mirror of https://github.com/ArduPilot/ardupilot
458 lines
15 KiB
C++
458 lines
15 KiB
C++
/// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*-
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#include <AP_HAL.h>
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#if CONFIG_HAL_BOARD == HAL_BOARD_PX4 || CONFIG_HAL_BOARD == HAL_BOARD_VRBRAIN
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#include "AP_InertialSensor_PX4.h"
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const extern AP_HAL::HAL& hal;
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#include <DataFlash.h>
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#include <sys/types.h>
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#include <sys/stat.h>
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#include <fcntl.h>
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#include <unistd.h>
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#include <drivers/drv_accel.h>
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#include <drivers/drv_gyro.h>
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#include <drivers/drv_hrt.h>
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#include <stdio.h>
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AP_InertialSensor_PX4::AP_InertialSensor_PX4(AP_InertialSensor &imu) :
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AP_InertialSensor_Backend(imu),
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_last_get_sample_timestamp(0),
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_last_sample_timestamp(0),
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_last_gyro_filter_hz(-1),
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_last_accel_filter_hz(-1)
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{
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for (uint8_t i=0; i<INS_MAX_INSTANCES; i++) {
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_delta_angle_accumulator[i].zero();
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_delta_velocity_accumulator[i].zero();
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_delta_velocity_dt[i] = 0.0f;
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}
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}
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/*
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detect the sensor
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*/
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AP_InertialSensor_Backend *AP_InertialSensor_PX4::detect(AP_InertialSensor &_imu)
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{
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AP_InertialSensor_PX4 *sensor = new AP_InertialSensor_PX4(_imu);
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if (sensor == NULL) {
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return NULL;
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}
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if (!sensor->_init_sensor()) {
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delete sensor;
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return NULL;
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}
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return sensor;
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}
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/*
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calculate the right queue depth for a device with the given sensor
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sample rate
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*/
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uint8_t AP_InertialSensor_PX4::_queue_depth(uint16_t sensor_sample_rate) const
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{
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uint16_t requested_sample_rate = get_sample_rate_hz();
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uint8_t min_depth = (sensor_sample_rate+requested_sample_rate-1)/requested_sample_rate;
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// add 5ms more worth of queue to account for possible timing jitter
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uint8_t ret = min_depth + (5 * sensor_sample_rate) / 1000;
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return ret;
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}
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bool AP_InertialSensor_PX4::_init_sensor(void)
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{
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// assumes max 3 instances
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_accel_fd[0] = open(ACCEL_BASE_DEVICE_PATH "0", O_RDONLY);
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_accel_fd[1] = open(ACCEL_BASE_DEVICE_PATH "1", O_RDONLY);
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_accel_fd[2] = open(ACCEL_BASE_DEVICE_PATH "2", O_RDONLY);
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_gyro_fd[0] = open(GYRO_BASE_DEVICE_PATH "0", O_RDONLY);
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_gyro_fd[1] = open(GYRO_BASE_DEVICE_PATH "1", O_RDONLY);
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_gyro_fd[2] = open(GYRO_BASE_DEVICE_PATH "2", O_RDONLY);
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_num_accel_instances = 0;
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_num_gyro_instances = 0;
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for (uint8_t i=0; i<INS_MAX_INSTANCES; i++) {
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if (_accel_fd[i] >= 0) {
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_num_accel_instances = i+1;
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_accel_instance[i] = _imu.register_accel();
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}
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if (_gyro_fd[i] >= 0) {
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_num_gyro_instances = i+1;
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_gyro_instance[i] = _imu.register_gyro();
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}
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}
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if (_num_accel_instances == 0) {
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return false;
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}
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if (_num_gyro_instances == 0) {
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return false;
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}
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for (uint8_t i=0; i<_num_gyro_instances; i++) {
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int fd = _gyro_fd[i];
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int devid = (ioctl(fd, DEVIOCGDEVICEID, 0) & 0x00FF0000)>>16;
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// software LPF off
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ioctl(fd, GYROIOCSLOWPASS, 0);
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// 2000dps range
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ioctl(fd, GYROIOCSRANGE, 2000);
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switch(devid) {
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case DRV_GYR_DEVTYPE_MPU6000:
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// hardware LPF off
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ioctl(fd, GYROIOCSHWLOWPASS, 256);
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// khz sampling
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ioctl(fd, GYROIOCSSAMPLERATE, 1000);
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// set queue depth
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ioctl(fd, SENSORIOCSQUEUEDEPTH, _queue_depth(1000));
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break;
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case DRV_GYR_DEVTYPE_L3GD20:
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// hardware LPF as high as possible
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ioctl(fd, GYROIOCSHWLOWPASS, 100);
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// ~khz sampling
