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ekf: refactor fake position control logic
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@ -54,6 +54,7 @@ px4_add_module(
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EKF/ekf_helper.cpp
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EKF/EKFGSF_yaw.cpp
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EKF/estimator_interface.cpp
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EKF/fake_pos_control.cpp
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EKF/gps_checks.cpp
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EKF/gps_control.cpp
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EKF/gps_fusion.cpp
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@ -41,6 +41,7 @@ add_library(ecl_EKF
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ekf_helper.cpp
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EKFGSF_yaw.cpp
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estimator_interface.cpp
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fake_pos_control.cpp
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gps_checks.cpp
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gps_control.cpp
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gps_fusion.cpp
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@ -1066,64 +1066,6 @@ void Ekf::controlDragFusion()
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}
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}
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void Ekf::controlFakePosFusion()
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{
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// if we aren't doing any aiding, fake position measurements at the last known position to constrain drift
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// Coincide fake measurements with baro data for efficiency with a minimum fusion rate of 5Hz
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if (!isHorizontalAidingActive()
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&& !(_control_status.flags.fuse_aspd && _control_status.flags.fuse_beta)) {
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// We now need to use a synthetic position observation to prevent unconstrained drift of the INS states.
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_using_synthetic_position = true;
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// Fuse synthetic position observations every 200msec
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if (isTimedOut(_time_last_fake_pos, (uint64_t)2e5)) {
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// Reset position and velocity states if we re-commence this aiding method
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if (isTimedOut(_time_last_fake_pos, (uint64_t)4e5)) {
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_last_known_posNE = _state.pos.xy();
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resetHorizontalPosition();
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resetVelocity();
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_fuse_hpos_as_odom = false;
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if (_time_last_fake_pos != 0) {
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_warning_events.flags.stopping_navigation = true;
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ECL_WARN("stopping navigation");
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}
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}
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_time_last_fake_pos = _time_last_imu;
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Vector3f fake_pos_obs_var;
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if (_control_status.flags.in_air && _control_status.flags.tilt_align) {
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fake_pos_obs_var(0) = fake_pos_obs_var(1) = sq(fmaxf(_params.pos_noaid_noise, _params.gps_pos_noise));
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} else if (_control_status.flags.vehicle_at_rest) {
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// Accelerate tilt fine alignment by fusing more
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// aggressively when the vehicle is at rest
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fake_pos_obs_var(0) = fake_pos_obs_var(1) = sq(0.1f);
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} else {
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fake_pos_obs_var(0) = fake_pos_obs_var(1) = sq(0.5f);
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}
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_gps_pos_innov.xy() = Vector2f(_state.pos) - _last_known_posNE;
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const Vector2f fake_pos_innov_gate(3.0f, 3.0f);
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fuseHorizontalPosition(_gps_pos_innov, fake_pos_innov_gate, fake_pos_obs_var,
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_gps_pos_innov_var, _gps_pos_test_ratio, true);
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}
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} else {
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_using_synthetic_position = false;
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}
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}
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void Ekf::controlAuxVelFusion()
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{
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bool data_ready = false;
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@ -382,8 +382,7 @@ private:
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uint64_t _time_last_flow_terrain_fuse{0}; ///< time the last fusion of optical flow measurements for terrain estimation were performed (uSec)
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uint64_t _time_last_arsp_fuse{0}; ///< time the last fusion of airspeed measurements were performed (uSec)
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uint64_t _time_last_beta_fuse{0}; ///< time the last fusion of synthetic sideslip measurements were performed (uSec)
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uint64_t _time_last_fake_pos{0}; ///< last time we faked position measurements to constrain tilt errors during operation without external aiding (uSec)
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uint64_t _time_last_fake_pos_fuse{0}; ///< last time we faked position measurements to constrain tilt errors during operation without external aiding (uSec)
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uint64_t _time_last_gps_yaw_fuse{0}; ///< time the last fusion of GPS yaw measurements were performed (uSec)
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uint64_t _time_last_gps_yaw_data{0}; ///< time the last GPS yaw measurement was available (uSec)
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uint8_t _nb_gps_yaw_reset_available{0}; ///< remaining number of resets allowed before switching to another aiding source
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@ -1009,6 +1008,11 @@ private:
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void stopFlowFusion();
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void startFakePosFusion();
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void resetFakePosFusion();
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void stopFakePosFusion();
