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Add landing_target_estimator for precision landing from @ndepal
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Lorenz Meier
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commit
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/****************************************************************************
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*
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* Copyright (c) 2013-2018 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 LandingTargetEstimator.cpp
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*
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* @author Nicolas de Palezieux (Sunflower Labs) <ndepal@gmail.com>
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* @author Mohammed Kabir <kabir@uasys.io>
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*
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*/
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#include <px4_config.h>
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#include <px4_defines.h>
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#include <drivers/drv_hrt.h>
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#include "LandingTargetEstimator.h"
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#define SEC2USEC 1000000.0f
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namespace landing_target_estimator
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{
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LandingTargetEstimator::LandingTargetEstimator() :
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_targetPosePub(nullptr),
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_targetInnovationsPub(nullptr),
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_paramHandle(),
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_vehicleLocalPosition_valid(false),
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_vehicleAttitude_valid(false),
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_sensorBias_valid(false),
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_new_irlockReport(false),
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_estimator_initialized(false),
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_faulty(false),
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_last_predict(0),
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_last_update(0)
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{
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_paramHandle.acc_unc = param_find("LTEST_ACC_UNC");
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_paramHandle.meas_unc = param_find("LTEST_MEAS_UNC");
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_paramHandle.pos_unc_init = param_find("LTEST_POS_UNC_IN");
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_paramHandle.vel_unc_init = param_find("LTEST_VEL_UNC_IN");
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_paramHandle.mode = param_find("LTEST_MODE");
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_paramHandle.scale_x = param_find("LTEST_SCALE_X");
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_paramHandle.scale_y = param_find("LTEST_SCALE_Y");
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// Initialize uORB topics.
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_initialize_topics();
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_check_params(true);
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}
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LandingTargetEstimator::~LandingTargetEstimator()
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{
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}
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void LandingTargetEstimator::update()
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{
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_check_params(false);
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_update_topics();
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/* predict */
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if (_estimator_initialized) {
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if (hrt_absolute_time() - _last_update > landing_target_estimator_TIMEOUT_US) {
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PX4_WARN("Timeout");
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_estimator_initialized = false;
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} else if (_vehicleLocalPosition_valid
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&& _vehicleLocalPosition.v_xy_valid) {
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float dt = (hrt_absolute_time() - _last_predict) / SEC2USEC;
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// predict target position with the help of accel data
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matrix::Vector3f a;
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if (_sensorBias_valid) {
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matrix::Quaternion<float> q_att(&_vehicleAttitude.q[0]);
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_R_att = matrix::Dcm<float>(q_att);
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a(0) = _sensorBias.accel_x;
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a(1) = _sensorBias.accel_y;
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a(2) = _sensorBias.accel_z;
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a = _R_att * a;
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} else {
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a.zero();
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}
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_kalman_filter_x.predict(dt, -a(0), _params.acc_unc);
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_kalman_filter_y.predict(dt, -a(1), _params.acc_unc);
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_last_predict = hrt_absolute_time();
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}
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}
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if (!_new_irlockReport) {
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// nothing to do
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return;
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}
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// mark this sensor measurement as consumed
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_new_irlockReport = false;
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if (!_vehicleAttitude_valid || !_vehicleLocalPosition_valid || !_vehicleLocalPosition.dist_bottom_valid) {
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// don't have the data needed for an update
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return;
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}
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if (!PX4_ISFINITE(_irlockReport.pos_y) || !PX4_ISFINITE(_irlockReport.pos_x)) {
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return;
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}
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// TODO account for sensor orientation as set by parameter
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// default orientation has camera x pointing in body y, camera y in body -x
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matrix::Vector<float, 3> sensor_ray; // ray pointing towards target in body frame
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sensor_ray(0) = -_irlockReport.pos_y * _params.scale_y; // forward
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sensor_ray(1) = _irlockReport.pos_x * _params.scale_x; // right
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sensor_ray(2) = 1.0f;
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// rotate the unit ray into the navigation frame, assume sensor frame = body frame
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matrix::Quaternion<float> q_att(&_vehicleAttitude.q[0]);
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_R_att = matrix::Dcm<float>(q_att);
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sensor_ray = _R_att * sensor_ray;
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if (fabsf(sensor_ray(2)) < 1e-6f) {
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// z component of measurement unsafe, don't use this measurement
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return;
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}
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float dist = _vehicleLocalPosition.dist_bottom;
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// scale the ray s.t. the z component has length of dist
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_rel_pos(0) = sensor_ray(0) / sensor_ray(2) * dist;
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_rel_pos(1) = sensor_ray(1) / sensor_ray(2) * dist;
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if (!_estimator_initialized) {
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PX4_INFO("Init");
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_kalman_filter_x.init(_rel_pos(0), 0, _params.pos_unc_init, _params.vel_unc_init);
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_kalman_filter_y.init(_rel_pos(1), 0, _params.pos_unc_init, _params.vel_unc_init);
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_estimator_initialized = true;
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_last_update = hrt_absolute_time();
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_last_predict = _last_update;
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} else {
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// update
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bool update_x = _kalman_filter_x.update(_rel_pos(0), _params.meas_unc * dist * dist);
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bool update_y = _kalman_filter_y.update(_rel_pos(1), _params.meas_unc * dist * dist);
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if (!update_x || !update_y) {
