• DocumentCode
    3268065
  • Title

    A study of longitudinal flight maneuvers for the CTOL aircraft model

  • Author

    Al-Hiddabi, Saif A. ; McClamroch, N. Harris

  • Author_Institution
    Dept. of Aerosp. Eng., Michigan Univ., Ann Arbor, MI, USA
  • Volume
    2
  • fYear
    1999
  • fDate
    1999
  • Firstpage
    1199
  • Abstract
    We study several flight control problems for a conventional aircraft take off and landing (CTOL) flight control model, a simplified model for aircraft longitudinal flight dynamics. In particular, we study the execution of a maneuver for which the aircraft is intended to follow a path in a vertical plane corresponding to specified change in altitude. We formulate the problem as a nonlinear tracking control problem. Controllers are developed for two cases: a non-aggressive maneuver, corresponding to a small altitude change, and an aggressive maneuver, corresponding to a large altitude change. We demonstrate the need to develop a controller that includes feedforward terms in order to achieve aggressive maneuvering. Our approach throughout is to make use of nonlinear control theory, which is complicated by the non-minimum phase characteristics of the CTOL model
  • Keywords
    aircraft control; closed loop systems; dynamics; feedback; feedforward; nonlinear control systems; CTOL aircraft model; flight control; longitudinal flight maneuvers; nonaggressive maneuver; nonlinear tracking control problem; nonminimum phase characteristics; vertical plane; Aerodynamics; Aerospace control; Aircraft propulsion; Control design; Control systems; Control theory; Drag; Equations; Liquid crystal on silicon; Motion control;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control Applications, 1999. Proceedings of the 1999 IEEE International Conference on
  • Conference_Location
    Kohala Coast, HI
  • Print_ISBN
    0-7803-5446-X
  • Type

    conf

  • DOI
    10.1109/CCA.1999.801143
  • Filename
    801143