DocumentCode
2593397
Title
An error bound for instantaneous coverage
Author
White, Allan L.
Author_Institution
NASA Langley Res. Center, Hampton, VA, USA
fYear
1991
fDate
29-31 Jan 1991
Firstpage
587
Lastpage
591
Abstract
An error bound is derived for a reliability model approximation method. The approximation method is appropriate for the semi-Markov models of reconfigurable systems that are designed to achieve extremely high reliability. The reliability model approximation method consists of replacing a detailed description of a reconfiguration process with the probabilities of the possible outcomes of the reconfiguration process. These probabilities are included in the model as instantaneous jumps from the fault-occurrence state. Since little time is spent in the reconfiguration states, instantaneous jumps are a close approximation to the original model. This approximation procedure is shown to produce an overestimation for the probability of system failure, and an error bound is derived for this overestimation
Keywords
error analysis; failure analysis; reliability; approximation method; error bound; fault-occurrence state; reconfigurable systems; reliability model; semi-Markov models; Aerospace control; Aircraft; Approximation methods; Computer architecture; Digital control; Digital systems; Life testing; NASA; Redundancy; System recovery;
fLanguage
English
Publisher
ieee
Conference_Titel
Reliability and Maintainability Symposium, 1991. Proceedings., Annual
Conference_Location
Orlando, FL
Print_ISBN
0-87942-661-6
Type
conf
DOI
10.1109/ARMS.1991.154503
Filename
154503
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