• DocumentCode
    2098582
  • Title

    H∞ control design method combined with exact model matching-design of longitudinal robust flight control system

  • Author

    Ohno, M. ; Takahama, M. ; Kimura, T. ; Tokuda, E.

  • Author_Institution
    Aerospace Syst. Works, Mitsubishi Heavy Ind. Ltd., Nagoya, Japan
  • fYear
    1993
  • fDate
    15-17 Dec 1993
  • Firstpage
    447
  • Abstract
    In this paper, a new method is proposed to design a robust flight control system which is low-sensitive and robust stable. This method can realize pole-zero assignment by exact model matching (EMM), moreover this can achieve disturbance minimizing by H∞ control methods (output estimation problem). The application of this method for a design of control augmentation system for the longitudinal flight control system of a typical small aircraft is also shown
  • Keywords
    aircraft control; control system synthesis; model reference adaptive control systems; optimal control; poles and zeros; stability; H∞ control design; control augmentation system; disturbance minimization; exact model matching; longitudinal flight control system; longitudinal robust flight control system; low-sensitivity system; output estimation problem; pole-zero assignment; small aircraft; Aerodynamics; Aerospace control; Aerospace industry; Aircraft; Content addressable storage; Control design; Design methodology; Robust control; State estimation; Transfer functions;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Decision and Control, 1993., Proceedings of the 32nd IEEE Conference on
  • Conference_Location
    San Antonio, TX
  • Print_ISBN
    0-7803-1298-8
  • Type

    conf

  • DOI
    10.1109/CDC.1993.325107
  • Filename
    325107
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=2098582