Detail publikace

Dynamic soaring of unmanned aerial vehicle within airliner wake vortex in climb regime

ZIKMUND, P. MATĚJŮ, J.

Originální název

Dynamic soaring of unmanned aerial vehicle within airliner wake vortex in climb regime

Typ

článek v časopise ve Web of Science, Jimp

Jazyk

angličtina

Originální abstrakt

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.

Klíčová slova

Dynamic soaring, Formation flight, Wake vortex, Self-sustained flight, Unmanned aerial vehicle

Autoři

ZIKMUND, P.; MATĚJŮ, J.

Vydáno

1. 11. 2017

Nakladatel

SAGE

ISSN

0954-4100

Periodikum

PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING

Ročník

231

Číslo

13

Stát

Spojené království Velké Británie a Severního Irska

Strany od

2479

Strany do

2486

Strany počet

8

URL

http://pig.sagepub.com/content/early/2016/09/02/0954410016667147.abstract

Plný text v Digitální knihovně

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"
}