Virtual target based optimal guidance law with impact angle and burst height constrains

Zhe Yang, Zhengjie Wang, Ningjun Fan

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

1 Citation (Scopus)

Abstract

With the development of missile and warhead, new performance requirements of guidance law such as impact angle and burst height constrains are paid more attention. In this paper, an optimal guidance law with impact angle and burst height constrains is researched based on the virtual target. Firstly, the general kinematic model of pursuit-evasion of the missile and target is established. Secondly, the virtual target scheme including its movement characteristics are proposed. And then, an optimal guidance law is designed to attack the virtual target using the θ-D method solving. Finally, a numerical simulation is conducted and the result shows that the guidance law proposed has a high accuracy and it can satisfy constrains of impact angle and burst height.

Original languageEnglish
Title of host publicationProceedings of 2015 7th International Conference on Modelling, Identification and Control, ICMIC 2015
PublisherInstitute of Electrical and Electronics Engineers Inc.
ISBN (Electronic)9780956715753
DOIs
Publication statusPublished - 16 Feb 2016
Event7th International Conference on Modelling, Identification and Control, ICMIC 2015 - Sousse, Tunisia
Duration: 18 Dec 201520 Dec 2015

Publication series

NameProceedings of 2015 7th International Conference on Modelling, Identification and Control, ICMIC 2015

Conference

Conference7th International Conference on Modelling, Identification and Control, ICMIC 2015
Country/TerritoryTunisia
CitySousse
Period18/12/1520/12/15

Keywords

  • burst height
  • guidance law
  • impact angle
  • optimal control
  • virtual target
  • θ-D method

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