DocumentCode
3332856
Title
Measuring robustness of a fault tolerant aerospace system
Author
Dingman, C.P. ; Marshall, J. ; Siewiorek, D.P.
Author_Institution
Dept. of Electr. & Comput. Eng., Carnegie Mellon Univ., Pittsburgh, PA, USA
fYear
1995
fDate
27-30 June 1995
Firstpage
522
Lastpage
527
Abstract
In commercial literature, the meaning of the term fault tolerant has become vague. We describe a system used to measure the robustness of a fault tolerant aerospace system developed at IBM, present the data collected during the project, and report conclusions and areas for future work.<>
Keywords
aerospace computing; fault tolerant computing; reliability; software fault tolerance; special purpose computers; system recovery; Advanced Spaceborne Computer Module; IBM; collected data; fault tolerant aerospace system; robustness measurement; Aerospace engineering; Benchmark testing; Computer errors; Drives; Fault tolerant systems; Laboratories; Military computing; Operating systems; Robustness; Software testing;
fLanguage
English
Publisher
ieee
Conference_Titel
Fault-Tolerant Computing, 1995. FTCS-25. Digest of Papers., Twenty-Fifth International Symposium on
Conference_Location
Pasadena, CA, USA
Print_ISBN
0-8186-7079-7
Type
conf
DOI
10.1109/FTCS.1995.466945
Filename
466945
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