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Impact of device level faults in a digital avionic processorThis study describes an experimental analysis of the impact of gate and device-level faults in the processor of a Bendix BDX-930 flight control system. Via mixed mode simulation, faults were injected at the gate (stuck-at) and at the transistor levels and, their propagation through the chip to the output pins was measured. The results show that there is little correspondence between a stuck-at and a device-level fault model, as far as error activity or detection within a functional unit is concerned. In so far as error activity outside the injected unit and at the output pins are concerned, the stuck-at and device models track each other. The stuck-at model, however, overestimates, by over 100 percent, the probability of fault propagation to the output pins. An evaluation of the Mean Error Durations and the Mean Time Between Errors at the output pins shows that the stuck-at model significantly underestimates (by 62 percent) the impact of an internal chip fault on the output pins. Finally, the study also quantifies the impact of device fault by location, both internally and at the output pins.
Document ID
19890008675
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Suk, Ho Kim
(Illinois Univ. Urbana-Champaign, IL, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1989
Subject Category
Computer Operations And Hardware
Report/Patent Number
CSG-99
NASA-CR-184783
UILU-ENG-89-2210
NAS 1.26:184783
Report Number: CSG-99
Report Number: NASA-CR-184783
Report Number: UILU-ENG-89-2210
Report Number: NAS 1.26:184783
Accession Number
89N18046
Funding Number(s)
CONTRACT_GRANT: NAG1-602
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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