Design of model rocket with integrated flight control system

but.event.date23.04.2024cs
but.event.titleSTUDENT EEICT 2024cs
dc.contributor.authorKadlec, Ondřej
dc.contributor.authorWalla, Petr
dc.date.accessioned2024-07-09T07:38:43Z
dc.date.available2024-07-09T07:38:43Z
dc.date.issued2024cs
dc.description.abstractThis 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.en
dc.formattextcs
dc.format.extent386-390cs
dc.format.mimetypeapplication/pdfen
dc.identifier.citationProceedings I of the 30st Conference STUDENT EEICT 2024: General papers. s. 386-390. ISBN 978-80-214-6231-1cs
dc.identifier.isbn978-80-214-6231-1
dc.identifier.issn2788-1334
dc.identifier.urihttps://hdl.handle.net/11012/249274
dc.language.isoencs
dc.publisherVysoké učení technické v Brně, Fakulta elektrotechniky a komunikačních technologiícs
dc.relation.ispartofProceedings I of the 30st Conference STUDENT EEICT 2024: General papersen
dc.relation.urihttps://www.eeict.cz/eeict_download/archiv/sborniky/EEICT_2024_sbornik_1.pdfcs
dc.rights© Vysoké učení technické v Brně, Fakulta elektrotechniky a komunikačních technologiícs
dc.rights.accessopenAccessen
dc.subjectrocketen
dc.subjectsolid propellant rocket motoren
dc.subjectrocket recoveryen
dc.subjectflight softwareen
dc.subjectground controlen
dc.titleDesign of model rocket with integrated flight control systemen
dc.type.driverconferenceObjecten
dc.type.statusPeer-revieweden
dc.type.versionpublishedVersionen
eprints.affiliatedInstitution.departmentFakulta elektrotechniky a komunikačních technologiícs
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