DocumentCode :
3632238
Title :
Attitude control of a quadrotor
Author :
I. Can Dikmen;Aydemir Arisoy;Hakan Temeltas
Author_Institution :
Air Force Academy, ASTIN, Istanbul/TURKEY
fYear :
2009
Firstpage :
722
Lastpage :
727
Abstract :
This study includes altitude stabilization, hovering control any desired position and attitude control of quadrotor. Classically PD controller derived and applied to this system. Inverse dynamic control, feedback linearization control and sliding mode control methods have used to derive as nonlinear controllers. Linear and nonlinear control techniques applied to attitude control of this vehicle. Derived control methods have been performed using computer simulations and compared the results according to this study objective.
Keywords :
"Sliding mode control","Linear feedback control systems","Vehicle dynamics","PD control","Unmanned aerial vehicles","Nonlinear dynamical systems","Control systems","Computer simulation","Propellers","Consumer electronics"
Publisher :
ieee
Conference_Titel :
Recent Advances in Space Technologies, 2009. RAST ´09. 4th International Conference on
Print_ISBN :
978-1-4244-3626-2;978-1-4244-3627-9
Type :
conf
DOI :
10.1109/RAST.2009.5158286
Filename :
5158286
Link To Document :
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