A semi-active gravity gradient attitude stabilization system (SAGS) providing active pitch control and semi-passive roll/yaw control has been developed. The design and development of the SAGS controller for space flight test on the NASA developed PAC secondary payload spacecraft are described and performance predictions are presented for the first flight test scheduled in August 1969. Initial in-orbit performance of Delta PAC-1 is summarized.


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    Titel :

    A Semi-Active Gravity Gradient Stabilization System


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Sabroff, A. E. (Autor:in) / Zaremba, J. G. (Autor:in) / Wheeler, P. C. (Autor:in) / Redisch, W. N. (Autor:in)

    Kongress:

    Aeronautic and Space Engineering and Manufacturing Meeting ; 1969



    Erscheinungsdatum :

    01.02.1969




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    A semi-active gravity gradient stabilization system

    Redisch, W. N. / Sabroff, A. E. / Wheeler, P. C. et al. | NTRS | 1969


    Evaluation of a semi-active gravity gradient system

    Nishinaga, R. G. / Wheeler, P. C. | NTRS | 1965



    Implementation of a semi-active gravity gradient controller.

    Hui, P. S. / Zaremba, J. G. | NTRS | 1968


    Gravity-gradient stabilization of satellites

    Kershner, R.B. | Engineering Index Backfile | 1963