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