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Formal design and verification of a reliable computing platform for real-time control. Phase 2: ResultsThe design and formal verification of the Reliable Computing Platform (RCP), a fault tolerant computing system for digital flight control applications is presented. The RCP uses N-Multiply Redundant (NMR) style redundancy to mask faults and internal majority voting to flush the effects of transient faults. The system is formally specified and verified using the Ehdm verification system. A major goal of this work is to provide the system with significant capability to withstand the effects of High Intensity Radiated Fields (HIRF).
Document ID
19920013077
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Butler, Ricky W.
(NASA Langley Research Center Hampton, VA, United States)
Divito, Ben L.
(Vigyan Research Associates, Inc., Hampton VA., United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1992
Subject Category
Computer Systems
Report/Patent Number
NASA-TM-104196
NAS 1.15:104196
Report Number: NASA-TM-104196
Report Number: NAS 1.15:104196
Accession Number
92N22320
Funding Number(s)
PROJECT: RTOP 505-64-10-05
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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