A proposed method whereby a system using a coding of vibratory tactile stimuli as an aid in aircraft control is considered. By this method, pitch, roll, and yaw accelerations are automatically transmitted as tactile stimuli to a ground control operator who steers an aircraft in the air. The system is described and analyzed. The advantages of receiving a combination of tactual and visual data, and making corrections based on the resultant are explained.


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    Titel :

    Aircraft Instrumentation and Display System-Adaptation of Tactile Link


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Hirsch, Joseph (Autor:in)

    Kongress:

    Pre-1964 SAE Technical Papers ; 1906



    Erscheinungsdatum :

    01.01.1962




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch





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    Demler, M.C. | Engineering Index Backfile | 1958