Title :
The Research of 3 DOF Helicopter Tracking Controller
Author :
Li, Ei-ran ; Shen, Tao
Abstract :
In this paper, an uncertain state-space model is implemented for a 3 DOF helicopter, the linear quadratic regulator (LQR) tracking control law is given and the robust tracking control law which is satisfied the request of R,Q and Hinfin is designed by means of linear matrix inequality (LMI). The results show the validity of this approach.
Keywords :
Hinfin control; aircraft control; helicopters; linear matrix inequalities; linear quadratic control; robust control; tracking; 3 DOF helicopter tracking controller; Hinfin control; LMI; linear matrix inequality; linear quadratic regulator; robust tracking control law; tracking control law; uncertain state-space model; Cybernetics; Design engineering; Differential equations; Helicopters; Machine learning; Mathematical model; Propellers; Robust control; Torque; Voltage; 3 DOF helicopter; LQR; Robust tracking control;
Conference_Titel :
Machine Learning and Cybernetics, 2007 International Conference on
Conference_Location :
Hong Kong
Print_ISBN :
978-1-4244-0973-0
Electronic_ISBN :
978-1-4244-0973-0
DOI :
10.1109/ICMLC.2007.4370211
