A Three-dimensional Guidance Law with Impact Angle Constraints

Luqu Xie, Bin Xin*, Shuai Cheng, Miao Guo, Yang Li, Yulong Ding

*Corresponding author for this work

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

Abstract

At present, there are few studies on three-dimensional guidance laws with terminal angle constraints for maneuvering targets. Based on Lyapunov stability theory and considering the coupling effect of yaw channel and pitch channel, this paper designed a nonlinear three-dimensional guidance law, which is suitable for stationary target, constant moving target and maneuvering target, and meets the constraints of miss distance and terminal impact angle. The guidance law has the advantages of simple structure, few parameters and easy engineering implementation. The simulation results show that the proposed guidance law is effective in intercepting different targets at different attack angles, and the guidance law has higher accuracy and reliability than other guidance laws.

Original languageEnglish
Title of host publicationProceedings of the 41st Chinese Control Conference, CCC 2022
EditorsZhijun Li, Jian Sun
PublisherIEEE Computer Society
Pages772-779
Number of pages8
ISBN (Electronic)9789887581536
DOIs
Publication statusPublished - 2022
Event41st Chinese Control Conference, CCC 2022 - Hefei, China
Duration: 25 Jul 202227 Jul 2022

Publication series

NameChinese Control Conference, CCC
Volume2022-July
ISSN (Print)1934-1768
ISSN (Electronic)2161-2927

Conference

Conference41st Chinese Control Conference, CCC 2022
Country/TerritoryChina
CityHefei
Period25/07/2227/07/22

Keywords

  • Guidance law
  • Impact angle constraints
  • Maneuvering target
  • Three-dimensional guidance

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