Disturbance observer based compound control for an air-breathing hypersonic vehicle

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2 Scopus citations

Abstract

A compound control method based on disturbance observer compensation and global fast terminal sliding model control is proposed for an air-breathing hypersonic vehicle (AHV) with considering matching uncertainty and model coupling that existed between longitudinal and lateral-directional. Firstly, we design robust tracking controller for the AHV using nonlinear dynamic inversion and global fast terminal sliding model control method. The terminal sliding model guaranteed the states of flight system converge in limited time, which speeds up convergence of tracking error. Secondly, model coupling is considered as external disturbance and wavelet neural network disturbance observer is used to approximate disturbance and inversion error in order to compensate robust tracking controller. Finally, Numerical simulations have demonstrated the effectiveness of the proposed approach.

Original languageEnglish
Title of host publicationProceedings of the 32nd Chinese Control Conference, CCC 2013
PublisherIEEE Computer Society
Pages632-637
Number of pages6
ISBN (Print)9789881563835
StatePublished - 18 Oct 2013
Event32nd Chinese Control Conference, CCC 2013 - Xi'an, China
Duration: 26 Jul 201328 Jul 2013

Publication series

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

Conference

Conference32nd Chinese Control Conference, CCC 2013
Country/TerritoryChina
CityXi'an
Period26/07/1328/07/13

Keywords

  • Disturbance observer
  • Hypersonic vehicle
  • Matching uncertainty
  • Model coupling
  • Sliding model

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