Root locus method is extended to two parameter problems by partitioning characteristic equation in even- and odd-powered polynomials that are then manipulated into root locus form; " stability curve" method presented simplifies system analysis and permits logical choice of numerical values for adjustable parameters; thus ready solution is obtained for problems that are cumbersome by conventional methods; method can be applied to some nonlinear systems to predict existence, frequency, and amplitude of limit cycles.


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    Title :

    Analysis and design of missile and aircraft control systems


    Additional title:

    J Aircraft


    Contributors:
    Han, K.W. (author) / Thaler, G.J. (author)

    Published in:

    Publication date :

    1967


    Size :

    4 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :




    AIRCRAFT MISSILE LAUNCHER

    POVETKIN OLEG VALENTINOVICH / PROKOP EV ARTEM LEONIDOVICH / BIKMUKHAMETOV IBRAGIM NURSAFOVICH et al. | European Patent Office | 2015

    Free access