#include #if CONFIG_HAL_BOARD == HAL_BOARD_QURT #include "AP_InertialSensor_QURT.h" const extern AP_HAL::HAL& hal; ObjectBuffer *mpu9250_mag_buffer = nullptr; AP_InertialSensor_QURT::AP_InertialSensor_QURT(AP_InertialSensor &imu) : AP_InertialSensor_Backend(imu) { } /* detect the sensor */ AP_InertialSensor_Backend *AP_InertialSensor_QURT::detect(AP_InertialSensor &_imu) { AP_InertialSensor_QURT *sensor = new AP_InertialSensor_QURT(_imu); if (sensor == nullptr) { return nullptr; } if (!sensor->init_sensor()) { delete sensor; return nullptr; } return sensor; } bool AP_InertialSensor_QURT::init_sensor(void) { gyro_instance = _imu.register_gyro(1000, 1); accel_instance = _imu.register_accel(1000, 1); mpu9250_mag_buffer = new ObjectBuffer(20); init_mpu9250(); return true; } /* handle data ready interrupt from mpu9250 */ extern "C" { static void *mpu_data_ready_trampoline(void *ctx); } static void *mpu_data_ready_trampoline(void *ctx) { ((AP_InertialSensor_QURT *)ctx)->data_ready(); return nullptr; } void AP_InertialSensor_QURT::init_mpu9250(void) { struct mpu9x50_config config; config.gyro_lpf = MPU9X50_GYRO_LPF_184HZ; config.acc_lpf = MPU9X50_ACC_LPF_184HZ; config.gyro_fsr = MPU9X50_GYRO_FSR_2000DPS; config.acc_fsr = MPU9X50_ACC_FSR_16G; config.gyro_sample_rate = MPU9x50_SAMPLE_RATE_1000HZ; config.compass_enabled = true; config.compass_sample_rate = MPU9x50_COMPASS_SAMPLE_RATE_100HZ; config.spi_dev_path = "/dev/spi-1"; int ret; ret = mpu9x50_validate_configuration(&config); if (ret != 0) { AP_HAL::panic("Bad MPU9x50 configuration"); } ret = mpu9x50_initialize(&config); if (ret != 0) { AP_HAL::panic("Failed to initialise mpu9250"); } mpu9x50_register_interrupt(65, mpu_data_ready_trampoline, this); HAP_PRINTF("Opened MPU9X50"); } void AP_InertialSensor_QURT::data_ready(void) { uint64_t now = AP_HAL::micros64(); struct mpu9x50_data data; int ret = mpu9x50_get_data(&data); if (ret == 0) { data.timestamp = now; buf.push(data); if (data.mag_data_ready) { mpu9250_mag_buffer->push(data); } } } void AP_InertialSensor_QURT::accumulate(void) { const float ACCEL_SCALE_1G = GRAVITY_MSS / 2048.0; const float GYRO_SCALE = 0.0174532 / 16.4; struct mpu9x50_data data; while (buf.pop(data)) { Vector3f accel(data.accel_raw[0]*ACCEL_SCALE_1G, data.accel_raw[1]*ACCEL_SCALE_1G, data.accel_raw[2]*ACCEL_SCALE_1G); Vector3f gyro(data.gyro_raw[0]*GYRO_SCALE, data.gyro_raw[1]*GYRO_SCALE, data.gyro_raw[2]*GYRO_SCALE); _rotate_and_correct_accel(accel_instance, accel); _rotate_and_correct_gyro(gyro_instance, gyro); _notify_new_gyro_raw_sample(gyro_instance, gyro, data.timestamp); _notify_new_accel_raw_sample(accel_instance, accel, data.timestamp); } } bool AP_InertialSensor_QURT::update(void) { accumulate(); update_accel(accel_instance); update_gyro(gyro_instance); return true; } #endif // HAL_BOARD_QURT