In this paper, a flight control law for a simplified F-14 aircraft model is designed based on variable structure control (VSC) theory. For m-input, q-output linear uncertain systems (q


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    Title :

    Variable structure robust flight control system for the F-14


    Contributors:


    Publication date :

    1997-01-01


    Size :

    1489869 byte




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English



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