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Three-dimensional finite-time guidance law with impact angle constraints

  • Harbin Institute of Technology

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

Abstract

To intercept stationary targets at desired impact angle, the three-dimensional terminal guidance problem has been investigated in this paper. Different from the traditional method of decoupling the engagement dynamics into two mutually orthogonal two-dimensional planes, the guidance law design is studied using three-dimensional coupled engagement dynamics. Because of the short terminal guidance time, the finite-time convergence guidance law is proposed in this paper on the basis of the fast nonsingular terminal sliding mode control theory, which guarantees finite-time convergence to the desired impact angle. Numerical simulations have demonstrated that the two guidance laws have effective performance and outperform the traditional terminal guidance laws.

Original languageEnglish
Title of host publicationProceedings of the 36th Chinese Control Conference, CCC 2017
EditorsTao Liu, Qianchuan Zhao
PublisherIEEE Computer Society
Pages5747-5753
Number of pages7
ISBN (Electronic)9789881563934
DOIs
StatePublished - 7 Sep 2017
Event36th Chinese Control Conference, CCC 2017 - Dalian, China
Duration: 26 Jul 201728 Jul 2017

Publication series

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

Conference

Conference36th Chinese Control Conference, CCC 2017
Country/TerritoryChina
CityDalian
Period26/07/1728/07/17

Keywords

  • Finite-time guidance law
  • Impact angle constraint
  • Terminal sliding mode control
  • Three-dimensional guidance law

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