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...

Full description

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/
http://irep.iium.edu.my/5293/
http://irep.iium.edu.my/5293/
http://irep.iium.edu.my/5293/1/icit2006.pdf