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310 lines
30 KiB
310 lines
30 KiB
/**************************************************************************** |
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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 drag_fusion.cpp |
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* body frame drag fusion methods used for multi-rotor wind estimation. |
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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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void Ekf::fuseDrag() |
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{ |
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float SH_ACC[4] = {}; // Variable used to optimise calculations of measurement jacobian |
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float H_ACC[24] = {}; // Observation Jacobian |
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float SK_ACC[9] = {}; // Variable used to optimise calculations of the Kalman gain vector |
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float Kfusion[24] = {}; // Kalman gain vector |
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// TODO: resolve variance vs stdDev bug |
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const float R_ACC = _params.drag_noise; // observation noise variance in specific force drag (m/sec**2)**2 |
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const float rho = fmaxf(_air_density, 0.1f); // air density (kg/m**3) |
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// calculate inverse of ballistic coefficient |
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if (_params.bcoef_x < 1.0f || _params.bcoef_y < 1.0f) { |
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return; |
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} |
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const float BC_inv_x = 1.0f / _params.bcoef_x; |
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const float BC_inv_y = 1.0f / _params.bcoef_y; |
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// get latest estimated orientation |
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const float q0 = _state.quat_nominal(0); |
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const float q1 = _state.quat_nominal(1); |
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const float q2 = _state.quat_nominal(2); |
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const float q3 = _state.quat_nominal(3); |
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// get latest velocity in earth frame |
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const float vn = _state.vel(0); |
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const float ve = _state.vel(1); |
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const float vd = _state.vel(2); |
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// get latest wind velocity in earth frame |
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const float vwn = _state.wind_vel(0); |
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const float vwe = _state.wind_vel(1); |
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// predicted specific forces |
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// calculate relative wind velocity in earth frame and rotate into body frame |
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const Vector3f rel_wind_earth(vn - vwn, ve - vwe, vd); |
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const Dcmf earth_to_body = quatToInverseRotMat(_state.quat_nominal); |
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const Vector3f rel_wind_body = earth_to_body * rel_wind_earth; |
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// perform sequential fusion of XY specific forces |
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for (uint8_t axis_index = 0; axis_index < 2; axis_index++) { |
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// calculate observation jacobiam and Kalman gain vectors |
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if (axis_index == 0) { |
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// Estimate the airspeed from the measured drag force and ballistic coefficient |
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const float mea_acc = _drag_sample_delayed.accelXY(axis_index) - _state.delta_vel_bias(axis_index) / _dt_ekf_avg; |
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const float airSpd = sqrtf((2.0f * fabsf(mea_acc)) / (BC_inv_x * rho)); |
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// Estimate the derivative of specific force wrt airspeed along the X axis |
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// Limit lower value to prevent arithmetic exceptions |
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const float Kacc = fmaxf(1e-1f, rho * BC_inv_x * airSpd); |
