Fault-tolerant controller based on integral sliding mode with prescribed performance for hypersonic re-entry vehicle

Fuhui Guo, Xiangdong Liu, Xingsheng Li

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

1 Citation (Scopus)

Abstract

This paper investigates a fault-tolerant controller (FTC) for the attitude tracking problem of hypersonic re-entry vehicle(HRV) against unknown actuator faults, which aims at improving both transient behavior and steady-state performance of defective system. Attitude dynamics of re-entry vehicle is modeled as control-oriented form. Based on the form, a FTC combining integral sliding mode with compensation scheme via fault observer is adopted to realize reference command tracking Meanwhile, a prescribed performance function (PPF) is chosen as an important constraint condition to increase convergence rate and reduce steady-state error especially when failure occurs. Simulation results illustrate that the proposed fault-tolerant controller succeeds in attitude tracking with better performance.

Original languageEnglish
Title of host publicationProceedings of the 38th Chinese Control Conference, CCC 2019
EditorsMinyue Fu, Jian Sun
PublisherIEEE Computer Society
Pages5012-5017
Number of pages6
ISBN (Electronic)9789881563972
DOIs
Publication statusPublished - Jul 2019
Event38th Chinese Control Conference, CCC 2019 - Guangzhou, China
Duration: 27 Jul 201930 Jul 2019

Publication series

NameChinese Control Conference, CCC
Volume2019-July
ISSN (Print)1934-1768
ISSN (Electronic)2161-2927

Conference

Conference38th Chinese Control Conference, CCC 2019
Country/TerritoryChina
CityGuangzhou
Period27/07/1930/07/19

Keywords

  • Attitude Control
  • Fault-Tolerant
  • Integral Sliding Mode
  • Prescribed Performance
  • Re-entry Vehicle

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