Data about the airspeed, altitude, pitch, acceleration, roll, fuel, and the list goes on and on.
这些数据包括飞行速度、高度、俯仰、加速度、晃动、燃油等情况。
2
So, variable structure control theory is used in Angle stabilization of roll, and model - following variable structure control theory is used in acceleration stabilization of pitch and yaw.