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SH_ACC[0] = sq(q0) + sq(q1) - sq(q2) - sq(q3); |
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SH_ACC[1] = vn - vwn; |
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SH_ACC[2] = ve - vwe; |
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SH_ACC[3] = 2.0f*q0*q3 + 2.0f*q1*q2; |
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H_ACC[0] = -Kacc*(2.0f*q0*SH_ACC[1] + 2.0f*q3*SH_ACC[2] - 2.0f*q2*vd); |
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H_ACC[1] = -Kacc*(2.0f*q1*SH_ACC[1] + 2.0f*q2*SH_ACC[2] + 2.0f*q3*vd); |
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H_ACC[2] = Kacc*(2.0f*q2*SH_ACC[1] - 2.0f*q1*SH_ACC[2] + 2.0f*q0*vd); |
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H_ACC[3] = -Kacc*(2.0f*q0*SH_ACC[2] - 2.0f*q3*SH_ACC[1] + 2.0f*q1*vd); |
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H_ACC[4] = -Kacc*SH_ACC[0]; |
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H_ACC[5] = -Kacc*SH_ACC[3]; |
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H_ACC[6] = Kacc*(2.0f*q0*q2 - 2.0f*q1*q3); |
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H_ACC[22] = Kacc*SH_ACC[0]; |
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H_ACC[23] = Kacc*SH_ACC[3]; |
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_drag_innov_var[0] = (R_ACC + Kacc*SH_ACC[0]*(Kacc*P(4,4)*SH_ACC[0] + Kacc*P(5,4)*SH_ACC[3] - Kacc*P(22,4)*SH_ACC[0] - Kacc*P(23,4)*SH_ACC[3] - Kacc*P(6,4)*(2.0f*q0*q2 - 2.0f*q1*q3) + Kacc*P(0,4)*(2.0f*q0*SH_ACC[1] + 2.0f*q3*SH_ACC[2] - 2.0f*q2*vd) + Kacc*P(1,4)*(2.0f*q1*SH_ACC[1] + 2.0f*q2*SH_ACC[2] + 2.0f*q3*vd) - Kacc*P(2,4)*(2.0f*q2*SH_ACC[1] - 2.0f*q1*SH_ACC[2] + 2.0f*q0*vd) + Kacc*P(3,4)*(2.0f*q0*SH_ACC[2] - 2.0f*q3*SH_ACC[1] + 2.0f*q1*vd)) + Kacc*SH_ACC[3]*(Kacc*P(4,5)*SH_ACC[0] + Kacc*P(5,5)*SH_ACC[3] - Kacc*P(22,5)*SH_ACC[0] - Kacc*P(23,5)*SH_ACC[3] - Kacc*P(6,5)*(2.0f*q0*q2 - 2.0f*q1*q3) + Kacc*P(0,5)*(2.0f*q0*SH_ACC[1] + 2.0f*q3*SH_ACC[2] - 2.0f*q2*vd) + Kacc*P(1,5)*(2.0f*q1*SH_ACC[1] + 2.0f*q2*SH_ACC[2] + 2.0f*q3*vd) - Kacc*P(2,5)*(2.0f*q2*SH_ACC[1] - 2.0f*q1*SH_ACC[2] + 2.0f*q0*vd) + Kacc*P(3,5)*(2.0f*q0*SH_ACC[2] - 2.0f*q3*SH_ACC[1] + 2.0f*q1*vd)) - Kacc*SH_ACC[0]*(Kacc*P(4,22)*SH_ACC[0] + Kacc*P(5,22)*SH_ACC[3] - Kacc*P(22,22)*SH_ACC[0] - Kacc*P(23,22)*SH_ACC[3] - Kacc*P(6,22)*(2.0f*q0*q2 - 2.0f*q1*q3) + Kacc*P(0,22)*(2.0f*q0*SH_ACC[1] + 2.0f*q3*SH_ACC[2] - 2.0f*q2*vd) + Kacc*P(1,22)*(2.0f*q1*SH_ACC[1] + 2.0f*q2*SH_ACC[2] + 2.0f*q3*vd) - Kacc*P(2,22)*(2.0f*q2*SH_ACC[1] - 2.0f*q1*SH_ACC[2] + 2.0f*q0*vd) + Kacc*P(3,22)*(2.0f*q0*SH_ACC[2] - 2.0f*q3*SH_ACC[1] + 2.0f*q1*vd)) - Kacc*SH_ACC[3]*(Kacc*P(4,23)*SH_ACC[0] + Kacc*P(5,23)*SH_ACC[3] - Kacc*P(22,23)*SH_ACC[0] - Kacc*P(23,23)*SH_ACC[3] - Kacc*P(6,23)*(2.0f*q0*q2 - 2.0f*q1*q3) + Kacc*P(0,23)*(2.0f*q0*SH_ACC[1] + 2.0f*q3*SH_ACC[2] - 2.0f*q2*vd) + Kacc*P(1,23)*(2.0f*q1*SH_ACC[1] + 2.0f*q2*SH_ACC[2] + 2.0f*q3*vd) - Kacc*P(2,23)*(2.0f*q2*SH_ACC[1] - 2.0f*q1*SH_ACC[2] + 2.0f*q0*vd) + Kacc*P(3,23)*(2.0f*q0*SH_ACC[2] - 2.0f*q3*SH_ACC[1] + 2.0f*q1*vd)) - Kacc*(2.0f*q0*q2 - 2.0f*q1*q3)*(Kacc*P(4,6)*SH_ACC[0] + Kacc*P(5,6)*SH_ACC[3] - Kacc*P(22,6)*SH_ACC[0] - Kacc*P(23,6)*SH_ACC[3] - Kacc*P(6,6)*(2.0f*q0*q2 - 2.0f*q1*q3) + Kacc*P(0,6)*(2.0f*q0*SH_ACC[1] + 2.0f*q3*SH_ACC[2] - 2.0f*q2*vd) + Kacc*P(1,6)*(2.0f*q1*SH_ACC[1] + 2.0f*q2*SH_ACC[2] + 2.0f*q3*vd) - Kacc*P(2,6)*(2.0f*q2*SH_ACC[1] - 2.0f*q1*SH_ACC[2] + 2.0f*q0*vd) + Kacc*P(3,6)*(2.0f*q0*SH_ACC[2] - 2.0f*q3*SH_ACC[1] + 2.0f*q1*vd)) + Kacc*(2.0f*q0*SH_ACC[1] + 2.0f*q3*SH_ACC[2] - 2.0f*q2*vd)*(Kacc*P(4,0)*SH_ACC[0] + Kacc*P(5,0)*SH_ACC[3] - Kacc*P(22,0)*SH_ACC[0] - Kacc*P(23,0)*SH_ACC[3] - Kacc*P(6,0)*(2.0f*q0*q2 - 2.0f*q1*q3) + Kacc*P(0,0)*(2.0f*q0*SH_ACC[1] + 2.0f*q3*SH_ACC[2] - 2.0f*q2*vd) + Kacc*P(1,0)*(2.0f*q1*SH_ACC[1] + 2.0f*q2*SH_ACC[2] + 2.0f*q3*vd) - Kacc*P(2,0)*(2.0f*q2*SH_ACC[1] - 2.0f*q1*SH_ACC[2] + 2.0f*q0*vd) + Kacc*P(3,0)*(2.0f*q0*SH_ACC[2] - 2.0f*q3*SH_ACC[1] + 2.0f*q1*vd)) + Kacc*(2.0f*q1*SH_ACC[1] + 2.0f*q2*SH_ACC[2] + 2.0f*q3*vd)*(Kacc*P(4,1)*SH_ACC[0] + Kacc*P(5,1)*SH_ACC[3] - Kacc*P(22,1)*SH_ACC[0] - Kacc*P(23,1)*SH_ACC[3] - Kacc*P(6,1)*(2.0f*q0*q2 - 2.0f*q1*q3) + Kacc*P(0,1)*(2.0f*q0*SH_ACC[1] + 2.0f*q3*SH_ACC[2] - 2.0f*q2*vd) + Kacc*P(1,1)*(2.0f*q1*SH_ACC[1] + 2.0f*q2*SH_ACC[2] + 2.0f*q3*vd) - Kacc*P(2,1)*(2.0f*q2*SH_ACC[1] - 2.0f*q1*SH_ACC[2] + 2.0f*q0*vd) + Kacc*P(3,1)*(2.0f*q0*SH_ACC[2] - 2.0f*q3*SH_ACC[1] + 2.0f*q1*vd)) - Kacc*(2.0f*q2*SH_ACC[1] - 2.0f*q1*SH_ACC[2] + 2.0f*q0*vd)*(Kacc*P(4,2)*SH_ACC[0] + Kacc*P(5,2)*SH_ACC[3] - Kacc*P(22,2)*SH_ACC[0] - Kacc*P(23,2)*SH_ACC[3] - Kacc*P(6,2)*(2.0f*q0*q2 - 2.0f*q1*q3) + Kacc*P(0,2)*(2.0f*q0*SH_ACC[1] + 2.0f*q3*SH_ACC[2] - 2.0f*q2*vd) + Kacc*P(1,2)*(2.0f*q1*SH_ACC[1] + 2.0f*q2*SH_ACC[2] + 2.0f*q3*vd) - Kacc*P(2,2)*(2.0f*q2*SH_ACC[1] - 2.0f*q1*SH_ACC[2] + 2.0f*q0*vd) + Kacc*P(3,2)*(2.0f*q0*SH_ACC[2] - 2.0f*q3*SH_ACC[1] + 2.0f*q1*vd)) + Kacc*(2.0f*q0*SH_ACC[2] - 2.0f*q3*SH_ACC[1] + 2.0f*q1*vd)*(Kacc*P(4,3)*SH_ACC[0] + Kacc*P(5,3)*SH_ACC[3] - Kacc*P(22,3)*SH_ACC[0] - Kacc*P(23,3)*SH_ACC[3] - Kacc*P(6,3)*(2.0f*q0*q2 - 2.0f*q1*q3) + Kacc*P(0,3)*(2.0f*q0*SH_ACC[1] + 2.0f*q3*SH_ACC[2] - 2.0f*q2*vd) + Kacc*P(1,3)*(2.0f*q1*SH_ACC[1] + 2.0f*q2*SH_ACC[2] + 2.0f*q3*vd) - Kacc*P(2,3)*(2.0f*q2*SH_ACC[1] - 2.0f*q1*SH_ACC[2] + 2.0f*q0*vd) + Kacc*P(3,3)*(2.0f*q0*SH_ACC[2] - 2.0f*q3*SH_ACC[1] + 2.0f*q1*vd))); |
