DocumentCode
711355
Title
Introducing radiation tolerant heterogeneous computers for small satellites
Author
Bruhn, Fredrik ; Brunberg, Kjell ; Hines, John ; Asplund, Lars ; Norgren, Magnus
Author_Institution
Sch. of Innovation, Design & Eng. (IDT), Malardalen Univ., Vasteras, Sweden
fYear
2015
fDate
7-14 March 2015
Firstpage
1
Lastpage
10
Abstract
This paper presents results and conclusions from design, manufacturing, and benchmarking of a heterogeneous computing low power fault tolerant computer, realized on an industrial Qseven® small form factor (SFF) platform. A heterogeneous computer in this context features multi-core processors (CPU), a graphical processing unit (GPU), and a field programmable gate array (FPGA). The x86 compatible CPU enables the use of vast amounts of commonly available software and operating systems, which can be used for space and harsh environments. The developed heterogeneous computer shares the same core architecture as game consoles such as Microsoft Xbox One and Sony Playstation 4 and has an aggregated computational performance in the TFLOP range. The processing power can be used for on-board intelligent data processing and higher degrees of autonomy in general. The module feature quad core 1.5 GHz 64 bit CPU (24 GFLOPs), 160 GPU shader cores (127 GFLOPs), and a 12 Mgate equivalent FPGA fabric with a safety critical ARM® Cortex-M3 MCU. Earlier space use applications of x86 processors have not been safety critical and were susceptible to radiation.
Keywords
fault tolerant computing; field programmable gate arrays; graphics processing units; multiprocessing systems; space vehicle electronics; spacecraft computers; FPGA; GPU; GPU shader cores; Microsoft Xbox One; SFF platform; Sony Playstation 4; TFLOP range; context feature multicore processors; field programmable gate array; frequency 1.5 GHz; game consoles; graphical processing unit; heterogeneous computing low power fault tolerant computer; industrial Qseven small form factor platform; on-board intelligent data processing; operating systems; safety critical ARM Cortex-M3 MCU; small satellites; x86 compatible CPU; Field programmable gate arrays; Graphics processing units; System-on-chip;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Conference, 2015 IEEE
Conference_Location
Big Sky, MT
Print_ISBN
978-1-4799-5379-0
Type
conf
DOI
10.1109/AERO.2015.7119158
Filename
7119158
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