• DocumentCode
    2428056
  • Title

    Design of an autoland controller for a carrier-based F-14 aircraft using H∞ output-feedback synthesis

  • Author

    Niewoehner, R.J. ; Kaminer, Isaac I.

  • Author_Institution
    Dept. of Aeronaut. & Astronaut., Naval Postgraduate Sch., Monterey, CA, USA
  • Volume
    3
  • fYear
    1994
  • fDate
    29 June-1 July 1994
  • Firstpage
    2501
  • Abstract
    The purpose of this paper is to present the results of a design effort to improve F-14 carrier landing performance by the incorporation of the direct lift control into the aircraft´s control system. This was done using a new design methodology whereby typical SISO design specifications were translated into the weighting functions of an H∞ output-feedback synthesis problem. Finally, a technique is presented for the simplification of the structured uncertainty model for the air vehicles.
  • Keywords
    H∞ control; aircraft control; control system synthesis; feedback; H∞ output-feedback synthesis; H∞ output-feedback synthesis problem; SISO design specifications; air vehicles; autoland controller; carrier-based F-14 aircraft; direct lift control; structured uncertainty model; weighting functions; Aerodynamics; Aerospace control; Aircraft; Automatic control; Bandwidth; Control system synthesis; Control systems; Design methodology; Mathematical model; Uncertainty;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    American Control Conference, 1994
  • Print_ISBN
    0-7803-1783-1
  • Type

    conf

  • DOI
    10.1109/ACC.1994.735009
  • Filename
    735009
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=2428056