Adelaide Research & Scholarship
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https://hdl.handle.net/2440/123370
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| Type: | Conference paper |
| Title: | Robust autopilot design with maximum stability radius |
| Author: | Akmeliawati, R. Chow, K.Y. |
| Citation: | 2006 IEEE International Conference on Industrial Technology - (ICIT), 2006, pp.1137-1142 |
| Publisher: | IEEE |
| Issue Date: | 2006 |
| ISBN: | 1424407265 9781424407255 |
| Conference Name: | IEEE International Conference on Industrial Technology (ICIT) (15 Dec 2006 - 17 Dec 2006 : Mumbai, India) |
| Statement of Responsibility: | 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 |
| DOI: | 10.1109/ICIT.2006.372330 |
| Published version: | http://dx.doi.org/10.1109/icit.2006.372330 |
| Appears in Collections: | Aurora harvest 4 Mechanical Engineering publications |
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