• DocumentCode
    2340069
  • Title

    Design of automatic carrier landing system using H∞ control

  • Author

    Suozhong, Yuan ; Yidong, Yang

  • Author_Institution
    Nanjing Univ. of Aeronaut. & Astronaut., China
  • Volume
    5
  • fYear
    2000
  • fDate
    2000
  • Firstpage
    3449
  • Abstract
    In this paper, the design of an automatic carrier landing system (ACLS) is accomplished using H-infinity techniques, in which the single input/output design specifications were translated into the weighting functions of the H-infinity synthesis problem. The objective of the design is to improve the ACLS´s path precision under the worst-case condition of a vertical gust during carrier landing. The design yields a satisfactory response
  • Keywords
    H∞ control; aircraft control; aircraft landing guidance; control system synthesis; marine systems; naval engineering computing; wind; H∞ control; H∞ synthesis problem; aircraft carriers; automatic carrier landing system design; flight control; input/output design specifications; path precision; vertical gust; weighting functions; worst-case condition; Automatic control; Control systems;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Intelligent Control and Automation, 2000. Proceedings of the 3rd World Congress on
  • Conference_Location
    Hefei
  • Print_ISBN
    0-7803-5995-X
  • Type

    conf

  • DOI
    10.1109/WCICA.2000.863180
  • Filename
    863180
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=2340069