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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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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/5293/1/icit2006.pdf
http://irep.iium.edu.my/5293/
http://dx.doi.org/10.1109/ICIT.2006.372330
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spelling my.iium.irep.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 REM 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
institution Universiti Islam Antarabangsa Malaysia
building IIUM Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider International Islamic University Malaysia
content_source IIUM Repository (IREP)
url_provider http://irep.iium.edu.my/
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/5293/1/icit2006.pdf
http://irep.iium.edu.my/5293/
http://dx.doi.org/10.1109/ICIT.2006.372330
_version_ 1643605509490606080
score 13.18916

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