Decoupling theory and robust servomechanism theory are applied to the design of linear multivariable systems with large parameter variations. In addition to being approximately decoupled in the transient period, the over-all system achieves tracking and disturbance rejection robustly in the steady state. An example in flight control system is given.


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    Titel :

    Design of flight control systems via robust decoupled servomechanism theory


    Beteiligte:
    Wang, S.-H. (Autor:in) / Davison, E. J. (Autor:in)

    Kongress:

    Joint Automatic Control Conference ; 1979 ; Denver, CO


    Erscheinungsdatum :

    01.01.1979


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :






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