mirror of
https://gitee.com/mirrors_PX4/PX4-Autopilot.git
synced 2026-05-02 05:04:08 +08:00
added base class for data storage
This commit is contained in:
parent
83079e0e11
commit
144aa9c461
@ -42,5 +42,7 @@ px4_add_module(
|
||||
l1/ecl_l1_pos_controller.cpp
|
||||
validation/data_validator.cpp
|
||||
validation/data_validator_group.cpp
|
||||
EKF/estimator_base.cpp
|
||||
EKF/ekf.cpp
|
||||
)
|
||||
# vim: set noet ft=cmake fenc=utf-8 ff=unix :
|
||||
|
||||
110
EKF/RingBuffer.h
Normal file
110
EKF/RingBuffer.h
Normal file
@ -0,0 +1,110 @@
|
||||
/****************************************************************************
|
||||
*
|
||||
* Copyright (C) 2012 PX4 Development Team. All rights reserved.
|
||||
*
|
||||
* 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 RingBuffer.h
|
||||
* @author Roman Bapst <bapstroman@gmail.com>
|
||||
* Template RingBuffer.
|
||||
*/
|
||||
|
||||
template <typename data_type>
|
||||
class RingBuffer
|
||||
{
|
||||
public:
|
||||
RingBuffer() {_buffer = NULL;};
|
||||
~RingBuffer() {delete _buffer;}
|
||||
|
||||
bool allocate(unsigned size)
|
||||
{
|
||||
if (size == 0) {
|
||||
return false;
|
||||
}
|
||||
|
||||
_buffer = new data_type[size];
|
||||
|
||||
if (_buffer == NULL) {
|
||||
return false;
|
||||
}
|
||||
|
||||
_size = size;
|
||||
return true;
|
||||
}
|
||||
|
||||
inline void push(data_type sample)
|
||||
{
|
||||
_buffer[_head] = sample;
|
||||
_head = (_head + 1) % _size;
|
||||
|
||||
// move tail if we overwrite it
|
||||
if (_head == _tail && _size > 1) {
|
||||
_tail = (_tail + 1) % _size;
|
||||
}
|
||||
}
|
||||
|
||||
inline data_type get_oldest()
|
||||
{
|
||||
return _buffer[_tail];
|
||||
}
|
||||
|
||||
inline bool pop_first_older_than(uint64_t timestamp, data_type &sample)
|
||||
{
|
||||
// start looking from oldest data of buffer
|
||||
for (unsigned i = 0; i < _size; i++) {
|
||||
unsigned index = (_tail + i) % _size;
|
||||
|
||||
if (timestamp >= _buffer[index].time_us) {
|
||||
sample = _buffer[_tail + i];
|
||||
// now we can set the tail to the item
|
||||
// which comes after the one we removed
|
||||
_tail = (_tail + i + 1);
|
||||
return true;
|
||||
}
|
||||
|
||||
if (index == _head) {
|
||||
// we have reached the head and haven't found anything
|
||||
return false;
|
||||
}
|
||||
}
|
||||
|
||||
return false;
|
||||
}
|
||||
|
||||
data_type &operator[](unsigned index)
|
||||
{
|
||||
return _buffer[index];
|
||||
}
|
||||
|
||||
private:
|
||||
data_type *_buffer;
|
||||
unsigned _head, _tail, _size;
|
||||
};
|
||||
98
EKF/ekf.cpp
Normal file
98
EKF/ekf.cpp
Normal file
@ -0,0 +1,98 @@
|
||||
/****************************************************************************
|
||||
*
|
||||
* Copyright (c) 2013 Estimation and Control Library (ECL). All rights reserved.
|
||||
*
|
||||
* 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 ECL 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 ekf.cpp
|
||||
* Definition of ekf attitude position estimator class.
|
||||
*
|
||||
* @author Roman Bast <bastroman@gmail.com>
|
||||
*
|
||||
*/
|
||||
|
||||
#include "ekf.h"
|
||||
|
||||
Ekf::Ekf()
|
||||
{
|
||||
|
||||
}
|
||||
|
||||
|
||||
Ekf::~Ekf()
|
||||
{
|
||||
|
||||
}
|
||||
|
||||
void Ekf::update()
|
||||
{
|
||||
if (!_filter_initialised) {
|
||||
_filter_initialised = initialiseFilter();
|
||||
}
|
||||
|
||||
if (!_filter_initialised) {
|
||||
return;
|
||||
}
|
||||
|
||||
// prediction
|
||||
if (_imu_updated) {
|
||||
predictState();
|
||||
predictCovariance();
|
||||
_imu_updated = false;
|
||||
}
|
||||
|
||||
// measurement updates
|
||||
if (_mag_buffer.pop_first_older_than(_imu_sample_delayed.time_us, _mag_sample_delayed)) {
|
||||
fuseMag();
|
||||
}
|
||||
|
||||
if (_baro_buffer.pop_first_older_than(_imu_sample_delayed.time_us, _baro_sample_delayed)) {
|
||||
_fuse_height = true;
|
||||
}
|
||||
|
||||
if (_gps_buffer.pop_first_older_than(_imu_sample_delayed.time_us, _gps_sample_delayed)) {
|
||||
_fuse_pos = true;
|
||||
_fuse_vel = true;
|
||||
}
|
||||
|
||||
if (_fuse_height || _fuse_pos || _fuse_vel) {
|
||||
fusePosVel();
|
||||
}
|
||||
|
||||
if (_range_buffer.pop_first_older_than(_imu_sample_delayed.time_us, _range_sample_delayed)) {
|
||||
fuseRange();
|
||||
}
|
||||
|
||||
if (_airspeed_buffer.pop_first_older_than(_imu_sample_delayed.time_us, _airspeed_sample_delayed)) {
|
||||
fuseAirspeed();
|
||||
}
|
||||
|
||||
}
|
||||
76
EKF/ekf.h
Normal file
76
EKF/ekf.h
Normal file
@ -0,0 +1,76 @@
|
||||
/****************************************************************************
|
||||
*
|
||||
* Copyright (c) 2013 Estimation and Control Library (ECL). All rights reserved.