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if (!_faulty) {
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_faulty = true;
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PX4_WARN("Landing target measurement rejected:%s%s", update_x ? "" : " x", update_y ? "" : " y");
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}
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} else {
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_faulty = false;
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}
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if (!_faulty) {
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// only publish if both measurements were good
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_target_pose.timestamp = _irlockReport.timestamp;
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float x, xvel, y, yvel, covx, covx_v, covy, covy_v;
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_kalman_filter_x.getState(x, xvel);
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_kalman_filter_x.getCovariance(covx, covx_v);
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_kalman_filter_y.getState(y, yvel);
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_kalman_filter_y.getCovariance(covy, covy_v);
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_target_pose.is_static = (_params.mode == TargetMode::Stationary);
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_target_pose.rel_pos_valid = true;
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_target_pose.rel_vel_valid = true;
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_target_pose.x_rel = x;
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_target_pose.y_rel = y;
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_target_pose.z_rel = dist;
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_target_pose.vx_rel = xvel;
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_target_pose.vy_rel = yvel;
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_target_pose.cov_x_rel = covx;
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_target_pose.cov_y_rel = covy;
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_target_pose.cov_vx_rel = covx_v;
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_target_pose.cov_vy_rel = covy_v;
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if (_vehicleLocalPosition_valid && _vehicleLocalPosition.xy_valid) {
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_target_pose.x_abs = x + _vehicleLocalPosition.x;
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_target_pose.y_abs = y + _vehicleLocalPosition.y;
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_target_pose.z_abs = dist + _vehicleLocalPosition.z;
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_target_pose.abs_pos_valid = true;
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} else {
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_target_pose.abs_pos_valid = false;
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}
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if (_targetPosePub == nullptr) {
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_targetPosePub = orb_advertise(ORB_ID(landing_target_pose), &_target_pose);
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} else {
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orb_publish(ORB_ID(landing_target_pose), _targetPosePub, &_target_pose);
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}
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_last_update = hrt_absolute_time();
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_last_predict = _last_update;
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}
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float innov_x, innov_cov_x, innov_y, innov_cov_y;
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_kalman_filter_x.getInnovations(innov_x, innov_cov_x);
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_kalman_filter_y.getInnovations(innov_y, innov_cov_y);
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_target_innovations.timestamp = _irlockReport.timestamp;
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_target_innovations.innov_x = innov_x;
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_target_innovations.innov_cov_x = innov_cov_x;
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_target_innovations.innov_y = innov_y;
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_target_innovations.innov_cov_y = innov_cov_y;
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if (_targetInnovationsPub == nullptr) {
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_targetInnovationsPub = orb_advertise(ORB_ID(landing_target_innovations), &_target_innovations);
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} else {
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orb_publish(ORB_ID(landing_target_innovations), _targetInnovationsPub, &_target_innovations);
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}
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}
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}
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void LandingTargetEstimator::_check_params(const bool force)
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{
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bool updated;
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parameter_update_s paramUpdate;
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orb_check(_parameterSub, &updated);
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if (updated) {
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orb_copy(ORB_ID(parameter_update), _parameterSub, ¶mUpdate);
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}
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if (updated || force) {
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_update_params();
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}
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}
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void LandingTargetEstimator::_initialize_topics()
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{
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// subscribe to position, attitude, arming and velocity changes
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_vehicleLocalPositionSub = orb_subscribe(ORB_ID(vehicle_local_position));
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_attitudeSub = orb_subscribe(ORB_ID(vehicle_attitude));
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_sensorBiasSub = orb_subscribe(ORB_ID(sensor_bias));
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_irlockReportSub = orb_subscribe(ORB_ID(irlock_report));
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_parameterSub = orb_subscribe(ORB_ID(parameter_update));
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}
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void LandingTargetEstimator::_update_topics()
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{
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_vehicleLocalPosition_valid = _orb_update(ORB_ID(vehicle_local_position), _vehicleLocalPositionSub,
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&_vehicleLocalPosition);
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_vehicleAttitude_valid = _orb_update(ORB_ID(vehicle_attitude), _attitudeSub, &_vehicleAttitude);
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_sensorBias_valid = _orb_update(ORB_ID(sensor_bias), _sensorBiasSub, &_sensorBias);
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_new_irlockReport = _orb_update(ORB_ID(irlock_report), _irlockReportSub, &_irlockReport);
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}
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bool LandingTargetEstimator::_orb_update(const struct orb_metadata *meta, int handle, void *buffer)
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{
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bool newData = false;
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// check if there is new data to grab
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if (orb_check(handle, &newData) != OK) {
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return false;
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}
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if (!newData) {
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return false;
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}
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if (orb_copy(meta, handle, buffer) != OK) {
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return false;
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}
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return true;
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}
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void LandingTargetEstimator::_update_params()
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{
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param_get(_paramHandle.acc_unc, &_params.acc_unc);
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param_get(_paramHandle.meas_unc, &_params.meas_unc);
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param_get(_paramHandle.pos_unc_init, &_params.pos_unc_init);
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param_get(_paramHandle.vel_unc_init, &_params.vel_unc_init);
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int mode = 0;
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param_get(_paramHandle.mode, &mode);
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_params.mode = (TargetMode)mode;
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param_get(_paramHandle.scale_x, &_params.scale_x);
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param_get(_paramHandle.scale_y, &_params.scale_y);
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}
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} // namespace landing_target_estimator
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