ardupilot/libraries/AP_InertialSensor/AP_InertialSensor_Backend.cpp

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#include <AP_HAL/AP_HAL.h>
#include "AP_InertialSensor.h"
#include "AP_InertialSensor_Backend.h"
#include <AP_Logger/AP_Logger.h>
#if AP_MODULE_SUPPORTED
#include <AP_Module/AP_Module.h>
#include <stdio.h>
#endif
#define SENSOR_RATE_DEBUG 0
const extern AP_HAL::HAL& hal;
AP_InertialSensor_Backend::AP_InertialSensor_Backend(AP_InertialSensor &imu) :
_imu(imu)
{
}
/*
notify of a FIFO reset so we don't use bad data to update observed sensor rate
*/
void AP_InertialSensor_Backend::notify_accel_fifo_reset(uint8_t instance)
{
_imu._sample_accel_count[instance] = 0;
_imu._sample_accel_start_us[instance] = 0;
}
/*
notify of a FIFO reset so we don't use bad data to update observed sensor rate
*/
void AP_InertialSensor_Backend::notify_gyro_fifo_reset(uint8_t instance)
{
_imu._sample_gyro_count[instance] = 0;
_imu._sample_gyro_start_us[instance] = 0;
}
// set the amount of oversamping a accel is doing
void AP_InertialSensor_Backend::_set_accel_oversampling(uint8_t instance, uint8_t n)
{
_imu._accel_over_sampling[instance] = n;
}
// set the amount of oversamping a gyro is doing
void AP_InertialSensor_Backend::_set_gyro_oversampling(uint8_t instance, uint8_t n)
{
_imu._gyro_over_sampling[instance] = n;
}
/*
update the sensor rate for FIFO sensors
FIFO sensors produce samples at a fixed rate, but the clock in the
sensor may vary slightly from the system clock. This slowly adjusts
the rate to the observed rate
*/
void AP_InertialSensor_Backend::_update_sensor_rate(uint16_t &count, uint32_t &start_us, float &rate_hz) const
{
uint32_t now = AP_HAL::micros();
if (start_us == 0) {
count = 0;
start_us = now;
} else {
count++;
if (now - start_us > 1000000UL) {
float observed_rate_hz = count * 1.0e6f / (now - start_us);
#if SENSOR_RATE_DEBUG
printf("RATE: %.1f should be %.1f\n", observed_rate_hz, rate_hz);
#endif
float filter_constant = 0.98f;
float upper_limit = 1.05f;
float lower_limit = 0.95f;
if (AP_HAL::millis() < 30000) {
// converge quickly for first 30s, then more slowly
filter_constant = 0.8f;
upper_limit = 2.0f;
lower_limit = 0.5f;
}
observed_rate_hz = constrain_float(observed_rate_hz, rate_hz*lower_limit, rate_hz*upper_limit);
rate_hz = filter_constant * rate_hz + (1-filter_constant) * observed_rate_hz;
count = 0;
start_us = now;
}
}
}
void AP_InertialSensor_Backend::_rotate_and_correct_accel(uint8_t instance, Vector3f &accel)
{
/*
accel calibration is always done in sensor frame with this
version of the code. That means we apply the rotation after the
offsets and scaling.
