Design of model rocket with integrated flight control system

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386-eeict-2024.pdf(2.19 MB)
Date
2024
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Mark
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Vysoké učení technické v Brně, Fakulta elektrotechniky a komunikačních technologií
Abstract
This article is describing design and construction of rocket model with solid propellant engine, which communicates in real-time with server. Purpose of this rocket is to engage in vertical flight and afterwards safely return back to the ground, while sending data and recieving orders. In scope of this thesis we developed desktop application versatile in use for controlling flights of model rockets.
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Keywords
rocket, solid propellant rocket motor, rocket recovery, flight software, ground control
Citation
Proceedings I of the 30st Conference STUDENT EEICT 2024: General papers. s. 386-390. ISBN 978-80-214-6231-1
https://www.eeict.cz/eeict_download/archiv/sborniky/EEICT_2024_sbornik_1.pdf
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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
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https://hdl.handle.net/11012/249274
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Student EEICT 2024: General Papers
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