• DocumentCode
    3109228
  • Title

    Helicopter Flight Control Law Design Using H∞ Techniques

  • Author

    Kureeemun, R. ; Walker, D.J. ; Manimala, B. ; Voskuijl, M.

  • Author_Institution
    research associate with the University of Liverpool, Flight Science and Technology Group, Department of Engineering, Brownlow Hill, Liverpool, L69 3GH, UK (phone: +44 1517946847, email: r.kureemun@liv.ac.uk).
  • fYear
    2005
  • fDate
    15-15 Dec. 2005
  • Firstpage
    1307
  • Lastpage
    1312
  • Abstract
    This paper describes the development of H∞controllers for two helicpter models. The study was first carried out using rigid body state feedback only and was then extended to include the rotor flap and lag states. It was observed that the H∞controllers gave better robustness and performance than the baseline controllers. Moreover, using rotor state feedback, it was posible to design high bandwidth controllers.
  • Keywords
    Aerospace control; Aircraft; Blades; Control system synthesis; Control systems; Helicopters; Mathematical model; Optimal control; Robust control; State feedback;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Decision and Control, 2005 and 2005 European Control Conference. CDC-ECC '05. 44th IEEE Conference on
  • Conference_Location
    Seville, Spain
  • Print_ISBN
    0-7803-9567-0
  • Type

    conf

  • DOI
    10.1109/CDC.2005.1582339
  • Filename
    1582339
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=3109228