设计了一种基于脉冲推力/气动力控制的高速动能导弹复合控制系统。首先建立了滚转导弹的数学模型,然后对脉冲推力/气动力复合控制系统工作流程进行了描述,设计了脉冲发动机点火策略;最后通过仿真算例对复合控制方法进行了验证和分析。仿真结果表明:设计的复合控制系统能够有效降低滚转高速动能导弹的发射初始扰动,具有一定的应用价值。

A compound control system of rolling high-speed kinetic energy missile based on impulse thrust/aerodynamic control is designed. Firstly, the mathematical model of rolling high-speed kinetic energy missile is established, then the working flow of the composite control system of impulse thrust/aerodynamic control is described, and the ignition strategy of the impulse engine is designed. Finally, the composite control method is verified and analyzed by a simulation example. The simulation results show that the designed composite control system can effectively reduce the initial disturbance of high-speed rolling kinetic energy missile at launch, and has certain application value.