DocumentCode :
2773152
Title :
Dynamic analysis and PID control for a quadrotor
Author :
Li, Jun ; Li, Yuntang
Author_Institution :
Coll. of Mech. & Electr. Eng., China Jiliang Univ., Hangzhou, China
fYear :
2011
fDate :
7-10 Aug. 2011
Firstpage :
573
Lastpage :
578
Abstract :
In order to analyze the dynamic characteristics and PID controller performance of a quadrotor, this paper firstly describes the architecture of the quadrotor and analyzes the dynamic model of it. Then, based on the classic scheme of PID control, this paper designs a controller, which aims to regulate the posture (position and orientation) of the 6 d.o.f. quadrotor. Thirdly, the dynamic model is implemented in Matlab/Simulink simulation, and the PID control parameters are obtained according to the simulation results. Finally, a quadrotor with PID controllers is designed and made. In order to do the experiment, a flying experiment for the quadrotor has been done. The results of flying experiment show that the PID controllers robustly stabilize the quadrotor.
Keywords :
aerospace robotics; control system synthesis; robot dynamics; robust control; three-term control; PID control design; dynamic model; quadrotor; robust stability; Aircraft; Attitude control; Carbon; Equations; Mathematical model; Optical fiber sensors; Rotors; Dynamic model; PID controller; Quadrotor;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Mechatronics and Automation (ICMA), 2011 International Conference on
Conference_Location :
Beijing
ISSN :
2152-7431
Print_ISBN :
978-1-4244-8113-2
Type :
conf
DOI :
10.1109/ICMA.2011.5985724
Filename :
5985724
Link To Document :
بازگشت