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.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    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:

    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

    Freier Zugriff


    AIRCRAFT IMPACT MISSILE SYSTEM

    DUROV DMITRIJ SERGEEVICH | Europäisches Patentamt | 2020

    Freier Zugriff