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
Link To Document :
بازگشت