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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    Title :

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


    Contributors:

    Publication date :

    2004-01-01



    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English





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