DocumentCode :
3660523
Title :
Dynamic surface control to correct for gyroscopic effect of propellers on quadrotor
Author :
Peng-jie Shao;Wen-han Dong;Xiu-xia Sun;Tuan-jie Ding;Quan Zou
Author_Institution :
Engineering Institute of Aeronautics and Astronautics, Air Force Engineering University, Xi´an, China, 710038
fYear :
2015
Firstpage :
2971
Lastpage :
2976
Abstract :
A dynamic surface controller is proposed to correct for gyroscopic effect from propellers on the motion of large quadrotor. The new control law accounts for adverse effect caused by the gyroscopic effect of propellers that the increased speed leads to high order of oscillation. The proposed controller rapidly converges when reaching the equilibrium point, dramatically improving the convergence speed compared to the classical PID control law. The stability of the closed-loop system is confirmed by Lyapunov stability theory and the results of numerical simulation.
Keywords :
"Propellers","Mathematical model","Rotors","Aerodynamics","Attitude control","Torque"
Publisher :
ieee
Conference_Titel :
Information and Automation, 2015 IEEE International Conference on
Type :
conf
DOI :
10.1109/ICInfA.2015.7279797
Filename :
7279797
Link To Document :
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