|
||||
*
|
||||
* 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 ECL 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 ekf.h
|
||||
* Definition of ekf attitude position estimator class.
|
||||
*
|
||||
* @author Roman Bast <bastroman@gmail.com>
|
||||
*
|
||||
*/
|
||||
|
||||
#include "estimator_base.h"
|
||||
|
||||
class Ekf : public EstimatorBase
|
||||
{
|
||||
public:
|
||||
|
||||
Ekf();
|
||||
~Ekf();
|
||||
|
||||
void update();
|
||||
|
||||
private:
|
||||
|
||||
bool _filter_initialised;
|
||||
|
||||
bool _fuse_height; // true if there is new baro data
|
||||
bool _fuse_pos; // true if there is new position data from gps
|
||||
bool _fuse_vel; // true if there is new velocity data from gps
|
||||
|
||||
bool initialiseFilter(void);
|
||||
|
||||
void predictState();
|
||||
|
||||
void predictCovariance();
|
||||
|
||||
void fusePosVel();
|
||||
|
||||
void fuseMag();
|
||||
|
||||
void fuseAirspeed();
|
||||
|
||||
void fuseRange();
|
||||
|
||||
|
||||
};
|
||||
403
EKF/estimator_base.cpp
Normal file
403
EKF/estimator_base.cpp
Normal file
@ -0,0 +1,403 @@
|
||||
/****************************************************************************
|
||||
*
|
||||
* Copyright (c) 2013 Estimation and Control Library (ECL). All rights reserved.
|
||||
*
|
||||
* 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 ECL 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 estimator_base.cpp
|
||||
* Definition of base class for attitude estimators
|
||||
*
|
||||
* @author Roman Bast <bastroman@gmail.com>
|
||||
*
|
||||
*/
|
||||
|
||||
#include <math.h>
|
||||
#include "estimator_base.h"
|
||||
#include <mathlib/mathlib.h>
|
||||
|
||||
|
||||
EstimatorBase::EstimatorBase()
|
||||
{
|
||||
}
|
||||
|
||||
EstimatorBase::~EstimatorBase()
|
||||
{
|
||||
|
||||
}
|
||||
|
||||
// read integrated imu data and store to buffer
|
||||
void EstimatorBase::setIMUData(uint64_t time_usec, uint64_t delta_ang_dt, uint64_t delta_vel_dt, float *delta_ang,
|
||||
float *delta_vel)
|
||||
{
|
||||
if (!_initialised) {
|
||||
initialiseVariables(time_usec);
|
||||
_initialised = true;
|
||||
_start_predict_enabled = true;
|
||||
}
|
||||
|
||||
float dt = (float)(time_usec - _time_last_imu) / 1000 / 1000;
|
||||
dt = math::max(dt, 1.0e-4f);
|
||||
dt = math::min(dt, 0.02f);
|
||||
|
||||
_time_last_imu = time_usec;
|
||||
|
||||
if (_imu_time_last > 0) {
|
||||
_dt_imu_avg = 0.8f * _dt_imu_avg + 0.2f * dt;
|
||||
}
|
||||
|
||||
// copy data
|
||||
imuSample imu_sample_new = {};
|
||||
memcpy(&imu_sample_new.delta_ang._data[0], delta_ang, sizeof(imu_sample_new.delta_ang._data));
|
||||
memcpy(&imu_sample_new.delta_vel._data[0], delta_vel, sizeof(imu_sample_new.delta_vel._data));
|
||||
|
||||
imu_sample_new.delta_ang_dt = delta_ang_dt / 1e6f;
|
||||
imu_sample_new.delta_vel_dt = delta_vel_dt / 1e6f;
|
||||
|
||||
imu_sample_new.time_us = time_usec;
|
||||
|
||||
imu_sample_new.delta_ang(0) = imu_sample_new.delta_ang(0) * _state.gyro_scale(0);
|
||||
imu_sample_new.delta_ang(1) = imu_sample_new.delta_ang(1) * _state.gyro_scale(1);
|
||||
imu_sample_new.delta_ang(2) = imu_sample_new.delta_ang(2) * _state.gyro_scale(2);
|
||||
|
||||
imu_sample_new.delta_ang -= _state.gyro_bias;
|
||||
imu_sample_new.delta_vel(2) -= _state.accel_z_bias;
|
||||
|
||||
_imu_down_sampled.delta_ang_dt += imu_sample_new.delta_ang_dt;
|
||||
_imu_down_sampled.delta_vel_dt += imu_sample_new.delta_vel_dt;
