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dc.contributor.advisorCollins, Daniel J.
dc.contributor.authorHsu, Ta-Chieh
dc.dateDecember 1989
dc.date.accessioned2013-01-23T22:07:44Z
dc.date.available2013-01-23T22:07:44Z
dc.date.issued1989-12
dc.identifier.urihttp://hdl.handle.net/10945/26886
dc.description.abstractH„ optimal control theory, based on singular value loop shaping, is used to synthesize a controller for the statically unstable longitudinal dynamics of X-29 aircraft. Two design cases are studied: 2-input 2-output; and 3-input 3-output cases. H„ theory provides a direct, effective procedure for synthesizing control laws satisfying specified performance objectives and robustness specifications. The 2 I/O case has better performance, a faster response and is more robust, than the 3 I/O case. Discussion and comparison of results are given.
dc.description.urihttp://archive.org/details/applicationofhin1094526886
dc.format.extent79 p.en_US
dc.language.isoen_US
dc.publisherMonterey, California. Naval Postgraduate Schoolen_US
dc.rightsCopyright is reserved by the copyright owner
dc.titleApplication of H infinity method to modern fighter configurationen_US
dc.typeThesisen_US
dc.contributor.secondreaderChang, Liang-Wey
dc.contributor.corporateNaval Postgraduate School (U.S.)
dc.contributor.departmentMechanical Engineering
dc.subject.authorH„ control theoryen_US
dc.subject.authorrobust control systemen_US
dc.subject.authorsensitivityen_US
dc.subject.authordisturbance attenuationen_US
dc.subject.authorX-29 controller synthesisen_US
dc.subject.authoraugmented planten_US
dc.subject.authorsmall gain problemen_US
dc.description.serviceCaptain, Republic of China on Taiwan Army
etd.thesisdegree.nameM.S. in Engineering Scienceen_US
etd.thesisdegree.nameM.S. in Mechanical Engineeringen_US
etd.thesisdegree.levelMastersen_US
etd.thesisdegree.disciplineEngineering Scienceen_US
etd.thesisdegree.disciplineMechanical Engineeringen_US
etd.thesisdegree.grantorNaval Postgraduate Schoolen_US
dc.description.distributionstatementApproved for public release; distribution is unlimited.


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