DocumentCode :
2637094
Title :
Problems of Micro-satellite OBC and solving method based on reconfiguration technique
Author :
Dan, Zhao ; Guodong, Xu ; Yunhai, Geng
Author_Institution :
Res. Center of Satellite Technol., Harbin Inst. of Technol., Harbin
fYear :
2008
fDate :
10-12 Dec. 2008
Firstpage :
1
Lastpage :
4
Abstract :
The objective of this work is to solve the problems of On-board Computer (OBC) in Micro-satellite. With the limit of size and weight, and the requirement of multifunction and high-performance, itpsilas almost impossible to design an eligible Micro-satellite OBC by regular methods. To address this issue, this paper researches reconfiguration technique, and proposes one OBC design based on it. The reconfigurable OBC can achieve the multifunction and high processing ability, and there are several measures to ensure the reliability.
Keywords :
artificial satellites; field programmable gate arrays; reconfigurable architectures; spacecraft computers; micro-satellite on-board computer; reconfiguration technique; Attitude control; Costs; Data processing; Design methodology; Extraterrestrial measurements; Field programmable gate arrays; Hardware; Microprocessors; Military computing; Military 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.2008.4776233
Filename :
4776233
Link To Document :
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