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bizhang_-obav/src/modules/commander/accelerometer_calibration.cpp

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/****************************************************************************
*
* Copyright (c) 2013-2020 PX4 Development Team. All rights reserved.
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*
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****************************************************************************/
/**
* @file accelerometer_calibration.cpp
*
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* Implementation of accelerometer calibration.
*
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* Transform acceleration vector to true orientation, scale and offset
*
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* ===== Model =====
* accel_corr = accel_T * (accel_raw - accel_offs)
*
* accel_corr[3] - fully corrected acceleration vector in body frame
* accel_T[3][3] - accelerometers transform matrix, rotation and scaling transform
* accel_raw[3] - raw acceleration vector
* accel_offs[3] - acceleration offset vector
*
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* ===== Calibration =====
*
* Reference vectors
* accel_corr_ref[6][3] = [ g 0 0 ] // nose up
* | -g 0 0 | // nose down
* | 0 g 0 | // left side down
* | 0 -g 0 | // right side down
* | 0 0 g | // on back
* [ 0 0 -g ] // level
* accel_raw_ref[6][3]
*
* accel_corr_ref[i] = accel_T * (accel_raw_ref[i] - accel_offs), i = 0...5
*
* 6 reference vectors * 3 axes = 18 equations
* 9 (accel_T) + 3 (accel_offs) = 12 unknown constants
*
* Find accel_offs
*
* accel_offs[i] = (accel_raw_ref[i*2][i] + accel_raw_ref[i*2+1][i]) / 2
*
* Find accel_T
*
* 9 unknown constants
* need 9 equations -> use 3 of 6 measurements -> 3 * 3 = 9 equations
*
* accel_corr_ref[i*2] = accel_T * (accel_raw_ref[i*2] - accel_offs), i = 0...2
*
* Solve separate system for each row of accel_T:
*
* accel_corr_ref[j*2][i] = accel_T[i] * (accel_raw_ref[j*2] - accel_offs), j = 0...2
*
* A * x = b
*
* x = [ accel_T[0][i] ]
* | accel_T[1][i] |
* [ accel_T[2][i] ]
*
* b = [ accel_corr_ref[0][i] ] // One measurement per side is enough
* | accel_corr_ref[2][i] |
* [ accel_corr_ref[4][i] ]
*
* a[i][j] = accel_raw_ref[i][j] - accel_offs[j], i = 0;2;4, j = 0...2
*
* Matrix A is common for all three systems:
* A = [ a[0][0] a[0][1] a[0][2] ]
* | a[2][0] a[2][1] a[2][2] |
* [ a[4][0] a[4][1] a[4][2] ]
*
* x = A^-1 * b
*
* accel_T = A^-1 * g
* g = 9.80665
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*
* ===== Rotation =====
*
* Calibrating using model:
* accel_corr = accel_T_r * (rot * accel_raw - accel_offs_r)
*
* Actual correction:
* accel_corr = rot * accel_T * (accel_raw - accel_offs)
*
* Known: accel_T_r, accel_offs_r, rot
* Unknown: accel_T, accel_offs
*
* Solution:
* accel_T_r * (rot * accel_raw - accel_offs_r) = rot * accel_T * (accel_raw - accel_offs)
* rot^-1 * accel_T_r * (rot * accel_raw - accel_offs_r) = accel_T * (accel_raw - accel_offs)
* rot^-1 * accel_T_r * rot * accel_raw - rot^-1 * accel_T_r * accel_offs_r = accel_T * accel_raw - accel_T * accel_offs)
* => accel_T = rot^-1 * accel_T_r * rot
* => accel_offs = rot^-1 * accel_offs_r
*
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* @author Anton Babushkin <anton.babushkin@me.com>
*/
#include "accelerometer_calibration.h"
#include "calibration_messages.h"
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#include "calibration_routines.h"
#include "commander_helper.h"
#include <px4_platform_common/defines.h>
#include <px4_platform_common/posix.h>
#include <px4_platform_common/time.h>
#include <drivers/drv_hrt.h>
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#include <lib/sensor_calibration/Accelerometer.hpp>
#include <lib/sensor_calibration/Utilities.hpp>
#include <lib/mathlib/mathlib.h>
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#include <lib/ecl/geo/geo.h>
#include <matrix/math.hpp>
#include <lib/conversion/rotation.h>
#include <lib/parameters/param.h>
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#include <lib/systemlib/err.h>
#include <lib/systemlib/mavlink_log.h>
#include <uORB/Subscription.hpp>
#include <uORB/SubscriptionBlocking.hpp>
#include <uORB/topics/sensor_accel.h>
#include <uORB/topics/vehicle_attitude.h>
using namespace matrix;
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using namespace time_literals;
static constexpr char sensor_name[] {"accel"};
static constexpr unsigned MAX_ACCEL_SENS = 3;
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/// Data passed to calibration worker routine
typedef struct {
orb_advert_t *mavlink_log_pub{nullptr};
unsigned done_count{0};
float accel_ref[MAX_ACCEL_SENS][detect_orientation_side_count][3] {};
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} accel_worker_data_t;
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// Read specified number of accelerometer samples, calculate average and dispersion.