*/
// rotate for sensor orientation
accel.rotate(_imu._accel_orientation[instance]);
// apply offsets
accel -= _imu._accel_offset[instance];
// apply scaling
const Vector3f &accel_scale = _imu._accel_scale[instance].get();
accel.x *= accel_scale.x;
accel.y *= accel_scale.y;
accel.z *= accel_scale.z;
// rotate to body frame
if (_imu._board_orientation == ROTATION_CUSTOM && _imu._custom_rotation) {
accel = *_imu._custom_rotation * accel;
} else {
accel.rotate(_imu._board_orientation);
}
}
void AP_InertialSensor_Backend::_rotate_and_correct_gyro(uint8_t instance, Vector3f &gyro)
{
// rotate for sensor orientation
gyro.rotate(_imu._gyro_orientation[instance]);
// gyro calibration is always assumed to have been done in sensor frame
gyro -= _imu._gyro_offset[instance];
if (_imu._board_orientation == ROTATION_CUSTOM && _imu._custom_rotation) {
gyro = *_imu._custom_rotation * gyro;
} else {
gyro.rotate(_imu._board_orientation);
}
}
/*
rotate gyro vector and add the gyro offset
*/
void AP_InertialSensor_Backend::_publish_gyro(uint8_t instance, const Vector3f &gyro)
{
_imu._gyro[instance] = gyro;
_imu._gyro_healthy[instance] = true;
// publish delta angle
_imu._delta_angle[instance] = _imu._delta_angle_acc[instance];
_imu._delta_angle_dt[instance] = _imu._delta_angle_acc_dt[instance];
_imu._delta_angle_valid[instance] = true;
}
void AP_InertialSensor_Backend::_notify_new_gyro_raw_sample(uint8_t instance,
const Vector3f &gyro,
uint64_t sample_us)
{
float dt;
_update_sensor_rate(_imu._sample_gyro_count[instance], _imu._sample_gyro_start_us[instance],
_imu._gyro_raw_sample_rates[instance]);
/*
we have two classes of sensors. FIFO based sensors produce data
at a very predictable overall rate, but the data comes in
bunches, so we use the provided sample rate for deltaT. Non-FIFO
sensors don't bunch up samples, but also tend to vary in actual
rate, so we use the provided sample_us to get the deltaT. The
difference between the two is whether sample_us is provided.
*/
if (sample_us != 0 && _imu._gyro_last_sample_us[instance] != 0) {
dt = (sample_us - _imu._gyro_last_sample_us[instance]) * 1.0e-6f;
} else {
// don't accept below 100Hz
if (_imu._gyro_raw_sample_rates[instance] < 100) {
return;
}
dt = 1.0f / _imu._gyro_raw_sample_rates[instance];
}
_imu._gyro_last_sample_us[instance] = sample_us;
#if AP_MODULE_SUPPORTED
// call gyro_sample hook if any
AP_Module::call_hook_gyro_sample(instance, dt, gyro);
#endif
// push gyros if optical flow present
if (hal.opticalflow)
hal.opticalflow->push_gyro(gyro.x, gyro.y, dt);
// compute delta angle
Vector3f delta_angle = (gyro + _imu._last_raw_gyro[instance]) * 0.5f * dt;
// compute coning correction
// see page 26 of:
// Tian et al (2010) Three-loop Integration of GPS and Strapdown INS with Coning and Sculling Compensation
// Available: http://www.sage.unsw.edu.au/snap/publications/tian_etal2010b.pdf
// see also examples/coning.py
Vector3f delta_coning = (_imu._delta_angle_acc[instance] +
_imu._last_delta_angle[instance] * (1.0f / 6.0f));
delta_coning = delta_coning % delta_angle;
delta_coning *= 0.5f;
{
WITH_SEMAPHORE(_sem);
// integrate delta angle accumulator
// the angles and coning corrections are accumulated separately in the
// referenced paper, but in simulation little difference was found between
// integrating together and integrating separately (see examples/coning.py)
_imu._delta_angle_acc[instance] += delta_angle + delta_coning;
_imu._delta_angle_acc_dt[instance] += dt;
// save previous delta angle for coning correction
_imu._last_delta_angle[instance] = delta_angle;
_imu._last_raw_gyro[instance] = gyro;
_imu._gyro_filtered[instance] = _imu._gyro_filter[instance].apply(gyro);
if (_imu._gyro_filtered[instance].is_nan() || _imu._gyro_filtered[instance].is_inf()) {
_imu._gyro_filter[instance].reset();
}
_imu._new_gyro_data[instance] = true;
}
log_gyro_raw(instance, sample_us, gyro);
