Control Unit For CubeSat
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Date
2017
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Mark
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Vysoké učení technické v Brně, Fakulta elektrotechniky a komunikačních technologií
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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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/
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Peer-reviewed
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en
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© Vysoké učení technické v Brně, Fakulta elektrotechniky a komunikačních technologií