forked from Archive/PX4-Autopilot
226 lines
7.6 KiB
C++
226 lines
7.6 KiB
C++
/****************************************************************************
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*
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* Copyright (c) 2015 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 terrain_estimator.cpp
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* Function for fusing rangefinder measurements to estimate terrain vertical position/
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*
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* @author Paul Riseborough <p_riseborough@live.com.au>
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*
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*/
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#include "ekf.h"
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#include <ecl.h>
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#include <mathlib/mathlib.h>
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bool Ekf::initHagl()
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{
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// get most recent range measurement from buffer
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const rangeSample &latest_measurement = _range_buffer.get_newest();
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if ((_time_last_imu - latest_measurement.time_us) < (uint64_t)2e5 && _R_rng_to_earth_2_2 > _params.range_cos_max_tilt) {
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// if we have a fresh measurement, use it to initialise the terrain estimator
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_terrain_vpos = _state.pos(2) + latest_measurement.rng * _R_rng_to_earth_2_2;
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// initialise state variance to variance of measurement
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_terrain_var = sq(_params.range_noise);
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// success
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return true;
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} else if (!_control_status.flags.in_air) {
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// if on ground we assume a ground clearance
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_terrain_vpos = _state.pos(2) + _params.rng_gnd_clearance;
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// Use the ground clearance value as our uncertainty
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_terrain_var = sq(_params.rng_gnd_clearance);
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// ths is a guess
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return false;
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} else {
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// no information - cannot initialise
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return false;
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}
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}
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void Ekf::runTerrainEstimator()
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{
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// Perform a continuity check on range finder data
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checkRangeDataContinuity();
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// Perform initialisation check
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if (!_terrain_initialised) {
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_terrain_initialised = initHagl();
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} else {
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// predict the state variance growth where the state is the vertical position of the terrain underneath the vehicle
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// process noise due to errors in vehicle height estimate
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_terrain_var += sq(_imu_sample_delayed.delta_vel_dt * _params.terrain_p_noise);
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// process noise due to terrain gradient
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_terrain_var += sq(_imu_sample_delayed.delta_vel_dt * _params.terrain_gradient) * (sq(_state.vel(0)) + sq(_state.vel(
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1)));
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// limit the variance to prevent it becoming badly conditioned
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_terrain_var = math::constrain(_terrain_var, 0.0f, 1e4f);
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// Fuse range finder data if available
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if (_range_data_ready && !_control_status.flags.rng_stuck) {
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fuseHagl();
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// update range sensor angle parameters in case they have changed
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// we do this here to avoid doing those calculations at a high rate
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_sin_tilt_rng = sinf(_params.rng_sens_pitch);
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_cos_tilt_rng = cosf(_params.rng_sens_pitch);
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}
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//constrain _terrain_vpos to be a minimum of _params.rng_gnd_clearance larger than _state.pos(2)
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if (_terrain_vpos - _state.pos(2) < _params.rng_gnd_clearance) {
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_terrain_vpos = _params.rng_gnd_clearance + _state.pos(2);
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}
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}
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// Update terrain validity
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update_terrain_valid();
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}
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void Ekf::fuseHagl()
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{
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// If the vehicle is excessively tilted, do not try to fuse range finder observations
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if (_R_rng_to_earth_2_2 > _params.range_cos_max_tilt) {
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// get a height above ground measurement from the range finder assuming a flat earth
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float meas_hagl = _range_sample_delayed.rng * _R_rng_to_earth_2_2;
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// predict the hagl from the vehicle position and terrain height
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float pred_hagl = _terrain_vpos - _state.pos(2);
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// calculate the innovation
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_hagl_innov = pred_hagl - meas_hagl;
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// calculate the observation variance adding the variance of the vehicles own height uncertainty
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float obs_variance = fmaxf(P[9][9], 0.0f) + sq(_params.range_noise) + sq(_params.range_noise_scaler * _range_sample_delayed.rng);
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// calculate the innovation variance - limiting it to prevent a badly conditioned fusion
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_hagl_innov_var = fmaxf(_terrain_var + obs_variance, obs_variance);
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// perform an innovation consistency check and only fuse data if it passes
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float gate_size = fmaxf(_params.range_innov_gate, 1.0f);
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_terr_test_ratio = sq(_hagl_innov) / (sq(gate_size) * _hagl_innov_var);
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if (!_inhibit_gndobs_use) {
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if (_terr_test_ratio <= 1.0f) {
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// calculate the Kalman gain
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float gain = _terrain_var / _hagl_innov_var;
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// correct the state
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_terrain_vpos -= gain * _hagl_innov;
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// correct the variance
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_terrain_var = fmaxf(_terrain_var * (1.0f - gain), 0.0f);
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// record last successful fusion event
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_time_last_hagl_fuse = _time_last_imu;
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_innov_check_fail_status.flags.reject_hagl = false;
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} else {
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// If we have been rejecting range data for too long, reset to measurement
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if (_time_last_imu - _time_last_hagl_fuse > (uint64_t)10E6) {
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_terrain_vpos = _state.pos(2) + meas_hagl;
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_terrain_var = obs_variance;
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} else {
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_innov_check_fail_status.flags.reject_hagl = true;
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}
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}
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}
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} else {
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_innov_check_fail_status.flags.reject_hagl = true;
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return;
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}
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}
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// return true if the terrain height estimate is valid
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bool Ekf::get_terrain_valid()
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{
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return _hagl_valid;
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}
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// determine terrain validity
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void Ekf::update_terrain_valid()
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{
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if (_terrain_initialised && _range_data_continuous && !_control_status.flags.rng_stuck &&
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(_time_last_imu - _time_last_hagl_fuse < (uint64_t)5e6)) {
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_hagl_valid = true;
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} else {
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_hagl_valid = false;
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}
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}
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// get the estimated vertical position of the terrain relative to the NED origin
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void Ekf::get_terrain_vert_pos(float *ret)
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{
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memcpy(ret, &_terrain_vpos, sizeof(float));
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}
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void Ekf::get_hagl_innov(float *hagl_innov)
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{
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memcpy(hagl_innov, &_hagl_innov, sizeof(_hagl_innov));
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}
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void Ekf::get_hagl_innov_var(float *hagl_innov_var)
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{
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memcpy(hagl_innov_var, &_hagl_innov_var, sizeof(_hagl_innov_var));
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}
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// check that the range finder data is continuous
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void Ekf::checkRangeDataContinuity()
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{
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// update range data continuous flag (2Hz ie 500 ms)
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/* Timing in micro seconds */
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/* Apply a 1.0 sec low pass filter to the time delta from the last range finder updates */
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_dt_last_range_update_filt_us = _dt_last_range_update_filt_us * (1.0f - _dt_update) + _dt_update *
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(_time_last_imu - _time_last_range);
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_dt_last_range_update_filt_us = fminf(_dt_last_range_update_filt_us, 1e6f);
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if (_dt_last_range_update_filt_us < 5e5f) {
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_range_data_continuous = true;
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} else {
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_range_data_continuous = false;
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}
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}
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