New approach to problem of designing intercoupled multiloop control systems; method illustrated by design of fully automatic air-speed-altitude control for Northrop F-61C airplane; by satisfying requirement that thrust and pitch attitude be controlled in cordination, method allows separate design of air speed and altitude control functions.


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    Title :

    Design method for automatic longitudinal control systems


    Additional title:

    Aeronautical Eng Rev


    Contributors:

    Published in:

    Publication date :

    1951


    Size :

    6 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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