Paper considers control system in which wing flaps and elevator are operated in response to signals of four types of airplane-motion sensors; gust response characteristic of such system is studied on basis of statistical concepts and formulated in mathematical terms; influence of system variables on alleviation is illustrated and utility of each sensor is discussed.


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    Titel :

    Analysis of gust-alleviation system for transport airplanes


    Weitere Titelangaben:

    Japan Soc Aeronautical Space Sciences -- Trans


    Beteiligte:
    Nakagawa, K. (Autor:in)


    Erscheinungsdatum :

    1964


    Format / Umfang :

    10 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


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