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(sub infinity), output-feedback synthesis problem. Finally, a technique is presented for the simplification of the Structured uncertainty model for the air vehicles.


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    Titel :

    Design of an AutoLand Controller for a Carrier-Based F-14 Aircraft Using H infinity Output-Feedback Synthesis


    Beteiligte:
    R. J. Niewoehner (Autor:in) / I. I. Kaminer (Autor:in)

    Erscheinungsdatum :

    1994


    Format / Umfang :

    6 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch






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