A circular orbit and constant atmospheric density was assumed. A computer program which determines equilibrium attitudes and the associated eigenvalues of these attitudes is presented. Demonstration of the use of this program was made using the former Skylab satellite as an example.


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    Titel :

    Equilibrium and Stability of a Satellite Influenced by Gravitational and Aerodynamic Torques


    Beteiligte:
    Z. J. Galaboff (Autor:in)

    Erscheinungsdatum :

    1981


    Format / Umfang :

    77 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch