• DocumentCode
    2132130
  • Title

    Rotorcraft control law design for rejection of atmospheric turbulence

  • Author

    Postlethwaite, I. ; Foster, N.P. ; Walker, D.J.

  • Author_Institution
    Leicester Univ., UK
  • Volume
    2
  • fYear
    1994
  • fDate
    21-24 March 1994
  • Firstpage
    1284
  • Abstract
    This paper will describe the results of an ongoing investigation into controller design for the rejection of atmospheric turbulence. The gust disturbance is considered as an extra input to the well-known Hinfinity mixed sensitivity design formulation. Results from the nonlinear simulations are presented, and these show significant improvement in the helicopters performance.
  • Keywords
    aircraft control; control system synthesis; helicopters; nonlinear control systems; optimal control; H infinity mixed sensitivity design formulation; atmospheric turbulence rejection; gust disturbance; helicopter; nonlinear simulations; rotorcraft control law design;
  • fLanguage
    English
  • Publisher
    iet
  • Conference_Titel
    Control, 1994. Control '94. International Conference on
  • Conference_Location
    Coventry, UK
  • Print_ISBN
    0-85296-610-5
  • Type

    conf

  • DOI
    10.1049/cp:19940322
  • Filename
    327288
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=2132130