DocumentCode :
3125892
Title :
PolySat´s Next Generation Avionics Design
Author :
Manyak, Greg ; Bellardo, John M.
Author_Institution :
Electr. Eng. Dept., California Polytech. State Univ., San Luis Obispo, CA, USA
fYear :
2011
fDate :
2-4 Aug. 2011
Firstpage :
69
Lastpage :
76
Abstract :
The CubeSat platform provides a unique challenge for flight software design due to the incredible size and power constraints. A number of tradeoffs must be made to balance effectiveness, fault tolerance, and cost. These basic requirements have been combined with the lessons learned from Cal Poly´s past 8-bit avionics system to design a significant revision based around a 32-bit microprocessor running Linux. This work analyzes both generations of avionics design, including a discussion of major design principles that are relevant to other CubeSat missions.
Keywords :
Linux; aerospace computing; artificial satellites; avionics; microprocessor chips; software fault tolerance; CubeSat missions; CubeSat platform; Linux; PolySat next generation avionic design; fault tolerance; flight software design; microprocessor; word length 32 bit; Aerospace electronics; Batteries; Fault tolerance; Hardware; Payloads; Satellites; Software; cubesat software design; fault tolerance;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Space Mission Challenges for Information Technology (SMC-IT), 2011 IEEE Fourth International Conference on
Conference_Location :
Palo Alto, CA
Print_ISBN :
978-1-4577-0712-4
Electronic_ISBN :
978-1-4577-0713-1
Type :
conf
DOI :
10.1109/SMC-IT.2011.13
Filename :
6007777
Link To Document :
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