DocumentCode
2833606
Title
Robust Autopilot Design with Maximum Stability Radius
Author
Akmeliawati, Rini ; Chow, Kuang Ye
Author_Institution
Monash Univ. Malaysia, Selangor
fYear
2006
fDate
15-17 Dec. 2006
Firstpage
1137
Lastpage
1142
Abstract
This paper presents the robust control design for aircraft autopilot. The controller provides a maximum stability radius to the closed-loop system. The technique uses the notion of complex stability radius and the Linear Matrix Inequalities (LMI) to obtain the feedback controller gain. The technique is illustrated on a feedback controller of an autopilot system of a twin engine civil aircraft. The results is compared to those that are obtained using a linear quadratic regulator (LQR) technique.
Keywords
aircraft control; closed loop systems; feedback; linear matrix inequalities; closed-loop system; feedback controller; linear matrix inequalities; linear quadratic regulator; maximum stability radius; robust autopilot design; twin engine civil aircraft; Adaptive control; Aerospace control; Aircraft propulsion; Automatic control; Control systems; Linear matrix inequalities; Military aircraft; Regulators; Robust control; Robust stability;
fLanguage
English
Publisher
ieee
Conference_Titel
Industrial Technology, 2006. ICIT 2006. IEEE International Conference on
Conference_Location
Mumbai
Print_ISBN
1-4244-0726-5
Electronic_ISBN
1-4244-0726-5
Type
conf
DOI
10.1109/ICIT.2006.372330
Filename
4237652
Link To Document