alternate complementary filter in euler with less approximations

This commit is contained in:
Gautier Hattenberger
2010-05-04 08:46:54 +00:00
parent 7e511cdef7
commit 7dfe36b206
@@ -0,0 +1,183 @@
/*
* $Id: booz2_filter_attitude_cmpl_euler.c 4675 2010-03-13 22:59:46Z poine $
*
* Copyright (C) 2008-2009 Antoine Drouin <poinix@gmail.com>
*
* This file is part of paparazzi.
*
* paparazzi is free software; you can redistribute it and/or modify
* it under the terms of the GNU General Public License as published by
* the Free Software Foundation; either version 2, or (at your option)
* any later version.
*
* paparazzi is distributed in the hope that it will be useful,
* but WITHOUT ANY WARRANTY; without even the implied warranty of
* MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
* GNU General Public License for more details.
*
* You should have received a copy of the GNU General Public License
* along with paparazzi; see the file COPYING. If not, write to
* the Free Software Foundation, 59 Temple Place - Suite 330,
* Boston, MA 02111-1307, USA.
*/
#include "booz2_filter_attitude_cmpl_euler.h"
#include "booz_imu.h"
#include "booz_ahrs_aligner.h"
#include "airframe.h"
#include "math/pprz_trig_int.h"
#include "math/pprz_algebra_int.h"
struct Int32Rates booz2_face_gyro_bias;
struct Int32Eulers booz2_face_measure;
struct Int32Eulers booz2_face_residual;
struct Int32Eulers booz2_face_uncorrected;
struct Int32Eulers booz2_face_corrected;
struct Int32Eulers measurement;
int32_t booz2_face_reinj_1;
void booz_ahrs_init(void) {
booz_ahrs.status = BOOZ_AHRS_UNINIT;
INT_EULERS_ZERO(booz_ahrs.ltp_to_body_euler);
INT_EULERS_ZERO(booz_ahrs.ltp_to_imu_euler);
INT32_QUAT_ZERO(booz_ahrs.ltp_to_body_quat);
INT32_QUAT_ZERO(booz_ahrs.ltp_to_imu_quat);
INT_RATES_ZERO(booz_ahrs.body_rate);
INT_RATES_ZERO(booz_ahrs.imu_rate);
INT_RATES_ZERO(booz2_face_gyro_bias);
booz2_face_reinj_1 = BOOZ2_FACE_REINJ_1;
INT_EULERS_ZERO(booz2_face_uncorrected);
}
void booz_ahrs_align(void) {
RATES_COPY( booz2_face_gyro_bias, booz_ahrs_aligner.lp_gyro);
booz_ahrs.status = BOOZ_AHRS_RUNNING;
}
#define F_UPDATE 512
#define PI_INTEG_EULER (INT32_ANGLE_PI * F_UPDATE)
#define TWO_PI_INTEG_EULER (INT32_ANGLE_2_PI * F_UPDATE)
#define INTEG_EULER_NORMALIZE(_a) { \
while (_a > PI_INTEG_EULER) _a -= TWO_PI_INTEG_EULER; \
while (_a < -PI_INTEG_EULER) _a += TWO_PI_INTEG_EULER; \
}
/*
*
* fc = 1/(2*pi*tau)
*
* alpha = dt / ( tau + dt )
*
*
* y(i) = alpha x(i) + (1-alpha) y(i-1)
* or
* y(i) = y(i-1) + alpha * (x(i) - y(i-1))
*
*
*/
void booz_ahrs_propagate(void) {
/* unbias gyro */
struct Int32Rates uf_rate;
RATES_DIFF(uf_rate, booz_imu.gyro, booz2_face_gyro_bias);
/* low pass rate */
RATES_ADD(booz_ahrs.imu_rate, uf_rate);
RATES_SDIV(booz_ahrs.imu_rate, booz_ahrs.imu_rate, 2);
/* integrate eulers */
struct Int32Eulers euler_dot;
INT32_EULERS_DOT_OF_RATES(euler_dot, booz_ahrs.ltp_to_imu_euler, booz_ahrs.imu_rate);
