• DocumentCode
    2146838
  • Title

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

  • Author

    Liao, Fang ; Jian Liang Wang ; Yang, Guang-hong

  • Author_Institution
    Sch. of Electr. & Electron. Eng., Nanyang Technol. Univ., Singapore
  • Volume
    1
  • fYear
    2003
  • fDate
    20-22 Aug. 2003
  • Firstpage
    112
  • 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.
  • Keywords
    Lyapunov methods; aircraft control; feedback; iterative methods; linear matrix inequalities; optimisation; tracking; H2 static output feedback; LMI; aircraft system; aircraft wing impairment; controller; horizontal stabilisers; iterative algorithm; iterative linear matrix inequalities; multiobjective optimization; parameter dependent Lyapunov functions; surface impairment faults; tracking control; Aerospace control; Aircraft; Control systems; Ear; Iterative algorithms; Linear systems; Lyapunov method; Stability; System testing; Uncertain systems;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Physics and Control, 2003. Proceedings. 2003 International Conference
  • Print_ISBN
    0-7803-7939-X
  • Type

    conf

  • DOI
    10.1109/PHYCON.2003.1236798
  • Filename
    1236798
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=2146838