The design and testing of an experimental pressure regulator satellite attitude control using electronic feedback are described. It is shown that, using readily available components, the regulator can maintain a controlled pressure from zero up to supply pressure to within an accuracy of a few per cent. The limitations of the experimental controller were shown to be due to the type of value and drive circuit used. (Author)


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    Titel :

    An Electronic Feedback Pressure Regulator


    Beteiligte:
    B. P. Day (Autor:in) / K. J. Omahony (Autor:in)

    Erscheinungsdatum :

    1972


    Format / Umfang :

    16 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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