A unique ground control system was designed and implemented to support and meet the stringent mission requirements of the SAS-1. The important features of the system are described with emphasis on the software used to control the orientation of the spacecraft. A summary of the system's operation during the SAS-1 mission is given along with a discussion of the performance of the software subsystems relative to the mission requirements.


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    Titel :

    SAS Attitude Support System


    Beteiligte:
    Snyder, J. L. (Autor:in) / Meyers, G. F. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1972-01-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




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