DocumentCode
574569
Title
Modeling and control of a tilt tri-rotor airplane
Author
Duc Anh Ta ; Fantoni, I. ; Lozano, Rogelio
fYear
2012
fDate
27-29 June 2012
Firstpage
131
Lastpage
136
Abstract
A helicopter offers the capability of hover, slow forward displacement, vertical take-off and landing while a conventional airplane has the performance of fast forward movement, long reach and superior endurance. The aim of this paper is to present the modelling and control of a tilt tri-rotor UAV´s configuration that combines the advantages of both rotary wing and fixed wing vehicle.
Keywords
autonomous aerial vehicles; helicopters; fast forward movement; fixed wing vehicle; helicopter; hover capability; rotary wing; slow forward displacement; tilt trirotor UAV; tilt trirotor airplane; vertical take-off and landing; Aerodynamics; Airplanes; DC motors; Force; Rotors; Vehicles;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference (ACC), 2012
Conference_Location
Montreal, QC
ISSN
0743-1619
Print_ISBN
978-1-4577-1095-7
Electronic_ISBN
0743-1619
Type
conf
DOI
10.1109/ACC.2012.6315155
Filename
6315155
Link To Document