Aerodynamic modeling of the Skywalker X8 Fixed-Wing Unmanned Aerial Vehicle

Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21230%2F18%3A00328410" target="_blank" >RIV/68407700:21230/18:00328410 - isvavai.cz</a>
Result on the web
<a href="https://ieeexplore.ieee.org/document/8453370" target="_blank" >https://ieeexplore.ieee.org/document/8453370</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.1109/ICUAS.2018.8453370" target="_blank" >10.1109/ICUAS.2018.8453370</a>

Result language
angličtina
Original language name
Aerodynamic modeling of the Skywalker X8 Fixed-Wing Unmanned Aerial Vehicle
Original language description
With advanced control, estimation and simulation requirements in unmanned aerial systems comes the need for sophisticated aerodynamic models. This paper reviews two common means for establishing such models; numerical design tools and wind tunnel testing, by presenting strengths and potential problems, in a ”lessons learned”-manner. As a case study throughout the paper, a six degrees-of-freedom aerodynamic model of the Skywalker X8 fixed-wing unmanned aerial vehicle is presented.
Czech name
—
Czech description
—

Project
<a href="/en/project/EF16_019%2F0000826" target="_blank" >EF16_019/0000826: Center of Advanced Aerospace Technology</a><br>
Continuities
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Publication year
2018
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Article name in the collection
UNMANNED AIRCRAFT SYSTEMS. INTERNATIONAL CONFERENCE. 2018. (ICUAS 2018)
ISBN
978-1-5386-1354-2
ISSN
2373-6720
e-ISSN
—
Number of pages
10
Pages from-to
826-835
Publisher name
Curran Associates
Place of publication
Red Hook, NY
Event location
Dallas, TX
Event date
Jun 11, 2018
Type of event by nationality
WRD - Celosvětová akce
UT code for WoS article
000454860700102

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