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Transient fault behavior in a microprocessor: A case studyAn experimental analysis is described which studies the susceptibility of a microprocessor based jet engine controller to upsets caused by current and voltage transients. A design automation environment which allows the run time injection of transients and the tracing from their impact device to the pin level is described. The resulting error data are categorized by the charge levels of the injected transients by location and by their potential to cause logic upsets, latched errors, and pin errors. The results show a 3 picoCouloumb threshold, below which the transients have little impact. An Arithmetic and Logic Unit transient is most likely to result in logic upsets and pin errors (i.e., impact the external environment). The transients in the countdown unit are potentially serious since they can result in latched errors, thus causing latent faults. Suggestions to protect the processor against these errors, by incorporating internal error detection and transient suppression techniques, are also made.
Document ID
19900008317
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Duba, Patrick
(Illinois Univ. Urbana-Champaign, IL, United States)
Date Acquired
September 6, 2013
Publication Date
November 1, 1989
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NAS 1.26:186240
UILU-ENG-89-2240
NASA-CR-186240
CSG-116
Report Number: NAS 1.26:186240
Report Number: UILU-ENG-89-2240
Report Number: NASA-CR-186240
Report Number: CSG-116
Accession Number
90N17633
Funding Number(s)
CONTRACT_GRANT: NAG1-602
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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