|
||||
|
||||
|
||||
Quaternion delta_q;
|
||||
delta_q.rotate(imu_sample_new.delta_ang);
|
||||
_q_down_sampled = _q_down_sampled * delta_q;
|
||||
_q_down_sampled.normalize();
|
||||
|
||||
matrix::Dcm<float> delta_R(delta_q.inversed());
|
||||
_imu_down_sampled.delta_vel = delta_R * _imu_down_sampled.delta_vel;
|
||||
_imu_down_sampled.delta_vel += imu_sample_new.delta_vel;
|
||||
|
||||
_imu_ticks++;
|
||||
|
||||
if ((_dt_imu_avg * _imu_ticks >= (float)(FILTER_UPDATE_PERRIOD_MS) / 1000 && _start_predict_enabled)
|
||||
|| (_dt_imu_avg * _imu_ticks >= 0.02f)) {
|
||||
_imu_down_sampled.delta_ang = _q_down_sampled.to_axis_angle();
|
||||
_imu_down_sampled.time_us = time_usec;
|
||||
|
||||
_imu_buffer.push(_imu_down_sampled);
|
||||
|
||||
_imu_down_sampled.delta_ang.setZero();
|
||||
_imu_down_sampled.delta_vel.setZero();
|
||||
_imu_down_sampled.delta_ang_dt = 0.0f;
|
||||
_imu_down_sampled.delta_vel_dt = 0.0f;
|
||||
_q_down_sampled(0) = 1.0f;
|
||||
_q_down_sampled(1) = _q_down_sampled(2) = _q_down_sampled(3) = 0.0f;
|
||||
|
||||
_imu_ticks = 0;
|
||||
|
||||
_imu_updated = true;
|
||||
|
||||
} else {
|
||||
|
||||
_imu_updated = false;
|
||||
}
|
||||
|
||||
|
||||
_imu_sample_delayed = _imu_buffer.get_oldest();
|
||||
}
|
||||
|
||||
|
||||
void EstimatorBase::setMagData(uint64_t time_usec, float *data)
|
||||
{
|
||||
|
||||
|
||||
if (time_usec - _time_last_mag > 70000) {
|
||||
|
||||
magSample mag_sample_new = {};
|
||||
mag_sample_new.time_us = time_usec - _params.mag_delay_ms * 1000;
|
||||
|
||||
|
||||
mag_sample_new.time_us -= FILTER_UPDATE_PERRIOD_MS * 1000 / 2;
|
||||
_time_last_mag = mag_sample_new.time_us;
|
||||
|
||||
|
||||
memcpy(&mag_sample_new.mag._data[0], data, sizeof(mag_sample_new.mag._data));
|
||||
|
||||
_mag_buffer.push(mag_sample_new);
|
||||
}
|
||||
}
|
||||
|
||||
void EstimatorBase::setGpsData(uint64_t time_usec, struct gps_message *gps)
|
||||
{
|
||||
|
||||
if (!_gps_initialised) {
|
||||
initialiseGPS(gps);
|
||||
return;
|
||||
}
|
||||
|
||||
|
||||
if (time_usec - _time_last_gps > 70000 && gps_is_good(gps)) {
|
||||
|
||||
gpsSample gps_sample_new = {};
|
||||
gps_sample_new.time_us = time_usec - _params.gps_delay_ms * 1000;
|
||||
|
||||
|
||||
gps_sample_new.time_us -= FILTER_UPDATE_PERRIOD_MS * 1000 / 2;
|
||||
_time_last_gps = gps_sample_new.time_us;
|
||||
|
||||
gps_sample_new.time_us = math::max(gps_sample_new.time_us, _imu_sample_delayed.time_us);
|
||||
|
||||
|
||||
memcpy(gps_sample_new.vel._data[0], gps->vel_ned, sizeof(gps_sample_new.vel._data));
|
||||
|
||||
_gps_speed_valid = gps->vel_ned_valid;
|
||||
|
||||
|
||||
float lpos_x = 0.0f;
|
||||
float lpos_y = 0.0f;
|
||||
map_projection_project(&_posRef, (gps->lat / 1.0e7), (gps->lon / 1.0e7), &lpos_x, &lpos_y);
|
||||
gps_sample_new.pos(0) = lpos_x;
|
||||
gps_sample_new.pos(1) = lpos_y;
|
||||
gps_sample_new.hgt = gps->alt / 1e3f;
|
||||
|
||||
_gps_buffer.push(gps_sample_new);
|
||||
}
|
||||
}
|
||||
|
||||
void EstimatorBase::setBaroData(uint64_t time_usec, float *data)
|
||||
{
|
||||
if (time_usec - _time_last_baro > 70000) {
|
||||
|
||||
baroSample baro_sample_new;
|
||||
baro_sample_new.hgt = *data;
|
||||
baro_sample_new.time_us = time_usec - _params.baro_delay_ms * 1000;
|
||||
|
||||
baro_sample_new.time_us -= FILTER_UPDATE_PERRIOD_MS * 1000 / 2;
|
||||
_time_last_baro = baro_sample_new.time_us;
|
||||
