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
格式: Conference or Workshop Item
语言:English
出版: 2007
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在线阅读: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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