Please use this identifier to cite or link to this item:
|Title:||Design and control for rotor-fixed wing hybrid aircraft|
Vertical take-off and landing
|Source:||Wang, X., Lin, H. (2011-07). Design and control for rotor-fixed wing hybrid aircraft. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 225 (7) : 831-847. ScholarBank@NUS Repository. https://doi.org/10.1177/2041302510394742|
|Abstract:||This article presents a model of rotor-fixed wing hybrid aircraft, which can operate as a helicopter as well as transition to fixed-wing flight. The control mission includes: hover, vertical take-off and landing, forward flight, from hover to forward flight, and vice versa. A backsteppingbased control method for the aircraft is designed to keep the flying height invariant during mode transitions from hover to forward flight and vice versa. The other control missions mentioned are not considered in this article. © Author 2011.|
|Source Title:||Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering|
|Appears in Collections:||Staff Publications|
Show full item record
Files in This Item:
There are no files associated with this item.
checked on Feb 22, 2018
WEB OF SCIENCETM
checked on Jan 23, 2018
checked on Feb 19, 2018
Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.