Techniques were developed for the unified design of multimode, variable authority automatic flight-control systems for powered-lift STOL and VTOL aircraft. A structure for such systems is developed to deal with the strong nonlinearities inherent in this class of aircraft, to admit automatic coupling with advanced air traffic control, and to admit a variety of active control tasks. The aircraft being considered is the augmentor wing jet STOL research aircraft. (Author)


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    Title :

    A Formal Structure for Advanced Automatic Flight-Control Systems


    Contributors:
    G. Meyer (author) / L. Cicolani (author)

    Publication date :

    1975


    Size :

    39 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





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