A majority of the current expert systems focus on the symbolic-oriented logic and inference mechanisms of artificial intelligence (AI). Common rule-based systems employ empirical associations and are not well suited to deal with problems often arising in engineering. Described is a prototype expert system which combines both symbolic and numeric computing. The expert system's configuration is presented and its application to a spacecraft attitude control problem is discussed.


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    Titel :

    Development of a Coupled Expert System for the Spacecraft Attitude Control Problem


    Beteiligte:
    K. Kawamura (Autor:in) / G. Beale (Autor:in) / J. Schaffer (Autor:in) / B. Hsieh (Autor:in) / S. Padalkar (Autor:in)

    Erscheinungsdatum :

    1987


    Format / Umfang :

    8 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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