空空导弹越肩发射侧向运动控制器设计

针对空空导弹越肩发射过程，设计了偏航及横滚运动的控制系统。首先分析了越肩发射过程中大攻角阶段的气动特性，提出了控制设计的目标，然后建立了包含未建模特性的偏航/横滚运动方程，在此基础上，利用滑模变结构理论设计了两通道的控制系统，仿真结果表明了该设计方法的有效性。

Control Design of Lateral Motion in Over-the-shoulder Launch of Air-to-air Missile

For the over-the-shoulder launch of air-to-air missile, control system of yaw movement and roll movement is designed. First, aerodynamic characteristic of the high angle of attack in over-the-shoulder launch is analyzed, and the aim of control design is proposed. Then, the mathematical model of yaw movement and roll movement, containing uncertainty, is established. Based on the mathematical model, control system of the two channel is designed using sliding mode theory. At last, simulation results show the effectiveness of the proposed design method.