forked from Archive/PX4-Autopilot
163 lines
5.1 KiB
C++
163 lines
5.1 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 vel_pos_fusion.cpp
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* Function for fusing gps and baro measurements/
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*
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* @author Roman Bast <bapstroman@gmail.com>
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*
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*/
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#include "ekf.h"
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void Ekf::fuseVelPosHeight()
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{
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bool fuse_map[6] = {};
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float innovations[6] = {};
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float R[6] = {};
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float Kfusion[24] = {};
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// calculate innovations
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if (_fuse_vel) {
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fuse_map[0] = fuse_map[1] = fuse_map[2] = true;
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innovations[0] = _state.vel(0) - _gps_sample_delayed.vel(0);
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innovations[1] = _state.vel(1) - _gps_sample_delayed.vel(1);
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innovations[2] = _state.vel(2) - _gps_sample_delayed.vel(2);
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R[0] = _params.gps_vel_noise;
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R[1] = _params.gps_vel_noise;
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R[2] = _params.gps_vel_noise;
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}
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if (_fuse_pos) {
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fuse_map[3] = fuse_map[4] = true;
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innovations[3] = _state.pos(0) - _gps_sample_delayed.pos(0);
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innovations[4] = _state.pos(1) - _gps_sample_delayed.pos(1);
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R[3] = _params.gps_pos_noise;
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R[4] = _params.gps_pos_noise;
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}
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if (_fuse_height) {
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fuse_map[5] = true;
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innovations[5] = _state.pos(2) - (-_baro_sample_delayed.hgt); // baro measurement has inversed z axis
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R[5] = _params.baro_noise;
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}
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// XXX Do checks here
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for (unsigned obs_index = 0; obs_index < 6; obs_index++) {
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if (!fuse_map[obs_index]) {
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continue;
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}
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unsigned state_index = obs_index + 3; // we start with vx and this is the 4. state
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// compute the innovation variance SK = HPH + R
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float S = P[state_index][state_index] + R[obs_index];
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S = 1.0f / S;
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// calculate kalman gain K = PHS
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for (int row = 0; row < 24; row++) {
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Kfusion[row] = P[row][state_index] * S;
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}
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// by definition the angle error state is zero at the fusion time
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_state.ang_error.setZero();
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// fuse the observation
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fuse(Kfusion, innovations[obs_index]);
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// correct the nominal quaternion
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Quaternion dq;
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dq.from_axis_angle(_state.ang_error);
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_state.quat_nominal = dq * _state.quat_nominal;
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_state.quat_nominal.normalize();
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// update covarinace matrix via Pnew = (I - KH)P
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float KHP[_k_num_states][_k_num_states] = {};
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for (unsigned row = 0; row < _k_num_states; row++) {
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for (unsigned column = 0; column < _k_num_states; column++) {
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KHP[row][column] = Kfusion[row] * P[state_index][column];
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}
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}
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for (unsigned row = 0; row < _k_num_states; row++) {
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for (unsigned column = 0; column < _k_num_states; column++) {
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P[row][column] = P[row][column] - KHP[row][column];
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}
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}
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makeSymmetrical();
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limitCov();
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}
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}
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void Ekf::fuse(float *K, float innovation)
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{
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for (unsigned i = 0; i < 3; i++) {
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_state.ang_error(i) = _state.ang_error(i) - K[i] * innovation;
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}
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for (unsigned i = 0; i < 3; i++) {
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_state.vel(i) = _state.vel(i) - K[i + 3] * innovation;
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}
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for (unsigned i = 0; i < 3; i++) {
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_state.pos(i) = _state.pos(i) - K[i + 6] * innovation;
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}
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for (unsigned i = 0; i < 3; i++) {
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_state.gyro_bias(i) = _state.gyro_bias(i) - K[i + 9] * innovation;
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}
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for (unsigned i = 0; i < 3; i++) {
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_state.gyro_scale(i) = _state.gyro_scale(i) - K[i + 12] * innovation;
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}
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_state.accel_z_bias -= K[15] * innovation;
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for (unsigned i = 0; i < 3; i++) {
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_state.mag_I(i) = _state.mag_I(i) - K[i + 16] * innovation;
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}
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for (unsigned i = 0; i < 3; i++) {
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_state.mag_B(i) = _state.mag_B(i) - K[i + 19] * innovation;
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}
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for (unsigned i = 0; i < 2; i++) {
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_state.wind_vel(i) = _state.wind_vel(i) - K[i + 22] * innovation;
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}
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}
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