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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    Titel :

    Aircraft instrumentation and display system-adaptation of tactile link


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Hirsch, J. (Autor:in)

    Kongress:

    SAE Meeting ; 1962



    Erscheinungsdatum :

    1962


    Format / Umfang :

    4 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



    Tactile Display for Aircraft Control

    D. H. Ross / R. A. Sanneman / W. H. Levison et al. | NTIS | 1973


    Aircraft instrumentation

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