static calibrate_return read_accelerometer_avg(float (&accel_avg)[MAX_ACCEL_SENS][detect_orientation_side_count][3],
unsigned orient, unsigned samples_num)
{
Vector3f accel_sum[MAX_ACCEL_SENS] {};
unsigned counts[MAX_ACCEL_SENS] {};
unsigned errcount = 0;
// sensor thermal corrections
uORB::Subscription sensor_correction_sub{ORB_ID(sensor_correction)};
sensor_correction_s sensor_correction{};
sensor_correction_sub.copy(&sensor_correction);
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uORB::SubscriptionBlocking<sensor_accel_s> accel_sub[MAX_ACCEL_SENS] {
{ORB_ID(sensor_accel), 0, 0},
{ORB_ID(sensor_accel), 0, 1},
{ORB_ID(sensor_accel), 0, 2},
};
/* use the first sensor to pace the readout, but do per-sensor counts */
while (counts[0] < samples_num) {
if (accel_sub[0].updatedBlocking(100000)) {
for (unsigned accel_index = 0; accel_index < MAX_ACCEL_SENS; accel_index++) {
sensor_accel_s arp;
if (accel_sub[accel_index].update(&arp)) {
// fetch optional thermal offset corrections in sensor/board frame
Vector3f offset{0, 0, 0};
sensor_correction_sub.update(&sensor_correction);
if (sensor_correction.timestamp > 0 && arp.device_id != 0) {
for (uint8_t correction_index = 0; correction_index < MAX_ACCEL_SENS; correction_index++) {
if (sensor_correction.accel_device_ids[correction_index] == arp.device_id) {
switch (correction_index) {
case 0:
offset = Vector3f{sensor_correction.accel_offset_0};
break;
case 1:
offset = Vector3f{sensor_correction.accel_offset_1};
break;
case 2:
offset = Vector3f{sensor_correction.accel_offset_2};
break;
}
}
}
}
accel_sum[accel_index] += Vector3f{arp.x, arp.y, arp.z} - offset;
counts[accel_index]++;
}
}
} else {
errcount++;
continue;
}
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if (errcount > samples_num / 10) {
return calibrate_return_error;
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}
}
// rotate sensor measurements from sensor to body frame using board rotation matrix
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const Dcmf board_rotation = calibration::GetBoardRotation();
for (unsigned s = 0; s < MAX_ACCEL_SENS; s++) {
accel_sum[s] = board_rotation * accel_sum[s];
}
for (unsigned s = 0; s < MAX_ACCEL_SENS; s++) {
const auto sum = accel_sum[s] / counts[s];
sum.copyTo(accel_avg[s][orient]);
}
return calibrate_return_ok;
}
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static calibrate_return accel_calibration_worker(detect_orientation_return orientation, void *data)
{
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static constexpr unsigned samples_num = 750;
accel_worker_data_t *worker_data = (accel_worker_data_t *)(data);
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calibration_log_info(worker_data->mavlink_log_pub, "[cal] Hold still, measuring %s side",
detect_orientation_str(orientation));
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read_accelerometer_avg(worker_data->accel_ref, orientation, samples_num);
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calibration_log_info(worker_data->mavlink_log_pub, "[cal] %s side result: [%8.4f %8.4f %8.4f]",
detect_orientation_str(orientation),
(double)worker_data->accel_ref[0][orientation][0],
(double)worker_data->accel_ref[0][orientation][1],
(double)worker_data->accel_ref[0][orientation][2]);
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worker_data->done_count++;
calibration_log_info(worker_data->mavlink_log_pub, CAL_QGC_PROGRESS_MSG, 17 * worker_data->done_count);
return calibrate_return_ok;
}
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int do_accel_calibration(orb_advert_t *mavlink_log_pub)
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{
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calibration_log_info(mavlink_log_pub, CAL_QGC_STARTED_MSG, sensor_name);
