DocumentCode :
2647790
Title :
Nonlinear state-dependent Riccati equation control of a quadrotor UAV
Author :
Voos, Holger
Author_Institution :
Faculty of Electrical Engineering and Computer Science, University of Applied Sciences Ravensburg-Weingarten, D-88241, P.O.-Box 1261, Germany
fYear :
2006
fDate :
4-6 Oct. 2006
Firstpage :
2547
Lastpage :
2552
Abstract :
Small quadrotor UAVs represent a very interesting class of small flying robots because of their ability to fly in- and outdoor. Therefore, these vehicles have an enormous potential for near-area surveillance and exploration. However, especially indoor flight is a difficult task for vehicle control which has to stabilize the desired velocity vector and the required attitude of the quadrotor. This paper mainly describes the development of such a nonlinear vehicle control system based on state-dependent Riccati equations (SDRE). The controller is integrated in an overall mission system concept for UAVs.
Keywords :
Aerodynamics; Aircraft; Control systems; Nonlinear equations; Riccati equations; Rotors; Sliding mode control; Surveillance; Unmanned aerial vehicles; Vehicle dynamics;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Computer Aided Control System Design, 2006 IEEE International Conference on Control Applications, 2006 IEEE International Symposium on Intelligent Control, 2006 IEEE
Conference_Location :
Munich, Germany
Print_ISBN :
0-7803-9797-5
Electronic_ISBN :
0-7803-9797-5
Type :
conf
DOI :
10.1109/CACSD-CCA-ISIC.2006.4777039
Filename :
4777039
Link To Document :
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