A flight control system design is presented, that can be implemented by analog hardware, to be used to control an aircraft with uncertain parameters. The design is based upon the use of modern control theory. The ideas are illustrated by considering control of STOL longitudinal dynamics.


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    Title :

    A practical scheme for adaptive aircraft flight control systems


    Contributors:
    Athans, M. (author) / Willner, D. (author)


    Publication date :

    1974-04-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English


    Keywords :




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