Paper extends reorientation schemes for satellites possessing inertial symmetry about spin-axis, to spinning satellites which are not designed with inertial symmetry; method of torquing described effects changes in spin-axis attitude by plane of satellite; 2-phase attitude control system is developed for asymmetric, spinning earth-satellite which is nominally oriented with its spin axis normal to plane of its orbit.


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    Titel :

    Two-pulse attitude control of asymmetric spinning satellite


    Weitere Titelangaben:

    Progress Astronautics Aeronautics


    Beteiligte:
    Wheeler, P.C. (Autor:in)


    Erscheinungsdatum :

    1964


    Format / Umfang :

    27 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Two-Pulse Attitude Control of an Asymmetric Spinning Satellite

    Langford, Robert C. / Mundo, Charles J. | AIAA | 1964


    Magnetic attitude control of spinning satellite

    Ergin, E.I. / Wheeler, P.C. | Engineering Index Backfile | 1965


    Magnetic attitude control of a spinning satellite.

    ERGIN, E. I. / WHEELER, P. C. | AIAA | 1965