Theoretical framework is presented for analyzing motion of multibody satellite system in gravity-oriented orbiting reference frame; it consists of expressions for forces and moments of body-force field in arbitrary bodies and of their utilization in Lagrange's equation to find equations of motion; it is applied to analysis of system designed for passive attitude stabilization; equations are linearized and separated into 2 groups (longitudinal and lateral), and solutions obtained; damping to half-amplitude in times of order of 0.3 orbit is possible in either system separately.


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    Titel :

    Dynamics of gravity-oriented orbiting systems with application to passive stabilization


    Weitere Titelangaben:

    AIAA J


    Beteiligte:
    Etkin, B. (Autor:in)

    Erschienen in:

    AIAA Journal ; 2 , n 6 ; p 1008-1014


    Erscheinungsdatum :

    1964


    Format / Umfang :

    7 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



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