|
||||
baro_sample_new.time_us = math::max(baro_sample_new.time_us, _imu_sample_delayed.time_us);
|
||||
|
||||
_baro_buffer.push(baro_sample_new);
|
||||
}
|
||||
}
|
||||
|
||||
void EstimatorBase::setAirspeedData(uint64_t time_usec, float *data)
|
||||
{
|
||||
if (time_usec > _time_last_airspeed) {
|
||||
airspeedSample airspeed_sample_new;
|
||||
airspeed_sample_new.airspeed = *data;
|
||||
airspeed_sample_new.time_us -= _params.airspeed_delay_ms * 1000;
|
||||
|
||||
airspeed_sample_new.time_us = time_usec -= FILTER_UPDATE_PERRIOD_MS * 1000 / 2;
|
||||
_time_last_airspeed = airspeed_sample_new.time_us;
|
||||
|
||||
_airspeed_buffer.push(airspeed_sample_new);
|
||||
}
|
||||
}
|
||||
|
||||
// set range data
|
||||
void EstimatorBase::setRangeData(uint64_t time_usec, float *data)
|
||||
{
|
||||
|
||||
}
|
||||
|
||||
// set optical flow data
|
||||
void EstimatorBase::setOpticalFlowData(uint64_t time_usec, float *data)
|
||||
{
|
||||
|
||||
}
|
||||
|
||||
void EstimatorBase::initialiseVariables(uint64_t time_usec)
|
||||
{
|
||||
_imu_buffer.allocate(IMU_BUFFER_LENGTH);
|
||||
_gps_buffer.allocate(OBS_BUFFER_LENGTH);
|
||||
_mag_buffer.allocate(OBS_BUFFER_LENGTH);
|
||||
_baro_buffer.allocate(OBS_BUFFER_LENGTH);
|
||||
_range_buffer.allocate(OBS_BUFFER_LENGTH);
|
||||
_airspeed_buffer.allocate(OBS_BUFFER_LENGTH);
|
||||
_flow_buffer.allocate(OBS_BUFFER_LENGTH);
|
||||
_output_buffer.allocate(IMU_BUFFER_LENGTH);
|
||||
|
||||
_state.ang_error.setZero();
|
||||
_state.vel.setZero();
|
||||
_state.pos.setZero();
|
||||
_state.gyro_bias.setZero();
|
||||
_state.gyro_scale(0) = 1.0f;
|
||||
_state.gyro_scale(1) = 1.0f;
|
||||
_state.gyro_scale(2) = 1.0f;
|
||||
_state.accel_z_bias = 0.0f;
|
||||
_state.mag_I.setZero();
|
||||
_state.mag_B.setZero();
|
||||
_state.wind_vel.setZero();
|
||||
_state.quat_nominal.setZero();
|
||||
_state.quat_nominal(0) = 1.0f;
|
||||
|
||||
_params.mag_delay_ms = 0;
|
||||
_params.baro_delay_ms = 0;
|
||||
_params.gps_delay_ms = 0;
|
||||
_params.airspeed_delay_ms = 0;
|
||||
_params.requiredEph = 10;
|
||||
_params.requiredEpv = 10;
|
||||
|
||||
_dt_imu_avg = 0.0f;
|
||||
_imu_time_last = time_usec;
|
||||
|
||||
_imu_sample_delayed.delta_ang.setZero();
|
||||
_imu_sample_delayed.delta_vel.setZero();
|
||||
_imu_sample_delayed.delta_ang_dt = 0.0f;
|
||||
_imu_sample_delayed.delta_vel_dt = 0.0f;
|
||||
_imu_sample_delayed.time_us = time_usec;
|
||||
|
||||
_imu_down_sampled.delta_ang.setZero();
|
||||
_imu_down_sampled.delta_vel.setZero();
|
||||
_imu_down_sampled.delta_ang_dt = 0.0f;
|
||||
_imu_down_sampled.delta_vel_dt = 0.0f;
|
||||
_imu_down_sampled.time_us = time_usec;
|
||||
|
||||
_q_down_sampled(0) = 1.0f;
|
||||
_q_down_sampled(1) = 0.0f;
|
||||
_q_down_sampled(2) = 0.0f;
|
||||
_q_down_sampled(3) = 0.0f;
|
||||
|
||||
_imu_ticks = 0;
|
||||
|
||||
_imu_updated = false;
|
||||
_start_predict_enabled = false;
|
||||
_initialised = false;
|
||||
_gps_initialised = false;
|
||||
_gps_speed_valid = false;
|
||||
|
||||
_time_last_imu = 0;
|
||||
_time_last_gps = 0;
|
||||
_time_last_mag = 0;
|
||||
_time_last_baro = 0;
|
||||
_time_last_range = 0;
|
||||
_time_last_airspeed = 0;
|
||||
|
||||
}
|
||||
|
||||
void EstimatorBase::initialiseGPS(struct gps_message *gps)
|
||||
{
|
||||
//Check if the GPS fix is good enough for us to use
|
||||
if (gps_is_good(gps)) {
|
||||
printf("gps is good\n");
|
||||
// Initialise projection
|
||||
double lat = gps->lat / 1.0e7;
|
||||
double lon = gps->lon / 1.0e7;
|
||||
map_projection_init(&_posRef, lat, lon);
|
||||
_gps_alt_ref = gps->alt / 1e3f;
|
||||
_gps_initialised = true;
|
||||
}
|
||||
}
|
||||
|
||||
bool EstimatorBase::gps_is_good(struct gps_message *gps)
|
||||
{
|
||||
// go through apm implementation of calcGpsGoodToAlign for fancier checks
|
||||
if ((gps->fix_type >= 3) && (gps->eph < _params.requiredEph) && (gps->epv < _params.requiredEpv)) {
|
||||
return true;
|
||||
|
||||
} else {
|
||||
return false;
|
||||
}
|
||||
}
|
||||
|
||||
void EstimatorBase::printStoredIMU()
|
||||
{
|
||||
printf("---------Printing IMU data buffer------------\n");
|
||||
|
||||
for (int i = 0; i < IMU_BUFFER_LENGTH; i++) {
|
||||
printIMU(&_imu_buffer[i]);
|
||||
}
|
||||
}
|
||||
|
||||
void EstimatorBase::printIMU(struct imuSample *data)
|
||||
{
|
||||
printf("time %i\n", data->time_us);
|
||||
printf("delta_ang_dt %.5f\n", (double)data->delta_ang_dt);
|
||||
printf("delta_vel_dt %.5f\n", (double)data->delta_vel_dt);
|
||||
printf("dA: %.5f %.5f %.5f \n", (double)data->delta_ang(0), (double)data->delta_ang(1), (double)data->delta_ang(2));
|
||||
printf("dV: %.5f %.5f %.5f \n\n", (double)data->delta_vel(0), (double)data->delta_vel(1), (double)data->delta_vel(2));
|
||||
}
|
||||
|
||||
void EstimatorBase::printQuaternion(Quaternion &q)
|
||||
{
|
||||
printf("q1 %.5f q2 %.5f q3 %.5f q4 %.5f\n", (double)q(0), (double)q(1), (double)q(2), (double)q(3));
|
||||
}
|
||||
|
||||
void EstimatorBase::print_imu_avg_time()
|
||||
{
|
||||
printf("dt_avg: %.5f\n", (double)_dt_imu_avg);
|
||||
}
|
||||
|
||||
void EstimatorBase::printStoredMag()
|
||||
{
|
||||
printf("---------Printing mag data buffer------------\n");
|
||||
|
||||
for (int i = 0; i < OBS_BUFFER_LENGTH; i++) {
|
||||
printMag(&_mag_buffer[i]);
|
||||
}
|
||||
}
|
||||
|
||||
void EstimatorBase::printMag(struct magSample *data)
|
||||
{
|
||||
printf("time %i\n", data->time_us);
|
||||
printf("mag: %.5f %.5f %.5f \n\n", (double)data->mag(0), (double)data->mag(1), (double)data->mag(2));
|
||||
|
||||
}
|
||||
|
||||
void EstimatorBase::printBaro(struct baroSample *data)
|
||||
{
|
||||
printf("time %i\n", data->time_us);
|
||||
printf("baro: %.5f\n\n", (double)data->hgt);
|
||||
}
|
||||
|
||||
void EstimatorBase::printStoredBaro()
|
||||
{
|
||||
printf("---------Printing baro data buffer------------\n");
|
||||
|
||||
for (int i = 0; i < OBS_BUFFER_LENGTH; i++) {
|
||||
printBaro(&_baro_buffer[i]);
|
||||
}
|
||||
}
|
||||
|
||||
void EstimatorBase::printGps(struct gpsSample *data)
|
||||
{
|
||||
printf("time %i\n", data->time_us);
|
||||
printf("gps pos: %.5f %.5f %.5f\n", (double)data->pos(0), (double)data->pos(1), (double)data->hgt);
|
||||
printf("gps vel %.5f %.5f %.5f\n\n", (double)data->vel(0), (double)data->vel(1), (double)data->vel(2));
|
||||
}
|
||||
|
||||
void EstimatorBase::printStoredGps()
|
||||
{
|
||||
printf("---------Printing GPS data buffer------------\n");
|
||||
|
||||
for (int i = 0; i < OBS_BUFFER_LENGTH; i++) {
|
||||
printGps(&_gps_buffer[i]);
|
||||
}
|
||||
}
|
||||
231
EKF/estimator_base.h
Normal file
231
EKF/estimator_base.h
Normal file
@ -0,0 +1,231 @@
|
||||
/****************************************************************************
|
||||
*
|
||||
* Copyright (c) 2013 Estimation and Control Library (ECL). All rights reserved.