}
void AP_InertialSensor_Backend::log_gyro_raw(uint8_t instance, const uint64_t sample_us, const Vector3f &gyro)
{
AP_Logger *logger = AP_Logger::get_singleton();
if (logger == nullptr) {
// should not have been called
return;
}
if (should_log_imu_raw()) {
uint64_t now = AP_HAL::micros64();
struct log_GYRO pkt = {
LOG_PACKET_HEADER_INIT((uint8_t)(LOG_GYR1_MSG+instance)),
time_us : now,
sample_us : sample_us?sample_us:now,
GyrX : gyro.x,
GyrY : gyro.y,
GyrZ : gyro.z
};
logger->WriteBlock(&pkt, sizeof(pkt));
} else {
if (!_imu.batchsampler.doing_sensor_rate_logging()) {
_imu.batchsampler.sample(instance, AP_InertialSensor::IMU_SENSOR_TYPE_GYRO, sample_us, gyro);
}
}
}
/*
rotate accel vector, scale and add the accel offset
*/
void AP_InertialSensor_Backend::_publish_accel(uint8_t instance, const Vector3f &accel)
{
_imu._accel[instance] = accel;
_imu._accel_healthy[instance] = true;
// publish delta velocity
_imu._delta_velocity[instance] = _imu._delta_velocity_acc[instance];
_imu._delta_velocity_dt[instance] = _imu._delta_velocity_acc_dt[instance];
_imu._delta_velocity_valid[instance] = true;
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if (_imu._accel_calibrator != nullptr && _imu._accel_calibrator[instance].get_status() == ACCEL_CAL_COLLECTING_SAMPLE) {
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Vector3f cal_sample = _imu._delta_velocity[instance];
//remove rotation
cal_sample.rotate_inverse(_imu._board_orientation);
// remove scale factors
const Vector3f &accel_scale = _imu._accel_scale[instance].get();
cal_sample.x /= accel_scale.x;
cal_sample.y /= accel_scale.y;
cal_sample.z /= accel_scale.z;
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//remove offsets
cal_sample += _imu._accel_offset[instance].get() * _imu._delta_velocity_dt[instance] ;
_imu._accel_calibrator[instance].new_sample(cal_sample, _imu._delta_velocity_dt[instance]);
}
}
void AP_InertialSensor_Backend::_notify_new_accel_raw_sample(uint8_t instance,
const Vector3f &accel,
uint64_t sample_us,
bool fsync_set)
{
float dt;
_update_sensor_rate(_imu._sample_accel_count[instance], _imu._sample_accel_start_us[instance],
_imu._accel_raw_sample_rates[instance]);
/*
we have two classes of sensors. FIFO based sensors produce data
at a very predictable overall rate, but the data comes in
bunches, so we use the provided sample rate for deltaT. Non-FIFO
sensors don't bunch up samples, but also tend to vary in actual
rate, so we use the provided sample_us to get the deltaT. The
difference between the two is whether sample_us is provided.
*/
if (sample_us != 0 && _imu._accel_last_sample_us[instance] != 0) {
dt = (sample_us - _imu._accel_last_sample_us[instance]) * 1.0e-6f;
} else {
// don't accept below 100Hz
if (_imu._accel_raw_sample_rates[instance] < 100) {
return;
}
dt = 1.0f / _imu._accel_raw_sample_rates[instance];
}
_imu._accel_last_sample_us[instance] = sample_us;
#if AP_MODULE_SUPPORTED
// call accel_sample hook if any
AP_Module::call_hook_accel_sample(instance, dt, accel, fsync_set);
#endif
_imu.calc_vibration_and_clipping(instance, accel, dt);
{
WITH_SEMAPHORE(_sem);
// delta velocity
_imu._delta_velocity_acc[instance] += accel * dt;
_imu._delta_velocity_acc_dt[instance] += dt;
_imu._accel_filtered[instance] = _imu._accel_filter[instance].apply(accel);
if (_imu._accel_filtered[instance].is_nan() || _imu._accel_filtered[instance].is_inf()) {
_imu._accel_filter[instance].reset();
}
_imu.set_accel_peak_hold(instance, _imu._accel_filtered[instance]);
_imu._new_accel_data[instance] = true;
}
log_accel_raw(instance, sample_us, accel);
}
void AP_InertialSensor_Backend::_notify_new_accel_sensor_rate_sample(uint8_t instance, const Vector3f &accel)
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{
if (!_imu.batchsampler.doing_sensor_rate_logging()) {
return;
}
