Dynamic soaring of unmanned aerial vehicle within airliner wake vortex in climb regime
Loading...
Date
Authors
Zikmund, Pavel
Matějů, Jiří
Advisor
Referee
Mark
Journal Title
Journal ISSN
Volume Title
Publisher
SAGE
0000-0002-5793-8628 Altmetrics
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.
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.
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.
Description
Citation
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING. 2017, vol. 231, issue 13, p. 2479-2486.
http://pig.sagepub.com/content/early/2016/09/02/0954410016667147.abstract
http://pig.sagepub.com/content/early/2016/09/02/0954410016667147.abstract
Document type
Peer-reviewed
Document version
Accepted version
Date of access to the full text
Language of document
en