Robust autopilot design with maximum stability radius

• 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

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...