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Exposed measurement noise covariance and process noise covariance as MAVLink parameters for attitude EKF

This commit is contained in:
Lorenz Meier 2012-10-03 14:45:55 +02:00
parent 921c391db4
commit 053ce0e2f8
4 changed files with 379 additions and 187 deletions
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1
apps/attitude_estimator_ekf/Makefile
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@ -36,6 +36,7 @@ PRIORITY = SCHED_PRIORITY_DEFAULT
STACKSIZE = 2048
CSRCS = attitude_estimator_ekf_main.c \
attitude_estimator_ekf_params.c \
codegen/eye.c \
codegen/attitudeKalmanfilter.c \
codegen/mrdivide.c \

370
apps/attitude_estimator_ekf/attitude_estimator_ekf_main.c
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@ -58,25 +58,20 @@
#include <uORB/topics/debug_key_value.h>
#include <uORB/topics/sensor_combined.h>
#include <uORB/topics/vehicle_attitude.h>
#include <uORB/topics/parameter_update.h>
#include <arch/board/up_hrt.h>
#include <systemlib/systemlib.h>
#include "codegen/attitudeKalmanfilter_initialize.h"
#include "codegen/attitudeKalmanfilter.h"
#include "attitude_estimator_ekf_params.h"
__EXPORT int attitude_estimator_ekf_main(int argc, char *argv[]);
// #define N_STATES 6
// #define PROJECTION_INITIALIZE_COUNTER_LIMIT 5000
// #define REPROJECTION_COUNTER_LIMIT 125
static unsigned int loop_interval_alarm = 6500; // loop interval in microseconds
static float dt = 1.0f;
/* 0, 0, -9.81, 1, 1, 1, wo (gyro offset), w */
/* state vector x has the following entries [ax,ay,az||mx,my,mz||wox,woy,woz||wx,wy,wz]' */
static float z_k[9]; /**< Measurement vector */
static float x_aposteriori_k[12]; /**< */
@ -94,6 +89,7 @@ static float P_aposteriori_k[144] = {100.f, 0, 0, 0, 0, 0, 0, 0, 0
0, 0, 0, 0, 0, 0, 0, 0, 0.0f, 0, 100.0f, 0,
0, 0, 0, 0, 0, 0, 0, 0, 0.0f, 0, 0, 100.0f,
};
static float P_aposteriori[144] = {100.f, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0,
0, 100.f, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0,
0, 0, 100.f, 0, 0, 0, 0, 0, 0, 0, 0, 0,
@ -107,11 +103,14 @@ static float P_aposteriori[144] = {100.f, 0, 0, 0, 0, 0, 0, 0, 0,
0, 0, 0, 0, 0, 0, 0, 0, 0.0f, 0, 100.0f, 0,
0, 0, 0, 0, 0, 0, 0, 0, 0.0f, 0, 0, 100.0f,
}; /**< init: diagonal matrix with big values */
// static float knownConst[15] = {1, 1, 1, 1, 1, 0.04, 4, 0.1, 70, 70, -2000, 9.81, 1, 4, 1}; /**< knownConst has the following entries [PrvaA,PrvarM,PrvarWO,PrvarW||MsvarA,MsvarM,MsvarW] */
/* output euler angles */
static float euler[3] = {0.0f, 0.0f, 0.0f};
static float Rot_matrix[9] = {1.f, 0, 0,
0, 1.f, 0,
0, 0, 1.f
}; /**< init: identity matrix */
0, 1.f, 0,
0, 0, 1.f
}; /**< init: identity matrix */
static bool thread_should_exit = false; /**< Deamon exit flag */
@ -223,6 +222,9 @@ int attitude_estimator_ekf_thread_main(int argc, char *argv[])
/* rate-limit raw data updates to 200Hz */
orb_set_interval(sub_raw, 4);
/* subscribe to param changes */
int sub_params = orb_subscribe(ORB_ID(parameter_update));
/* advertise attitude */
orb_advert_t pub_att = orb_advertise(ORB_ID(vehicle_attitude), &att);
@ -241,18 +243,19 @@ int attitude_estimator_ekf_thread_main(int argc, char *argv[])