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ioctl(fd, GYROIOCSSAMPLERATE, 800);
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// 10ms queue depth
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ioctl(fd, SENSORIOCSQUEUEDEPTH, _queue_depth(800));
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break;
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default:
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break;
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}
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}
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for (uint8_t i=0; i<_num_accel_instances; i++) {
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int fd = _accel_fd[i];
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int devid = (ioctl(fd, DEVIOCGDEVICEID, 0) & 0x00FF0000)>>16;
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// software LPF off
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ioctl(fd, ACCELIOCSLOWPASS, 0);
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// 16g range
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ioctl(fd, ACCELIOCSRANGE, 16);
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switch(devid) {
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case DRV_ACC_DEVTYPE_MPU6000:
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// hardware LPF off
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ioctl(fd, ACCELIOCSHWLOWPASS, 256);
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// khz sampling
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ioctl(fd, ACCELIOCSSAMPLERATE, 1000);
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// 10ms queue depth
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ioctl(fd, SENSORIOCSQUEUEDEPTH, _queue_depth(1000));
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break;
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case DRV_ACC_DEVTYPE_LSM303D:
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// hardware LPF to ~1/10th sample rate for antialiasing
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ioctl(fd, ACCELIOCSHWLOWPASS, 194);
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// ~khz sampling
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ioctl(fd, ACCELIOCSSAMPLERATE, 1600);
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ioctl(fd,SENSORIOCSPOLLRATE, 1600);
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// 10ms queue depth
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ioctl(fd, SENSORIOCSQUEUEDEPTH, _queue_depth(1600));
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break;
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default:
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break;
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}
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}
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_set_accel_filter_frequency(_accel_filter_cutoff());
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_set_gyro_filter_frequency(_gyro_filter_cutoff());
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#if CONFIG_HAL_BOARD == HAL_BOARD_VRBRAIN
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_product_id = AP_PRODUCT_ID_VRBRAIN;
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#else
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#if defined(CONFIG_ARCH_BOARD_PX4FMU_V2)
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_product_id = AP_PRODUCT_ID_PX4_V2;
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#else
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_product_id = AP_PRODUCT_ID_PX4;
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#endif
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#endif
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return true;
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}
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/*
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set the accel filter frequency
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*/
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void AP_InertialSensor_PX4::_set_accel_filter_frequency(uint8_t filter_hz)
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{
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for (uint8_t i=0; i<_num_accel_instances; i++) {
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int samplerate = ioctl(_accel_fd[i], ACCELIOCGSAMPLERATE, 0);
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if(samplerate < 100 || samplerate > 2000) {
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// sample rate doesn't seem sane, turn off filter
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_accel_filter[i].set_cutoff_frequency(0, 0);
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} else {
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_accel_filter[i].set_cutoff_frequency(samplerate, filter_hz);
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}
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}
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}
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/*
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set the gyro filter frequency
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*/
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void AP_InertialSensor_PX4::_set_gyro_filter_frequency(uint8_t filter_hz)
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{
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for (uint8_t i=0; i<_num_gyro_instances; i++) {
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int samplerate = ioctl(_gyro_fd[i], GYROIOCGSAMPLERATE, 0);
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if(samplerate < 100 || samplerate > 2000) {
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// sample rate doesn't seem sane, turn off filter
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_gyro_filter[i].set_cutoff_frequency(0, 0);
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} else {
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_gyro_filter[i].set_cutoff_frequency(samplerate, filter_hz);
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}
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}
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}
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bool AP_InertialSensor_PX4::update(void)
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{
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// get the latest sample from the sensor drivers
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_get_sample();
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for (uint8_t k=0; k<_num_accel_instances; k++) {
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Vector3f accel = _accel_in[k];
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// calling _publish_accel sets the sensor healthy,
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// so we only want to do this if we have new data from it
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if (_last_accel_timestamp[k] != _last_accel_update_timestamp[k]) {
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_publish_accel(_accel_instance[k], accel, false);
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_publish_delta_velocity(_accel_instance[k], _delta_velocity_accumulator[k], _delta_velocity_dt[k]);
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_last_accel_update_timestamp[k] = _last_accel_timestamp[k];
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}
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}
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for (uint8_t k=0; k<_num_gyro_instances; k++) {
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Vector3f gyro = _gyro_in[k];
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// calling _publish_accel sets the sensor healthy,
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// so we only want to do this if we have new data from it
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if (_last_gyro_timestamp[k] != _last_gyro_update_timestamp[k]) {
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_publish_gyro(_gyro_instance[k], gyro, false);
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_publish_delta_angle(_gyro_instance[k], _delta_angle_accumulator[k]);
