Finite-time tracking control with prescribed performance for hypersonic flight vehicle

Fan Jiang*, Shiyue Liu, Xinguo Ma, Fuze Sun

*Corresponding author for this work

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

Abstract

Considering the attitude tracking problem of the hypersonic flight vehicle (HFV) during the reentry phase, a sliding mode control scheme based on finite-time prescribed performance control method is investigated in this paper. To facilitate the controller design, the dynamics model of HFV is developed and transformed into a control-oriented model by feedback linearization (FBL) technique. Then, a finite-time terminal sliding mode controller is designed based on a novel finite-time performance function. The controller is designed to guarantee the convergence of the tracking error within an exact finite time and improve the transient performance of the control system. Finally, the effectiveness of the proposed controller is validated through numerical simulation.

Original languageEnglish
Title of host publicationProceedings of the 43rd Chinese Control Conference, CCC 2024
EditorsJing Na, Jian Sun
PublisherIEEE Computer Society
Pages883-888
Number of pages6
ISBN (Electronic)9789887581581
DOIs
Publication statusPublished - 2024
Event43rd Chinese Control Conference, CCC 2024 - Kunming, China
Duration: 28 Jul 202431 Jul 2024

Publication series

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

Conference

Conference43rd Chinese Control Conference, CCC 2024
Country/TerritoryChina
CityKunming
Period28/07/2431/07/24

Keywords

  • Attitude control
  • Hypersonic flight vehicle
  • Prescribed performance
  • Sliding mode control

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