DocumentCode :
487107
Title :
Failure Model Determination in a Knowledge-Based Control System
Author :
Huang, Chien Y. ; Stengel, Robert F.
Author_Institution :
Princeton University, Department of Mechanical and Aerospace Engineering, Princeton, NJ 08544; Former Graduate student, Grumman Aerospace Corporation
fYear :
1987
fDate :
10-12 June 1987
Firstpage :
1643
Lastpage :
1648
Abstract :
A technique for determining the most probable failure state of a restructurable control system is presented. The approach is to build a knowledge base that contains and makes use of inference mechanisms to deduce the most likely failures given the symptoms. The analysis is first carried out in a local sense, where only probabilistic information and causality are used to generate failure models, then in a global sense, where the models are grouped and heuristics are used to prune the number of candidate models. Procedures are illustrated using failure patterns of a generic database as well as a fault scenario for a hypothetical helicopter flight control system. It is concluded that the methods are potentially capable of handling generic failures and thus are useful in truly restructable control systems.
Keywords :
Aerospace control; Aerospace engineering; Circuit faults; Control system synthesis; Control systems; Databases; Failure analysis; Helicopters; Inference mechanisms; Information analysis;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
American Control Conference, 1987
Conference_Location :
Minneapolis, MN, USA
Type :
conf
Filename :
4789577
Link To Document :
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