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ZIKMUND, P.; MATĚJŮ, J.
Original Title
Dynamic soaring of unmanned aerial vehicle within airliner wake vortex in climb regime
English Title
Type
WoS Article
Original Abstract
The paper presents an analysis of an unmanned aerial vehicle gliding in an airliner wake vortex using the dynamic soaring principle. The presented results provide insight into energy balance and controllability of the unmanned aerial vehicle flying in an airliner wake vortex.
English abstract
Keywords
Dynamic soaring, Formation flight, Wake vortex, Self-sustained flight, Unmanned aerial vehicle
Key words in English
Authors
RIV year
2018
Released
01.11.2017
Publisher
SAGE
ISBN
0954-4100
Periodical
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING
Volume
231
Number
13
State
United Kingdom of Great Britain and Northern Ireland
Pages from
2479
Pages to
2486
Pages count
8
URL
http://pig.sagepub.com/content/early/2016/09/02/0954410016667147.abstract
Full text in the Digital Library
http://hdl.handle.net/11012/63674
BibTex
@article{BUT128483, author="Pavel {Zikmund} and Jiří {Matějů}", title="Dynamic soaring of unmanned aerial vehicle within airliner wake vortex in climb regime", journal="PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING", year="2017", volume="231", number="13", pages="2479--2486", doi="10.1177/0954410016667147", issn="0954-4100", url="http://pig.sagepub.com/content/early/2016/09/02/0954410016667147.abstract" }