Flight Endurance Measurement of a Multicopter UAS

Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F60162694%3AG43__%2F19%3A00537214" target="_blank" >RIV/60162694:G43__/19:00537214 - isvavai.cz</a>
Result on the web
<a href="http://dx.doi.org/10.1109/MILTECHS.2019.8870033" target="_blank" >http://dx.doi.org/10.1109/MILTECHS.2019.8870033</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.1109/MILTECHS.2019.8870033" target="_blank" >10.1109/MILTECHS.2019.8870033</a>

Result language
angličtina
Original language name
Flight Endurance Measurement of a Multicopter UAS
Original language description
This article describes the flight endurance measurements of current commercially available multicopter. Endurance, as one of the most comprehensive parameter of this machine, is influenced by a number of factors as altitude, weather conditions, character of the flight, load and energy capacity. The theoretical description of influencing factors is complemented by practical flight tests, based on measurements on the representative Yuneec Typhoon H hexacopter carried out both in the Czech Republic region and at the Bagram Air Field (BAF) in Afghanistan. These measurements can be the basis for the future measurement of flight performances of multicopters, which are about to be introduced into the Czech Army operation service.
Czech name
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Czech description
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Publication year
2019
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Article name in the collection
International Conference on Military Technologies (ICMT) 2019
ISBN
978-172814593-8
ISSN
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e-ISSN
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Number of pages
6
Pages from-to
8870033
Publisher name
Institute of Electrical and Electronics Engineers Inc.
Place of publication
Brno
Event location
Brno, Czech Republic
Event date
May 30, 2019
Type of event by nationality
WRD - Celosvětová akce
UT code for WoS article
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