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