Reliable H2 static output-feedback tracking control against aircraft wing/control surface impairment

Fang Liao, Jian Liang Wang, Guang Hong Yang

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

8 Citations (Scopus)

Abstract

This paper presents a novel reliable tracking control approach for an aircraft system with wing/control surface impairment faults. The approach is based on multiobjective optimization via affine parameter-dependent Lyapunov functions and an iterative Linear Matrix Inequalities (LMIs) algorithm. The solutions of an initial stabilizing controller used by the iterative algorithm are further studied. The application to an aircraft similar to F-16 with control surface impairment in the horizontal stabilisators illustrates the effectiveness of the proposed approach.

Original languageEnglish
Title of host publicationPhysics and Control
Subtitle of host publicationGeneral Problems and Applications
EditorsI.V. Miroshnik, A.N. Churilov, N.N. Bolotnik, P.V. Pakshin, A.S. Kovaleva, S.D. Zemlyakov, Alexander L. Fradkov, E. Jonckheere
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages112-117
Number of pages6
ISBN (Electronic)078037939X, 9780780379398
DOIs
Publication statusPublished - 2003
Externally publishedYes
Event1st International Conference Physics and Control, PhysCon 2003 - Saint Petersburg, Russian Federation
Duration: 20 Aug 200322 Aug 2003

Publication series

Name2003 International Conference Physics and Control, PhysCon 2003 - Proceedings
Volume1

Conference

Conference1st International Conference Physics and Control, PhysCon 2003
Country/TerritoryRussian Federation
CitySaint Petersburg
Period20/08/0322/08/03

Keywords

  • Aerospace control
  • Aircraft
  • Control systems
  • Ear
  • Iterative algorithms
  • Linear systems
  • Lyapunov method
  • Stability
  • System testing
  • Uncertain systems

ASJC Scopus subject areas

  • Civil and Structural Engineering
  • Control and Systems Engineering
  • Control and Optimization

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