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一种新型多弹编队控制器设计方法研究

  • 魏诗卉 1 ,
  • 杨春伟 1 ,
  • 刘炳琪 1 ,
  • 王继平 1 ,
  • 张振林 2
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  • 1 96901部队, 北京 100096
  • 2 西北工业大学航天学院, 西安 710072

魏诗卉(1978—),女,山东广饶人,研究员级高级工程师,博士,研究方向:飞行器导航、制导与控制。

收稿日期: 2021-12-06

  网络出版日期: 2025-02-03

Research on a New Multi-missile Formation Controller Design Method

  • WEI Shihui 1 ,
  • YANG Chunwei 1 ,
  • LIU Bingqi 1 ,
  • WANG Jiping 1 ,
  • ZHANG Zhenlin 2
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  • 1 No.96901 Unit, Beijing 100096, China
  • 2 School of Astronautics, Northwestern Polytechnical University, Xi’an 710072, China

Received date: 2021-12-06

  Online published: 2025-02-03

摘要

针对多导弹编队问题,提出了一种将领弹看作虚拟目标,在视线系下进行多导弹编队控制器设计的新型编队控制方法。首先,将领弹看作虚拟目标,建立了视线系下从弹和虚拟目标之间的相对运动方程;其次,将弹目距离、视线倾角和视线偏角看作状态变量,计算出实际值与期望值间的误差以及误差的一阶和二阶导数,然后采用滑模变结构控制理论设计了多导弹编队控制器;最后,针对一领弹二从弹的编队结构进行仿真验证。仿真结果表明所提方法的可行性和有效性。

本文引用格式

魏诗卉 , 杨春伟 , 刘炳琪 , 王继平 , 张振林 . 一种新型多弹编队控制器设计方法研究[J]. 弹箭与制导学报, 2022 , 42(3) : 69 -73 . DOI: 10.15892/j.cnki.djzdxb.2022.03.014

Abstract

Aiming at the problem of multi-missile formation, this paper proposes a new type of formation control method that regards the leader missile as a virtual target and designs the multi-missile formation controller under the line of sight system. Firstly, the leader projectile is regarded as a virtual target, and the relative motion equation between the follower projectile and the virtual target under the line of sight system is established. Secondly, the projectile-eye distance, the line of sight inclination angle and the line of sight deflection are regarded as state variables, and the actual value and the expected value are calculated. Then, the multi-missile formation controller is designed by using sliding mode variable structure control theory. Finally, the formation structure of one lead missile and two follower missiles is simulated and verified. The simulation results show the feasibility and effectiveness of the method.

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