Relative Maneuver and Minimum Effort Guidance Under Gravity

Lan Wei, Yadong Chen*, Dawei Liu, Shuai Dong, Junhui Liu

*Corresponding author for this work

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

Abstract

This paper considers the guidance problem from a relative motion perspective. Acceleration, caused by gravity, of the interceptor is considered as the target's relative maneuver. The optimal guidance problem is designed to minimize the interceptor's real control effort, that is the normal acceleration in addition to gravity. Then the minimum effort guidance law is derived, where the relative maneuver caused by gravity is utilized rather than overcome during guidance. Finally, the performance of the proposed guidance law is proved through numerical simulations.

Original languageEnglish
Title of host publication2023 42nd Chinese Control Conference, CCC 2023
PublisherIEEE Computer Society
Pages3743-3747
Number of pages5
ISBN (Electronic)9789887581543
DOIs
Publication statusPublished - 2023
Event42nd Chinese Control Conference, CCC 2023 - Tianjin, China
Duration: 24 Jul 202326 Jul 2023

Publication series

NameChinese Control Conference, CCC
Volume2023-July
ISSN (Print)1934-1768
ISSN (Electronic)2161-2927

Conference

Conference42nd Chinese Control Conference, CCC 2023
Country/TerritoryChina
CityTianjin
Period24/07/2326/07/23

Keywords

  • Optimal guidance
  • PNG
  • minimum effort

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