forked from Archive/PX4-Autopilot
219 lines
6.9 KiB
C++
219 lines
6.9 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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* @author Siddharth Bharat Purohit <siddharthbharatpurohit@gmail.com>
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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::fuseHorizontalVelocity(const Vector3f &innov, const Vector2f &innov_gate,
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const Vector3f &obs_var, Vector3f &innov_var, Vector2f &test_ratio)
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{
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innov_var(0) = P[4][4] + obs_var(0);
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innov_var(1) = P[5][5] + obs_var(1);
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test_ratio(0) = fmaxf( sq(innov(0)) / (sq(innov_gate(0)) * innov_var(0)),
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sq(innov(1)) / (sq(innov_gate(0)) * innov_var(1)));
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bool innov_check_pass = (test_ratio(0) <= 1.0f);
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if (innov_check_pass)
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{
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_time_last_hor_vel_fuse = _time_last_imu;
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_innov_check_fail_status.flags.reject_hor_vel = false;
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fuseVelPosHeight(innov(0),innov_var(0),0);
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fuseVelPosHeight(innov(1),innov_var(1),1);
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return true;
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}else{
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_innov_check_fail_status.flags.reject_hor_vel = true;
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return false;
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}
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}
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bool Ekf::fuseVerticalVelocity(const Vector3f &innov, const Vector2f &innov_gate,
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const Vector3f &obs_var, Vector3f &innov_var, Vector2f &test_ratio)
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{
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innov_var(2) = P[6][6] + obs_var(2);
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test_ratio(1) = sq(innov(2)) / (sq(innov_gate(1)) * innov_var(2));
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bool innov_check_pass = (test_ratio(1) <= 1.0f);
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if (innov_check_pass) {
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_time_last_ver_vel_fuse = _time_last_imu;
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_innov_check_fail_status.flags.reject_ver_vel = false;
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fuseVelPosHeight(innov(2),innov_var(2),2);
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return true;
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}else{
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_innov_check_fail_status.flags.reject_ver_vel = true;
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return false;
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}
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}
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bool Ekf::fuseHorizontalPosition(const Vector3f &innov, const Vector2f &innov_gate,
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const Vector3f &obs_var, Vector3f &innov_var, Vector2f &test_ratio)
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{
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innov_var(0) = P[7][7] + obs_var(0);
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innov_var(1) = P[8][8] + obs_var(1);
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test_ratio(0) = fmaxf( sq(innov(0)) / (sq(innov_gate(0)) * innov_var(0)),
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sq(innov(1)) / (sq(innov_gate(0)) * innov_var(1)));
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bool innov_check_pass = (test_ratio(0) <= 1.0f) || !_control_status.flags.tilt_align;
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if (innov_check_pass) {
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if (!_fuse_hpos_as_odom) {
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_time_last_hor_pos_fuse = _time_last_imu;
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} else {
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_time_last_delpos_fuse = _time_last_imu;
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}
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_innov_check_fail_status.flags.reject_hor_pos = false;
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fuseVelPosHeight(innov(0),innov_var(0),3);
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fuseVelPosHeight(innov(1),innov_var(1),4);
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return true;
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}else{
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_innov_check_fail_status.flags.reject_hor_pos = true;
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return false;
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}
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}
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bool Ekf::fuseVerticalPosition(const Vector3f &innov, const Vector2f &innov_gate,
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const Vector3f &obs_var, Vector3f &innov_var, Vector2f &test_ratio)
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{
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innov_var(2) = P[9][9] + obs_var(2);
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test_ratio(1) = sq(innov(2)) / (sq(innov_gate(1)) * innov_var(2));
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bool innov_check_pass = (test_ratio(1) <= 1.0f) || !_control_status.flags.tilt_align;
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if (innov_check_pass) {
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_time_last_hgt_fuse = _time_last_imu;
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_innov_check_fail_status.flags.reject_ver_pos = false;
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fuseVelPosHeight(innov(2),innov_var(2),5);
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return true;
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}else{
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_innov_check_fail_status.flags.reject_ver_pos = true;
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return false;
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}
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}
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// Helper function that fuses a single velocity or position measurement
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void Ekf::fuseVelPosHeight(const float innov, const float innov_var, const int obs_index)
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{
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float Kfusion[24] = {}; // Kalman gain vector for any single observation - sequential fusion is used.
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unsigned state_index = obs_index + 4; // we start with vx and this is the 4. state
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// calculate kalman gain K = PHS, where S = 1/innovation variance
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for (int row = 0; row < _k_num_states; row++) {
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Kfusion[row] = P[row][state_index] / innov_var;
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}
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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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// if the covariance correction will result in a negative variance, then
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// the covariance matrix is unhealthy and must be corrected
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bool healthy = true;
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for (int i = 0; i < _k_num_states; i++) {
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if (P[i][i] < KHP[i][i]) {
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// zero rows and columns
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zeroRows(P, i, i);
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zeroCols(P, i, i);
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healthy = false;
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setVelPosFaultStatus(obs_index, true);
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} else {
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setVelPosFaultStatus(obs_index, false);
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}
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}
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// only apply covariance and state corrections if healthy
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if (healthy) {
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// apply the covariance corrections
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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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// correct the covariance matrix for gross errors
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fixCovarianceErrors();
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// apply the state corrections
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fuse(Kfusion, innov);
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}
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}
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void Ekf::setVelPosFaultStatus(const int index, const bool status)
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{
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if (index == 0) {
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_fault_status.flags.bad_vel_N = status;
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} else if (index == 1) {
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_fault_status.flags.bad_vel_E = status;
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} else if (index == 2) {
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_fault_status.flags.bad_vel_D = status;
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} else if (index == 3) {
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_fault_status.flags.bad_pos_N = status;
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} else if (index == 4) {
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_fault_status.flags.bad_pos_E = status;
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} else if (index == 5) {
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_fault_status.flags.bad_pos_D = status;
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}
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}
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