forked from Archive/PX4-Autopilot
140 lines
4.9 KiB
C++
140 lines
4.9 KiB
C++
/****************************************************************************
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*
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* Copyright (c) 2019 Estimation and Control Library (ECL). 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 ECL 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 range_finder_checks.cpp
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* Perform checks on range finder data in order to evaluate validity.
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*
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*
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*/
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#include "ekf.h"
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// check that the range finder data is continuous
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void Ekf::updateRangeDataContinuity()
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{
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// update range data continuous flag (1Hz ie 2000 ms)
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/* Timing in micro seconds */
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/* Apply a 2.0 sec low pass filter to the time delta from the last range finder updates */
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float alpha = 0.5f * _dt_update;
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_dt_last_range_update_filt_us = _dt_last_range_update_filt_us * (1.0f - alpha) + alpha *
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(_imu_sample_delayed.time_us - _range_sample_delayed.time_us);
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_dt_last_range_update_filt_us = fminf(_dt_last_range_update_filt_us, 4e6f);
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}
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void Ekf::updateRangeDataValidity()
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{
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updateRangeDataContinuity();
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// check if out of date
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if ((_imu_sample_delayed.time_us - _range_sample_delayed.time_us) > 2 * RNG_MAX_INTERVAL) {
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_rng_hgt_valid = false;
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return;
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}
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// Don't allow faulty flag to clear unless range data is continuous
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if (!_rng_hgt_valid && !isRangeDataContinuous()) {
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return;
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}
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// Don't run the checks after this unless we have retrieved new data from the buffer
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if (!_range_data_ready) {
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return;
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}
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if (_range_sample_delayed.quality == 0) {
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_time_bad_rng_signal_quality = _imu_sample_delayed.time_us;
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_rng_hgt_valid = false;
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} else if (_imu_sample_delayed.time_us - _time_bad_rng_signal_quality > (unsigned)_params.range_signal_hysteresis_ms) {
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_rng_hgt_valid = true;
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}
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// Check if excessively tilted
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if (_R_rng_to_earth_2_2 < _params.range_cos_max_tilt) {
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_rng_hgt_valid = false;
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return;
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}
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// Check if out of range
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if ((_range_sample_delayed.rng > _rng_valid_max_val)
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|| (_range_sample_delayed.rng < _rng_valid_min_val)) {
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if (_control_status.flags.in_air) {
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_rng_hgt_valid = false;
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return;
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} else {
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// Range finders can fail to provide valid readings when resting on the ground
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// or being handled by the user, which prevents use of as a primary height sensor.
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// To work around this issue, we replace out of range data with the expected on ground value.
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_range_sample_delayed.rng = _params.rng_gnd_clearance;
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return;
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}
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}
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updateRangeDataStuck();
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_rng_hgt_valid = _rng_hgt_valid && !_control_status.flags.rng_stuck;
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}
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void Ekf::updateRangeDataStuck()
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{
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// Check for "stuck" range finder measurements when range was not valid for certain period
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// This handles a failure mode observed with some lidar sensors
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if (((_range_sample_delayed.time_us - _time_last_rng_ready) > (uint64_t)10e6) &&
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_control_status.flags.in_air) {
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// require a variance of rangefinder values to check for "stuck" measurements
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if (_rng_stuck_max_val - _rng_stuck_min_val > _params.range_stuck_threshold) {
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_time_last_rng_ready = _range_sample_delayed.time_us;
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_rng_stuck_min_val = 0.0f;
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_rng_stuck_max_val = 0.0f;
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_control_status.flags.rng_stuck = false;
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} else {
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if (_range_sample_delayed.rng > _rng_stuck_max_val) {
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_rng_stuck_max_val = _range_sample_delayed.rng;
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}
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if (_rng_stuck_min_val < 0.1f || _range_sample_delayed.rng < _rng_stuck_min_val) {
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_rng_stuck_min_val = _range_sample_delayed.rng;
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}
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_control_status.flags.rng_stuck = true;
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}
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} else {
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_time_last_rng_ready = _range_sample_delayed.time_us;
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}
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}
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