Development of flight simulation and supporting elements; control system dynamics element heart of which is closed-loop electro-hydraulic servo system, is described; system takes force signal from force transducer on stick to computer model which computes commanded stick position and sends it to high-response hydraulic servo which positions stick; test results show that friction is most significant control system property in small stick deflection range of flying.


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    Titel :

    Flight control studies in small stick deflection area


    Weitere Titelangaben:

    AIAA -- Simulation Aerospace Flight Conference -- Tech Papers


    Beteiligte:
    Bird, D. (Autor:in)

    Kongress:

    AIAA Meeting -- Simulation for Aerospace Flight Conference ; 1963 Simulators



    Erscheinungsdatum :

    1963


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :