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


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    Title :

    Aircraft instrumentation and display system-adaptation of tactile link


    Additional title:

    SAE -- Paper


    Contributors:
    Hirsch, J. (author)

    Conference:

    SAE Meeting ; 1962



    Publication date :

    1962


    Size :

    4 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English





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