DocumentCode
2791322
Title
Design of a New On-Board Computer for the New KOMPSAT Bus
Author
Kim, Day-Young ; Kwon, Ki-Ho ; Choi, Jong-Wook ; Lee, Jong-In ; Kim, Hak-Jung
Author_Institution
Korea Aerosp. Res. Inst., Taejon
fYear
2005
fDate
5-12 March 2005
Firstpage
1
Lastpage
12
Abstract
KARI initiated to design a new on-board computer, which will be a key element of spacecraft electrical components, as the demands on reusability, expandability, and scalability of satellite bus has been increasingly required to easily accommodate various payloads of nature space programs in Korea. The new on-board computer adopted centralized processing architecture with ERC32 CPU by utilizing functional modular design concepts. The functional modules consist of software execution platform, TC-TM module including fault management, and integrated 10 processing module. The space wire standard provides a standard communication interface between modules. It allows simple cross-strap design for redundancy management and increases reusability of the modules. Power conversion modules and reconfiguration control unit embedded in the on-board computer will increase flexibility for module management. This paper presents summarized design process with several trade studies to finalize the design of the new onboard computer for the new KOMPSAT bus
Keywords
aerospace instrumentation; artificial satellites; redundancy; ERC32 CPU; KARI; KOMPSAT bus; adopted centralized processing; communication interface; fault management; functional modules; module reusability; on-board computer; power conversion modules; redundancy management; satellite bus; software execution platform; space programs; space wire standard; spacecraft electrical components; Communication standards; Communication system control; Computer architecture; Payloads; Power conversion; Redundancy; Satellites; Scalability; Space vehicles; Wire;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Conference, 2005 IEEE
Conference_Location
Big Sky, MT
Print_ISBN
0-7803-8870-4
Type
conf
DOI
10.1109/AERO.2005.1559535
Filename
1559535
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