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Fault-tolerant flight control for an air-breathing hypersonic vehicle using multivariable sliding mode and neural network

  • Peng Li
  • , Xiang Yu
  • , Jianjun Ma
  • , Zhiqiang Zheng
  • National University of Defense Technology
  • Concordia University
  • Hunan University

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

Abstract

This paper presents a fault-tolerant control (FTC) with integration of neural network (NN) and multivariable sliding mode approaches for an air-breathing hypersonic vehicle (AHV), where both partial loss of effectiveness faults and bias faults in actuators are considered. A radial bias function NN (RBFNN) is derived using on-line updating law to approximate the lumped uncertainties, which consists of actuator faults and system uncertainties. A finite-time convergent multivariable sliding mode control (SMC) is developed against system uncertainties and actuator faults. Simulation results of a generic AHV are provided to demonstrate the effectiveness of the proposed FTC scheme.

Original languageEnglish
Title of host publicationProceedings of the 36th Chinese Control Conference, CCC 2017
EditorsTao Liu, Qianchuan Zhao
PublisherIEEE Computer Society
Pages7247-7252
Number of pages6
ISBN (Electronic)9789881563934
DOIs
StatePublished - 7 Sep 2017
Externally publishedYes
Event36th Chinese Control Conference, CCC 2017 - Dalian, China
Duration: 26 Jul 201728 Jul 2017

Publication series

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

Conference

Conference36th Chinese Control Conference, CCC 2017
Country/TerritoryChina
CityDalian
Period26/07/1728/07/17

Keywords

  • Fault-tolerant control
  • air-breathing hypersonic vehicle
  • multivariable sliding mode
  • neural network

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