• DocumentCode
    487477
  • Title

    H∞-optimal design for helicopter control

  • Author

    Yue, Andrew ; Postlethwaite, Ian

  • Author_Institution
    University of Oxford, Department of Engineering Science, Oxford, OX1 3PJ, England.
  • fYear
    1988
  • fDate
    15-17 June 1988
  • Firstpage
    1679
  • Lastpage
    1684
  • Abstract
    This paper presents the results of a study into the use of H∞ - optimization for the design of robust feedback control laws for improving the handling qualities of a battlefield helicopter. Control laws are designed for precise control of pitch and roll attitude, yaw rate and heave velocity in in the hover flight condition.
  • Keywords
    Bandwidth; Design engineering; Design optimization; Frequency domain analysis; Helicopters; Nonlinear dynamical systems; Robust control; Transfer functions; Uncertainty; Velocity control;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    American Control Conference, 1988
  • Conference_Location
    Atlanta, Ga, USA
  • Type

    conf

  • Filename
    4789990
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=487477