Payload and orbital factors affecting satellite attitude control are reviewed and attitude control systems design is discussed. Gravity gradient, solar stabilization, aerodynamic stabilization, magnetic stabilization, spin stabilization, momentum bias/dual spin, momentum exchange, and mass expulsion are described. Attitude control of the GEOS, Meteosat, TD-1, OTS, and MAROTS satellites is outlined.


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    Titel :

    Control and Stabilization of ESA (European Space Agency) Satellites


    Beteiligte:
    D. N. Soo (Autor:in)

    Erscheinungsdatum :

    1977


    Format / Umfang :

    6 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch






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