• DocumentCode
    486586
  • Title

    Time Scale Analysis of a Digital Flight Control System

  • Author

    Naidu, D.S. ; Price, D.B.

  • Author_Institution
    NASA Langley Research Center, Hampton, VA 23665
  • fYear
    1986
  • fDate
    18-20 June 1986
  • Firstpage
    509
  • Lastpage
    510
  • Abstract
    In this paper, we consider the fifth order discrete model of an aircraft (longitudinal) control system which possesses three slow (velocity, pitch angle and altitude) and two fast (angle of attack and pitch angular velocity) modes and exhibits a two-time scale property. Using the recent results of the time scale analysis of discrete control systems, the high-order discrete model is decoupled into low-order slow and fast subsystems. The results of the decoupled system are found to be in excellent agreement with those of the original system.
  • Keywords
    Aerospace control; Aerospace safety; Aircraft; Angular velocity; Angular velocity control; Bismuth; Control system analysis; Control system synthesis; NASA; Riccati equations;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    American Control Conference, 1986
  • Conference_Location
    Seattle, WA, USA
  • Type

    conf

  • Filename
    4788993