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
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