• DocumentCode
    489694
  • Title

    Control of a High Performance Aircraft with Unacceptable Zerodynamics

  • Author

    Gopalswamy, Swaminathan ; Hedrick, J. Karl

  • fYear
    1992
  • fDate
    24-26 June 1992
  • Firstpage
    1834
  • Lastpage
    1838
  • Abstract
    Nonlinear control techniques such as sliding control cannot be directly applied to control the dynamics of many high performance aircraft such as the AFTI-FI6, as they exhibit unacceptable zerodynamics. Traditionally, approximations have been resorted to, to overcome this problem. In this paper, we apply an "output redefinition" technique to systematically overcome the serodynamics problem, resulting in precise, local, tracking. Computer simulations of high g-commands illustrate that while acceptable tracking can be achieved through the output-redefinition technique, standard nonlinear techniques fail.
  • Keywords
    Actuators; Aerodynamics; Aerospace control; Aerospace engineering; Aircraft propulsion; Computer simulation; Control systems; High performance computing; Nonlinear control systems; Sliding mode control;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    American Control Conference, 1992
  • Conference_Location
    Chicago, IL, USA
  • Print_ISBN
    0-7803-0210-9
  • Type

    conf

  • Filename
    4792429