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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    Titel :

    Analysis and design of missile and aircraft control systems


    Weitere Titelangaben:

    J Aircraft


    Beteiligte:
    Han, K.W. (Autor:in) / Thaler, G.J. (Autor:in)

    Erschienen in:

    Journal of Aircraft ; 4 , n 2 ; p 121-124


    Erscheinungsdatum :

    1967


    Format / Umfang :

    4 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :




    AIRCRAFT MISSILE LAUNCHER

    POVETKIN OLEG VALENTINOVICH / PROKOP EV ARTEM LEONIDOVICH / BIKMUKHAMETOV IBRAGIM NURSAFOVICH et al. | Europäisches Patentamt | 2015

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