mirror of https://github.com/ArduPilot/ardupilot
AP_InertialSensor_PX4: explicitly configure sensors, publish deltas
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@ -22,6 +22,10 @@ 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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{
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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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}
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}
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/*
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@ -62,14 +66,76 @@ bool AP_InertialSensor_PX4::_init_sensor(void)
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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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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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if (_num_gyro_instances == 0) {
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return false;
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}
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_default_filter_hz = _default_filter();
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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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// 10ms queue depth
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ioctl(fd, SENSORIOCSQUEUEDEPTH, 10);
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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, 8);
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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, 10);
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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, 16);
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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_filter_frequency(_imu.get_filter());
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#if CONFIG_HAL_BOARD == HAL_BOARD_VRBRAIN
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@ -90,13 +156,25 @@ bool AP_InertialSensor_PX4::_init_sensor(void)
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void AP_InertialSensor_PX4::_set_filter_frequency(uint8_t filter_hz)
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{
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if (filter_hz == 0) {
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filter_hz = _default_filter_hz;
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filter_hz = _default_filter();
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}
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for (uint8_t i=0; i<_num_gyro_instances; i++) {
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ioctl(_gyro_fd[i], GYROIOCSLOWPASS, filter_hz);
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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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for (uint8_t i=0; i<_num_accel_instances; i++) {
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ioctl(_accel_fd[i], ACCELIOCSLOWPASS, filter_hz);
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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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@ -110,7 +188,8 @@ bool AP_InertialSensor_PX4::update(void)
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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);
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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]);
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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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@ -120,11 +199,17 @@ bool AP_InertialSensor_PX4::update(void)
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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);
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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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}
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if (_last_filter_hz != _imu.get_filter()) {
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_set_filter_frequency(_imu.get_filter());
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_last_filter_hz = _imu.get_filter();
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@ -133,26 +218,91 @@ bool AP_InertialSensor_PX4::update(void)
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return true;
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}
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void AP_InertialSensor_PX4::_get_sample(void)
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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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// 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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}
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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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}
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void AP_InertialSensor_PX4::_get_sample()
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{
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for (uint8_t i=0; i<_num_accel_instances; i++) {
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struct accel_report accel_report;
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struct accel_report accel_report;
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while (_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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_accel_in[i] = Vector3f(accel_report.x, accel_report.y, accel_report.z);
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_last_accel_timestamp[i] = accel_report.timestamp;
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_set_accel_error_count(_accel_instance[i], accel_report.error_count);
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_new_accel_sample(i, accel_report);
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}
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}
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for (uint8_t i=0; i<_num_gyro_instances; i++) {
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struct gyro_report gyro_report;
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struct gyro_report gyro_report;
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while (_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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_gyro_in[i] = Vector3f(gyro_report.x, gyro_report.y, gyro_report.z);
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_last_gyro_timestamp[i] = gyro_report.timestamp;
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_set_gyro_error_count(_gyro_instance[i], gyro_report.error_count);
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_new_gyro_sample(i, gyro_report);
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}
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}
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_last_get_sample_timestamp = hal.scheduler->micros64();
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@ -13,6 +13,9 @@
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#include <uORB/uORB.h>
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#include <uORB/topics/sensor_combined.h>
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#include <Filter.h>
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#include <LowPassFilter2p.h>
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class AP_InertialSensor_PX4 : public AP_InertialSensor_Backend
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{
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public:
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@ -41,9 +44,11 @@ private:
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uint64_t _last_get_sample_timestamp;
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uint64_t _last_sample_timestamp;
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void _new_accel_sample(uint8_t i, accel_report &accel_report);
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void _new_gyro_sample(uint8_t i, gyro_report &gyro_report);
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// support for updating filter at runtime
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uint8_t _last_filter_hz;
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uint8_t _default_filter_hz;
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void _set_filter_frequency(uint8_t filter_hz);
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@ -58,6 +63,15 @@ private:
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// from the backend indexes
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uint8_t _accel_instance[INS_MAX_INSTANCES];
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uint8_t _gyro_instance[INS_MAX_INSTANCES];
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// Low Pass filters for gyro and accel
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LowPassFilter2pVector3f _accel_filter[INS_MAX_INSTANCES];
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LowPassFilter2pVector3f _gyro_filter[INS_MAX_INSTANCES];
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Vector3f _delta_angle_accumulator[INS_MAX_INSTANCES];
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Vector3f _delta_velocity_accumulator[INS_MAX_INSTANCES];
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Vector3f _last_delAng[INS_MAX_INSTANCES];
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Vector3f _last_gyro[INS_MAX_INSTANCES];
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};
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#endif // CONFIG_HAL_BOARD
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#endif // __AP_INERTIAL_SENSOR_PX4_H__
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