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A fuzzy guidance law design with terminal-angle constraint

  • Harbin Institute of Technology

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

Abstract

In this paper, a kind of reference trajectory of line-of-sight angle based on the optimal control theory is given, which can make the missile hit the ground fixed target accurately and satisfy the demand for terminal-angle constraint. Then, the corresponding fuzzy control law is designed to achieve the tracking of the reference trajectory of line-of-sight angle. Simulation results show that the proposed fuzzy guidance law has high control precision and can meet the demand for terminal-angle constraint.

Original languageEnglish
Title of host publicationProceedings of the 33rd Chinese Control Conference, CCC 2014
EditorsShengyuan Xu, Qianchuan Zhao
PublisherIEEE Computer Society
Pages749-753
Number of pages5
ISBN (Electronic)9789881563842
DOIs
StatePublished - 11 Sep 2014
EventProceedings of the 33rd Chinese Control Conference, CCC 2014 - Nanjing, China
Duration: 28 Jul 201430 Jul 2014

Publication series

NameProceedings of the 33rd Chinese Control Conference, CCC 2014
ISSN (Print)1934-1768
ISSN (Electronic)2161-2927

Conference

ConferenceProceedings of the 33rd Chinese Control Conference, CCC 2014
Country/TerritoryChina
CityNanjing
Period28/07/1430/07/14

Keywords

  • Terminal-angle constraint
  • fuzzy control
  • line-of-sight angle tracking
  • optimal control

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