The attitude determination and control system (ADCS) is a key subsystem in small spacecraft which, for example, find application in Earth observation. This paper details the basic design of a candidate ADCS to achieve high pointing accuracies at `reasonable' cost. Also the expected performance of this system is examined together with estimates of the overall mass power and energy requirements which clearly will have a major influence on whether or not the basic design is accepted for further development.


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    Titel :

    Attitude determination and control for small spacecraft


    Beteiligte:
    Marteru, F. (Autor:in) / Gabriel, S.R. (Autor:in) / Rogers, E. (Autor:in)

    Erscheinungsdatum :

    1996-01-01


    Format / Umfang :

    6 pages



    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch




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