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if (_drag_innov_var[0] < R_ACC) { |
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return; |
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} |
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SK_ACC[0] = 1.0f/_drag_innov_var[0]; |
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SK_ACC[1] = 2.0f*q0*SH_ACC[2] - 2.0f*q3*SH_ACC[1] + 2.0f*q1*vd; |
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SK_ACC[2] = 2.0f*q2*SH_ACC[1] - 2.0f*q1*SH_ACC[2] + 2.0f*q0*vd; |
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SK_ACC[3] = 2.0f*q0*SH_ACC[1] + 2.0f*q3*SH_ACC[2] - 2.0f*q2*vd; |
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SK_ACC[4] = 2.0f*q1*SH_ACC[1] + 2.0f*q2*SH_ACC[2] + 2.0f*q3*vd; |
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SK_ACC[5] = 2.0f*q0*q2 - 2.0f*q1*q3; |
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SK_ACC[6] = SH_ACC[3]; |
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// Don't allow modification of any states other than wind velocity at this stage of development - we only need a wind estimate. |
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// Kfusion[0] = -SK_ACC[0]*(Kacc*P(0,4)*SH_ACC[0] - Kacc*P(0,22)*SH_ACC[0] + Kacc*P(0,0)*SK_ACC[3] - Kacc*P(0,2)*SK_ACC[2] + Kacc*P(0,3)*SK_ACC[1] + Kacc*P(0,1)*SK_ACC[4] + Kacc*P(0,5)*SK_ACC[6] - Kacc*P(0,6)*SK_ACC[5] - Kacc*P(0,23)*SK_ACC[6]); |
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// Kfusion[1] = -SK_ACC[0]*(Kacc*P(1,4)*SH_ACC[0] - Kacc*P(1,22)*SH_ACC[0] + Kacc*P(1,0)*SK_ACC[3] - Kacc*P(1,2)*SK_ACC[2] + Kacc*P(1,3)*SK_ACC[1] + Kacc*P(1,1)*SK_ACC[4] + Kacc*P(1,5)*SK_ACC[6] - Kacc*P(1,6)*SK_ACC[5] - Kacc*P(1,23)*SK_ACC[6]); |
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// Kfusion[2] = -SK_ACC[0]*(Kacc*P(2,4)*SH_ACC[0] - Kacc*P(2,22)*SH_ACC[0] + Kacc*P(2,0)*SK_ACC[3] - Kacc*P(2,2)*SK_ACC[2] + Kacc*P(2,3)*SK_ACC[1] + Kacc*P(2,1)*SK_ACC[4] + Kacc*P(2,5)*SK_ACC[6] - Kacc*P(2,6)*SK_ACC[5] - Kacc*P(2,23)*SK_ACC[6]); |
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// Kfusion[3] = -SK_ACC[0]*(Kacc*P(3,4)*SH_ACC[0] - Kacc*P(3,22)*SH_ACC[0] + Kacc*P(3,0)*SK_ACC[3] - Kacc*P(3,2)*SK_ACC[2] + Kacc*P(3,3)*SK_ACC[1] + Kacc*P(3,1)*SK_ACC[4] + Kacc*P(3,5)*SK_ACC[6] - Kacc*P(3,6)*SK_ACC[5] - Kacc*P(3,23)*SK_ACC[6]); |
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// Kfusion[4] = -SK_ACC[0]*(Kacc*P(4,4)*SH_ACC[0] - Kacc*P(4,22)*SH_ACC[0] + Kacc*P(4,0)*SK_ACC[3] - Kacc*P(4,2)*SK_ACC[2] + Kacc*P(4,3)*SK_ACC[1] + Kacc*P(4,1)*SK_ACC[4] + Kacc*P(4,5)*SK_ACC[6] - Kacc*P(4,6)*SK_ACC[5] - Kacc*P(4,23)*SK_ACC[6]); |
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// Kfusion[5] = -SK_ACC[0]*(Kacc*P(5,4)*SH_ACC[0] - Kacc*P(5,22)*SH_ACC[0] + Kacc*P(5,0)*SK_ACC[3] - Kacc*P(5,2)*SK_ACC[2] + Kacc*P(5,3)*SK_ACC[1] + Kacc*P(5,1)*SK_ACC[4] + Kacc*P(5,5)*SK_ACC[6] - Kacc*P(5,6)*SK_ACC[5] - Kacc*P(5,23)*SK_ACC[6]); |
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// Kfusion[6] = -SK_ACC[0]*(Kacc*P(6,4)*SH_ACC[0] - Kacc*P(6,22)*SH_ACC[0] + Kacc*P(6,0)*SK_ACC[3] - Kacc*P(6,2)*SK_ACC[2] + Kacc*P(6,3)*SK_ACC[1] + Kacc*P(6,1)*SK_ACC[4] + Kacc*P(6,5)*SK_ACC[6] - Kacc*P(6,6)*SK_ACC[5] - Kacc*P(6,23)*SK_ACC[6]); |
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// Kfusion[7] = -SK_ACC[0]*(Kacc*P(7,4)*SH_ACC[0] - Kacc*P(7,22)*SH_ACC[0] + Kacc*P(7,0)*SK_ACC[3] - Kacc*P(7,2)*SK_ACC[2] + Kacc*P(7,3)*SK_ACC[1] + Kacc*P(7,1)*SK_ACC[4] + Kacc*P(7,5)*SK_ACC[6] - Kacc*P(7,6)*SK_ACC[5] - Kacc*P(7,23)*SK_ACC[6]); |
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// Kfusion[8] = -SK_ACC[0]*(Kacc*P(8,4)*SH_ACC[0] - Kacc*P(8,22)*SH_ACC[0] + Kacc*P(8,0)*SK_ACC[3] - Kacc*P(8,2)*SK_ACC[2] + Kacc*P(8,3)*SK_ACC[1] + Kacc*P(8,1)*SK_ACC[4] + Kacc*P(8,5)*SK_ACC[6] - Kacc*P(8,6)*SK_ACC[5] - Kacc*P(8,23)*SK_ACC[6]); |
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// Kfusion[9] = -SK_ACC[0]*(Kacc*P(9,4)*SH_ACC[0] - Kacc*P(9,22)*SH_ACC[0] + Kacc*P(9,0)*SK_ACC[3] - Kacc*P(9,2)*SK_ACC[2] + Kacc*P(9,3)*SK_ACC[1] + Kacc*P(9,1)*SK_ACC[4] + Kacc*P(9,5)*SK_ACC[6] - Kacc*P(9,6)*SK_ACC[5] - Kacc*P(9,23)*SK_ACC[6]); |
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// Kfusion[10] = -SK_ACC[0]*(Kacc*P(10,4)*SH_ACC[0] - Kacc*P(10,22)*SH_ACC[0] + Kacc*P(10,0)*SK_ACC[3] - Kacc*P(10,2)*SK_ACC[2] + Kacc*P(10,3)*SK_ACC[1] + Kacc*P(10,1)*SK_ACC[4] + Kacc*P(10,5)*SK_ACC[6] - Kacc*P(10,6)*SK_ACC[5] - Kacc*P(10,23)*SK_ACC[6]); |
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// Kfusion[11] = -SK_ACC[0]*(Kacc*P(11,4)*SH_ACC[0] - Kacc*P(11,22)*SH_ACC[0] + Kacc*P(11,0)*SK_ACC[3] - Kacc*P(11,2)*SK_ACC[2] + Kacc*P(11,3)*SK_ACC[1] + Kacc*P(11,1)*SK_ACC[4] + Kacc*P(11,5)*SK_ACC[6] - Kacc*P(11,6)*SK_ACC[5] - Kacc*P(11,23)*SK_ACC[6]); |
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// Kfusion[12] = -SK_ACC[0]*(Kacc*P(12,4)*SH_ACC[0] - Kacc*P(12,22)*SH_ACC[0] + Kacc*P(12,0)*SK_ACC[3] - Kacc*P(12,2)*SK_ACC[2] + Kacc*P(12,3)*SK_ACC[1] + Kacc*P(12,1)*SK_ACC[4] + Kacc*P(12,5)*SK_ACC[6] - Kacc*P(12,6)*SK_ACC[5] - Kacc*P(12,23)*SK_ACC[6]); |
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// Kfusion[13] = -SK_ACC[0]*(Kacc*P(13,4)*SH_ACC[0] - Kacc*P(13,22)*SH_ACC[0] + Kacc*P(13,0)*SK_ACC[3] - Kacc*P(13,2)*SK_ACC[2] + Kacc*P(13,3)*SK_ACC[1] + Kacc*P(13,1)*SK_ACC[4] + Kacc*P(13,5)*SK_ACC[6] - Kacc*P(13,6)*SK_ACC[5] - Kacc*P(13,23)*SK_ACC[6]); |
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// Kfusion[14] = -SK_ACC[0]*(Kacc*P(14,4)*SH_ACC[0] - Kacc*P(14,22)*SH_ACC[0] + Kacc*P(14,0)*SK_ACC[3] - Kacc*P(14,2)*SK_ACC[2] + Kacc*P(14,3)*SK_ACC[1] + Kacc*P(14,1)*SK_ACC[4] + Kacc*P(14,5)*SK_ACC[6] - Kacc*P(14,6)*SK_ACC[5] - Kacc*P(14,23)*SK_ACC[6]); |
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// Kfusion[15] = -SK_ACC[0]*(Kacc*P(15,4)*SH_ACC[0] - Kacc*P(15,22)*SH_ACC[0] + Kacc*P(15,0)*SK_ACC[3] - Kacc*P(15,2)*SK_ACC[2] + Kacc*P(15,3)*SK_ACC[1] + Kacc*P(15,1)*SK_ACC[4] + Kacc*P(15,5)*SK_ACC[6] - Kacc*P(15,6)*SK_ACC[5] - Kacc*P(15,23)*SK_ACC[6]); |
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// Kfusion[16] = -SK_ACC[0]*(Kacc*P(16,4)*SH_ACC[0] - Kacc*P(16,22)*SH_ACC[0] + Kacc*P(16,0)*SK_ACC[3] - Kacc*P(16,2)*SK_ACC[2] + Kacc*P(16,3)*SK_ACC[1] + Kacc*P(16,1)*SK_ACC[4] + Kacc*P(16,5)*SK_ACC[6] - Kacc*P(16,6)*SK_ACC[5] - Kacc*P(16,23)*SK_ACC[6]); |
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// Kfusion[17] = -SK_ACC[0]*(Kacc*P(17,4)*SH_ACC[0] - Kacc*P(17,22)*SH_ACC[0] + Kacc*P(17,0)*SK_ACC[3] - Kacc*P(17,2)*SK_ACC[2] + Kacc*P(17,3)*SK_ACC[1] + Kacc*P(17,1)*SK_ACC[4] + Kacc*P(17,5)*SK_ACC[6] - Kacc*P(17,6)*SK_ACC[5] - Kacc*P(17,23)*SK_ACC[6]); |
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// Kfusion[18] = -SK_ACC[0]*(Kacc*P(18,4)*SH_ACC[0] - Kacc*P(18,22)*SH_ACC[0] + Kacc*P(18,0)*SK_ACC[3] - Kacc*P(18,2)*SK_ACC[2] + Kacc*P(18,3)*SK_ACC[1] + Kacc*P(18,1)*SK_ACC[4] + Kacc*P(18,5)*SK_ACC[6] - Kacc*P(18,6)*SK_ACC[5] - Kacc*P(18,23)*SK_ACC[6]); |
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// Kfusion[19] = -SK_ACC[0]*(Kacc*P(19,4)*SH_ACC[0] - Kacc*P(19,22)*SH_ACC[0] + Kacc*P(19,0)*SK_ACC[3] - Kacc*P(19,2)*SK_ACC[2] + Kacc*P(19,3)*SK_ACC[1] + Kacc*P(19,1)*SK_ACC[4] + Kacc*P(19,5)*SK_ACC[6] - Kacc*P(19,6)*SK_ACC[5] - Kacc*P(19,23)*SK_ACC[6]); |
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// Kfusion[20] = -SK_ACC[0]*(Kacc*P(20,4)*SH_ACC[0] - Kacc*P(20,22)*SH_ACC[0] + Kacc*P(20,0)*SK_ACC[3] - Kacc*P(20,2)*SK_ACC[2] + Kacc*P(20,3)*SK_ACC[1] + Kacc*P(20,1)*SK_ACC[4] + Kacc*P(20,5)*SK_ACC[6] - Kacc*P(20,6)*SK_ACC[5] - Kacc*P(20,23)*SK_ACC[6]); |
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// Kfusion[21] = -SK_ACC[0]*(Kacc*P(21,4)*SH_ACC[0] - Kacc*P(21,22)*SH_ACC[0] + Kacc*P(21,0)*SK_ACC[3] - Kacc*P(21,2)*SK_ACC[2] + Kacc*P(21,3)*SK_ACC[1] + Kacc*P(21,1)*SK_ACC[4] + Kacc*P(21,5)*SK_ACC[6] - Kacc*P(21,6)*SK_ACC[5] - Kacc*P(21,23)*SK_ACC[6]); |
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Kfusion[22] = -SK_ACC[0]*(Kacc*P(22,4)*SH_ACC[0] - Kacc*P(22,22)*SH_ACC[0] + Kacc*P(22,0)*SK_ACC[3] - Kacc*P(22,2)*SK_ACC[2] + Kacc*P(22,3)*SK_ACC[1] + Kacc*P(22,1)*SK_ACC[4] + Kacc*P(22,5)*SK_ACC[6] - Kacc*P(22,6)*SK_ACC[5] - Kacc*P(22,23)*SK_ACC[6]); |
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Kfusion[23] = -SK_ACC[0]*(Kacc*P(23,4)*SH_ACC[0] - Kacc*P(23,22)*SH_ACC[0] + Kacc*P(23,0)*SK_ACC[3] - Kacc*P(23,2)*SK_ACC[2] + Kacc*P(23,3)*SK_ACC[1] + Kacc*P(23,1)*SK_ACC[4] + Kacc*P(23,5)*SK_ACC[6] - Kacc*P(23,6)*SK_ACC[5] - Kacc*P(23,23)*SK_ACC[6]); |
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// calculate the predicted acceleration and innovation measured along the X body axis |
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float drag_sign; |
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if (rel_wind_body(axis_index) >= 0.0f) { |
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drag_sign = 1.0f; |
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} else { |
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drag_sign = -1.0f; |
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} |
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const float predAccel = -BC_inv_x * 0.5f * rho * sq(rel_wind_body(axis_index)) * drag_sign; |
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_drag_innov[axis_index] = predAccel - mea_acc; |
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_drag_test_ratio[axis_index] = sq(_drag_innov[axis_index]) / (25.0f * _drag_innov_var[axis_index]); |
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} else if (axis_index == 1) { |
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// Estimate the airspeed from the measured drag force and ballistic coefficient |
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const float mea_acc = _drag_sample_delayed.accelXY(axis_index) - _state.delta_vel_bias(axis_index) / _dt_ekf_avg; |
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const float airSpd = sqrtf((2.0f * fabsf(mea_acc)) / (BC_inv_y * rho)); |
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// Estimate the derivative of specific force wrt airspeed along the X axis |
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// Limit lower value to prevent arithmetic exceptions |
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const float Kacc = fmaxf(1e-1f, rho * BC_inv_y * airSpd); |
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SH_ACC[0] = sq(q0) - sq(q1) + sq(q2) - sq(q3); |
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SH_ACC[1] = vn - vwn; |
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SH_ACC[2] = ve - vwe; |
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H_ACC[0] = -Kacc*(2.0f*q0*SH_ACC[2] - 2.0f*q3*SH_ACC[1] + 2.0f*q1*vd); |
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H_ACC[1] = -Kacc*(2.0f*q2*SH_ACC[1] - 2.0f*q1*SH_ACC[2] + 2.0f*q0*vd); |
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H_ACC[2] = -Kacc*(2.0f*q1*SH_ACC[1] + 2.0f*q2*SH_ACC[2] + 2.0f*q3*vd); |
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H_ACC[3] = Kacc*(2.0f*q0*SH_ACC[1] + 2.0f*q3*SH_ACC[2] - 2.0f*q2*vd); |
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H_ACC[4] = Kacc*(2.0f*q0*q3 - 2.0f*q1*q2); |
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H_ACC[5] = -Kacc*SH_ACC[0]; |
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H_ACC[6] = -Kacc*(2.0f*q0*q1 + 2.0f*q2*q3); |
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H_ACC[22] = -2.0f*Kacc*(q0*q3 - q1*q2); |
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H_ACC[23] = Kacc*SH_ACC[0]; |
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_drag_innov_var[1] = (R_ACC + Kacc*SH_ACC[0]*(Kacc*P(5,5)*SH_ACC[0] - Kacc*P(23,5)*SH_ACC[0] - Kacc*P(4,5)*(2.0f*q0*q3 - 2.0f*q1*q2) + Kacc*P(6,5)*(2.0f*q0*q1 + 2.0f*q2*q3) + 2*Kacc*P(22,5)*(q0*q3 - q1*q2) + Kacc*P(0,5)*(2.0f*q0*SH_ACC[2] - 2.0f*q3*SH_ACC[1] + 2.0f*q1*vd) + Kacc*P(1,5)*(2.0f*q2*SH_ACC[1] - 2.0f*q1*SH_ACC[2] + 2.0f*q0*vd) + Kacc*P(2,5)*(2.0f*q1*SH_ACC[1] + 2.0f*q2*SH_ACC[2] + 2.0f*q3*vd) - Kacc*P(3,5)*(2.0f*q0*SH_ACC[1] + 2.0f*q3*SH_ACC[2] - 2.0f*q2*vd)) - Kacc*SH_ACC[0]*(Kacc*P(5,23)*SH_ACC[0] - Kacc*P(23,23)*SH_ACC[0] - Kacc*P(4,23)*(2.0f*q0*q3 - 2.0f*q1*q2) + Kacc*P(6,23)*(2.0f*q0*q1 + 2.0f*q2*q3) + 2*Kacc*P(22,23)*(q0*q3 - q1*q2) + Kacc*P(0,23)*(2.0f*q0*SH_ACC[2] - 2.0f*q3*SH_ACC[1] + 2.0f*q1*vd) + Kacc*P(1,23)*(2.0f*q2*SH_ACC[1] - 2.0f*q1*SH_ACC[2] + 2.0f*q0*vd) + Kacc*P(2,23)*(2.0f*q1*SH_ACC[1] + 2.0f*q2*SH_ACC[2] + 2.0f*q3*vd) - Kacc*P(3,23)*(2.0f*q0*SH_ACC[1] + 2.0f*q3*SH_ACC[2] - 2.0f*q2*vd)) - Kacc*(2.0f*q0*q3 - 2.0f*q1*q2)*(Kacc*P(5,4)*SH_ACC[0] - Kacc*P(23,4)*SH_ACC[0] - Kacc*P(4,4)*(2.0f*q0*q3 - 2.0f*q1*q2) + Kacc*P(6,4)*(2.0f*q0*q1 + 2.0f*q2*q3) + 2*Kacc*P(22,4)*(q0*q3 - q1*q2) + Kacc*P(0,4)*(2.0f*q0*SH_ACC[2] - 2.0f*q3*SH_ACC[1] + 2.0f*q1*vd) + Kacc*P(1,4)*(2.0f*q2*SH_ACC[1] - 2.0f*q1*SH_ACC[2] + 2.0f*q0*vd) + Kacc*P(2,4)*(2.0f*q1*SH_ACC[1] + 2.0f*q2*SH_ACC[2] + 2.0f*q3*vd) - Kacc*P(3,4)*(2.0f*q0*SH_ACC[1] + 2.0f*q3*SH_ACC[2] - 2.0f*q2*vd)) + Kacc*(2.0f*q0*q1 + 2.0f*q2*q3)*(Kacc*P(5,6)*SH_ACC[0] - Kacc*P(23,6)*SH_ACC[0] - Kacc*P(4,6)*(2.0f*q0*q3 - 2.0f*q1*q2) + Kacc*P(6,6)*(2.0f*q0*q1 + 2.0f*q2*q3) + 2*Kacc*P(22,6)*(q0*q3 - q1*q2) + Kacc*P(0,6)*(2.0f*q0*SH_ACC[2] - 2.0f*q3*SH_ACC[1] + 2.0f*q1*vd) + Kacc*P(1,6)*(2.0f*q2*SH_ACC[1] - 2.0f*q1*SH_ACC[2] + 2.0f*q0*vd) + Kacc*P(2,6)*(2.0f*q1*SH_ACC[1] + 2.0f*q2*SH_ACC[2] + 2.0f*q3*vd) - Kacc*P(3,6)*(2.0f*q0*SH_ACC[1] + 2.0f*q3*SH_ACC[2] - 2.0f*q2*vd)) + 2*Kacc*(q0*q3 - q1*q2)*(Kacc*P(5,22)*SH_ACC[0] - Kacc*P(23,22)*SH_ACC[0] - Kacc*P(4,22)*(2.0f*q0*q3 - 2.0f*q1*q2) + Kacc*P(6,22)*(2.0f*q0*q1 + 2.0f*q2*q3) + 2*Kacc*P(22,22)*(q0*q3 - q1*q2) + Kacc*P(0,22)*(2.0f*q0*SH_ACC[2] - 2.0f*q3*SH_ACC[1] + 2.0f*q1*vd) + Kacc*P(1,22)*(2.0f*q2*SH_ACC[1] - 2.0f*q1*SH_ACC[2] + 2.0f*q0*vd) + Kacc*P(2,22)*(2.0f*q1*SH_ACC[1] + 2.0f*q2*SH_ACC[2] + 2.0f*q3*vd) - Kacc*P(3,22)*(2.0f*q0*SH_ACC[1] + 2.0f*q3*SH_ACC[2] - 2.0f*q2*vd)) + Kacc*(2.0f*q0*SH_ACC[2] - 2.0f*q3*SH_ACC[1] + 2.0f*q1*vd)*(Kacc*P(5,0)*SH_ACC[0] - Kacc*P(23,0)*SH_ACC[0] - Kacc*P(4,0)*(2.0f*q0*q3 - 2.0f*q1*q2) + Kacc*P(6,0)*(2.0f*q0*q1 + 2.0f*q2*q3) + 2*Kacc*P(22,0)*(q0*q3 - q1*q2) + Kacc*P(0,0)*(2.0f*q0*SH_ACC[2] - 2.0f*q3*SH_ACC[1] + 2.0f*q1*vd) + Kacc*P(1,0)*(2.0f*q2*SH_ACC[1] - 2.0f*q1*SH_ACC[2] + 2.0f*q0*vd) + Kacc*P(2,0)*(2.0f*q1*SH_ACC[1] + 2.0f*q2*SH_ACC[2] + 2.0f*q3*vd) - Kacc*P(3,0)*(2.0f*q0*SH_ACC[1] + 2.0f*q3*SH_ACC[2] - 2.0f*q2*vd)) + Kacc*(2.0f*q2*SH_ACC[1] - 2.0f*q1*SH_ACC[2] + 2.0f*q0*vd)*(Kacc*P(5,1)*SH_ACC[0] - Kacc*P(23,1)*SH_ACC[0] - Kacc*P(4,1)*(2.0f*q0*q3 - 2.0f*q1*q2) + Kacc*P(6,1)*(2.0f*q0*q1 + 2.0f*q2*q3) + 2*Kacc*P(22,1)*(q0*q3 - q1*q2) + Kacc*P(0,1)*(2.0f*q0*SH_ACC[2] - 2.0f*q3*SH_ACC[1] + 2.0f*q1*vd) + Kacc*P(1,1)*(2.0f*q2*SH_ACC[1] - 2.0f*q1*SH_ACC[2] + 2.0f*q0*vd) + Kacc*P(2,1)*(2.0f*q1*SH_ACC[1] + 2.0f*q2*SH_ACC[2] + 2.0f*q3*vd) - Kacc*P(3,1)*(2.0f*q0*SH_ACC[1] + 2.0f*q3*SH_ACC[2] - 2.0f*q2*vd)) + Kacc*(2.0f*q1*SH_ACC[1] + 2.0f*q2*SH_ACC[2] + 2.0f*q3*vd)*(Kacc*P(5,2)*SH_ACC[0] - Kacc*P(23,2)*SH_ACC[0] - Kacc*P(4,2)*(2.0f*q0*q3 - 2.0f*q1*q2) + Kacc*P(6,2)*(2.0f*q0*q1 + 2.0f*q2*q3) + 2*Kacc*P(22,2)*(q0*q3 - q1*q2) + Kacc*P(0,2)*(2.0f*q0*SH_ACC[2] - 2.0f*q3*SH_ACC[1] + 2.0f*q1*vd) + Kacc*P(1,2)*(2.0f*q2*SH_ACC[1] - 2.0f*q1*SH_ACC[2] + 2.0f*q0*vd) + Kacc*P(2,2)*(2.0f*q1*SH_ACC[1] + 2.0f*q2*SH_ACC[2] + 2.0f*q3*vd) - Kacc*P(3,2)*(2.0f*q0*SH_ACC[1] + 2.0f*q3*SH_ACC[2] - 2.0f*q2*vd)) - Kacc*(2.0f*q0*SH_ACC[1] + 2.0f*q3*SH_ACC[2] - 2.0f*q2*vd)*(Kacc*P(5,3)*SH_ACC[0] - Kacc*P(23,3)*SH_ACC[0] - Kacc*P(4,3)*(2.0f*q0*q3 - 2.0f*q1*q2) + Kacc*P(6,3)*(2.0f*q0*q1 + 2.0f*q2*q3) + 2*Kacc*P(22,3)*(q0*q3 - q1*q2) + Kacc*P(0,3)*(2.0f*q0*SH_ACC[2] - 2.0f*q3*SH_ACC[1] + 2.0f*q1*vd) + Kacc*P(1,3)*(2.0f*q2*SH_ACC[1] - 2.0f*q1*SH_ACC[2] + 2.0f*q0*vd) + Kacc*P(2,3)*(2.0f*q1*SH_ACC[1] + 2.0f*q2*SH_ACC[2] + 2.0f*q3*vd) - Kacc*P(3,3)*(2.0f*q0*SH_ACC[1] + 2.0f*q3*SH_ACC[2] - 2.0f*q2*vd))); |
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if (_drag_innov_var[1] < R_ACC) { |
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// calculation is badly conditioned |
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return; |
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} |
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SK_ACC[0] = 1.0f/_drag_innov_var[1]; |
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SK_ACC[1] = 2.0f*q0*SH_ACC[1] + 2.0f*q3*SH_ACC[2] - 2.0f*q2*vd; |
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SK_ACC[2] = 2.0f*q2*SH_ACC[1] - 2.0f*q1*SH_ACC[2] + 2.0f*q0*vd; |
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SK_ACC[3] = 2.0f*q0*SH_ACC[2] - 2.0f*q3*SH_ACC[1] + 2.0f*q1*vd; |
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SK_ACC[4] = 2.0f*q1*SH_ACC[1] + 2.0f*q2*SH_ACC[2] + 2.0f*q3*vd; |
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SK_ACC[5] = 2.0f*q0*q3 - 2.0f*q1*q2; |
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SK_ACC[6] = q0*q3 - q1*q2; |
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SK_ACC[7] = 2.0f*q0*q1 + 2.0f*q2*q3; |
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SK_ACC[8] = SH_ACC[0]; |
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// Don't allow modification of any states other than wind velocity at this stage of development - we only need a wind estimate. |
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// Kfusion[0] = -SK_ACC[0]*(Kacc*P(0,0)*SK_ACC[3] + Kacc*P(0,1)*SK_ACC[2] - Kacc*P(0,3)*SK_ACC[1] + Kacc*P(0,2)*SK_ACC[4] - Kacc*P(0,4)*SK_ACC[5] + Kacc*P(0,5)*SK_ACC[8] + Kacc*P(0,6)*SK_ACC[7] + 2*Kacc*P(0,22)*SK_ACC[6] - Kacc*P(0,23)*SK_ACC[8]); |
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// Kfusion[1] = -SK_ACC[0]*(Kacc*P(1,0)*SK_ACC[3] + Kacc*P(1,1)*SK_ACC[2] - Kacc*P(1,3)*SK_ACC[1] + Kacc*P(1,2)*SK_ACC[4] - Kacc*P(1,4)*SK_ACC[5] + Kacc*P(1,5)*SK_ACC[8] + Kacc*P(1,6)*SK_ACC[7] + 2*Kacc*P(1,22)*SK_ACC[6] - Kacc*P(1,23)*SK_ACC[8]); |
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// Kfusion[2] = -SK_ACC[0]*(Kacc*P(2,0)*SK_ACC[3] + Kacc*P(2,1)*SK_ACC[2] - Kacc*P(2,3)*SK_ACC[1] + Kacc*P(2,2)*SK_ACC[4] - Kacc*P(2,4)*SK_ACC[5] + Kacc*P(2,5)*SK_ACC[8] + Kacc*P(2,6)*SK_ACC[7] + 2*Kacc*P(2,22)*SK_ACC[6] - Kacc*P(2,23)*SK_ACC[8]); |
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// Kfusion[3] = -SK_ACC[0]*(Kacc*P(3,0)*SK_ACC[3] + Kacc*P(3,1)*SK_ACC[2] - Kacc*P(3,3)*SK_ACC[1] + Kacc*P(3,2)*SK_ACC[4] - Kacc*P(3,4)*SK_ACC[5] + Kacc*P(3,5)*SK_ACC[8] + Kacc*P(3,6)*SK_ACC[7] + 2*Kacc*P(3,22)*SK_ACC[6] - Kacc*P(3,23)*SK_ACC[8]); |
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// Kfusion[4] = -SK_ACC[0]*(Kacc*P(4,0)*SK_ACC[3] + Kacc*P(4,1)*SK_ACC[2] - Kacc*P(4,3)*SK_ACC[1] + Kacc*P(4,2)*SK_ACC[4] - Kacc*P(4,4)*SK_ACC[5] + Kacc*P(4,5)*SK_ACC[8] + Kacc*P(4,6)*SK_ACC[7] + 2*Kacc*P(4,22)*SK_ACC[6] - Kacc*P(4,23)*SK_ACC[8]); |
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// Kfusion[5] = -SK_ACC[0]*(Kacc*P(5,0)*SK_ACC[3] + Kacc*P(5,1)*SK_ACC[2] - Kacc*P(5,3)*SK_ACC[1] + Kacc*P(5,2)*SK_ACC[4] - Kacc*P(5,4)*SK_ACC[5] + Kacc*P(5,5)*SK_ACC[8] + Kacc*P(5,6)*SK_ACC[7] + 2*Kacc*P(5,22)*SK_ACC[6] - Kacc*P(5,23)*SK_ACC[8]); |
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// Kfusion[6] = -SK_ACC[0]*(Kacc*P(6,0)*SK_ACC[3] + Kacc*P(6,1)*SK_ACC[2] - Kacc*P(6,3)*SK_ACC[1] + Kacc*P(6,2)*SK_ACC[4] - Kacc*P(6,4)*SK_ACC[5] + Kacc*P(6,5)*SK_ACC[8] + Kacc*P(6,6)*SK_ACC[7] + 2*Kacc*P(6,22)*SK_ACC[6] - Kacc*P(6,23)*SK_ACC[8]); |
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// Kfusion[7] = -SK_ACC[0]*(Kacc*P(7,0)*SK_ACC[3] + Kacc*P(7,1)*SK_ACC[2] - Kacc*P(7,3)*SK_ACC[1] + Kacc*P(7,2)*SK_ACC[4] - Kacc*P(7,4)*SK_ACC[5] + Kacc*P(7,5)*SK_ACC[8] + Kacc*P(7,6)*SK_ACC[7] + 2*Kacc*P(7,22)*SK_ACC[6] - Kacc*P(7,23)*SK_ACC[8]); |
