DocumentCode
3186556
Title
Cross channel dependency requirements of the multipath redundant avionics suite
Author
Martin, Fred ; Adams, Darryl
Author_Institution
General Dynamics, San Diego, CA, USA
fYear
1992
fDate
18-22 May 1992
Firstpage
200
Abstract
Requirements for cross channel dependencies in the multipath redundant avionics suite (MPRAS) architecture are described. MPRAS is a data synchronous avionics architecture for space launch vehicle applications. The MPRAS cross channel data link (CCDL) provides the mechanism, required by data synchronous architectures, to exchange data and maintain synchronization among redundant channels. MPRAS architectural requirements impose a variety of characteristics for cross channel dependencies which make traditional CCDL solutions unacceptable for MPRAS target applications. The MPRAS CCDL requirements have led to a CCDL design which maintains resilience to faults, does not introduce large cross channel bandwidth reductions, and meets the other established MPRAS CCDL requirements. A review of fault-tolerant system principles applicable to CCDL issues is presented as well as a top-level functional description of the MPRAS CCDL design
Keywords
aerospace computing; aircraft instrumentation; computer architecture; fault tolerant computing; redundancy; architecture; cross channel data link; cross channel dependencies; data synchronous avionics; fault-tolerant system; multipath redundant avionics; space launch vehicle; synchronization; Aerospace electronics; Backplanes; Fault detection; Fault tolerance; Fault tolerant systems; Hardware; Packaging; Redundancy; Vehicle dynamics; Voting;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace and Electronics Conference, 1992. NAECON 1992., Proceedings of the IEEE 1992 National
Conference_Location
Dayton, OH
Print_ISBN
0-7803-0652-X
Type
conf
DOI
10.1109/NAECON.1992.220645
Filename
220645
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