导弹协同作战编队飞行控制系统研究

提出了具有3个回路的导弹协同作战编队飞行控制系统，分别对3个回路进行设计分析，并重点分析导弹的四维制导控制外回路和编队控制回路。面向具有过载自动驾驶仪内回路的增广飞控系统，设计了基于总能量控制理论的高度/速度解耦控制器，能够实现导弹制导控制外回路的高度/速度解耦。基于导弹编队队形的位置偏差关系设计了导弹编队控制器，最后综合3个回路构成了导弹编队飞行控制系统。仿真结果表明，各回路以及导弹编队控制系统具有很好的控制性能，能够快速、稳定地完成导弹编队的队形调整动作，进而实现任务规划系统对导弹编队提出的作战任务。

Research on flight control system for missiles cooperative engagement formation

The missiles formation flight control system including of missile inner-loop controller; outer-loop and formation controller is described. The missile formation flight controller and missile outer-loop controller are emphatically analyzed. Facing the augmentative flight control system possessing overload autopilot as a missile inner-loop, a decoupled controller based on the total energy control theory is designed. A combination of proportion and differential control of the position error is used in the design of the missile formation flight controller to generate the control command for the single missile. Simulation result demonstrates that each loop and the missiles formation controller are capable of controlling, and the reconfigure action could be achieved rapidly and stably, and then the engagement mission presented by the mission planning system could be implemented.