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// Kfusion[8] = -SK_ACC[0]*(Kacc*P(8,0)*SK_ACC[3] + Kacc*P(8,1)*SK_ACC[2] - Kacc*P(8,3)*SK_ACC[1] + Kacc*P(8,2)*SK_ACC[4] - Kacc*P(8,4)*SK_ACC[5] + Kacc*P(8,5)*SK_ACC[8] + Kacc*P(8,6)*SK_ACC[7] + 2*Kacc*P(8,22)*SK_ACC[6] - Kacc*P(8,23)*SK_ACC[8]); |
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// Kfusion[9] = -SK_ACC[0]*(Kacc*P(9,0)*SK_ACC[3] + Kacc*P(9,1)*SK_ACC[2] - Kacc*P(9,3)*SK_ACC[1] + Kacc*P(9,2)*SK_ACC[4] - Kacc*P(9,4)*SK_ACC[5] + Kacc*P(9,5)*SK_ACC[8] + Kacc*P(9,6)*SK_ACC[7] + 2*Kacc*P(9,22)*SK_ACC[6] - Kacc*P(9,23)*SK_ACC[8]); |
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// Kfusion[10] = -SK_ACC[0]*(Kacc*P(10,0)*SK_ACC[3] + Kacc*P(10,1)*SK_ACC[2] - Kacc*P(10,3)*SK_ACC[1] + Kacc*P(10,2)*SK_ACC[4] - Kacc*P(10,4)*SK_ACC[5] + Kacc*P(10,5)*SK_ACC[8] + Kacc*P(10,6)*SK_ACC[7] + 2*Kacc*P(10,22)*SK_ACC[6] - Kacc*P(10,23)*SK_ACC[8]); |
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// Kfusion[11] = -SK_ACC[0]*(Kacc*P(11,0)*SK_ACC[3] + Kacc*P(11,1)*SK_ACC[2] - Kacc*P(11,3)*SK_ACC[1] + Kacc*P(11,2)*SK_ACC[4] - Kacc*P(11,4)*SK_ACC[5] + Kacc*P(11,5)*SK_ACC[8] + Kacc*P(11,6)*SK_ACC[7] + 2*Kacc*P(11,22)*SK_ACC[6] - Kacc*P(11,23)*SK_ACC[8]); |
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// Kfusion[12] = -SK_ACC[0]*(Kacc*P(12,0)*SK_ACC[3] + Kacc*P(12,1)*SK_ACC[2] - Kacc*P(12,3)*SK_ACC[1] + Kacc*P(12,2)*SK_ACC[4] - Kacc*P(12,4)*SK_ACC[5] + Kacc*P(12,5)*SK_ACC[8] + Kacc*P(12,6)*SK_ACC[7] + 2*Kacc*P(12,22)*SK_ACC[6] - Kacc*P(12,23)*SK_ACC[8]); |
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// Kfusion[13] = -SK_ACC[0]*(Kacc*P(13,0)*SK_ACC[3] + Kacc*P(13,1)*SK_ACC[2] - Kacc*P(13,3)*SK_ACC[1] + Kacc*P(13,2)*SK_ACC[4] - Kacc*P(13,4)*SK_ACC[5] + Kacc*P(13,5)*SK_ACC[8] + Kacc*P(13,6)*SK_ACC[7] + 2*Kacc*P(13,22)*SK_ACC[6] - Kacc*P(13,23)*SK_ACC[8]); |
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// Kfusion[14] = -SK_ACC[0]*(Kacc*P(14,0)*SK_ACC[3] + Kacc*P(14,1)*SK_ACC[2] - Kacc*P(14,3)*SK_ACC[1] + Kacc*P(14,2)*SK_ACC[4] - Kacc*P(14,4)*SK_ACC[5] + Kacc*P(14,5)*SK_ACC[8] + Kacc*P(14,6)*SK_ACC[7] + 2*Kacc*P(14,22)*SK_ACC[6] - Kacc*P(14,23)*SK_ACC[8]); |
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// Kfusion[15] = -SK_ACC[0]*(Kacc*P(15,0)*SK_ACC[3] + Kacc*P(15,1)*SK_ACC[2] - Kacc*P(15,3)*SK_ACC[1] + Kacc*P(15,2)*SK_ACC[4] - Kacc*P(15,4)*SK_ACC[5] + Kacc*P(15,5)*SK_ACC[8] + Kacc*P(15,6)*SK_ACC[7] + 2*Kacc*P(15,22)*SK_ACC[6] - Kacc*P(15,23)*SK_ACC[8]); |
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// Kfusion[16] = -SK_ACC[0]*(Kacc*P(16,0)*SK_ACC[3] + Kacc*P(16,1)*SK_ACC[2] - Kacc*P(16,3)*SK_ACC[1] + Kacc*P(16,2)*SK_ACC[4] - Kacc*P(16,4)*SK_ACC[5] + Kacc*P(16,5)*SK_ACC[8] + Kacc*P(16,6)*SK_ACC[7] + 2*Kacc*P(16,22)*SK_ACC[6] - Kacc*P(16,23)*SK_ACC[8]); |
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// Kfusion[17] = -SK_ACC[0]*(Kacc*P(17,0)*SK_ACC[3] + Kacc*P(17,1)*SK_ACC[2] - Kacc*P(17,3)*SK_ACC[1] + Kacc*P(17,2)*SK_ACC[4] - Kacc*P(17,4)*SK_ACC[5] + Kacc*P(17,5)*SK_ACC[8] + Kacc*P(17,6)*SK_ACC[7] + 2*Kacc*P(17,22)*SK_ACC[6] - Kacc*P(17,23)*SK_ACC[8]); |
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// Kfusion[18] = -SK_ACC[0]*(Kacc*P(18,0)*SK_ACC[3] + Kacc*P(18,1)*SK_ACC[2] - Kacc*P(18,3)*SK_ACC[1] + Kacc*P(18,2)*SK_ACC[4] - Kacc*P(18,4)*SK_ACC[5] + Kacc*P(18,5)*SK_ACC[8] + Kacc*P(18,6)*SK_ACC[7] + 2*Kacc*P(18,22)*SK_ACC[6] - Kacc*P(18,23)*SK_ACC[8]); |
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// Kfusion[19] = -SK_ACC[0]*(Kacc*P(19,0)*SK_ACC[3] + Kacc*P(19,1)*SK_ACC[2] - Kacc*P(19,3)*SK_ACC[1] + Kacc*P(19,2)*SK_ACC[4] - Kacc*P(19,4)*SK_ACC[5] + Kacc*P(19,5)*SK_ACC[8] + Kacc*P(19,6)*SK_ACC[7] + 2*Kacc*P(19,22)*SK_ACC[6] - Kacc*P(19,23)*SK_ACC[8]); |
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// Kfusion[20] = -SK_ACC[0]*(Kacc*P(20,0)*SK_ACC[3] + Kacc*P(20,1)*SK_ACC[2] - Kacc*P(20,3)*SK_ACC[1] + Kacc*P(20,2)*SK_ACC[4] - Kacc*P(20,4)*SK_ACC[5] + Kacc*P(20,5)*SK_ACC[8] + Kacc*P(20,6)*SK_ACC[7] + 2*Kacc*P(20,22)*SK_ACC[6] - Kacc*P(20,23)*SK_ACC[8]); |
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// Kfusion[21] = -SK_ACC[0]*(Kacc*P(21,0)*SK_ACC[3] + Kacc*P(21,1)*SK_ACC[2] - Kacc*P(21,3)*SK_ACC[1] + Kacc*P(21,2)*SK_ACC[4] - Kacc*P(21,4)*SK_ACC[5] + Kacc*P(21,5)*SK_ACC[8] + Kacc*P(21,6)*SK_ACC[7] + 2*Kacc*P(21,22)*SK_ACC[6] - Kacc*P(21,23)*SK_ACC[8]); |
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Kfusion[22] = -SK_ACC[0]*(Kacc*P(22,0)*SK_ACC[3] + Kacc*P(22,1)*SK_ACC[2] - Kacc*P(22,3)*SK_ACC[1] + Kacc*P(22,2)*SK_ACC[4] - Kacc*P(22,4)*SK_ACC[5] + Kacc*P(22,5)*SK_ACC[8] + Kacc*P(22,6)*SK_ACC[7] + 2*Kacc*P(22,22)*SK_ACC[6] - Kacc*P(22,23)*SK_ACC[8]); |
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Kfusion[23] = -SK_ACC[0]*(Kacc*P(23,0)*SK_ACC[3] + Kacc*P(23,1)*SK_ACC[2] - Kacc*P(23,3)*SK_ACC[1] + Kacc*P(23,2)*SK_ACC[4] - Kacc*P(23,4)*SK_ACC[5] + Kacc*P(23,5)*SK_ACC[8] + Kacc*P(23,6)*SK_ACC[7] + 2*Kacc*P(23,22)*SK_ACC[6] - Kacc*P(23,23)*SK_ACC[8]); |
