Passive, 3-axes stabilization system described relies solely on gravity gradient to provide damping and restoring torques for vertically oriented satellite; damping is effected by energy dissipation of any relative motion that exists between main satellite body and suitably connected auxiliary body; it is shown that single auxiliary body having single degree of freedom can be positioned to introduce inertial coupling that permits attitude motions about all 3 axes to be damped; analysis presented leads to solution of optimum system parameters for example configuration.


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    Titel :

    Exploitation of inertial coupling in passive gravity-gradient stabilized satellites


    Weitere Titelangaben:

    J Spacecraft Rockets


    Beteiligte:
    Tinling, B.E. (Autor:in) / Merrick, V.K. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1964


    Format / Umfang :

    7 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :