", HGT_SRC_NAME);
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_information_events.flags.reset_hgt_to_gps = true;
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resetVerticalPositionTo(-(measurement - bias_est.getBias()), measurement_var);
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bias_est.setBias(_state.pos(2) + measurement);
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// reset vertical velocity
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if (PX4_ISFINITE(gps_sample.vel(2)) && (_params.gnss_ctrl & GnssCtrl::VEL)) {
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// use 1.5 as a typical ratio of vacc/hacc
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resetVerticalVelocityTo(gps_sample.vel(2), sq(math::max(1.5f * gps_sample.sacc, _params.gps_vel_noise)));
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} else {
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resetVerticalVelocityToZero();
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}
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aid_src.time_last_fuse = _time_delayed_us;
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} else if (is_fusion_failing) {
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// Some other height source is still working
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ECL_WARN("stopping %s height fusion, fusion failing", HGT_SRC_NAME);
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stopGpsHgtFusion();
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}
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} else {
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ECL_WARN("stopping %s height fusion, continuing conditions failing", HGT_SRC_NAME);
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stopGpsHgtFusion();
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}
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} else {
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if (starting_conditions_passing) {
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if (_params.height_sensor_ref == HeightSensor::GNSS) {
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ECL_INFO("starting %s height fusion, resetting height", HGT_SRC_NAME);
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_height_sensor_ref = HeightSensor::GNSS;
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_information_events.flags.reset_hgt_to_gps = true;
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resetVerticalPositionTo(-measurement, measurement_var);
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bias_est.reset();
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} else {
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ECL_INFO("starting %s height fusion", HGT_SRC_NAME);
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bias_est.setBias(_state.pos(2) + measurement);
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}
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aid_src.time_last_fuse = _time_delayed_us;
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bias_est.setFusionActive();
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_control_status.flags.gps_hgt = true;
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}
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}
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} else if (_control_status.flags.gps_hgt
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&& !isNewestSampleRecent(_time_last_gps_buffer_push, 2 * GNSS_MAX_INTERVAL)) {
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// No data anymore. Stop until it comes back.
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ECL_WARN("stopping %s height fusion, no data", HGT_SRC_NAME);
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stopGpsHgtFusion();
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}
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}
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void Ekf::stopGpsHgtFusion()
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{
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if (_control_status.flags.gps_hgt) {
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if (_height_sensor_ref == HeightSensor::GNSS) {
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_height_sensor_ref = HeightSensor::UNKNOWN;
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}
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_gps_hgt_b_est.setFusionInactive();
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resetEstimatorAidStatus(_aid_src_gnss_hgt);
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_control_status.flags.gps_hgt = false;
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}
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}
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