Annual Reliability and Maintainability Symposium, 2005. Proceedings.
DOI: 10.1109/rams.2005.1408374
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AMSAA maturity projection model based on stein estimation

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Cited by 9 publications
(10 citation statements)
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“…The failure intensities for the collection of failure modes found in a complex system are shown to be adequately modeled as a random realization from a gamma distribution in both [17] and [18]. Using a gamma distribution in this way also recognizes what may be referred to as the vital few, trivial many property among mode failure intensities.…”
Section: Failure Mode Posterior Distributionmentioning
confidence: 99%
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“…The failure intensities for the collection of failure modes found in a complex system are shown to be adequately modeled as a random realization from a gamma distribution in both [17] and [18]. Using a gamma distribution in this way also recognizes what may be referred to as the vital few, trivial many property among mode failure intensities.…”
Section: Failure Mode Posterior Distributionmentioning
confidence: 99%
“…The posterior expected number of failure modes is found by first defining the indicator function for the unobserved failure mode as mode occurs by time otherwise (17) The posterior predicted mean of is found by examining the posterior probability that the unobserved failure mode is observed by some time . The likelihood of observing a failure mode by time is given from Assumption 3 in Section II.A as (18) Using the posterior distribution on the mode failure intensity in (4) with the , , and set to 0 for an unobserved failure mode, the unconditional marginal distribution for can be found by calculating the joint distribution of (4) and (18), and then marginalizing with respect to . The unconditional -expected value is given by (19) Summing over all unobserved modes in the system yields (20) and taking the limit as becomes large results in (21) Because is a Bernoulli random variable, summing over the unobserved modes yields a Binomial random variable.…”
Section: G Failure Modes Observed During Follow-on Testingmentioning
confidence: 99%
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“…Denoting this failure intensity by r(T), where T denotes the duration of Phase I, the ACPM assessment of r(T)is based on: (1) the A and B-mode failure data generated during Phase I test duration, T; and (2) assessments of the FEFs for the B-modes surfaced during Phase I. Since the assessments of the FEFs are often largely based on engineering judgment, the resulting assessment, r (T) , of the system failure intensity after corrective action implementations is called a reliability projection (as opposed to a demonstrated assessment, which would be based solely on test data) [7]. The ACPM and estimation procedure was motivated by the desire to replace the widely used "adjustment procedure".…”
Section: Amsaa-crow Projection Model (Acpm)mentioning
confidence: 99%
“…This equation arises from considering the problem of estimating the system MTBF at the start of a new test phase after implementing corrective actions to failure modes surfaced in a proceeding test phase. This MTBF projection has been documented in [4] and is described in Section 4. Section 5 contains simulation results.…”
Section: Introductionmentioning
confidence: 99%