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...
| Главные авторы: | , |
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| Формат: | Proceeding Paper |
| Язык: | English |
| Опубликовано: |
2007
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| Предметы: | |
| Online-ссылка: | http://irep.iium.edu.my/5293/1/icit2006.pdf |