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Journal of Projectiles, Rockets, Missiles and Guidance >

2014 , Vol. 34 >Issue 1: 13 - 15,20

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2014.01.017

MISSILES AND GUIDANCE TECHNOLOGY

Research on Multi-missile Cooperative Guidance with Angle Constraint

  • ZHANG Baofeng ,
  • SONG Junhong ,
  • SONG Shenmin
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  • Center of Control Theory and Guidance Technology, Harbin Institute of Technology, Harbin 150001, China

Received date: 2013-04-24

  Online published: 2025-05-29

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Abstract

The paper is devoted to design a kind of cooperative guidance law of missiles with angle constraint for relative motion between missile and target in two-dimension plane. Two kinds of guidance law satisfy the attack time and terminal angle are proposed respectively by use of sliding mode variable structure control. To take account of time-coordination and angle constraint, a reasonable distribution is taken to make missiles choose the law in different situation. Time-to-go estimate is considered as the interactive information among missiles to obtain the common attack time. The simulation results demonstrate the method is valid.

Key words： guidance law; SMVSC; coordinated attack; angle constraint

Cite this article

ZHANG Baofeng , SONG Junhong , SONG Shenmin . Research on Multi-missile Cooperative Guidance with Angle Constraint[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2014 , 34(1) : 13 -15,20 . DOI: 10.15892/j.cnki.djzdxb.2014.01.017

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