Control Unit For CubeSat

Horký, Jan

Control Unit For CubeSat

but.event.date	27.04.2017	cs
but.event.title	Student EEICT 2017	cs
dc.contributor.author	Horký, Jan
dc.date.accessioned	2020-05-07T09:40:28Z
dc.date.available	2020-05-07T09:40:28Z
dc.date.issued	2017	cs
dc.description.abstract	The 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.format	text	cs
dc.format.extent	248-250	cs
dc.format.mimetype	application/pdf	en
dc.identifier.citation	Proceedings of the 23st Conference STUDENT EEICT 2017. s. 248-250. ISBN 978-80-214-5496-5	cs
dc.identifier.isbn	978-80-214-5496-5
dc.identifier.uri	http://hdl.handle.net/11012/187097
dc.language.iso	en	cs
dc.publisher	Vysoké učení technické v Brně, Fakulta elektrotechniky a komunikačních technologií	cs
dc.relation.ispartof	Proceedings of the 23st Conference STUDENT EEICT 2017	en
dc.relation.uri	http://www.feec.vutbr.cz/EEICT/	cs
dc.rights	© Vysoké učení technické v Brně, Fakulta elektrotechniky a komunikačních technologií	cs
dc.rights.access	openAccess	en
dc.subject	Space	en
dc.subject	CubeSat	en
dc.subject	Control Unit	en
dc.subject	Radiation	en
dc.subject	FPGA	en
dc.title	Control Unit For CubeSat	en
dc.type.driver	conferenceObject	en
dc.type.status	Peer-reviewed	en
dc.type.version	publishedVersion	en
eprints.affiliatedInstitution.department	Fakulta elektrotechniky a komunikačních technologií	cs

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