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: | , |
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Format: | Conference or Workshop Item |
Language: | English |
Published: |
2007
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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 |