uint64_t sensor_last_timestamp[3] = {0, 0, 0};
float sensor_update_hz[3] = {0.0f, 0.0f, 0.0f};
/* process noise covariance */
float q[12];
/* measurement noise covariance */
float r[9];
/* output euler angles */
float euler[3] = {0.0f, 0.0f, 0.0f};
struct attitude_estimator_ekf_params ekf_params;
struct attitude_estimator_ekf_param_handles ekf_param_handles;
/* initialize parameter handles */
parameters_init(&ekf_param_handles);
/* Main loop*/
while (!thread_should_exit) {
struct pollfd fds[1] = {
struct pollfd fds[2] = {
{ .fd = sub_raw, .events = POLLIN },
{ .fd = sub_params, .events = POLLIN }
};
int ret = poll(fds, 1, 1000);
@ -262,180 +265,173 @@ int attitude_estimator_ekf_thread_main(int argc, char *argv[])
/* XXX this means no sensor data - should be critical or emergency */
printf("[attitude estimator ekf] WARNING: Not getting sensor data - sensor app running?\n");
} else {
/* only update parameters if they changed */
if (fds[1].revents & POLLIN) {
/* read from param to clear updated flag */
struct parameter_update_s update;
orb_copy(ORB_ID(parameter_update), sub_params, &update);
orb_copy(ORB_ID(sensor_combined), sub_raw, &raw);
/* Calculate data time difference in seconds */
dt = (raw.timestamp - last_measurement) / 1000000.0f;
last_measurement = raw.timestamp;
uint8_t update_vect[3] = {0, 0, 0};
/* Fill in gyro measurements */
if (sensor_last_count[0] != raw.gyro_counter) {
update_vect[0] = 1;
sensor_last_count[0] = raw.gyro_counter;
sensor_update_hz[0] = 1e6f / (raw.timestamp - sensor_last_timestamp[0]);
sensor_last_timestamp[0] = raw.timestamp;
/* update parameters */
parameters_update(&ekf_param_handles, &ekf_params);
}
z_k[0] = raw.gyro_rad_s[0];
z_k[1] = raw.gyro_rad_s[1];
z_k[2] = raw.gyro_rad_s[2];
/* only run filter if sensor values changed */
if (fds[0].revents & POLLIN) {
/* update accelerometer measurements */
if (sensor_last_count[1] != raw.accelerometer_counter) {
update_vect[1] = 1;
sensor_last_count[1] = raw.accelerometer_counter;
sensor_update_hz[1] = 1e6f / (raw.timestamp - sensor_last_timestamp[1]);
sensor_last_timestamp[1] = raw.timestamp;
/* get latest measurements */
orb_copy(ORB_ID(sensor_combined), sub_raw, &raw);
/* Calculate data time difference in seconds */
dt = (raw.timestamp - last_measurement) / 1000000.0f;
last_measurement = raw.timestamp;
uint8_t update_vect[3] = {0, 0, 0};
/* Fill in gyro measurements */
if (sensor_last_count[0] != raw.gyro_counter) {
update_vect[0] = 1;
sensor_last_count[0] = raw.gyro_counter;
sensor_update_hz[0] = 1e6f / (raw.timestamp - sensor_last_timestamp[0]);
sensor_last_timestamp[0] = raw.timestamp;
}
z_k[0] = raw.gyro_rad_s[0];
z_k[1] = raw.gyro_rad_s[1];
z_k[2] = raw.gyro_rad_s[2];
/* update accelerometer measurements */
if (sensor_last_count[1] != raw.accelerometer_counter) {
update_vect[1] = 1;
sensor_last_count[1] = raw.accelerometer_counter;
sensor_update_hz[1] = 1e6f / (raw.timestamp - sensor_last_timestamp[1]);
sensor_last_timestamp[1] = raw.timestamp;
}
z_k[3] = raw.accelerometer_m_s2[0];
z_k[4] = raw.accelerometer_m_s2[1];
z_k[5] = raw.accelerometer_m_s2[2];
/* update magnetometer measurements */
