DocumentCode
2339565
Title
Run-time control design of micro-satellite OBC based on reconfigurable architecture
Author
Guo-dong, Xu ; Dan, Zhao ; Shi-jie, Sui ; Sheng-chang, Lan
Author_Institution
Res. Center of Satellite Technol., Harbin Inst. of Technol., Harbin
fYear
2009
fDate
25-27 May 2009
Firstpage
2591
Lastpage
2595
Abstract
To address the issues of on-board computer (OBC) design by traditional method for micro-satellite, an advanced OBC based on reconfigurable architecture was presented, and its run-time control scheduling was designed. This reconfigurable OBC could implement supervision which ensured the running status, function reconfiguration which switched its current control modes, restoring reconfiguration through searching and shielding the problem region, and software/hardware upgrading reconfiguration which could accomplish in orbit. Semi-physical simulation platform composed with OBC prototype board, DSpace simulator and laboratory terminal was established, then the performance and run-time control scheduling of this OBC was proved in the platform.
Keywords
aerospace control; artificial satellites; reconfigurable architectures; DSpace simulator; OBC prototype board; current control modes; laboratory terminal; microsatellite OBC; on-board computer design; reconfigurable architecture; run-time control scheduling design; software-hardware reconfiguration; Control design; Current control; Design methodology; Hardware; Laboratories; Processor scheduling; Reconfigurable architectures; Runtime; Software prototyping; Virtual prototyping; On-Board Computer; micro-satellite; reconfiguration technique; run-time control; simi-physical simulation;
fLanguage
English
Publisher
ieee
Conference_Titel
Industrial Electronics and Applications, 2009. ICIEA 2009. 4th IEEE Conference on
Conference_Location
Xi´an
Print_ISBN
978-1-4244-2799-4
Electronic_ISBN
978-1-4244-2800-7
Type
conf
DOI
10.1109/ICIEA.2009.5138676
Filename
5138676
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