The patent application relates to a system for autonomously unloading accumulated angular momentum on space craft reaction wheels in the attitude control systems with external torques generated by the interaction of spacecraft magnetic dipoles with the earth's magnetic field.


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    Titel :

    Spacecraft Closed Loop Three-Axis Momentum Unloading System


    Beteiligte:
    J. S. Pistiner (Autor:in)

    Erscheinungsdatum :

    1975


    Format / Umfang :

    8 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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