• DocumentCode
    754515
  • Title

    VSTOL first flight on an H/sub infinity / control law

  • Author

    Hyde, R.A. ; Glover, K. ; Shanks, G.T.

  • Author_Institution
    Dept. of Eng., Cambridge Univ., UK
  • Volume
    6
  • Issue
    1
  • fYear
    1995
  • Firstpage
    11
  • Lastpage
    16
  • Abstract
    An H/sub infinity / control law has been successfully flight tested on the DRA Bedford Harrier. This and subsequent flight tests demonstrated the practicality and power of H/sub infinity / as a design tool for systems with multiple inputs and outputs. The technique has potential both to reduce design time, and to improve robustness and performance for such systems. This article discusses the development of the control law and some of the challenging implementation issues which had to be addressed in order to bridge the gap between theory and practice.<>
  • Keywords
    aerospace control; aircraft control; control system CAD; military aircraft; DRA Bedford Harrier; H/sub infinity / control law; VSTOL; advanced short take off and vertical landing aircraft; aerodynamic control; control law; design time; design tool; flight control; flight tested; multiple inputs; multiple outputs; performance; robustness; Aerospace control; Aircraft control; Control systems; Design automation; Military aircraft;
  • fLanguage
    English
  • Journal_Title
    Computing & Control Engineering Journal
  • Publisher
    iet
  • ISSN
    0956-3385
  • Type

    jour

  • DOI
    10.1049/cce:19950107
  • Filename
    372707