Implementing Falut Tolerance in the COTS-Based X2000 Architecture: A Case Study on IEEE 1394

Chau, S. N.; Tai, A. T.; Alkalai, L.; Luong, H. H.

NASA NTRS · 20060035844

Implementing Falut Tolerance in the COTS-Based X2000 Architecture: A Case Study on IEEE 1394

Chau, S. N.·Tai, A. T.·Alkalai, L.·Luong, H. H.

Abstract

Among other challenges from NASA's X2000 Technology Development Program, affordability and miniaturizaton are prominent criteria, which 1) preclude the traditional solutions for mission reliability that rely on customer-built hardware and extensive component/subsystem replication, and 2) call for commercial-of-the-shelf (COTS) based approaches incorporating novel, practical fault tolerance techniques.

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IEEE 1394 bus interface commercial-off-th-shelf spaceborne systems stack tree topology fault tolerance realization

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Chau, S. N., Tai, A. T., Alkalai, L., Luong, H. H.. 1998-06-23. Implementing Falut Tolerance in the COTS-Based X2000 Architecture: A Case Study on IEEE 1394. https://ntrs.nasa.gov/citations/20060035844

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