EULERS_ADD(booz2_face_corrected, euler_dot);
/* low pass measurement */
EULERS_ADD(booz2_face_measure, measurement);
EULERS_SDIV(booz2_face_measure, booz2_face_measure, 2);
/* compute residual */
EULERS_DIFF(booz2_face_residual, booz2_face_measure, booz2_face_corrected);
INTEG_EULER_NORMALIZE(booz2_face_residual.psi);
struct Int32Eulers correction;
/* compute a correction */
EULERS_SDIV(correction, booz2_face_residual, booz2_face_reinj_1);
/* correct estimation */
EULERS_ADD(booz2_face_corrected, correction);
INTEG_EULER_NORMALIZE(booz2_face_corrected.psi);
/* Compute LTP to IMU eulers */
EULERS_SDIV(booz_ahrs.ltp_to_imu_euler, booz2_face_corrected, F_UPDATE);
/* Compute LTP to IMU quaternion */
INT32_QUAT_OF_EULERS(booz_ahrs.ltp_to_imu_quat, booz_ahrs.ltp_to_imu_euler);
/* Compute LTP to IMU rotation matrix */
INT32_RMAT_OF_EULERS(booz_ahrs.ltp_to_imu_rmat, booz_ahrs.ltp_to_imu_euler);
/* Compute LTP to BODY quaternion */
INT32_QUAT_COMP_INV(booz_ahrs.ltp_to_body_quat, booz_ahrs.ltp_to_imu_quat, booz_imu.body_to_imu_quat);
/* Compute LTP to BODY rotation matrix */
INT32_RMAT_COMP_INV(booz_ahrs.ltp_to_body_rmat, booz_ahrs.ltp_to_imu_rmat, booz_imu.body_to_imu_rmat);
/* compute LTP to BODY eulers */
INT32_EULERS_OF_RMAT(booz_ahrs.ltp_to_body_euler, booz_ahrs.ltp_to_body_rmat);
/* compute body rates */
INT32_RMAT_TRANSP_RATEMULT(booz_ahrs.body_rate, booz_imu.body_to_imu_rmat, booz_ahrs.imu_rate);
}
void booz_ahrs_update_accel(void) {
/* build a measurement assuming constant acceleration ?!! */
INT32_ATAN2(measurement.phi, -booz_imu.accel.y, -booz_imu.accel.z);
int32_t cphi;
PPRZ_ITRIG_COS(cphi, measurement.phi);
int32_t cphi_ax = -INT_MULT_RSHIFT(cphi, booz_imu.accel.x, INT32_TRIG_FRAC);
INT32_ATAN2(measurement.theta, -cphi_ax, -booz_imu.accel.z);
measurement.phi *= F_UPDATE;
measurement.theta *= F_UPDATE;
}
/* measure psi assuming magnetic vector is in earth plan (md = 0) */
void booz_ahrs_update_mag(void) {
int32_t sphi;
PPRZ_ITRIG_SIN(sphi, booz_ahrs.ltp_to_imu_euler.phi);
int32_t cphi;
PPRZ_ITRIG_COS(cphi, booz_ahrs.ltp_to_imu_euler.phi);
int32_t stheta;
PPRZ_ITRIG_SIN(stheta, booz_ahrs.ltp_to_imu_euler.theta);
int32_t ctheta;
PPRZ_ITRIG_COS(ctheta, booz_ahrs.ltp_to_imu_euler.theta);
int32_t sphi_stheta = (sphi*stheta)>>INT32_TRIG_FRAC;
int32_t cphi_stheta = (cphi*stheta)>>INT32_TRIG_FRAC;
//int32_t sphi_ctheta = (sphi*ctheta)>>INT32_TRIG_FRAC;
//int32_t cphi_ctheta = (cphi*ctheta)>>INT32_TRIG_FRAC;
const int32_t mn =
ctheta * booz_imu.mag.x +
sphi_stheta * booz_imu.mag.y +
cphi_stheta * booz_imu.mag.z;
const int32_t me =
0 * booz_imu.mag.x +
cphi * booz_imu.mag.y +
-sphi * booz_imu.mag.z;
//const int32_t md =
// -stheta * booz_imu.mag.x +
// sphi_ctheta * booz_imu.mag.y +
// cphi_ctheta * booz_imu.mag.z;
float m_psi = -atan2(me, mn);
measurement.psi = ((m_psi)*(float)(1<<(INT32_ANGLE_FRAC))*F_UPDATE);
}