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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    Title :

    Autonomous spacecraft design methodology


    Contributors:

    Conference:

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


    Publication date :

    1984-01-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English






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    Waddell, R.L. | Tema Archive | 1986