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void fuseFakePosition();
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void setVelPosFaultStatus(const int index, const bool status);
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// reset the quaternion states and covariances to the new yaw value, preserving the roll and pitch
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125
src/modules/ekf2/EKF/fake_pos_control.cpp
Normal file
125
src/modules/ekf2/EKF/fake_pos_control.cpp
Normal file
@ -0,0 +1,125 @@
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/****************************************************************************
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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 fake_pos_control.cpp
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* Control functions for ekf fake position fusion
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*/
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#include "ekf.h"
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void Ekf::controlFakePosFusion()
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{
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// If we aren't doing any aiding, fake position measurements at the last known position to constrain drift
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// During intial tilt aligment, fake position is used to perform a "quasi-stationary" leveling of the EKF
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const bool fake_pos_data_ready = isTimedOut(_time_last_fake_pos_fuse, (uint64_t)2e5); // Fuse fake position at a limited rate
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if (fake_pos_data_ready) {
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const bool continuing_conditions_passing = !isHorizontalAidingActive();
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const bool starting_conditions_passing = continuing_conditions_passing;
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if (_using_synthetic_position) {
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if (continuing_conditions_passing) {
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fuseFakePosition();
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const bool is_fusion_failing = isTimedOut(_time_last_fake_pos_fuse, (uint64_t)4e5);
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if (is_fusion_failing) {
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resetFakePosFusion();
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}
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} else {
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stopFakePosFusion();
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}
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} else {
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if (starting_conditions_passing) {
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startFakePosFusion();
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if (_control_status.flags.tilt_align) {
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// The fake position fusion is not started for initial alignement
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_warning_events.flags.stopping_navigation = true;
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ECL_WARN("stopping navigation");
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}
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}
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}
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}
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}
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void Ekf::startFakePosFusion()
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{
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if (!_using_synthetic_position) {
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_using_synthetic_position = true;
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_fuse_hpos_as_odom = false; // TODO: needed?
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resetFakePosFusion();
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}
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}
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void Ekf::resetFakePosFusion()
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{
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_last_known_posNE = _state.pos.xy();
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resetHorizontalPosition();
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resetVelocity();
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_time_last_fake_pos_fuse = _time_last_imu;
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}
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void Ekf::stopFakePosFusion()
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{
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_using_synthetic_position = false;
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}
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void Ekf::fuseFakePosition()
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{
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Vector3f fake_pos_obs_var;
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if (_control_status.flags.in_air && _control_status.flags.tilt_align) {
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fake_pos_obs_var(0) = fake_pos_obs_var(1) = sq(fmaxf(_params.pos_noaid_noise, _params.gps_pos_noise));
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} else if (_control_status.flags.vehicle_at_rest) {
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// Accelerate tilt fine alignment by fusing more
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// aggressively when the vehicle is at rest
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fake_pos_obs_var(0) = fake_pos_obs_var(1) = sq(0.1f);
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} else {
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fake_pos_obs_var(0) = fake_pos_obs_var(1) = sq(0.5f);
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}
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_gps_pos_innov.xy() = Vector2f(_state.pos) - _last_known_posNE;
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const Vector2f fake_pos_innov_gate(3.0f, 3.0f);
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if (fuseHorizontalPosition(_gps_pos_innov, fake_pos_innov_gate, fake_pos_obs_var,
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_gps_pos_innov_var, _gps_pos_test_ratio, true)) {
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_time_last_fake_pos_fuse = _time_last_imu;
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}
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}
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@ -67,7 +67,7 @@ public:
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SensorSimulator _sensor_simulator;
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// Duration of initalization with only providing baro,mag and IMU
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const uint32_t _init_duration_s{4};
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const uint32_t _init_duration_s{5};
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protected:
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double _latitude {0.0};
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