Diagram representing aircraft in either its lateral or longitudinal motion, used to explain aircraft response in antisymmetric stick fixed case; generalized autopilot is added to aircraft diagram and method of analyzing combination by conventional servo techniques indicated; how estimate can be made of effects on stability of nonlinearities in output member of control system.


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    Title :

    Application of block diagram representation to aircraft stability analysis


    Additional title:

    Aeronautical Quarterly


    Contributors:

    Published in:

    Publication date :

    1958


    Size :

    21 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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