The purpose of the report is to present a flight control system design, 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. (Author)


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    Title :

    Practical Scheme for Adaptive Aircraft Flight Control Systems


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

    Publication date :

    1973


    Size :

    23 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English






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