/**************************************************************************** * * Copyright (c) 2021 PX4. All rights reserved. * * Redistribution and use in source and binary forms, with or without * modification, are permitted provided that the following conditions * are met: * * 1. Redistributions of source code must retain the above copyright * notice, this list of conditions and the following disclaimer. * 2. Redistributions in binary form must reproduce the above copyright * notice, this list of conditions and the following disclaimer in * the documentation and/or other materials provided with the * distribution. * 3. Neither the name PX4 nor the names of its contributors may be * used to endorse or promote products derived from this software * without specific prior written permission. * * THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS * "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT * LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS * FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE * COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, * INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, * BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS * OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED * AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT * LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN * ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE * POSSIBILITY OF SUCH DAMAGE. * ****************************************************************************/ /** * @file height_fusion.cpp * Function for fusing height (range, baro, GNSS alt, ...) measurements */ #include "ekf.h" void Ekf::updateBaroHgt(const baroSample &baro_sample, estimator_aid_source_1d_s &baro_hgt) { // reset flags resetEstimatorAidStatus(baro_hgt); // innovation gate size const float innov_gate = fmaxf(_params.baro_innov_gate, 1.f); // measurement variance - user parameter defined const float measurement_var = sq(fmaxf(_params.baro_noise, 0.01f)); const float measurement = baro_sample.hgt; // vertical position innovation - baro measurement has opposite sign to earth z axis baro_hgt.observation = -(measurement - _baro_b_est.getBias()); baro_hgt.observation_variance = measurement_var + _baro_b_est.getBiasVar(); baro_hgt.innovation = _state.pos(2) - baro_hgt.observation; baro_hgt.innovation_variance = P(9, 9) + baro_hgt.observation_variance; // Compensate for positive static pressure transients (negative vertical position innovations) // caused by rotor wash ground interaction by applying a temporary deadzone to baro innovations. if (_control_status.flags.gnd_effect && (_params.gnd_effect_deadzone > 0.f)) { const float deadzone_start = 0.0f; const float deadzone_end = deadzone_start + _params.gnd_effect_deadzone; if (baro_hgt.innovation < -deadzone_start) { if (baro_hgt.innovation <= -deadzone_end) { baro_hgt.innovation += deadzone_end; } else { baro_hgt.innovation = -deadzone_start; } } } setEstimatorAidStatusTestRatio(baro_hgt, innov_gate); // special case if there is bad vertical acceleration data, then don't reject measurement, // but limit innovation to prevent spikes that could destabilise the filter if (_fault_status.flags.bad_acc_vertical && baro_hgt.innovation_rejected) { const float innov_limit = innov_gate * sqrtf(baro_hgt.innovation_variance); baro_hgt.innovation = math::constrain(baro_hgt.innovation, -innov_limit, innov_limit); baro_hgt.innovation_rejected = false; } baro_hgt.fusion_enabled = _control_status.flags.baro_hgt; baro_hgt.timestamp_sample = baro_sample.time_us; // update the bias estimator before updating the main filter but after // using its current state to compute the vertical position innovation _baro_b_est.setMaxStateNoise(_params.baro_noise); _baro_b_est.setProcessNoiseSpectralDensity(_params.baro_bias_nsd); _baro_b_est.fuseBias(measurement - (-_state.pos(2)) , measurement_var + P(9, 9)); } void Ekf::fuseBaroHgt(estimator_aid_source_1d_s &baro_hgt) { if (baro_hgt.fusion_enabled && !baro_hgt.innovation_rejected && fuseVelPosHeight(baro_hgt.innovation, baro_hgt.innovation_variance, 5)) { baro_hgt.fused = true; baro_hgt.time_last_fuse = _imu_sample_delayed.time_us; } } void Ekf::updateRngHgt(estimator_aid_source_1d_s &rng_hgt) { // reset flags resetEstimatorAidStatus(rng_hgt); // measurement variance - user parameter defined const float measurement_var = fmaxf(sq(_params.range_noise) + sq(_params.range_noise_scaler * _range_sensor.getDistBottom()), 0.01f); const float measurement = math::max(_range_sensor.getDistBottom(), _params.rng_gnd_clearance); // innovation gate size const float innov_gate = fmaxf(_params.range_innov_gate, 1.f); // vertical position innovation, use range finder with tilt correction rng_hgt.observation = -(measurement - _rng_hgt_b_est.getBias()); rng_hgt.observation_variance = measurement_var + _rng_hgt_b_est.getBiasVar(); rng_hgt.innovation = _state.pos(2) - rng_hgt.observation; rng_hgt.innovation_variance = P(9, 9) + rng_hgt.observation_variance; setEstimatorAidStatusTestRatio(rng_hgt, innov_gate); // special case if there is bad vertical acceleration data, then don't reject measurement, // but limit innovation to prevent spikes that could destabilise the filter if (_fault_status.flags.bad_acc_vertical && rng_hgt.innovation_rejected) { const float innov_limit = innov_gate * sqrtf(rng_hgt.innovation_variance); rng_hgt.innovation = math::constrain(rng_hgt.innovation, -innov_limit, innov_limit); rng_hgt.innovation_rejected = false; } rng_hgt.fusion_enabled = _control_status.flags.rng_hgt; rng_hgt.timestamp_sample = _range_sensor.getSampleAddress()->time_us; // update the bias estimator before updating the main filter but after // using its current state to compute the vertical position innovation const float rng_noise = sqrtf(measurement_var); _rng_hgt_b_est.setMaxStateNoise(rng_noise); _rng_hgt_b_est.setProcessNoiseSpectralDensity(_params.rng_hgt_bias_nsd); _rng_hgt_b_est.fuseBias(measurement - (-_state.pos(2)) , measurement_var + P(9, 9)); } void Ekf::fuseRngHgt(estimator_aid_source_1d_s &rng_hgt) { if (rng_hgt.fusion_enabled && !rng_hgt.innovation_rejected && fuseVelPosHeight(rng_hgt.innovation, rng_hgt.innovation_variance, 5)) { rng_hgt.fused = true; rng_hgt.time_last_fuse = _imu_sample_delayed.time_us; } } void Ekf::fuseEvHgt() { const float measurement = _ev_sample_delayed.pos(2); const float measurement_var = fmaxf(_ev_sample_delayed.posVar(2), sq(0.01f)); const float bias = _ev_hgt_b_est.getBias(); const float bias_var = _ev_hgt_b_est.getBiasVar(); _ev_hgt_b_est.setMaxStateNoise(sqrtf(measurement_var)); _ev_hgt_b_est.setProcessNoiseSpectralDensity(_params.ev_hgt_bias_nsd); _ev_hgt_b_est.fuseBias(measurement - _state.pos(2), measurement_var + P(9, 9)); // calculate the innovation assuming the external vision observation is in local NED frame const float obs = measurement - bias; const float obs_var = measurement_var + bias_var; // innovation gate size float innov_gate = fmaxf(_params.ev_pos_innov_gate, 1.f); updateVerticalPositionAidSrcStatus(_ev_sample_delayed.time_us, obs, obs_var, innov_gate, _aid_src_ev_hgt); _aid_src_ev_hgt.fusion_enabled = _control_status.flags.ev_hgt; fuseVerticalPosition(_aid_src_ev_hgt); }