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calibration::Accelerometer calibrations[MAX_ACCEL_SENS] {};
unsigned active_sensors = 0;
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for (uint8_t cur_accel = 0; cur_accel < MAX_ACCEL_SENS; cur_accel++) {
uORB::SubscriptionData<sensor_accel_s> accel_sub{ORB_ID(sensor_accel), cur_accel};
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if (accel_sub.advertised() && (accel_sub.get().device_id != 0) && (accel_sub.get().timestamp > 0)) {
calibrations[cur_accel].set_device_id(accel_sub.get().device_id);
active_sensors++;
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} else {
calibrations[cur_accel].Reset();
}
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// reset calibration index to match uORB numbering
calibrations[cur_accel].set_calibration_index(cur_accel);
}
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if (active_sensors == 0) {
calibration_log_critical(mavlink_log_pub, CAL_ERROR_SENSOR_MSG);
return PX4_ERROR;
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} else if (active_sensors > MAX_ACCEL_SENS) {
calibration_log_critical(mavlink_log_pub, "Detected %u accels, but will calibrate only %u", active_sensors,
MAX_ACCEL_SENS);
}
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/* measure and calculate offsets & scales */
accel_worker_data_t worker_data{};
worker_data.mavlink_log_pub = mavlink_log_pub;
bool data_collected[detect_orientation_side_count] {};
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if (calibrate_from_orientation(mavlink_log_pub, data_collected, accel_calibration_worker, &worker_data,
false) == calibrate_return_ok) {
const Dcmf board_rotation = calibration::GetBoardRotation();
const Dcmf board_rotation_t = board_rotation.transpose();
for (unsigned i = 0; i < MAX_ACCEL_SENS; i++) {
if (i < active_sensors) {
// calculate offsets
Vector3f offset{};
// X offset: average X from TAIL_DOWN + NOSE_DOWN
const Vector3f accel_tail_down{worker_data.accel_ref[i][ORIENTATION_TAIL_DOWN]};
const Vector3f accel_nose_down{worker_data.accel_ref[i][ORIENTATION_NOSE_DOWN]};
offset(0) = (accel_tail_down(0) + accel_nose_down(0)) * 0.5f;
// Y offset: average Y from LEFT + RIGHT
const Vector3f accel_left{worker_data.accel_ref[i][ORIENTATION_LEFT]};
const Vector3f accel_right{worker_data.accel_ref[i][ORIENTATION_RIGHT]};
offset(1) = (accel_left(1) + accel_right(1)) * 0.5f;
// Z offset: average Z from UPSIDE_DOWN + RIGHTSIDE_UP
const Vector3f accel_upside_down{worker_data.accel_ref[i][ORIENTATION_UPSIDE_DOWN]};
const Vector3f accel_rightside_up{worker_data.accel_ref[i][ORIENTATION_RIGHTSIDE_UP]};
offset(2) = (accel_upside_down(2) + accel_rightside_up(2)) * 0.5f;
// transform matrix
Matrix3f mat_A;
mat_A.row(0) = accel_tail_down - offset;
mat_A.row(1) = accel_left - offset;
mat_A.row(2) = accel_upside_down - offset;
// calculate inverse matrix for A: simplify matrices mult because b has only one non-zero element == g at index i
const Matrix3f accel_T = mat_A.I() * CONSTANTS_ONE_G;
// update calibration
const Vector3f accel_offs_rotated{board_rotation_t *offset};
calibrations[i].set_offset(accel_offs_rotated);
const Matrix3f accel_T_rotated{board_rotation_t *accel_T * board_rotation};
calibrations[i].set_scale(accel_T_rotated.diag());
#if defined(DEBUD_BUILD)
PX4_INFO("accel %d: offset", i);
offset.print();
PX4_INFO("accel %d: bT * offset", i);
accel_offs_rotated.print();
PX4_INFO("accel %d: mat_A", i);
mat_A.print();
PX4_INFO("accel %d: accel_T", i);
accel_T.print();
PX4_INFO("accel %d: bT * accel_T * b", i);
accel_T_rotated.print();
#endif // DEBUD_BUILD
}
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// save all calibrations including empty slots
