Control Unit For CubeSat
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Date
Authors
Horký, Jan
Advisor
Referee
Mark
Journal Title
Journal ISSN
Volume Title
Publisher
Vysoké učení technické v Brně, Fakulta elektrotechniky a komunikačních technologií
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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.
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Citation
Proceedings of the 23st Conference STUDENT EEICT 2017. s. 248-250. ISBN 978-80-214-5496-5
http://www.feec.vutbr.cz/EEICT/
http://www.feec.vutbr.cz/EEICT/
Document type
Peer-reviewed
Document version
Published version
Date of access to the full text
Language of document
en