if (sensor_last_count[2] != raw.magnetometer_counter) {
update_vect[2] = 1;
sensor_last_count[2] = raw.magnetometer_counter;
sensor_update_hz[2] = 1e6f / (raw.timestamp - sensor_last_timestamp[2]);
sensor_last_timestamp[2] = raw.timestamp;
}
z_k[6] = raw.magnetometer_ga[0];
z_k[7] = raw.magnetometer_ga[1];
z_k[8] = raw.magnetometer_ga[2];
uint64_t now = hrt_absolute_time();
unsigned int time_elapsed = now - last_run;
last_run = now;
if (time_elapsed > loop_interval_alarm) {
//TODO: add warning, cpu overload here
// if (overloadcounter == 20) {
// printf("CPU OVERLOAD DETECTED IN ATTITUDE ESTIMATOR EKF (%lu > %lu)\n", time_elapsed, loop_interval_alarm);
// overloadcounter = 0;
// }
overloadcounter++;
}
int32_t z_k_sizes = 9;
// float u[4] = {0.0f, 0.0f, 0.0f, 0.0f};
static bool const_initialized = false;
/* initialize with good values once we have a reasonable dt estimate */
if (!const_initialized /*&& dt < 0.05 && dt > 0.005*/)
{
dt = 0.005f;
parameters_update(&ekf_param_handles, &ekf_params);
x_aposteriori_k[0] = z_k[0];
x_aposteriori_k[1] = z_k[1];
x_aposteriori_k[2] = z_k[2];
x_aposteriori_k[3] = 0.0f;
x_aposteriori_k[4] = 0.0f;
x_aposteriori_k[5] = 0.0f;
x_aposteriori_k[6] = z_k[3];
x_aposteriori_k[7] = z_k[4];
x_aposteriori_k[8] = z_k[5];
x_aposteriori_k[9] = z_k[6];
x_aposteriori_k[10] = z_k[7];
x_aposteriori_k[11] = z_k[8];
const_initialized = true;
}
/* do not execute the filter if not initialized */
if (!const_initialized) {
continue;
}
dt = 0.004f;
uint64_t timing_start = hrt_absolute_time();
// attitudeKalmanfilter(dt, update_vect, z_k, &z_k_sizes, u, x_aposteriori_k, P_aposteriori_k, knownConst, euler,
// Rot_matrix, x_aposteriori, P_aposteriori);
attitudeKalmanfilter(update_vect, dt, z_k, x_aposteriori_k, P_aposteriori_k, ekf_params.q, ekf_params.r,
euler, Rot_matrix, x_aposteriori, P_aposteriori);
/* swap values for next iteration */
memcpy(P_aposteriori_k, P_aposteriori, sizeof(P_aposteriori_k));
memcpy(x_aposteriori_k, x_aposteriori, sizeof(x_aposteriori_k));
uint64_t timing_diff = hrt_absolute_time() - timing_start;
// /* print rotation matrix every 200th time */
if (printcounter % 200 == 0) {
// printf("x apo:\n%8.4f\t%8.4f\t%8.4f\n%8.4f\t%8.4f\t%8.4f\n%8.4f\t%8.4f\t%8.4f\n",
// x_aposteriori[0], x_aposteriori[1], x_aposteriori[2],
// x_aposteriori[3], x_aposteriori[4], x_aposteriori[5],
// x_aposteriori[6], x_aposteriori[7], x_aposteriori[8]);
// }
printf("EKF attitude iteration: %d, runtime: %d us, dt: %d us (%d Hz)\n", loopcounter, (int)timing_diff, (int)(dt * 1000000.0f), (int)(1.0f / dt));
printf("roll: %8.4f\tpitch: %8.4f\tyaw:%8.4f\n", (double)euler[0], (double)euler[1], (double)euler[2]);
printf("update rates gyro: %8.4f\taccel: %8.4f\tmag:%8.4f\n", (double)sensor_update_hz[0], (double)sensor_update_hz[1], (double)sensor_update_hz[2]);
// printf("\n%d\t%d\t%d\n%d\t%d\t%d\n%d\t%d\t%d\n", (int)(Rot_matrix[0] * 100), (int)(Rot_matrix[1] * 100), (int)(Rot_matrix[2] * 100),
// (int)(Rot_matrix[3] * 100), (int)(Rot_matrix[4] * 100), (int)(Rot_matrix[5] * 100),
// (int)(Rot_matrix[6] * 100), (int)(Rot_matrix[7] * 100), (int)(Rot_matrix[8] * 100));
}
// int i = printcounter % 9;
