Generic on-board-computer hardware and software development for nanosatellite applications

dc.contributor.advisorLee, Regina
dc.contributor.advisorQuine, Brendan
dc.creatorBorschiov, Konstantin
dc.date.accessioned2016-08-03T16:51:36Z
dc.date.available2016-08-03T16:51:36Z
dc.date.copyright2012-11
dc.date.issued2012-11
dc.degree.disciplineEarth & Space Science
dc.degree.levelMaster's
dc.degree.nameMSc - Master of Science
dc.description.abstractThis study outlines the results obtained from the development of a generic nanosatellite on-board-computer (OBC). The nanosatellite OBC is a non-mission specific design and as such it must be adaptable to changing mission requirements in order to be suitable for varying nanosatellite missions. Focus is placed on the commercial-off-the-shelf (COTS) principle where commercial components are used and evaluated for their potential performance in nanosatellite applications. The OBC design is prototyped and subjected to tests to evaluate its performance and its feasibility to survive in space.
dc.identifier.urihttp://hdl.handle.net/10315/31692
dc.rightsAuthor owns copyright, except where explicitly noted. Please contact the author directly with licensing requests.
dc.subject.keywordsgeneric-on-board-computer
dc.subject.keywordsnanosatellite applications
dc.subject.keywordsOBC
dc.subject.keywordsspace
dc.titleGeneric on-board-computer hardware and software development for nanosatellite applications
dc.typeElectronic Thesis or Dissertation

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