A preliminary control system design for the YF-16 CCV aircraft in its longitudinal mode satisfying its flying qualities specifications is investigated. The design is shown to be robustly stable when the actuator model and the unstable pole in the airframe model of the aircraft are subjected to structured uncertainties. Very recent tools of robust stability analysis are utilized to accomplish this goal.<>


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    Title :

    A robustly stable preliminary control systems design for the YF-16 CCV aircraft


    Contributors:


    Publication date :

    1995-01-01


    Size :

    1038345 byte




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English




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