A methodology for autonomous spacecraft design blends autonomy requirements with traditional mission requirements and assesses the impact of autonomy upon the total system resources available to support fault-tolerance and automation. A baseline functional design can be examined for autonomy implementation impacts, and the costs, risk, and benefits of various options can be assessed. The result of the process is a baseline design that includes autonomous control functions.


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    Titel :

    Autonomous spacecraft design methodology


    Beteiligte:
    Divita, E. L. (Autor:in) / Turner, P. R. (Autor:in)

    Kongress:

    IECEC ''84: Advanced energy systems - Their role in our future ; 1984 ; San Francisco, CA


    Erscheinungsdatum :

    01.01.1984


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch






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