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Guidance law based on finite time consensus theory for simultaneous arrival

  • Harbin Institute of Technology

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

Abstract

A guidance law is designed for simultaneous arrival by cooperative control theory. The main contributions of research work presented in this paper include: (1) problem of multiple flight vehicles simultaneous arrival is converted to the problem of multiple flight vehicles system consensus, and (2) in addition, the problem of consensus is solving by finite time consensus technology. Method to estimate the time-to-go of flight vehicle is presented. Salvo attack is described in this paper. Simulations of a three flight vehicles again one target case is presented to demonstrate the effectiveness of the proposed approaches.

Original languageEnglish
Title of host publicationProceedings of the 35th Chinese Control Conference, CCC 2016
EditorsJie Chen, Qianchuan Zhao, Jie Chen
PublisherIEEE Computer Society
Pages5519-5524
Number of pages6
ISBN (Electronic)9789881563910
DOIs
StatePublished - 26 Aug 2016
Event35th Chinese Control Conference, CCC 2016 - Chengdu, China
Duration: 27 Jul 201629 Jul 2016

Publication series

NameChinese Control Conference, CCC
Volume2016-August
ISSN (Print)1934-1768
ISSN (Electronic)2161-2927

Conference

Conference35th Chinese Control Conference, CCC 2016
Country/TerritoryChina
CityChengdu
Period27/07/1629/07/16

Keywords

  • Guidance law
  • consensus
  • simultaneous arrival

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