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// calculate the predicted acceleration and innovation measured along the Y body axis |
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float drag_sign; |
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if (rel_wind_body(axis_index) >= 0.0f) { |
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drag_sign = 1.0f; |
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} else { |
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drag_sign = -1.0f; |
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} |
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const float predAccel = -BC_inv_y * 0.5f * rho * sq(rel_wind_body(axis_index)) * drag_sign; |
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_drag_innov[axis_index] = predAccel - mea_acc; |
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_drag_test_ratio[axis_index] = sq(_drag_innov[axis_index]) / (25.0f * _drag_innov_var[axis_index]); |
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} |
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// if the innovation consistency check fails then don't fuse the sample |
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if (_drag_test_ratio[axis_index] <= 1.0f) { |
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// apply covariance correction via P_new = (I -K*H)*P |
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// first calculate expression for KHP |
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// then calculate P - KHP |
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matrix::SquareMatrix<float, _k_num_states> KHP; |
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float KH[9]; |
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for (unsigned row = 0; row < _k_num_states; row++) { |
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KH[0] = Kfusion[row] * H_ACC[0]; |
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KH[1] = Kfusion[row] * H_ACC[1]; |
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KH[2] = Kfusion[row] * H_ACC[2]; |
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KH[3] = Kfusion[row] * H_ACC[3]; |
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KH[4] = Kfusion[row] * H_ACC[4]; |
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KH[5] = Kfusion[row] * H_ACC[5]; |
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KH[6] = Kfusion[row] * H_ACC[6]; |
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KH[7] = Kfusion[row] * H_ACC[22]; |
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KH[8] = Kfusion[row] * H_ACC[23]; |
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for (unsigned column = 0; column < _k_num_states; column++) { |
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float tmp = KH[0] * P(0,column); |
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tmp += KH[1] * P(1,column); |
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tmp += KH[2] * P(2,column); |
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tmp += KH[3] * P(3,column); |
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tmp += KH[4] * P(4,column); |
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tmp += KH[5] * P(5,column); |
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tmp += KH[6] * P(6,column); |
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tmp += KH[7] * P(22,column); |
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tmp += KH[8] * P(23,column); |
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KHP(row,column) = tmp; |
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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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//_fault_status.flags.bad_sideslip = false; |
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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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P.uncorrelateCovarianceSetVariance<1>(i, 0.0f); |
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//flag as unhealthy |
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healthy = false; |
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// update individual measurement health status |
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//_fault_status.flags.bad_sideslip = true; |
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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(true); |
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// apply the state corrections |
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fuse(Kfusion, _drag_innov[axis_index]); |
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} |
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} |
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} |
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}
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