DocumentCode
1712049
Title
Application of Space Station Freedom (SSF) DMS technology to fault tolerant avionics systems
Author
Smith, T.J.
Author_Institution
IBM, Houston, TX, USA
fYear
1992
Firstpage
120
Lastpage
126
Abstract
The Space Station Freedom (SSF) is developing a space-qualified Data Management System (DMS) packaged with standard modules and backplanes as well as Ada software capabilities. The SSF architecture must be augmented with tight processor synchronization and cross-strapped input/output capabilities to implement N-modular redundant (NMR) system voting. There are many architectural variations available to implement NMR. A fault-tolerant testbed (FTTB) is being used at IBM to evaluate which architectures have the least impact on the SSF technology base. Developments in the FTTB thus far support the conclusion that the SSF technology can be a cost-effective point of departure for implementation of future fault-tolerance avionics architectures since it offers a standard hardware and software base
Keywords
aerospace computer control; aerospace computing; aircraft instrumentation; computer architecture; fault tolerant computing; military standards; redundancy; Ada software; Data Management System; IBM; N-modular redundant (NMR) system voting; Space Station Freedom; backplanes; cost-effectiveness; cross-strapped input/output; fault-tolerant testbed; processor synchronization; standard modules; Application software; Computer architecture; Fault tolerance; Nuclear magnetic resonance; Software development management; Software packages; Software standards; Space stations; Space technology; Standards development;
fLanguage
English
Publisher
ieee
Conference_Titel
Digital Avionics Systems Conference, 1992. Proceedings., IEEE/AIAA 11th
Conference_Location
Seattle, WA
Print_ISBN
0-7803-0820-4
Type
conf
DOI
10.1109/DASC.1992.282172
Filename
282172
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