Beispiel #1
0
void GCS_MAVLINK::send_raw_imu(const AP_InertialSensor &ins, const Compass &compass)
{
    const Vector3f &accel = ins.get_accel(0);
    const Vector3f &gyro = ins.get_gyro(0);
    const Vector3f &mag = compass.get_field(0);

    mavlink_msg_raw_imu_send(
        chan,
        hal.scheduler->micros(),
        accel.x * 1000.0f / GRAVITY_MSS,
        accel.y * 1000.0f / GRAVITY_MSS,
        accel.z * 1000.0f / GRAVITY_MSS,
        gyro.x * 1000.0f,
        gyro.y * 1000.0f,
        gyro.z * 1000.0f,
        mag.x,
        mag.y,
        mag.z);
#if INS_MAX_INSTANCES > 1
    if (ins.get_gyro_count() <= 1 &&
        ins.get_accel_count() <= 1 &&
        compass.get_count() <= 1) {
        return;
    }
    const Vector3f &accel2 = ins.get_accel(1);
    const Vector3f &gyro2 = ins.get_gyro(1);
    const Vector3f &mag2 = compass.get_field(1);
    mavlink_msg_scaled_imu2_send(
        chan,
        hal.scheduler->millis(),
        accel2.x * 1000.0f / GRAVITY_MSS,
        accel2.y * 1000.0f / GRAVITY_MSS,
        accel2.z * 1000.0f / GRAVITY_MSS,
        gyro2.x * 1000.0f,
        gyro2.y * 1000.0f,
        gyro2.z * 1000.0f,
        mag2.x,
        mag2.y,
        mag2.z);        
#endif
}
void GCS_MAVLINK::send_raw_imu(const AP_InertialSensor &ins, const Compass &compass)
{
    const Vector3f &accel = ins.get_accel(0);
    const Vector3f &gyro = ins.get_gyro(0);
    Vector3f mag;
    if (compass.get_count() >= 1) {
        mag = compass.get_field(0);
    } else {
        mag.zero();
    }

    mavlink_msg_raw_imu_send(
        chan,
        AP_HAL::micros(),
        accel.x * 1000.0f / GRAVITY_MSS,
        accel.y * 1000.0f / GRAVITY_MSS,
        accel.z * 1000.0f / GRAVITY_MSS,
        gyro.x * 1000.0f,
        gyro.y * 1000.0f,
        gyro.z * 1000.0f,
        mag.x,
        mag.y,
        mag.z);

    if (ins.get_gyro_count() <= 1 &&
            ins.get_accel_count() <= 1 &&
            compass.get_count() <= 1) {
        return;
    }
    const Vector3f &accel2 = ins.get_accel(1);
    const Vector3f &gyro2 = ins.get_gyro(1);
    if (compass.get_count() >= 2) {
        mag = compass.get_field(1);
    } else {
        mag.zero();
    }
    mavlink_msg_scaled_imu2_send(
        chan,
        AP_HAL::millis(),
        accel2.x * 1000.0f / GRAVITY_MSS,
        accel2.y * 1000.0f / GRAVITY_MSS,
        accel2.z * 1000.0f / GRAVITY_MSS,
        gyro2.x * 1000.0f,
        gyro2.y * 1000.0f,
        gyro2.z * 1000.0f,
        mag.x,
        mag.y,
        mag.z);

    if (ins.get_gyro_count() <= 2 &&
            ins.get_accel_count() <= 2 &&
            compass.get_count() <= 2) {
        return;
    }
    const Vector3f &accel3 = ins.get_accel(2);
    const Vector3f &gyro3 = ins.get_gyro(2);
    if (compass.get_count() >= 3) {
        mag = compass.get_field(2);
    } else {
        mag.zero();
    }
    mavlink_msg_scaled_imu3_send(
        chan,
        AP_HAL::millis(),
        accel3.x * 1000.0f / GRAVITY_MSS,
        accel3.y * 1000.0f / GRAVITY_MSS,
        accel3.z * 1000.0f / GRAVITY_MSS,
        gyro3.x * 1000.0f,
        gyro3.y * 1000.0f,
        gyro3.z * 1000.0f,
        mag.x,
        mag.y,
        mag.z);
}