DocumentCode
1939442
Title
Smartphone qualification & linux-based tools for CubeSat computing payloads
Author
Bridges, C.P. ; Yeomans, B. ; Iacopino, C. ; Frame, T.E. ; Schofield, A. ; Kenyon, S. ; Sweeting, M.N.
Author_Institution
Surrey Space Centre, University of Surrey, Guildford, United Kingdom
fYear
2013
fDate
2-9 March 2013
Firstpage
1
Lastpage
10
Abstract
Modern computers are now far in advance of satellite systems and leveraging of these technologies for space applications could lead to cheaper and more capable spacecraft. Together with NASA AMES´s PhoneSat, the STRaND-1 nanosatellite team has been developing and designing new ways to include smart-phone technologies to the popular CubeSat platform whilst mitigating numerous risks. Surrey Space Centre (SSC) and Surrey Satellite Technology Ltd. (SSTL) have led in qualifying state-of-the-art COTS technologies and capabilities - contributing to numerous low-cost satellite missions. The focus of this paper is to answer if 1) modern smart-phone software is compatible for fast and low-cost development as required by CubeSats, and 2) if the components utilised are robust to the space environment. The STRaND-1 smart-phone payload software explored in this paper is united using various open-source Linux tools and generic interfaces found in terrestrial systems. A major result from our developments is that many existing software and hardware processes are more than sufficient to provide autonomous and operational payload object-to-object and file-based management solutions. The paper will provide methodologies on the software chains and tools used for the STRaND-1 smartphone computing platform, the hardware built with space qualification results (thermal, thermal vacuum, and TID radiation), and how they can be implemented in future missions.
Keywords
Hardware; Linux; Method of moments; NASA; Robustness; Satellites; Wheels;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Conference, 2013 IEEE
Conference_Location
Big Sky, MT
ISSN
1095-323X
Print_ISBN
978-1-4673-1812-9
Type
conf
DOI
10.1109/AERO.2013.6497349
Filename
6497349
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