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_last_gyro_update_timestamp[k] = _last_gyro_timestamp[k];
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}
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}
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for (uint8_t i=0; i<INS_MAX_INSTANCES; i++) {
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_delta_angle_accumulator[i].zero();
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_delta_velocity_accumulator[i].zero();
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_delta_velocity_dt[i] = 0.0f;
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}
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if (_last_accel_filter_hz != _accel_filter_cutoff()) {
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_set_accel_filter_frequency(_accel_filter_cutoff());
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_last_accel_filter_hz = _accel_filter_cutoff();
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}
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if (_last_gyro_filter_hz != _gyro_filter_cutoff()) {
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_set_gyro_filter_frequency(_gyro_filter_cutoff());
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_last_gyro_filter_hz = _gyro_filter_cutoff();
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}
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return true;
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}
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void AP_InertialSensor_PX4::_new_accel_sample(uint8_t i, accel_report &accel_report)
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{
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Vector3f accel = Vector3f(accel_report.x, accel_report.y, accel_report.z);
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uint8_t frontend_instance = _accel_instance[i];
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// apply corrections
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_rotate_and_correct_accel(frontend_instance, accel);
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// apply filter for control path
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_accel_in[i] = _accel_filter[i].apply(accel);
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// compute time since last sample
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float dt = (accel_report.timestamp - _last_accel_timestamp[i]) * 1.0e-6f;
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// compute delta velocity
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Vector3f delVel = Vector3f(accel.x, accel.y, accel.z) * dt;
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// integrate delta velocity accumulator
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_delta_velocity_accumulator[i] += delVel;
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_delta_velocity_dt[i] += dt;
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// save last timestamp
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_last_accel_timestamp[i] = accel_report.timestamp;
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// report error count
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_set_accel_error_count(frontend_instance, accel_report.error_count);
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// publish a temperature (for logging purposed only)
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_publish_temperature(frontend_instance, accel_report.temperature);
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#ifdef AP_INERTIALSENSOR_PX4_DEBUG
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_accel_dt_max[i] = max(_accel_dt_max[i],dt);
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_accel_meas_count[i] ++;
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if(_accel_meas_count[i] >= 10000) {
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uint32_t tnow = hal.scheduler->micros();
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::printf("a%d %.2f Hz max %.8f s\n", frontend_instance, 10000.0f/((tnow-_accel_meas_count_start_us[i])*1.0e-6f),_accel_dt_max[i]);
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_accel_meas_count_start_us[i] = tnow;
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_accel_meas_count[i] = 0;
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_accel_dt_max[i] = 0;
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}
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#endif // AP_INERTIALSENSOR_PX4_DEBUG
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}
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void AP_InertialSensor_PX4::_new_gyro_sample(uint8_t i, gyro_report &gyro_report)
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{
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Vector3f gyro = Vector3f(gyro_report.x, gyro_report.y, gyro_report.z);
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uint8_t frontend_instance = _gyro_instance[i];
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// apply corrections
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_rotate_and_correct_gyro(frontend_instance, gyro);
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// apply filter for control path
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_gyro_in[i] = _gyro_filter[i].apply(gyro);
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// compute time since last sample - not more than 50ms
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float dt = min((gyro_report.timestamp - _last_gyro_timestamp[i]) * 1.0e-6f, 0.05f);
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// compute delta angle
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Vector3f delAng = (gyro+_last_gyro[i]) * 0.5f * dt;
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/* compute coning correction
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* see page 26 of:
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* Tian et al (2010) Three-loop Integration of GPS and Strapdown INS with Coning and Sculling Compensation
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* Available: http://www.sage.unsw.edu.au/snap/publications/tian_etal2010b.pdf
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* see also examples/coning.py
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*/
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Vector3f delConing = ((_delta_angle_accumulator[i]+_last_delAng[i]*(1.0f/6.0f)) % delAng) * 0.5f;
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// integrate delta angle accumulator
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// the angles and coning corrections are accumulated separately in the
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// referenced paper, but in simulation little difference was found between
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// integrating together and integrating separately (see examples/coning.py)
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_delta_angle_accumulator[i] += delAng + delConing;
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// save previous delta angle for coning correction
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_last_delAng[i] = delAng;
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_last_gyro[i] = gyro;
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// save last timestamp
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_last_gyro_timestamp[i] = gyro_report.timestamp;
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// report error count
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_set_gyro_error_count(_gyro_instance[i], gyro_report.error_count);
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#ifdef AP_INERTIALSENSOR_PX4_DEBUG
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_gyro_dt_max[i] = max(_gyro_dt_max[i],dt);
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_gyro_meas_count[i] ++;
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if(_gyro_meas_count[i] >= 10000) {
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uint32_t tnow = hal.scheduler->micros();
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::printf("g%d %.2f Hz max %.8f s\n", frontend_instance, 10000.0f/((tnow-_gyro_meas_count_start_us[i])*1.0e-6f), _gyro_dt_max[i]);