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_imu.batchsampler.sample(instance, AP_InertialSensor::IMU_SENSOR_TYPE_ACCEL, AP_HAL::micros64(), accel);
}
void AP_InertialSensor_Backend::_notify_new_gyro_sensor_rate_sample(uint8_t instance, const Vector3f &gyro)
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{
if (!_imu.batchsampler.doing_sensor_rate_logging()) {
return;
}
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_imu.batchsampler.sample(instance, AP_InertialSensor::IMU_SENSOR_TYPE_GYRO, AP_HAL::micros64(), gyro);
}
void AP_InertialSensor_Backend::log_accel_raw(uint8_t instance, const uint64_t sample_us, const Vector3f &accel)
{
AP_Logger *logger = AP_Logger::get_singleton();
if (logger == nullptr) {
// should not have been called
return;
}
if (should_log_imu_raw()) {
uint64_t now = AP_HAL::micros64();
struct log_ACCEL pkt = {
LOG_PACKET_HEADER_INIT((uint8_t)(LOG_ACC1_MSG+instance)),
time_us : now,
sample_us : sample_us?sample_us:now,
AccX : accel.x,
AccY : accel.y,
AccZ : accel.z
};
logger->WriteBlock(&pkt, sizeof(pkt));
} else {
if (!_imu.batchsampler.doing_sensor_rate_logging()) {
_imu.batchsampler.sample(instance, AP_InertialSensor::IMU_SENSOR_TYPE_ACCEL, sample_us, accel);
}
}
}
void AP_InertialSensor_Backend::_set_accel_max_abs_offset(uint8_t instance,
float max_offset)
{
_imu._accel_max_abs_offsets[instance] = max_offset;
}
// set accelerometer error_count
void AP_InertialSensor_Backend::_set_accel_error_count(uint8_t instance, uint32_t error_count)
{
_imu._accel_error_count[instance] = error_count;
}
// set gyro error_count
void AP_InertialSensor_Backend::_set_gyro_error_count(uint8_t instance, uint32_t error_count)
{
_imu._gyro_error_count[instance] = error_count;
}
// increment accelerometer error_count
void AP_InertialSensor_Backend::_inc_accel_error_count(uint8_t instance)
{
_imu._accel_error_count[instance]++;
}
// increment gyro error_count
void AP_InertialSensor_Backend::_inc_gyro_error_count(uint8_t instance)
{
_imu._gyro_error_count[instance]++;
}
// return the requested sample rate in Hz
uint16_t AP_InertialSensor_Backend::get_sample_rate_hz(void) const
{
// enum can be directly cast to Hz
return (uint16_t)_imu._sample_rate;
}
/*
publish a temperature value for an instance
*/
void AP_InertialSensor_Backend::_publish_temperature(uint8_t instance, float temperature)
{
_imu._temperature[instance] = temperature;
/* give the temperature to the control loop in order to keep it constant*/
if (instance == 0) {
hal.util->set_imu_temp(temperature);
}
}
/*
common gyro update function for all backends
*/
void AP_InertialSensor_Backend::update_gyro(uint8_t instance)
{
WITH_SEMAPHORE(_sem);
if (_imu._new_gyro_data[instance]) {
_publish_gyro(instance, _imu._gyro_filtered[instance]);
_imu._new_gyro_data[instance] = false;
}
// possibly update filter frequency
if (_last_gyro_filter_hz[instance] != _gyro_filter_cutoff()) {
_imu._gyro_filter[instance].set_cutoff_frequency(_gyro_raw_sample_rate(instance), _gyro_filter_cutoff());
_last_gyro_filter_hz[instance] = _gyro_filter_cutoff();
}
}
/*
common accel update function for all backends
*/
void AP_InertialSensor_Backend::update_accel(uint8_t instance)
{
WITH_SEMAPHORE(_sem);
if (_imu._new_accel_data[instance]) {
_publish_accel(instance, _imu._accel_filtered[instance]);
_imu._new_accel_data[instance] = false;
}
// possibly update filter frequency
if (_last_accel_filter_hz[instance] != _accel_filter_cutoff()) {
_imu._accel_filter[instance].set_cutoff_frequency(_accel_raw_sample_rate(instance), _accel_filter_cutoff());
_last_accel_filter_hz[instance] = _accel_filter_cutoff();
}
}
bool AP_InertialSensor_Backend::should_log_imu_raw() const
{
if (_imu._log_raw_bit == (uint32_t)-1) {
// tracker does not set a bit
return false;
}
const AP_Logger *logger = AP_Logger::get_singleton();
if (logger == nullptr) {
return false;
}
if (!logger->should_log(_imu._log_raw_bit)) {
return false;
}
return true;
}