DocumentCode
2639599
Title
FPGA On-Board Computer design based on hierarchical fault tolerance
Author
Xing, Lei ; Sun, Zhaowei ; Xu, Guodong
Author_Institution
Res. Center of Satellite Technol., Harbin Inst. of Technol., Harbin
fYear
2008
fDate
10-12 Dec. 2008
Firstpage
1
Lastpage
5
Abstract
Safety is a crucial requirement of On-Board Computer (OBC) design of a satellite, especially for the new type OBC--takes FPGA as central processor. Upon that this paper proposes a plan of FPGA OBC design and adds hierarchical fault tolerant concept to enhance the reliability of the OBC system. The fault tolerant architecture can be divided into three hierarchic ranks, containing single-CPU reconfiguration, component unit transfer and dual-CPU subrogation. One of the above fault manage mode will be chosen to deal with problems according to error situation in-orbit. In the worst cases, all three modes may be used. The last part of the paper gives the functional verification approach under development for the hierarchical fault tolerant OBC design.
Keywords
artificial satellites; fault tolerant computing; field programmable gate arrays; reconfigurable architectures; spacecraft computers; FPGA on-board computer design; component unit transfer; dual-CPU subrogation; fault management mode; fault tolerant architecture; functional verification; hierarchical fault tolerance; reliability; satellite; single-CPU reconfiguration; Aerospace electronics; Computer architecture; Computer displays; Fault tolerance; Fault tolerant systems; Field programmable gate arrays; Kernel; Payloads; Safety; Satellites;
fLanguage
English
Publisher
ieee
Conference_Titel
Systems and Control in Aerospace and Astronautics, 2008. ISSCAA 2008. 2nd International Symposium on
Conference_Location
Shenzhen
Print_ISBN
978-1-4244-3908-9
Electronic_ISBN
978-1-4244-2386-6
Type
conf
DOI
10.1109/ISSCAA.2008.4776381
Filename
4776381
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