Non-linear averaged-value models are derived for the twelve-pulse rectifiers that typically form the input stage of more electric aircraft actuator and motor drive systems. Double-wound delta-star and autotransformer configurations are considered. The models allow rectifier and drive system interactions to be examined analytically, or through rapid simulation. The models are validated by comparison with a detailed circuit simulation. (6 pages)


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    Titel :

    Averaged-value models of twelve-pulse rectifiers for aerospace applications


    Beteiligte:
    Baghramian, A. (Autor:in) / Forsyth, A.J. (Autor:in)

    Erscheinungsdatum :

    01.01.2004



    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch





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