DocumentCode :
548367
Title :
Reduced order modeling for Unmanned Aerial Vehicle
Author :
Gadewadikar, J. ; Kuljaca, O. ; Horvat, K.
Author_Institution :
Syst. Res. Inst., Alcorn State Univ., Lorman, MS, USA
fYear :
2011
fDate :
23-27 May 2011
Firstpage :
664
Lastpage :
667
Abstract :
This paper presents a reduced order modeling procedure for Rotary wing Unmanned Aerial Vehicles. There is a growing interest in developing control strategies for unmanned autonomous helicopters, in particular a small scale one. The procedure for deriving a six degrees-of-freedom module form standard 12th order rigid body dynamics is given.
Keywords :
aerospace components; aircraft control; reduced order systems; remotely operated vehicles; reduced order modeling; rotary wing unmanned aerial vehicle; unmanned autonomous helicopter; Aerodynamics; Barium; Equations; Helicopters; Mathematical model; Reduced order systems; Vehicle dynamics;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
MIPRO, 2011 Proceedings of the 34th International Convention
Conference_Location :
Opatija
Print_ISBN :
978-1-4577-0996-8
Type :
conf
Filename :
5967137
Link To Document :
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