Systems analysis approach to problems involved in obtaining and maintaining 24-hr equatorial satellite; consideration of orbit ascent, initial longitude positioning, and control of satellite drift away from desired stationary longitude; orbit control system, including ground based tracking and command stations, computations and control center, and satellite subsystems, which will provide satisfactory stationary orbit is synthesized; capability of control system was tested by computer simulation; results indicate that synthesized system provides satisfactory stationary orbit in presence of likely system errors.


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    Titel :

    Longitude positioning and orbit control of 24-hour equatorial satellite


    Weitere Titelangaben:

    AIAA J


    Beteiligte:
    Kang, G. (Autor:in) / Kenehan, M.F. (Autor:in)

    Erschienen in:

    AIAA Journal ; 2 , n 6


    Erscheinungsdatum :

    1964


    Format / Umfang :

    9 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :