Stability of plane librations of near-earth satellite subjected to aerodynamic and gravity gradient torques is examined for general case of eccentric orbit; stability boundaries are determined numerically and presented in terms of nondimensional configuration and orbit parameters; examples of both stable and unstable angular motions; configurations are analyzed to illustrate degree of aerodynamic attitude stabilization possible in orbit with practical vehicles.


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    Titel :

    Dynamic stability of aerodynamically responsive satellites


    Weitere Titelangaben:

    J Aerospace Sciences


    Beteiligte:
    Schrello, D.M. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1962


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



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