|
||||
*
|
||||
* 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 ECL 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 estimator_base.h
|
||||
* Definition of base class for attitude estimators
|
||||
*
|
||||
* @author Roman Bast <bastroman@gmail.com>
|
||||
*
|
||||
*/
|
||||
|
||||
#include <stdint.h>
|
||||
#include <matrix/matrix/math.hpp>
|
||||
#include <lib/geo/geo.h>
|
||||
#include "RingBuffer.h"
|
||||
|
||||
struct gps_message {
|
||||
uint64_t time_usec;
|
||||
int32_t lat; // Latitude in 1E-7 degrees
|
||||
int32_t lon; // Longitude in 1E-7 degrees
|
||||
int32_t alt; // Altitude in 1E-3 meters (millimeters) above MSL
|
||||
uint8_t fix_type; // 0-1: no fix, 2: 2D fix, 3: 3D fix, 4: RTCM code differential, 5: Real-Time
|
||||
float eph; // GPS HDOP horizontal dilution of position in m
|
||||
float epv; // GPS VDOP horizontal dilution of position in m
|
||||
uint64_t time_usec_vel; // Timestamp for velocity informations
|
||||
float vel_m_s; // GPS ground speed (m/s)
|
||||
float vel_ned[3]; // GPS ground speed NED
|
||||
bool vel_ned_valid; // GPS ground speed is valid
|
||||
};
|
||||
|
||||
class EstimatorBase
|
||||
{
|
||||
public:
|
||||
EstimatorBase();
|
||||
~EstimatorBase();
|
||||
|
||||
// set delta angle imu data
|
||||
void setIMUData(uint64_t time_usec, uint64_t delta_ang_dt, uint64_t delta_vel_dt, float *delta_ang, float *delta_vel);
|
||||
|
||||
// set magnetometer data
|
||||
void setMagData(uint64_t time_usec, float *data);
|
||||
|
||||
// set gps data
|
||||
void setGpsData(uint64_t time_usec, struct gps_message *gps);
|
||||
|
||||
// set baro data
|
||||
void setBaroData(uint64_t time_usec, float *data);
|
||||
|
||||
// set airspeed data
|
||||
void setAirspeedData(uint64_t time_usec, float *data);
|
||||
|
||||
// set range data
|
||||
void setRangeData(uint64_t time_usec, float *data);
|
||||
|
||||
// set optical flow data
|
||||
void setOpticalFlowData(uint64_t time_usec, float *data);
|
||||
|
||||
protected:
|
||||
|
||||
typedef matrix::Vector<float, 2> Vector2f;
|
||||
typedef matrix::Vector<float, 3> Vector3f;
|
||||
typedef matrix::Quaternion<float> Quaternion;
|
||||
typedef matrix::Matrix<float, 3, 3> Matrix3f;
|
||||
|
||||
struct stateSample {
|
||||
Vector3f ang_error;
|
||||
Vector3f vel;
|
||||
Vector3f pos;
|
||||
Vector3f gyro_bias;
|
||||
Vector3f gyro_scale;
|
||||
float accel_z_bias;
|
||||
Vector3f mag_I;
|
||||
Vector3f mag_B;
|
||||
Vector2f wind_vel;
|
||||
Quaternion quat_nominal;
|
||||
} _state;
|
||||
|
||||
struct outputSample {
|
||||
Quaternion quat_nominal;
|
||||
Vector3f vel;
|
||||
Vector3f pos;
|
||||
};
|
||||
|
||||
struct imuSample {
|
||||
Vector3f delta_ang;
|
||||
Vector3f delta_vel;
|
||||
float delta_ang_dt;
|
||||
float delta_vel_dt;
|
||||
uint32_t time_us;
|
||||
};
|
||||
|
||||
struct gpsSample {
|
||||
Vector2f pos;
|
||||
float hgt;
|
||||
Vector3f vel;
|
||||
uint32_t time_us;
|
||||
};
|
||||
|
||||
struct magSample {
|
||||
Vector3f mag;
|
||||
uint32_t time_us;
|
||||
};
|
||||
|
||||
struct baroSample {
|
||||
float hgt;
|
||||
uint32_t time_us;
|
||||
};
|
||||
|
||||
struct rangeSample {
|
||||
float rng;
|
||||
uint32_t time_us;
|
||||
};
|
||||
|
||||
struct airspeedSample {
|
||||
float airspeed;
|
||||
uint32_t time_us;
|
||||
};
|
||||
|
||||
struct flowSample {
|
||||
Vector2f flowRadXY;
|
||||
Vector2f flowRadXYcomp;
|
||||
uint32_t time_us;
|
||||
};
|
||||
|
||||
struct {
|
||||
uint32_t mag_delay_ms;
|
||||
uint32_t baro_delay_ms;
|
||||
uint32_t gps_delay_ms;
|
||||
uint32_t airspeed_delay_ms;
|
||||
float requiredEph;
|
||||
float requiredEpv;
|
||||
} _params;
|
||||
|
||||
|
||||
static const uint8_t OBS_BUFFER_LENGTH = 5;
|
||||
static const uint8_t IMU_BUFFER_LENGTH = 25;
|
||||
static const unsigned FILTER_UPDATE_PERRIOD_MS = 10;
|
||||
|
||||
float _dt_imu_avg;
|
||||
uint32_t _imu_time_last;
|
||||
|
||||
imuSample _imu_sample_delayed;
|
||||
imuSample _imu_down_sampled;
|
||||
Quaternion
|
||||
_q_down_sampled;
|
||||
|
||||
magSample _mag_sample_delayed;
|
||||
baroSample _baro_sample_delayed;
|
||||
gpsSample _gps_sample_delayed;
|
||||
rangeSample _range_sample_delayed;
|
||||
airspeedSample _airspeed_sample_delayed;
|
||||
flowSample _flow_sample_delayed;
|
||||
|
||||
struct map_projection_reference_s _posRef;
|
||||
float _gps_alt_ref;
|
||||
|
||||
|
||||
uint32_t _imu_ticks;
|
||||
|
||||
bool _imu_updated;
|
||||
bool _start_predict_enabled;
|
||||
bool _initialised;
|
||||
bool _gps_initialised;
|
||||
bool _gps_speed_valid;
|
||||
|
||||
RingBuffer<imuSample> _imu_buffer;
|
||||
RingBuffer<gpsSample> _gps_buffer;
|
||||
RingBuffer<magSample> _mag_buffer;
|
||||
RingBuffer<baroSample> _baro_buffer;
|
||||
RingBuffer<rangeSample> _range_buffer;
|
||||
RingBuffer<airspeedSample> _airspeed_buffer;
|
||||
RingBuffer<flowSample> _flow_buffer;
|
||||
RingBuffer<outputSample> _output_buffer;
|
||||
|
||||
uint64_t _time_last_imu;
|
||||
uint64_t _time_last_gps;
|
||||
uint64_t _time_last_mag;
|
||||
uint64_t _time_last_baro;
|
||||
uint64_t _time_last_range;
|
||||
uint64_t _time_last_airspeed;
|
||||
|
||||
|
||||
void initialiseVariables(uint64_t timestamp);
|
||||
|
||||
void initialiseGPS(struct gps_message *gps);
|
||||
|
||||
bool gps_is_good(struct gps_message *gps);
|
||||
|
||||
public:
|
||||
void printIMU(struct imuSample *data);
|
||||
void printStoredIMU();
|
||||
void printQuaternion(Quaternion &q);
|
||||
void print_imu_avg_time();
|
||||
void printMag(struct magSample *data);
|
||||
void printStoredMag();
|
||||
void printBaro(struct baroSample *data);
|
||||
void printStoredBaro();
|
||||
void printGps(struct gpsSample *data);
|
||||
void printStoredGps();
|
||||
};
|
||||
|
||||
44
EKF/tests/base/CMakeLists.txt
Normal file
44
EKF/tests/base/CMakeLists.txt
Normal file
@ -0,0 +1,44 @@
|
||||
############################################################################
|
||||
#
|
||||
# Copyright (c) 2015 ECL Development Team. All rights reserved.
|
||||
#
|
||||
# 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 ECL 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.
|
||||
#
|
||||
############################################################################
|
||||
px4_add_module(
|
||||
MODULE lib__ecl__EKF__tests__base
|
||||
MAIN base
|
||||
STACK 4096
|
||||
COMPILE_FLAGS
|
||||
-Os
|
||||
SRCS
|
||||
base.cpp
|
||||
DEPENDS
|
||||
platforms__common
|
||||
)
|
||||
# vim: set noet ft=cmake fenc=utf-8 ff=unix :
|
||||
150
EKF/tests/base/base.cpp
Normal file
150
EKF/tests/base/base.cpp
Normal file
@ -0,0 +1,150 @@
|
||||
/****************************************************************************
|
||||
*
|
||||
* Copyright (C) 2012 PX4 Development Team. All rights reserved.
|
||||
*
|
||||
* 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 base.cpp
|
||||
*
|
||||
* Tests for the estimator base class
|
||||
*/
|
||||
|
||||
#include <cstdio>
|
||||
#include <random>
|
||||
#include "../../estimator_base.h"
|
||||
|
||||
extern "C" __EXPORT int base_main(int argc, char *argv[]);
|
||||
|
||||
int base_main(int argc, char *argv[])
|
||||
{
|
||||
EstimatorBase *base = new EstimatorBase();
|
||||
|
||||
// Test1: feed in fake imu data and check if delta angles are summed correclty
|
||||
float delta_vel[3] = { 0.002f, 0.002f, 0.002f};
|
||||
float delta_ang[3] = { -0.1f, 0.2f, 0.3f};
|
||||
uint32_t time_usec = 1000;
|
||||
|
||||
|
||||
// simulate 400 Hz imu rate, filter should downsample to 100Hz
|
||||
// feed in 2 seconds of data
|
||||
for (int i = 0; i < 800; i++) {
|
||||
base->setIMUData(time_usec, 2500, 2500, delta_ang, delta_vel);
|
||||
time_usec += 2500;
|
||||
}
|
||||
|
||||
//base->printStoredIMU();
|
||||
|
||||
|
||||
// Test2: feed fake imu data and check average imu delta t
|
||||
// simulate 400 Hz imu rate, filter should downsample to 100Hz
|
||||
// feed in 2 seconds of data
|
||||
for (int i = 0; i < 800; i++) {
|
||||
base->setIMUData(time_usec, 2500, 2500, delta_ang, delta_vel);
|
||||
//base->print_imu_avg_time();
|
||||
time_usec += 2500;
|
||||
}
|
||||
|
||||
// Test3: feed in slow imu data, filter should now take every sample
|
||||
for (int i = 0; i < 800; i++) {
|
||||
base->setIMUData(time_usec, 2500, 2500, delta_ang, delta_vel);
|
||||
time_usec += 30000;
|
||||
}
|
||||
|
||||
//base->printStoredIMU();
|
||||
|
||||
// Test4: Feed in mag data at 50 Hz (too fast), check if filter samples correctly
|
||||
float mag[3] = {0.2f, 0.0f, 0.4f};
|
||||
|
||||
for (int i = 0; i < 100; i++) {
|
||||
base->setMagData(time_usec, mag);
|
||||
time_usec += 20000;
|
||||
}
|
||||
|
||||
//base->printStoredMag();
|
||||
|
||||
// Test5: Feed in baro data at 50 Hz (too fast), check if filter samples correctly
|
||||
float baro = 120.22f;;
|
||||
time_usec = 100000;
|
||||
|
||||
for (int i = 0; i < 100; i++) {
|
||||
base->setBaroData(time_usec, &baro);
|
||||
baro += 10.0f;
|
||||
time_usec += 20000;
|
||||
}
|
||||
|
||||
//base->printStoredBaro();
|
||||
|
||||
// Test 5: Run everything rogether in one run
|
||||
std::default_random_engine generator;
|
||||
std::uniform_int_distribution<int> distribution(-200, 200);
|
||||
|
||||
int imu_sample_period = 2500;
|
||||
uint64_t timer = 2000; // simulation start time
|
||||
uint64_t timer_last = timer;
|
||||
|
||||
float airspeed = 0.0f;
|
||||
|
||||
struct gps_message gps = {};
|
||||
gps.lat = 40 * 1e7; // Latitude in 1E-7 degrees
|
||||
gps.lon = 5 * 1e7; // Longitude in 1E-7 degrees
|
||||
gps.alt = 200 * 1e3; // Altitude in 1E-3 meters (millimeters) above MSL
|
||||
gps.fix_type = 4; // 0-1: no fix, 2: 2D fix, 3: 3D fix, 4: RTCM code differential, 5: Real-Time
|
||||
gps.eph = 5.0f; // GPS HDOP horizontal dilution of position in m
|
||||
gps.epv = 5.0f; // GPS VDOP horizontal dilution of position in m
|
||||
gps.vel_ned_valid = true; // GPS ground speed is valid
|
||||
|
||||
// simulate two seconds
|
||||
for (int i = 0; i < 800; i++) {
|
||||
timer += (imu_sample_period + distribution(generator));
|
||||
|
||||
if ((timer - timer_last) > 70000) {
|
||||
base->setAirspeedData(timer, &airspeed);
|
||||
}
|
||||
|
||||
gps.time_usec = timer;
|
||||
gps.time_usec_vel = timer;
|
||||
base->setIMUData(timer, timer - timer_last, timer - timer_last, delta_ang, delta_vel);
|
||||
base->setMagData(timer, mag);
|
||||
base->setBaroData(timer, &baro);
|
||||
base->setGpsData(timer, &gps);
|
||||
base->print_imu_avg_time();
|
||||
|
||||
timer_last = timer;
|
||||
|
||||
}
|
||||
|
||||
base->printStoredIMU();
|
||||
base->printStoredBaro();
|
||||
base->printStoredMag();
|
||||
base->printStoredGps();
|
||||
|
||||
return 0;
|
||||
}
|
||||
Loading…
x
Reference in New Issue
Block a user