A Full-trajectory Design Method for a Waverider Hypersonic Vehicle with Boost-glide-attack Process

Haoming Shi, Zhiqi Niu, Lu Hun, Penghui Zhang, Feifei Wang, Liangyu Zhao*

*Corresponding author for this work

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

Abstract

A guidance controller is designed for the boost-glide waverider hypersonic vehicle, which can meet the requirements of the whole flight. The task of reaching the desired altitude and velocity at the end of the boost phase will be achieved through the controller. So that the vehicle can perform long distance maneuvers in the condition of quasi-balanced glide, and finally dive to hit the target. The performance of the controller is verified by simulation. The guidance controller can make the hypersonic vehicle to complete the flight task and meet the control requirements of hypersonic vehicle maneuver.

Original languageEnglish
Title of host publicationProceedings - 2023 38th Youth Academic Annual Conference of Chinese Association of Automation, YAC 2023
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages756-761
Number of pages6
ISBN (Electronic)9798350303636
DOIs
Publication statusPublished - 2023
Event38th Youth Academic Annual Conference of Chinese Association of Automation, YAC 2023 - Hefei, China
Duration: 27 Aug 202329 Aug 2023

Publication series

NameProceedings - 2023 38th Youth Academic Annual Conference of Chinese Association of Automation, YAC 2023

Conference

Conference38th Youth Academic Annual Conference of Chinese Association of Automation, YAC 2023
Country/TerritoryChina
CityHefei
Period27/08/2329/08/23

Keywords

  • dive guidance
  • full-trajectory
  • hypersonic vehicle
  • quasi-balanced glide

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