DocumentCode :
1746907
Title :
A hybrid PCI/VME architecture for space
Author :
Walls, Buddy ; McClelland, Michael ; Persyn, Steven
Author_Institution :
Southwest Res. Inst., San Antonio, TX, USA
Volume :
5
fYear :
2001
fDate :
2001
Firstpage :
2227
Abstract :
Southwest Research Institute has developed a hybrid space system architecture incorporating both the VME and PCI buses. The combined architecture allows the incorporation of heritage space qualified VME modules with new high performance PCI modules, reducing development cost and providing risk mitigation at the system level. The core of the hybrid architecture is the SwRI PCI to VME Bridge (PVB), a high performance interface between the two buses. The PVB was initially prototyped using standard commercial FPGA technology, then subsequently migrated to radiation tolerant implementation, with the ultimate goal of a radiation hardened ASIC in Q4-2001
Keywords :
aerospace computing; application specific integrated circuits; field programmable gate arrays; radiation hardening (electronics); space vehicle electronics; system buses; FPGA; PCI bus; PCI to VME Bridge; VME bus; heritage space qualified VME modules; high performance PCI modules; high performance interface; hybrid space system architecture; radiation hardened ASIC; radiation tolerant implementatio; reduced development cost; software support; syetem level risk mitigation; Aerospace industry; Application specific integrated circuits; Bridges; Costs; Defense industry; Field programmable gate arrays; Military standards; Prototypes; Standards development; Throughput;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Conference, 2001, IEEE Proceedings.
Conference_Location :
Big Sky, MT
Print_ISBN :
0-7803-6599-2
Type :
conf
DOI :
10.1109/AERO.2001.931180
Filename :
931180
Link To Document :
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