bool AP_IMU_INS::update(void) { //float gyros[3]; //float accels[3]; _ins->update(); //_ins->get_gyros(gyros); //_ins->get_accels(accels); _sample_time = _ins->sample_time(); // convert corrected gyro readings to delta acceleration // _gyro.x = /*_gyro.x * 0.7 + 0.3 **/ _calibrated(0, _ins->gyro[0]); _gyro.y = /*_gyro.y * 0.7 + 0.3 **/ _calibrated(1, _ins->gyro[1]); _gyro.z = /*_gyro.z * 0.7 + 0.3 **/ _calibrated(2, _ins->gyro[2]); // convert corrected accelerometer readings to acceleration // _accel.x = _calibrated(3, _ins->accel[0]); _accel.y = _calibrated(4, _ins->accel[1]); _accel.z = _calibrated(5, _ins->accel[2]); // always updated return true; }
bool AP_IMU_INS::update(void) { float gyros[3]; float accels[3]; _ins->update(); _ins->get_gyros(gyros); _ins->get_accels(accels); _sample_time = _ins->sample_time(); // convert corrected gyro readings to delta acceleration // _gyro.x = _calibrated(0, gyros[0]); _gyro.y = _calibrated(1, gyros[1]); _gyro.z = _calibrated(2, gyros[2]); // convert corrected accelerometer readings to acceleration // _accel.x = _calibrated(3, accels[0]); _accel.y = _calibrated(4, accels[1]); _accel.z = _calibrated(5, accels[2]); // always updated return true; }