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|Title:||Robust autopilot design with maximum stability radius|
|Citation:||2006 IEEE International Conference on Industrial Technology - (ICIT), 2006 / pp.1137-1142|
|Conference Name:||IEEE International Conference on Industrial Technology (ICIT) (15 Dec 2006 - 17 Dec 2006 : Mumbai, India)|
|Rini Akmeliawati and Kuang Ye Chow|
|Abstract:||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 is illustrated on a feedback controller of an autopilot system of a twin engine civil aircraft. The results is compared to those that are obtained using a linear quadratic regulator (LQR) technique.|
|Rights:||© 2006 IEEE|
|Appears in Collections:||Mechanical Engineering publications|
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