• DocumentCode
    2299318
  • Title

    The propulsive-only flight control problem

  • Author

    Biezad, Daniel J.

  • Author_Institution
    Cal Poly State Univ., San Luis Obispo, CA
  • fYear
    1991
  • fDate
    20-24 May 1991
  • Firstpage
    494
  • Abstract
    Attitude control of aircraft using only the throttles is investigated. The long time constants of both the engines and the aircraft dynamics, together with the coupling between longitudinal and lateral aircraft modes, make piloted flight with failed control surfaces hazardous, especially when trying to land. The author documents the results of in-flight operation using simulated failed flight controls and ground simulations of piloted propulsive-only control to touchdown. Augmentation control laws to assist the pilot are described using both optimal control and classical feedback methods. Piloted simulation using augmentation shows that simple and effective augmented control can be achieved in a wide variety of failed configurations
  • Keywords
    aerospace propulsion; aerospace simulation; aircraft; attitude control; feedback; optimal control; aerospace propulsion; aircraft dynamics; aircraft engine; augmented control; coupling; feedback; ground simulations; in-flight operation; optimal control; piloted flight; propulsive-only flight control; throttles; Aerospace control; Aerospace simulation; Aircraft propulsion; Control systems; Engines; Feedback; Geometry; Military aircraft; Optimal control; Stress control;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace and Electronics Conference, 1991. NAECON 1991., Proceedings of the IEEE 1991 National
  • Conference_Location
    Dayton, OH
  • Print_ISBN
    0-7803-0085-8
  • Type

    conf

  • DOI
    10.1109/NAECON.1991.165797
  • Filename
    165797