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.
Development of a Coupled Expert System for the Spacecraft Attitude Control Problem
1987
8 pages
Report
Keine Angabe
Englisch
NTIS | 1968
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