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Journal of Projectiles, Rockets, Missiles and Guidance >

2022 , Vol. 42 >Issue 3: 69 - 73

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2022.03.014

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

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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.

Key words： multi-missile formation; sliding mode variable structure; the line of sight

Cite this article

WEI Shihui , YANG Chunwei , LIU Bingqi , WANG Jiping , ZHANG Zhenlin . Research on a New Multi-missile Formation Controller Design Method[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2022 , 42(3) : 69 -73 . DOI: 10.15892/j.cnki.djzdxb.2022.03.014

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