DocumentCode
1925100
Title
The Research of 3 DOF Helicopter Tracking Controller
Author
Li, Ei-ran ; Shen, Tao
Volume
1
fYear
2007
fDate
19-22 Aug. 2007
Firstpage
578
Lastpage
582
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;
fLanguage
English
Publisher
ieee
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
Type
conf
DOI
10.1109/ICMLC.2007.4370211
Filename
4370211
Link To Document