Please use this identifier to cite or link to this item: http://hdl.handle.net/2440/123370
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Type: Conference paper
Title: Robust autopilot design with maximum stability radius
Author: Akmeliawati, R.
Chow, K.Y.
Citation: 2006 IEEE International Conference on Industrial Technology - (ICIT), 2006 / pp.1137-1142
Publisher: IEEE
Issue Date: 2006
ISBN: 1424407265
9781424407255
Conference Name: IEEE International Conference on Industrial Technology (ICIT) (15 Dec 2006 - 17 Dec 2006 : Mumbai, India)
Statement of
Responsibility: 
Rini Akmeliawati and Kuang Ye Chow
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.
Rights: © 2006 IEEE
RMID: 1000013859
DOI: 10.1109/ICIT.2006.372330
Appears in Collections:Mechanical Engineering publications

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