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Terminal guidance law design based on predictive control for aerodynamic missile with side window detection

  • Harbin Institute of Technology

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

Abstract

In this paper, terminal guidance problem for aerodynamic missile with side window detection is considered. Firstly, the description of side window constraint is given. In order to formulate this guidance problem as a control problem with input constraint, side window constraint is transformed into attack angle constraint. Then the terminal guidance law is designed based on predictive control. Simulation results are given to show the effectiveness of the proposed guidance law design approach.

Original languageEnglish
Title of host publicationProceedings of the 34th Chinese Control Conference, CCC 2015
EditorsQianchuan Zhao, Shirong Liu
PublisherIEEE Computer Society
Pages5212-5217
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

  • Aerodynamic missile
  • predictive control
  • side window constraint
  • terminal guidance law

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