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New results in fault latency modellingStudies carried out by McGough and Swern (1981, 1983) are summarized. In these studies, an avionics processor was simulated and a series of fault injection experiments was carried out to determine the degree of fault latency in a redundant flight control system that employed comparison monitoring as the exclusive means of failure detection. A determination was also made of the fault coverage of a typical self-test program. The summary presented stresses that a self-test program should be designed to capitalize on the hardware mechanization of the processor. If this is not done, subtests tend to repeatedly exercise the same hardware components while neglecting to exercise a substantial proportion of the remainder. It is also pointed out that fault latency is relatively independent of both the length and instruction mix of a program. A significant difference is found in fault coverage assessed using pin-level and gate-level fault models.
Document ID
19830060542
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Mcgough, J. G.
(Bendix Corp. Teterboro, NJ, United States)
Swern, F. L.
(Bendix Corp. Teterboro, NJ, United States)
Bavuso, S.
(NASA Langley Research Center Langley, VA, United States)
Date Acquired
August 11, 2013
Publication Date
January 1, 1983
Subject Category
Computer Operations And Hardware
Report/Patent Number
AIAA PAPER 83-2303
Meeting Information
Meeting: Guidance and Control Conference
Location: Gatlinburg, TN
Start Date: August 15, 1983
End Date: August 17, 1983
Accession Number
83A41760
Distribution Limits
Public
Copyright
Other

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