This paper specifically addresses a class of resonant power processing equipment designed to be used in an integrated, high frequency (20 kHz domain), utility power system for large, multi-user spacecraft and other aerospace vehicles. It describes a hardware approach, which has been the basis for parametric and physical data used to justify the selection of high frequency AC as the PMAD baseline for the Space Station. Heated discussions during the process of that selection have shown that there is a general lack of understanding in the Aerospace industry about the operation of resonant equipment, when used as direct-output inverters and the various converters associated with a large, complex system. This paper is part of a larger effort undertaken by NASA and General Dynamics to be sure that all potential Space Station contractors and other aerospace power system designers fully understand and can comfortably use this technology, which is now widely used in the commercial sector. In this paper, we will examine control requirements, stability, and operational modes; and their hardware impacts from an integrated system point of view. The current Space Station PMAD system will provide the overall requirements model to develop an understanding of the performance of this type of system with regard to: Regulation; Power Bus stability and voltage control; Source impedance; Transient response; Power Factor effects; Limits and overloads.


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    Titel :

    Control considerations for high frequency, resonant, power processing equipment used in large systems


    Weitere Titelangaben:

    Ueberlegungen zur Steuerung von Hochfrequenz-Resonanz-Energieumrichtern fuer grosse Raumfahrzeuge


    Beteiligte:
    Mildice, J.W. (Autor:in) / Schreiner, K.E. (Autor:in) / Wolff, F. (Autor:in)


    Erscheinungsdatum :

    1987


    Format / Umfang :

    6 Seiten, 5 Bilder, 3 Quellen


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch







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