DocumentCode :
2824174
Title :
Rotary wing UAV position control using backstepping
Author :
Ahmed, Bilal ; Pota, Hemanshu R. ; Garratt, Matt
Author_Institution :
Univ. of New South Wales, Canberra
fYear :
2007
fDate :
12-14 Dec. 2007
Firstpage :
1957
Lastpage :
1962
Abstract :
This paper presents a novel position control method for rotary wing UAVs using the backstepping approach. The algorithm, motivated by backstepping control for general rigid body dynamics, is extended for underactuated UAV including the flybar and flapping dynamics when stability derivatives are not available. Further work is needed to include servo dynamics and to make the algorithm robust to model uncertainty to make it suitable for practical implementation.
Keywords :
helicopters; position control; remotely operated vehicles; stability; vehicle dynamics; velocity control; backstepping method; flapping dynamics; general rigid body dynamics; rotary wing UAV position control; unmanned aerial vehicle; Aerodynamics; Backstepping; Blades; Control systems; Equations; Helicopters; Position control; Tail; Unmanned aerial vehicles; Velocity control;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Decision and Control, 2007 46th IEEE Conference on
Conference_Location :
New Orleans, LA
ISSN :
0191-2216
Print_ISBN :
978-1-4244-1497-0
Electronic_ISBN :
0191-2216
Type :
conf
DOI :
10.1109/CDC.2007.4434589
Filename :
4434589
Link To Document :
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