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Validation of fault-free behavior of a reliable multiprocessor system - FTMP: A case studyA program of experiments has been conducted at NASA-Langley to test the fault-free performance of a Fault-Tolerant Multiprocessor (FTMP) avionics system for next-generation aircraft. Baseline measurements of an operating FTMP system were obtained with respect to the following parameters: instruction execution time, frame size, and the variation of clock ticks. The mechanisms of frame stretching were also investigated. The experimental results are summarized in a table. Areas of interest for future tests are identified, with emphasis given to the implementation of a synthetic workload generation mechanism on FTMP.
Document ID
19850065606
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Clune, E.
(Carnegie-Mellon Univ. Pittsburgh, PA, United States)
Segall, Z.
(Carnegie-Mellon Univ. Pittsburgh, PA, United States)
Siewiorek, D.
(Carnegie-Mellon University Pittsburgh, PA, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1984
Subject Category
Aircraft Instrumentation
Meeting Information
Meeting: 1984 American Control Conference
Location: San Diego, CA
Start Date: June 6, 1984
End Date: June 8, 1984
Accession Number
85A47757
Funding Number(s)
CONTRACT_GRANT: NAG1-190
Distribution Limits
Public
Copyright
Other

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