DocumentCode :
381667
Title :
Feasibility of using SA1100 processor in micro satellite environment
Author :
Barnard, Arthur
Author_Institution :
Dept. of Electr. & Electron. Eng., Stellenbosch Univ., South Africa
Volume :
4
fYear :
2002
fDate :
2002
Abstract :
After SUNSAT was launched in 1999 and the possibility of developing another micro satellite emerged, areas of possible improvement were identified. Among the suggestions that emerged was the idea of developing an onboard computer for a micro satellite, using one of the new generation low power processors. The processor had to meet guideline specifications derived from the experience gained by researchers and students involved with the SUNSAT project. This paper reports on the process of choosing one of these processors, Intel´s StrongARM SA1100 and the subsequent testing of the feasibility of using it as an onboard computer. The feasibility test included comparing the processor´s specifications to those required and designing an evaluation board for this processor to test its ease of use and programmability.
Keywords :
aerospace computing; artificial satellites; avionics; special purpose computers; Intel StrongARM SA1100; SUNSAT; low power processors; micro satellite environment; onboard computer; programmability; specifications; Buildings; Costs; Debugging; Guidelines; Manufacturing processes; Microprocessors; Power generation; Power system reliability; Satellites; Testing;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Conference Proceedings, 2002. IEEE
Print_ISBN :
0-7803-7231-X
Type :
conf
DOI :
10.1109/AERO.2002.1036899
Filename :
1036899
Link To Document :
بازگشت