Robust autopilot design with maximum stability radius

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...

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Bibliographic Details
Main Authors:	Akmeliawati, Rini, Kuang, Ye Chow
Format:	Conference or Workshop Item
Language:	English
Published:	2007
Subjects:	TJ212 Control engineering TK Electrical engineering. Electronics Nuclear engineering
Online Access:	http://irep.iium.edu.my/5293/ http://irep.iium.edu.my/5293/ http://irep.iium.edu.my/5293/ http://irep.iium.edu.my/5293/1/icit2006.pdf

id	iium-5293
recordtype	eprints
spelling	iium-52932012-05-23T01:22:06Z http://irep.iium.edu.my/5293/ Robust autopilot design with maximum stability radius Akmeliawati, Rini Kuang, Ye Chow TJ212 Control engineering TK Electrical engineering. Electronics Nuclear engineering 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. 2007 Conference or Workshop Item PeerReviewed application/pdf en http://irep.iium.edu.my/5293/1/icit2006.pdf Akmeliawati, Rini and Kuang, Ye Chow (2007) Robust autopilot design with maximum stability radius. In: IEEE International Conference on Industrial Technology, 2006. ICIT 2006., 15-17 Dec, 2006, Mumbai. http://dx.doi.org/10.1109/ICIT.2006.372330 doi:10.1109/ICIT.2006.372330
repository_type	Digital Repository
institution_category	Local University
institution	International Islamic University Malaysia
building	IIUM Repository
collection	Online Access
language	English
topic	TJ212 Control engineering TK Electrical engineering. Electronics Nuclear engineering
spellingShingle	TJ212 Control engineering TK Electrical engineering. Electronics Nuclear engineering Akmeliawati, Rini Kuang, Ye Chow Robust autopilot design with maximum stability radius
description	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.
format	Conference or Workshop Item
author	Akmeliawati, Rini Kuang, Ye Chow
author_facet	Akmeliawati, Rini Kuang, Ye Chow
author_sort	Akmeliawati, Rini
title	Robust autopilot design with maximum stability radius
title_short	Robust autopilot design with maximum stability radius
title_full	Robust autopilot design with maximum stability radius
title_fullStr	Robust autopilot design with maximum stability radius
title_full_unstemmed	Robust autopilot design with maximum stability radius
title_sort	robust autopilot design with maximum stability radius
publishDate	2007
url	http://irep.iium.edu.my/5293/ http://irep.iium.edu.my/5293/ http://irep.iium.edu.my/5293/ http://irep.iium.edu.my/5293/1/icit2006.pdf
first_indexed	2023-09-18T20:13:49Z
last_indexed	2023-09-18T20:13:49Z
_version_	1777407653860868096

Robust autopilot design with maximum stability radius

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