The paper designed aerodynamic control system of pith and yaw channels and roll angle stabilization system, by using unsteady-state error follow-up control theory and state observation station theory in modern control theory.

• 本文使用现代控制理论中的无静差跟踪控制系统理论与状态观测器理论，设计了俯仰、偏航两个通道的气动力控制系统和滚转角稳定系统。