To utilize ability of military aircraft to fly in all attitudes, or to enable civil VTOL passenger aircraft to accomplish vertical takeoff, some all-attitude gyro reference element is required; instrument problems obstructing development of such idealized master stable platform; features of 2-gyro, 4-axis, all attitude control system; its functions, basic elements and components.


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    Title :

    New stable platform for today's aircraft today


    Additional title:

    Aeronautical Eng Rev


    Contributors:

    Published in:

    Publication date :

    1958


    Size :

    7 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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