calibrations[i].ParametersSave();
}
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param_notify_changes();
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/* if there is a any preflight-check system response, let the barrage of messages through */
px4_usleep(200000);
calibration_log_info(mavlink_log_pub, CAL_QGC_DONE_MSG, sensor_name);
px4_usleep(600000); /* give this message enough time to propagate */
return PX4_OK;
}
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calibration_log_critical(mavlink_log_pub, CAL_QGC_FAILED_MSG, sensor_name);
return PX4_ERROR;
}
int do_accel_calibration_quick(orb_advert_t *mavlink_log_pub)
{
#if !defined(CONSTRAINED_FLASH)
PX4_INFO("Accelerometer quick calibration");
bool success = false;
// sensor thermal corrections (optional)
uORB::Subscription sensor_correction_sub{ORB_ID(sensor_correction)};
sensor_correction_s sensor_correction{};
sensor_correction_sub.copy(&sensor_correction);
uORB::Subscription accel_sub[MAX_ACCEL_SENS] {
{ORB_ID(sensor_accel), 0},
{ORB_ID(sensor_accel), 1},
{ORB_ID(sensor_accel), 2},
};
/* use the first sensor to pace the readout, but do per-sensor counts */
for (unsigned accel_index = 0; accel_index < MAX_ACCEL_SENS; accel_index++) {
sensor_accel_s arp{};
Vector3f accel_sum{};
unsigned count = 0;
while (accel_sub[accel_index].update(&arp)) {
// fetch optional thermal offset corrections in sensor/board frame
if ((arp.timestamp > 0) && (arp.device_id != 0)) {
Vector3f offset{0, 0, 0};
if (sensor_correction.timestamp > 0) {
for (uint8_t correction_index = 0; correction_index < MAX_ACCEL_SENS; correction_index++) {
if (sensor_correction.accel_device_ids[correction_index] == arp.device_id) {
switch (correction_index) {
case 0:
offset = Vector3f{sensor_correction.accel_offset_0};
break;
case 1:
offset = Vector3f{sensor_correction.accel_offset_1};
break;
case 2:
offset = Vector3f{sensor_correction.accel_offset_2};
break;
}
}
}
}
const Vector3f accel{Vector3f{arp.x, arp.y, arp.z} - offset};
if (count > 0) {
const Vector3f diff{accel - (accel_sum / count)};
if (diff.norm() < 1.f) {
accel_sum += Vector3f{arp.x, arp.y, arp.z} - offset;
count++;
}
} else {
accel_sum = accel;
count = 1;
}
}
}
if ((count > 0) && (arp.device_id != 0)) {
bool calibrated = false;
const Vector3f accel_avg = accel_sum / count;
Vector3f offset{0.f, 0.f, 0.f};
uORB::SubscriptionData<vehicle_attitude_s> attitude_sub{ORB_ID(vehicle_attitude)};
attitude_sub.update();
if (attitude_sub.advertised() && attitude_sub.get().timestamp != 0) {
// use vehicle_attitude if available
const vehicle_attitude_s &att = attitude_sub.get();
const matrix::Quatf q{att.q};
const Vector3f accel_ref = q.conjugate_inversed(Vector3f{0.f, 0.f, -CONSTANTS_ONE_G});
// sanity check angle between acceleration vectors
const float angle = AxisAnglef(Quatf(accel_avg, accel_ref)).angle();
if (angle <= math::radians(10.f)) {
offset = accel_avg - accel_ref;
calibrated = true;
}
}
if (!calibrated) {
// otherwise simply normalize to gravity and remove offset
Vector3f accel{accel_avg};
accel.normalize();
accel = accel * CONSTANTS_ONE_G;
offset = accel_avg - accel;
calibrated = true;
}
calibration::Accelerometer calibration{arp.device_id};
// reset cal index to uORB
calibration.set_calibration_index(accel_index);
if (!calibrated || (offset.norm() > CONSTANTS_ONE_G)
|| !PX4_ISFINITE(offset(0))
|| !PX4_ISFINITE(offset(1))
|| !PX4_ISFINITE(offset(2))) {
PX4_ERR("accel %d quick calibrate failed", accel_index);
} else {
calibration.set_offset(offset);
success = true;
}
calibration.ParametersSave();
calibration.PrintStatus();
}
}
if (success) {
param_notify_changes();
return PX4_OK;
}
#endif // !CONSTRAINED_FLASH
return PX4_ERROR;
}