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Study on advanced information processing systemIssues related to the reliability of a redundant system with large main memory are addressed. In particular, the Fault-Tolerant Processor (FTP) for Advanced Launch System (ALS) is used as a basis for our presentation. When the system is free of latent faults, the probability of system crash due to nearly-coincident channel faults is shown to be insignificant even when the outputs of computing channels are infrequently voted on. In particular, using channel error maskers (CEMs) is shown to improve reliability more effectively than increasing the number of channels for applications with long mission times. Even without using a voter, most memory errors can be immediately corrected by CEMs implemented with conventional coding techniques. In addition to their ability to enhance system reliability, CEMs--with a low hardware overhead--can be used to reduce not only the need of memory realignment, but also the time required to realign channel memories in case, albeit rare, such a need arises. Using CEMs, we have developed two schemes, called Scheme 1 and Scheme 2, to solve the memory realignment problem. In both schemes, most errors are corrected by CEMs, and the remaining errors are masked by a voter.
Document ID
19920010294
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Shin, Kang G.
(Michigan Univ. Ann Arbor, MI, United States)
Liu, Jyh-Charn
(Michigan Univ. Ann Arbor, MI, United States)
Date Acquired
September 6, 2013
Publication Date
February 1, 1992
Publication Information
Publisher: NASA. Langley Research Center
Subject Category
Statistics And Probability
Report/Patent Number
NASA-CR-4428
NAS 1.26:4428
Report Number: NASA-CR-4428
Report Number: NAS 1.26:4428
Accession Number
92N19536
Funding Number(s)
PROJECT: RTOP 946-01-00-61
CONTRACT_GRANT: NAG1-981
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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