A solid state turn coordinator display which employs light emitting diodes (LED's) as the display medium was developed to demonstrate the feasibility of such displays for aircraft applications. The input to the display is supplied by a fluidic inertial rate sensor used in an aircraft wing leveler system. The display is composed of the LED radial display face and the electronics necessary to address and drive the individual lines of LED's. Three levels of brightness are provided to compensate for the different amounts of ambient light present in the cockpit.


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    Titel :

    Solid-state turn coordinator display


    Beteiligte:
    Meredith, B. D. (Autor:in) / Crouch, R. K. (Autor:in) / Kelly, W. L., IV (Autor:in)

    Erscheinungsdatum :

    01.08.1975


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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