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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    Titel :

    Practical Scheme for Adaptive Aircraft Flight Control Systems


    Beteiligte:
    M. Athans (Autor:in) / D. Willner (Autor:in)

    Erscheinungsdatum :

    1973


    Format / Umfang :

    23 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch






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