Artificial satellites move in elliptical orbits round planet; in order to survey that planet they must face it; therefore, satellite must be turned at same rate as rate of rotation of planet-satellite line; rate of turn of satellite which must be supplied by attitude control system is calculated; work will be of use in design of attitude control systems for communications, reconnaissance and survey satellites and for entry and re-entry of manned satellites.


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    Titel :

    Orientation of satellite in elliptical orbit


    Weitere Titelangaben:

    Spaceflight


    Beteiligte:
    Hilton, W.F. (Autor:in) / Taylor, B.M. (Autor:in)

    Erschienen in:

    Spaceflight ; 9 , n 5


    Erscheinungsdatum :

    1967


    Format / Umfang :

    2 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



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