DocumentCode
2818608
Title
Three approaches to reliability analysis
Author
Palumbo, Daniel L.
Author_Institution
NASA Langley Res. Center, Hampton, VA, USA
fYear
1989
fDate
22-26 May 1989
Firstpage
308
Abstract
It is noted that current reliability analysis tools differ not only in their solution techniques, but also in their approach to model abstraction. The analyst must be satisfied with the constraints that are intrinsic to any combination of solution technique and model abstraction. To get a better idea of the nature of these constraints, three reliability analysis tools (HARP, ASSIST/SURE, and CAME) were used to model portions of the Integrated Airframe/Propulsion Control System architecture. When presented with the example problem, all three tools failed to produce correct results. In all cases, either the tool or the model had to be modified. It is suggested that most of the difficulty is rooted in the large model size and long computational times which are characteristic of Markov model solutions
Keywords
Markov processes; aerospace computing; aerospace control; aerospace propulsion; reliability; ASSIST/SURE; CAME; HARP; Integrated Airframe/Propulsion Control System architecture; Markov model; aerospace computing; integrated aerospace propulsion control; model abstraction; reliability analysis; Aerospace control; Computer architecture; Computer displays; Computer network reliability; Control system synthesis; Failure analysis; Mesh networks; Network interfaces; Power system modeling; Power system reliability;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace and Electronics Conference, 1989. NAECON 1989., Proceedings of the IEEE 1989 National
Conference_Location
Dayton, OH
Type
conf
DOI
10.1109/NAECON.1989.40229
Filename
40229
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