DocumentCode :
2542522
Title :
A hybrid approach to space power control utilizing expert systems and numerical techniques
Author :
Gholdston, E.W. ; Janik, D.F. ; Newton, K.A.
Author_Institution :
Rockwell Int., Canoga Park, CA, USA
fYear :
1989
fDate :
6-11 Aug 1989
Firstpage :
177
Abstract :
The feasibility of combining the advantages of conventional control processing techniques with an expert system for space power system control is discussed. The results reported here focus on diagnostic evaluation and control of specific components and assemblies in the Rocketdyne Space Power Laboratory. Operating data and failure mode analyses are used to formulate the initial object-oriented rule base for the expert system running under the Nexpert operating shell. Online tests in the laboratory environment have been encouraging, demonstrating that the interface necessary for cooperative operation between a central controlling processor and an expert system is feasible
Keywords :
aerospace computing; expert systems; numerical methods; power system computer control; space vehicle power plants; Nexpert operating shell; aerospace computing; computerised control; expert system; interface; numerical techniques; object-oriented rule base; space power system control; Assembly; Control systems; Diagnostic expert systems; Expert systems; Failure analysis; Laboratories; Power control; Power system control; Process control; System testing;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Energy Conversion Engineering Conference, 1989. IECEC-89., Proceedings of the 24th Intersociety
Conference_Location :
Washington, DC
Type :
conf
DOI :
10.1109/IECEC.1989.74459
Filename :
74459
Link To Document :
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