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_gyro_meas_count_start_us[i] = tnow;
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_gyro_meas_count[i] = 0;
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_gyro_dt_max[i] = 0;
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}
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#endif // AP_INERTIALSENSOR_PX4_DEBUG
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}
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void AP_InertialSensor_PX4::_get_sample()
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{
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for (uint8_t i=0; i<max(_num_accel_instances,_num_gyro_instances);i++) {
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struct accel_report accel_report;
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struct gyro_report gyro_report;
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bool gyro_valid = _get_gyro_sample(i,gyro_report);
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bool accel_valid = _get_accel_sample(i,accel_report);
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while(gyro_valid || accel_valid) {
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// interleave accel and gyro samples by time - this will allow sculling corrections later
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// check the next gyro measurement to see if it needs to be integrated first
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if(gyro_valid && accel_valid && gyro_report.timestamp <= accel_report.timestamp) {
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_new_gyro_sample(i,gyro_report);
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gyro_valid = _get_gyro_sample(i,gyro_report);
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continue;
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}
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// if not, try to integrate an accelerometer sample
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if(accel_valid) {
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_new_accel_sample(i,accel_report);
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accel_valid = _get_accel_sample(i,accel_report);
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continue;
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}
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// if not, we've only got gyro samples left in the buffer
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if(gyro_valid) {
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_new_gyro_sample(i,gyro_report);
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gyro_valid = _get_gyro_sample(i,gyro_report);
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}
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}
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}
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_last_get_sample_timestamp = hal.scheduler->micros64();
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}
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bool AP_InertialSensor_PX4::_get_accel_sample(uint8_t i, struct accel_report &accel_report)
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{
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if (i<_num_accel_instances &&
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_accel_fd[i] != -1 &&
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::read(_accel_fd[i], &accel_report, sizeof(accel_report)) == sizeof(accel_report) &&
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accel_report.timestamp != _last_accel_timestamp[i]) {
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DataFlash_Class *dataflash = get_dataflash();
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if (dataflash != NULL) {
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struct log_ACCEL pkt = {
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LOG_PACKET_HEADER_INIT((uint8_t)(LOG_ACC1_MSG+i)),
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time_us : hal.scheduler->micros64(),
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sample_us : accel_report.timestamp,
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AccX : accel_report.x,
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AccY : accel_report.y,
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AccZ : accel_report.z
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};
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dataflash->WriteBlock(&pkt, sizeof(pkt));
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}
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return true;
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}
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return false;
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}
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bool AP_InertialSensor_PX4::_get_gyro_sample(uint8_t i, struct gyro_report &gyro_report)
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{
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if (i<_num_gyro_instances &&
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_gyro_fd[i] != -1 &&
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::read(_gyro_fd[i], &gyro_report, sizeof(gyro_report)) == sizeof(gyro_report) &&
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gyro_report.timestamp != _last_gyro_timestamp[i]) {
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DataFlash_Class *dataflash = get_dataflash();
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if (dataflash != NULL) {
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struct log_GYRO pkt = {
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LOG_PACKET_HEADER_INIT((uint8_t)(LOG_GYR1_MSG+i)),
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time_us : hal.scheduler->micros64(),
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sample_us : gyro_report.timestamp,
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GyrX : gyro_report.x,
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GyrY : gyro_report.y,
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GyrZ : gyro_report.z
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};
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dataflash->WriteBlock(&pkt, sizeof(pkt));
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}
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return true;
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}
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return false;
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}
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bool AP_InertialSensor_PX4::gyro_sample_available(void)
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{
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_get_sample();
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for (uint8_t i=0; i<_num_gyro_instances; i++) {
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if (_last_gyro_timestamp[i] != _last_gyro_update_timestamp[i]) {
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return true;
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}
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}
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return false;
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}
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bool AP_InertialSensor_PX4::accel_sample_available(void)
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{
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_get_sample();
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for (uint8_t i=0; i<_num_accel_instances; i++) {
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if (_last_accel_timestamp[i] != _last_accel_update_timestamp[i]) {
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return true;
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}
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}
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return false;
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}
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#endif // CONFIG_HAL_BOARD
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