BEACON eSpace at Jet Propulsion Laboratory >
JPL Technical Report Server >
JPL TRS 1992+ >
Please use this identifier to cite or link to this item:
|Title: ||Implementing Falut Tolerance in the COTS-Based X2000 Architecture: A Case Study on IEEE 1394|
|Authors: ||Chau, S. N.|
Tai, A. T.
Luong, H. H.
|Issue Date: ||23-Jun-1998 |
|Citation: ||Munich, Germany|
|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.|
|Appears in Collections:||JPL TRS 1992+|
Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.