DocumentCode
1712121
Title
Using failure modes and effects simulation as a means of reliability analysis
Author
Palumbo, Daniel L.
Author_Institution
NASA Langley Res. Center, Hampton, VA, USA
fYear
1992
Firstpage
102
Lastpage
107
Abstract
Failure modes and effects simulation analysis (FMES) is introduced as an effective way to do both failure modes and effect analysis (FMEA) and reliability analysis. Using FMES, a system is described as a connected set of components. A component is defined by its interconnects (inputs and outputs), its state (the component and its outputs can occupy different states), and its behavioral description. Behavioral descriptions characterize how changes occur in the component and its output states. The FMES technique has been evaluated in a tool called the Reliability Estimation Testbed (REST). A reliability modeling language (RML) was developed as part of REST to support FMES. REST and the RML have been used to analyze a system consisting of a quad computer connected to two reconfiguring mesh networks and several quad redundant devices, a system totaling 100 components. On more than one occasion the FMES approach has produced analyses which uncovered errors in hand-generated models
Keywords
aerospace computing; aircraft instrumentation; digital simulation; failure analysis; reliability; Reliability Estimation Testbed; failure modes; fault tolerant avionics; quad computer; quad redundant devices; reconfiguring mesh networks; reliability analysis; reliability modeling language; Analytical models; Circuits; Computer network reliability; Failure analysis; LAN interconnection; Light emitting diodes; NASA; Resistors; System recovery; Testing;
fLanguage
English
Publisher
ieee
Conference_Titel
Digital Avionics Systems Conference, 1992. Proceedings., IEEE/AIAA 11th
Conference_Location
Seattle, WA
Print_ISBN
0-7803-0820-4
Type
conf
DOI
10.1109/DASC.1992.282175
Filename
282175
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