Algebraic functions for each plane of motion, roll, pitch, and yaw, of airframe derived, assuming there is no cross coupling between planes; by use of suitable parameters they have been put in standard servomechanism form, thus assisting design and analysis of control systems for airframes.


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    Title :

    Derivation and use of aerodynamic transfer functions of airframes


    Additional title:

    Roy Aeronautical Soc -- J


    Contributors:

    Published in:

    Publication date :

    1955


    Size :

    19 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :



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