• DocumentCode
    1598657
  • Title

    An H∞ design for aircraft longitudinal flight control

  • Author

    Li, X.P. ; Chang, B.C.

  • Author_Institution
    Dept. of Mech. Eng. & Mech., Drexel Univ., Philadelphia, PA, USA
  • fYear
    1992
  • Firstpage
    596
  • Abstract
    Step-by-step procedures for applying H∞ control theory to systems design are given. An actual aircraft longitudinal flight control design problem is used to illustrate this process. With the robust controller obtained, simulations and analyses are performed on the closed-loop system
  • Keywords
    aircraft control; closed loop systems; control system synthesis; optimal control; H∞ control; aircraft control; closed-loop system; longitudinal flight control; robust controller; systems design; Aerospace control; Aircraft; Control systems; Control theory; H infinity control; Linear feedback control systems; Robust control; Robust stability; State-space methods; Transfer functions;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control Applications, 1992., First IEEE Conference on
  • Conference_Location
    Dayton, OH
  • Print_ISBN
    0-7803-0047-5
  • Type

    conf

  • DOI
    10.1109/CCA.1992.269782
  • Filename
    269782
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=1598657