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Fault-tolerant parallel processors for avionics with reduced maintenanceArchitectural issues and approaches for implementing fault-tolerant parallel processors in avionics systems and other dedicated applications requiring high levels of dependability are discussed. For these systems it is desirable to provide both a high degree of fault tolerance and a system that can operate for extended periods of time without external maintenance. With current technology it is possible to operate dependably for months between maintenance events. The longer-term goal should be maintenance-free operation (a computer that outlasts its host system). It is argued that new high-density packaging techniques may make this type of long-life fault-tolerant design an attractive choice in controlling the life-cycle costs of the next generation of systems.
Document ID
19910070011
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Rennels, David A.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Rohr, John A.
(JPL Pasadena, CA, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1990
Subject Category
Computer Systems
Meeting Information
Meeting: IEEE/AIAA/NASA Digital Avionics Systems Conference
Location: Virginia Beach, VA
Country: United States
Start Date: October 15, 1990
End Date: October 18, 1990
Accession Number
91A54634
Distribution Limits
Public
Copyright
Other

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