DocumentCode
2909723
Title
Implementation of a Dependable Multiprocessor CubeSat
Author
Samson, John R., Jr.
Author_Institution
Aerosp., Defense & Space Syst., Honeywell Int., Inc., Clearwater, FL, USA
fYear
2011
fDate
5-12 March 2011
Firstpage
1
Lastpage
10
Abstract
Space applications have been, and will continue to be, subject to severe size, weight, and power constraints. The need for and the use of high performance embedded computing in space exacerbates the size, weight, and power problems. Flying high performance embedded computing in CubeSat applications presents particularly unique problems which require unique solutions. Fortunately, there are three technologies that make flying high performance embedded computing on CubeSats feasible: 1) the availability of high power CubeSats, 2) the availability of small, light-weight, low-power, Commercial-Off-The-Shelf (COTS) Computer-on-Module (COM), e.g., Gumstix™, technologies which are potential solutions to the size, weight, and power problems, and 3) platform-, technology-, and application-independent Dependable Multiprocessor Middleware (DMM), which allows COTS COM technologies to be used in space applications. The paper provides a brief overview of these three technologies and presents the results of investigations of DM CubeSat implementations to date.
Keywords
aerospace computing; embedded systems; middleware; multiprocessing systems; space research; CubeSat; commercial off the shelf computer on module; dependable multiprocessor middleware; flying high performance embedded computing; space exacerbates; Control systems; Delta modulation; Fault tolerance; Fault tolerant systems; Hardware; Middleware; Space technology;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Conference, 2011 IEEE
Conference_Location
Big Sky, MT
ISSN
1095-323X
Print_ISBN
978-1-4244-7350-2
Type
conf
DOI
10.1109/AERO.2011.5747461
Filename
5747461
Link To Document