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dc.contributor.authorHorký, Jan
dc.date.accessioned2020-05-07T09:40:28Z
dc.date.available2020-05-07T09:40:28Z
dc.date.issued2017cs
dc.identifier.citationProceedings of the 23st Conference STUDENT EEICT 2017. s. 248-250. ISBN 978-80-214-5496-5cs
dc.identifier.isbn978-80-214-5496-5
dc.identifier.urihttp://hdl.handle.net/11012/187097
dc.description.abstractThe aim of the project was to design a CubeSat control unit. The board is composed of commercial parts yet reliable in the space environment. Because of its benefits, an FPGA was selected as the core of the board. The FPGA is periodically checked for errors and reset if an error is found. The unit has various sensors to monitor its condition and can do necessary measures. Two MRAMs allow to store a golden bitstream and upload new bitstream in flight.en
dc.formattextcs
dc.format.extent248-250cs
dc.format.mimetypeapplication/pdfen
dc.language.isoencs
dc.publisherVysoké učení technické v Brně, Fakulta elektrotechniky a komunikačních technologiícs
dc.relation.ispartofProceedings of the 23st Conference STUDENT EEICT 2017en
dc.relation.urihttp://www.feec.vutbr.cz/EEICT/cs
dc.rights© Vysoké učení technické v Brně, Fakulta elektrotechniky a komunikačních technologiícs
dc.subjectSpaceen
dc.subjectCubeSaten
dc.subjectControl Uniten
dc.subjectRadiationen
dc.subjectFPGAen
dc.titleControl Unit For CubeSaten
eprints.affiliatedInstitution.departmentFakulta elektrotechniky a komunikačních technologiícs
but.event.date27.04.2017cs
but.event.titleStudent EEICT 2017cs
dc.rights.accessopenAccessen
dc.type.driverconferenceObjecten
dc.type.statusPeer-revieweden
dc.type.versionPublishers's versionen


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