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:
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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Institution: Universiti Islam Antarabangsa Malaysia
Language: English
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