// // for (int i = 0; i < 9; i++) {
// char name[10];
// sprintf(name, "xapo #%d", i);
// memcpy(dbg.key, name, sizeof(dbg.key));
// dbg.value = x_aposteriori[i];
// orb_publish(ORB_ID(debug_key_value), pub_dbg, &dbg);
printcounter++;
if (last_data > 0 && raw.timestamp - last_data > 12000) printf("[attitude estimator ekf] sensor data missed! (%llu)\n", raw.timestamp - last_data);
last_data = raw.timestamp;
/* send out */
att.timestamp = raw.timestamp;
att.roll = euler[0];
att.pitch = euler[1];
att.yaw = euler[2];
att.rollspeed = x_aposteriori[0];
att.pitchspeed = x_aposteriori[1];
att.yawspeed = x_aposteriori[2];
/* copy offsets */
memcpy(&att.rate_offsets, &(x_aposteriori[3]), sizeof(att.rate_offsets));
/* copy rotation matrix */
memcpy(&att.R, Rot_matrix, sizeof(Rot_matrix));
att.R_valid = true;
// Broadcast
orb_publish(ORB_ID(vehicle_attitude), pub_att, &att);
}
z_k[3] = raw.accelerometer_m_s2[0];
z_k[4] = raw.accelerometer_m_s2[1];
z_k[5] = raw.accelerometer_m_s2[2];
/* update magnetometer measurements */
if (sensor_last_count[2] != raw.magnetometer_counter) {
update_vect[2] = 1;
sensor_last_count[2] = raw.magnetometer_counter;
sensor_update_hz[2] = 1e6f / (raw.timestamp - sensor_last_timestamp[2]);
sensor_last_timestamp[2] = raw.timestamp;
}
z_k[6] = raw.magnetometer_ga[0];
z_k[7] = raw.magnetometer_ga[1];
z_k[8] = raw.magnetometer_ga[2];
uint64_t now = hrt_absolute_time();
unsigned int time_elapsed = now - last_run;
last_run = now;
if (time_elapsed > loop_interval_alarm) {
//TODO: add warning, cpu overload here
// if (overloadcounter == 20) {
// printf("CPU OVERLOAD DETECTED IN ATTITUDE ESTIMATOR EKF (%lu > %lu)\n", time_elapsed, loop_interval_alarm);
// overloadcounter = 0;
// }
overloadcounter++;
}
int32_t z_k_sizes = 9;
// float u[4] = {0.0f, 0.0f, 0.0f, 0.0f};
static bool const_initialized = false;
/* initialize with good values once we have a reasonable dt estimate */
if (!const_initialized /*&& dt < 0.05 && dt > 0.005*/)
{
dt = 0.005f;
q[0] = 1e1f;
q[1] = 1e1f;
q[2] = 1e1f;
/* process noise gyro offset covariance */
q[3] = 1e-4f;
q[4] = 1e-4f;
q[5] = 1e-4f;
q[6] = 1e-1f;
q[7] = 1e-1f;
q[8] = 1e-1f;
q[9] = 1e-1f;
q[10] = 1e-1f;
q[11] = 1e-1f;
r[0]= 1e-2f;
r[1]= 1e-2f;
r[2]= 1e-2f;
r[3]= 1e-1f;
r[4]= 1e-1f;
r[5]= 1e-1f;
r[6]= 1e-1f;
r[7]= 1e-1f;
r[8]= 1e-1f;
x_aposteriori_k[0] = z_k[0];
x_aposteriori_k[1] = z_k[1];
x_aposteriori_k[2] = z_k[2];
x_aposteriori_k[3] = 0.0f;
x_aposteriori_k[4] = 0.0f;
x_aposteriori_k[5] = 0.0f;
x_aposteriori_k[6] = z_k[3];
x_aposteriori_k[7] = z_k[4];
x_aposteriori_k[8] = z_k[5];
x_aposteriori_k[9] = z_k[6];
x_aposteriori_k[10] = z_k[7];
x_aposteriori_k[11] = z_k[8];
const_initialized = true;
}
/* do not execute the filter if not initialized */
if (!const_initialized) {
continue;
}
dt = 0.004f;
uint64_t timing_start = hrt_absolute_time();
// attitudeKalmanfilter(dt, update_vect, z_k, &z_k_sizes, u, x_aposteriori_k, P_aposteriori_k, knownConst, euler,
// Rot_matrix, x_aposteriori, P_aposteriori);
attitudeKalmanfilter(update_vect, dt, z_k, x_aposteriori_k, P_aposteriori_k, q, r,
euler, Rot_matrix, x_aposteriori, P_aposteriori);
/* swap values for next iteration */
