Multi-missile cooperative guidance using coordination variables

  • Shiyu Zhao*
  • , Rui Zhou
  • *Corresponding author for this work

Research output: Contribution to journalArticlepeer-review

Abstract

A two-level cooperative guidance architecture for multi-missile attack is proposed. The architecture is composed with local guidance for each missile on the lower level and a coordination strategy on the upper le-vel. It provides a general solution to some categories of multi-missile cooperative control problems. Based on the notion of decentralized guidance and centralized coordination, an application of the architecture to the salvo attack is investigated. A new practical cooperative guidance law, which could automatically guide missiles to hit the stationary target simultaneously, is devised. It is a combination of the guidance law with constraint on guidance time and the coordination strategy based on coordination variables. The cooperative guidance law is quite feasible because of its analytical form, and it is suboptimal in the sense of control energy. Numerical simulations are presented to demonstrate the effectiveness of the cooperative guidance law.

Original languageEnglish
Pages (from-to)1605-1611
Number of pages7
JournalHangkong Xuebao/Acta Aeronautica et Astronautica Sinica
Volume29
Issue number6
StatePublished - Nov 2008

Keywords

  • Cooperative guidance
  • Coordination strategy
  • Coordination variable
  • Guidance law
  • Multi-missile

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