Please use this identifier to cite or link to this item: https://er.nau.edu.ua/handle/NAU/25369
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dc.contributor.authorTupitsin, Nikolayen
dc.contributor.authorMalakhov, Sergeyen
dc.contributor.authorShcherbina, Lizaen
dc.date.accessioned2017-03-17T07:39:19Z-
dc.date.available2017-03-17T07:39:19Z-
dc.date.issued2015-10-
dc.identifier.isbn978-1-4673-6566-6-
dc.identifier.urihttp://er.nau.edu.ua/handle/NAU/25369-
dc.descriptionUkraine Section SP/AES Joint Chapteren
dc.description.abstractIn article the initial constructive part of springboard is proposed. Also, the calculation and analysis of unmanned aerial vehicle initial conditions at takeoff with spring-loaded final part of springboard are executed. The two technical contrivances as spring-loaded final part were considered: elastically restrained plate and spring-loaded bridge.en
dc.language.isoenen
dc.publisherOsvita Ukrainyen
dc.relation.ispartofseriesCFP1529V-PRT;Session A, 59-62en
dc.relation.ispartofseriesIEEE 3rd International Conference;en
dc.subjectunmanned aerial vehicleen
dc.titleCalculation and Analysis of Initial Conditions at Takeoff of UAV with Springboarden
dc.typeArticleen
dc.specialityAdvanced Methods of Computer-Aided Design, Aerodynamics, Flight-Technical Characteristics, Durability of UAVen
Appears in Collections:Матеріали наукових, науково-практичних конференцій кафедри авіаційних комп'ютерно-інтегрованих комплексів

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