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Please use this identifier to cite or link to this item: https://hdl.handle.net/2440/123370
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dc.contributor.authorAkmeliawati, R.-
dc.contributor.authorChow, K.Y.-
dc.date.issued2006-
dc.identifier.citation2006 IEEE International Conference on Industrial Technology - (ICIT), 2006, pp.1137-1142-
dc.identifier.isbn1424407265-
dc.identifier.isbn9781424407255-
dc.identifier.urihttp://hdl.handle.net/2440/123370-
dc.description.abstractThis 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.-
dc.description.statementofresponsibilityRini Akmeliawati and Kuang Ye Chow-
dc.language.isoen-
dc.publisherIEEE-
dc.rights© 2006 IEEE-
dc.source.urihttp://dx.doi.org/10.1109/icit.2006.372330-
dc.titleRobust autopilot design with maximum stability radius-
dc.typeConference paper-
dc.contributor.conferenceIEEE International Conference on Industrial Technology (ICIT) (15 Dec 2006 - 17 Dec 2006 : Mumbai, India)-
dc.identifier.doi10.1109/ICIT.2006.372330-
pubs.publication-statusPublished-
dc.identifier.orcidAkmeliawati, R. [0000-0003-0660-2312]-
Appears in Collections:Aurora harvest 4
Mechanical Engineering publications

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