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A forward view on reliable computers for flight controlThe requirements for fault-tolerant computers for flight control of commercial aircraft are examined; it is concluded that the reliability requirements far exceed those typically quoted for space missions. Examination of circuit technology and alternative computer architectures indicates that the desired reliability can be achieved with several different computer structures, though there are obvious advantages to those that are more economic, more reliable, and, very importantly, more certifiable as to fault tolerance. Progress in this field is expected to bring about better computer systems that are more rigorously designed and analyzed even though computational requirements are expected to increase significantly.
Document ID
19760024087
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Goldberg, J.
(Stanford Research Inst. Menlo Park, CA, United States)
Wensley, J. H.
(Stanford Research Inst. Menlo Park, CA, United States)
Date Acquired
August 8, 2013
Publication Date
August 1, 1976
Publication Information
Publication: NASA. Dryden Flight Res. Center Advanced Control Technol. and its Potential for Future Transport Aircraft
Subject Category
Aircraft Stability And Control
Accession Number
76N31175
Funding Number(s)
CONTRACT_GRANT: NAS1-10920
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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