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Coordinated guidance strategy for heterogeneous missiles intercepting hypersonic weapon

  • Beihang University

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

Abstract

To solve the defense problem of hypersonic weapon, a coordinated guidance strategy based on modified proportional navigation guidance law and consensus algorithms for heterogeneous interceptor missiles is proposed. The heterogeneous missiles are classified into leader missile and follower missiles. The leader missile is equipped with high-performance seeker, intercepting the target under modified proportional navigation guidance law. The low-cost follower missiles track the leader missile by consensus algorithms. A consensus tracking protocol which can be used to guide the heterogeneous missiles hitting the target simultaneously is investigated. The Necessary and sufficient conditions for heterogeneous missiles to intercept the hypersonic weapon are presented. Finally the effectiveness of the coordinated guidance strategy is demonstrated by numerical simulations.

Original languageEnglish
Title of host publicationProceedings of the 34th Chinese Control Conference, CCC 2015
EditorsQianchuan Zhao, Shirong Liu
PublisherIEEE Computer Society
Pages5170-5175
Number of pages6
ISBN (Electronic)9789881563897
DOIs
StatePublished - 11 Sep 2015
Event34th Chinese Control Conference, CCC 2015 - Hangzhou, China
Duration: 28 Jul 201530 Jul 2015

Publication series

NameChinese Control Conference, CCC
Volume2015-September
ISSN (Print)1934-1768
ISSN (Electronic)2161-2927

Conference

Conference34th Chinese Control Conference, CCC 2015
Country/TerritoryChina
CityHangzhou
Period28/07/1530/07/15

Keywords

  • Consensus Tracking
  • Coordinated Guidance
  • Hypersonic Vehicle
  • Modified Proportional Navigation Guidance Law

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