memcpy(P_aposteriori_k, P_aposteriori, sizeof(P_aposteriori_k));
memcpy(x_aposteriori_k, x_aposteriori, sizeof(x_aposteriori_k));
uint64_t timing_diff = hrt_absolute_time() - timing_start;
// /* print rotation matrix every 200th time */
if (printcounter % 200 == 0) {
// printf("x apo:\n%8.4f\t%8.4f\t%8.4f\n%8.4f\t%8.4f\t%8.4f\n%8.4f\t%8.4f\t%8.4f\n",
// x_aposteriori[0], x_aposteriori[1], x_aposteriori[2],
// x_aposteriori[3], x_aposteriori[4], x_aposteriori[5],
// x_aposteriori[6], x_aposteriori[7], x_aposteriori[8]);
// }
printf("EKF attitude iteration: %d, runtime: %d us, dt: %d us (%d Hz)\n", loopcounter, (int)timing_diff, (int)(dt * 1000000.0f), (int)(1.0f / dt));
printf("roll: %8.4f\tpitch: %8.4f\tyaw:%8.4f\n", (double)euler[0], (double)euler[1], (double)euler[2]);
printf("update rates gyro: %8.4f\taccel: %8.4f\tmag:%8.4f\n", (double)sensor_update_hz[0], (double)sensor_update_hz[1], (double)sensor_update_hz[2]);
// printf("\n%d\t%d\t%d\n%d\t%d\t%d\n%d\t%d\t%d\n", (int)(Rot_matrix[0] * 100), (int)(Rot_matrix[1] * 100), (int)(Rot_matrix[2] * 100),
// (int)(Rot_matrix[3] * 100), (int)(Rot_matrix[4] * 100), (int)(Rot_matrix[5] * 100),
// (int)(Rot_matrix[6] * 100), (int)(Rot_matrix[7] * 100), (int)(Rot_matrix[8] * 100));
}
// int i = printcounter % 9;
// // for (int i = 0; i < 9; i++) {
// char name[10];
// sprintf(name, "xapo #%d", i);
// memcpy(dbg.key, name, sizeof(dbg.key));
// dbg.value = x_aposteriori[i];
// orb_publish(ORB_ID(debug_key_value), pub_dbg, &dbg);
printcounter++;
if (last_data > 0 && raw.timestamp - last_data > 12000) printf("[attitude estimator ekf] sensor data missed! (%llu)\n", raw.timestamp - last_data);
last_data = raw.timestamp;
/* send out */
att.timestamp = raw.timestamp;
att.roll = euler[0];
att.pitch = euler[1];
att.yaw = euler[2];
att.rollspeed = x_aposteriori[0];
att.pitchspeed = x_aposteriori[1];
att.yawspeed = x_aposteriori[2];
/* copy offsets */
memcpy(&att.rate_offsets, &(x_aposteriori[3]), sizeof(att.rate_offsets));
/* copy rotation matrix */
memcpy(&att.R, Rot_matrix, sizeof(Rot_matrix));
att.R_valid = true;
// Broadcast
orb_publish(ORB_ID(vehicle_attitude), pub_att, &att);
}
loopcounter++;

131
apps/attitude_estimator_ekf/attitude_estimator_ekf_params.c Normal file
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@ -0,0 +1,131 @@
/****************************************************************************
*
* Copyright (C) 2012 PX4 Development Team. All rights reserved.
* Author: Tobias Naegeli <naegelit@student.ethz.ch>
* Lorenz Meier <lm@inf.ethz.ch>
*
* 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 attitude_estimator_ekf_params.c
*
* Parameters for EKF filter
*/
#include "attitude_estimator_ekf_params.h"
/* Extended Kalman Filter covariances */
/* gyro process noise */
PARAM_DEFINE_FLOAT(EKF_ATT_Q0, 1e1f);
PARAM_DEFINE_FLOAT(EKF_ATT_Q1, 1e1f);
PARAM_DEFINE_FLOAT(EKF_ATT_Q2, 1e1f);
/* gyro offsets process noise */
PARAM_DEFINE_FLOAT(EKF_ATT_Q3, 1e-4f);
PARAM_DEFINE_FLOAT(EKF_ATT_Q4, 1e-4f);
PARAM_DEFINE_FLOAT(EKF_ATT_Q5, 1e-4f);
/* accelerometer process noise */
PARAM_DEFINE_FLOAT(EKF_ATT_Q6, 1e-1f);
PARAM_DEFINE_FLOAT(EKF_ATT_Q7, 1e-1f);
