Multiple Angle Impact Guidance Law Design for Hypersonic Guided Rockets

Jinping Li, Zhaoyong Mao, Yajun Li, Guannan Chang

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

Abstract

To Guarantee the warhead effectiveness, it usually requires that the hypersonic guided rocket attacks the target with a designated and sufficient large impact angle. To address such problem, a new multiple angle impact guidance law is proposed in this paper. Firstly, the design process of the proposed guidance law with impact angle constraint is presented. Then, the implementation approach of the developed guidance law is analyzed. Finally, the correctness and validity of the guidance law are verified by the simulation of the closed-loop 6-dof model.

Original languageEnglish
Title of host publicationProceedings of 2022 International Conference on Autonomous Unmanned Systems, ICAUS 2022
EditorsWenxing Fu, Mancang Gu, Yifeng Niu
PublisherSpringer Science and Business Media Deutschland GmbH
Pages1349-1355
Number of pages7
ISBN (Print)9789819904785
DOIs
StatePublished - 2023
EventInternational Conference on Autonomous Unmanned Systems, ICAUS 2022 - Xi'an, China
Duration: 23 Sep 202225 Sep 2022

Publication series

NameLecture Notes in Electrical Engineering
Volume1010 LNEE
ISSN (Print)1876-1100
ISSN (Electronic)1876-1119

Conference

ConferenceInternational Conference on Autonomous Unmanned Systems, ICAUS 2022
Country/TerritoryChina
CityXi'an
Period23/09/2225/09/22

Keywords

  • Hypersonic rockets
  • Impact angle constraint
  • Implementation approach
  • Multiple angle impact

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