Robust tracking control for the hypersonic flight vehicle via backstepping method

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Abstract

The problem of output tracking control is addressed for the longitudinal dynamics of a generic hypersonic flight vehicle. For the altitude subsystem and velocity subsystem, the dynamics is transformed into block-triangular form where the backstepping scheme is used. This problem is challenging due to the nonlinear uncertain complex interactions between the altitude and velocity subsystems. A new design approach of robust controller is proposed by combining standard backstepping with signal compensation method. It is shown that semiglobal robust stability and semiglobal robust practical tracking property of the closed-loop system can be ensured and the tracking error can be made as small as desired.

Original languageEnglish
Title of host publicationProceedings of the 33rd Chinese Control Conference, CCC 2014
EditorsShengyuan Xu, Qianchuan Zhao
PublisherIEEE Computer Society
Pages4306-4311
Number of pages6
ISBN (Electronic)9789881563842
DOIs
StatePublished - 11 Sep 2014
Externally publishedYes
EventProceedings of the 33rd Chinese Control Conference, CCC 2014 - Nanjing, China
Duration: 28 Jul 201430 Jul 2014

Publication series

NameProceedings of the 33rd Chinese Control Conference, CCC 2014
ISSN (Print)1934-1768
ISSN (Electronic)2161-2927

Conference

ConferenceProceedings of the 33rd Chinese Control Conference, CCC 2014
Country/TerritoryChina
CityNanjing
Period28/07/1430/07/14

Keywords

  • Backstepping
  • Hypersonic vehicle
  • MIMO
  • Nonlinear
  • Robust

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