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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    Title :

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


    Contributors:

    Publication date :

    1994


    Size :

    6 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English






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