PARAM_DEFINE_FLOAT(EKF_ATT_Q8, 1e-1f);
/* magnetometer process noise */
PARAM_DEFINE_FLOAT(EKF_ATT_Q9, 1e-1f);
PARAM_DEFINE_FLOAT(EKF_ATT_Q10, 1e-1f);
PARAM_DEFINE_FLOAT(EKF_ATT_Q11, 1e-1f);
/* gyro measurement noise */
PARAM_DEFINE_FLOAT(EKF_ATT_R0, 1e-2f);
PARAM_DEFINE_FLOAT(EKF_ATT_R1, 1e-2f);
PARAM_DEFINE_FLOAT(EKF_ATT_R2, 1e-2f);
/* accelerometer measurement noise */
PARAM_DEFINE_FLOAT(EKF_ATT_R3, 1e-1f);
PARAM_DEFINE_FLOAT(EKF_ATT_R4, 1e-1f);
PARAM_DEFINE_FLOAT(EKF_ATT_R5, 1e-1f);
/* magnetometer measurement noise */
PARAM_DEFINE_FLOAT(EKF_ATT_R6, 1e-1f);
PARAM_DEFINE_FLOAT(EKF_ATT_R7, 1e-1f);
PARAM_DEFINE_FLOAT(EKF_ATT_R8, 1e-1f);
int parameters_init(struct attitude_estimator_ekf_param_handles *h)
{
/* PID parameters */
h->q0 = param_find("EKF_ATT_Q0");
h->q1 = param_find("EKF_ATT_Q1");
h->q2 = param_find("EKF_ATT_Q2");
h->q3 = param_find("EKF_ATT_Q3");
h->q4 = param_find("EKF_ATT_Q4");
h->q5 = param_find("EKF_ATT_Q5");
h->q6 = param_find("EKF_ATT_Q6");
h->q7 = param_find("EKF_ATT_Q7");
h->q8 = param_find("EKF_ATT_Q8");
h->q9 = param_find("EKF_ATT_Q9");
h->q10 = param_find("EKF_ATT_Q10");
h->q11 = param_find("EKF_ATT_Q11");
h->r0 = param_find("EKF_ATT_R0");
h->r1 = param_find("EKF_ATT_R1");
h->r2 = param_find("EKF_ATT_R2");
h->r3 = param_find("EKF_ATT_R3");
h->r4 = param_find("EKF_ATT_R4");
h->r5 = param_find("EKF_ATT_R5");
h->r6 = param_find("EKF_ATT_R6");
h->r7 = param_find("EKF_ATT_R7");
h->r8 = param_find("EKF_ATT_R8");
return OK;
}
int parameters_update(const struct attitude_estimator_ekf_param_handles *h, struct attitude_estimator_ekf_params *p)
{
param_get(h->q0, &(p->q[0]));
param_get(h->q1, &(p->q[1]));
param_get(h->q2, &(p->q[2]));
param_get(h->q3, &(p->q[3]));
param_get(h->q4, &(p->q[4]));
param_get(h->q5, &(p->q[5]));
param_get(h->q6, &(p->q[6]));
param_get(h->q7, &(p->q[7]));
param_get(h->q8, &(p->q[8]));
param_get(h->q9, &(p->q[9]));
param_get(h->q10, &(p->q[10]));
param_get(h->q11, &(p->q[11]));
param_get(h->r0, &(p->r[0]));
param_get(h->r1, &(p->r[1]));
param_get(h->r2, &(p->r[2]));
param_get(h->r3, &(p->r[3]));
param_get(h->r4, &(p->r[4]));
param_get(h->r5, &(p->r[5]));
param_get(h->r6, &(p->r[6]));
param_get(h->r7, &(p->r[7]));
param_get(h->r8, &(p->r[8]));
return OK;
}

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/****************************************************************************
*
* Copyright (C) 2012 PX4 Development Team. All rights reserved.
* Author: Tobias Naegeli <naegelit@student.ethz.ch>
* Lorenz Meier <lm@inf.ethz.ch>
*
* 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 attitude_estimator_ekf_params.h
*
* Parameters for EKF filter
*/
#include <systemlib/param/param.h>
struct attitude_estimator_ekf_params {
float r[9];
float q[12];
};
struct attitude_estimator_ekf_param_handles {
param_t r0, r1, r2, r3, r4, r5, r6, r7, r8;
param_t q0, q1, q2, q3, q4, q5, q6, q7, q8, q9, q10, q11;
};
/**
* Initialize all parameter handles and values
*
*/
int parameters_init(struct attitude_estimator_ekf_param_handles *h);
/**
* Update all parameters
*
*/
int parameters_update(const struct attitude_estimator_ekf_param_handles *h, struct attitude_estimator_ekf_params *p);