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doi:10.1016/0954-1810(96)00019-2 
Copyright © 1996 Published by Elsevier Science Ltd.
An expert system for design of spacecraft attitude control systems
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S. A. Butyrin, V. P. Makarov, R. R. Mukumov, Ye. Somov and S. N. Vassilyev
Received 15 January 1996;
accepted 15 February 1996. ;
Available online 8 May 1998.
Abstract
In the aspect of further development of investigations in automatic theorem proving, complicated systems modeling and analysis of their control systems and making such systems more intelligent, we consider problems of elaboration of a hybrid expert system (ES) for design of gyromoment system of attitude control for spacecraft.
Author Keywords: automatic theorem proving; intelligent design; control systems; spacecraft; constructive logic; intelligent interface
