Publication detail

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

ZIKMUND, P. MATĚJŮ, J.

Original Title

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

Type

journal article in Web of Science

Language

English

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.

Keywords

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

Authors

ZIKMUND, P.; MATĚJŮ, J.

Released

1. 11. 2017

Publisher

SAGE

ISBN

0954-4100

Periodical

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

Year of study

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"
}