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dc.contributor.authorLiaw, DCen_US
dc.contributor.authorSong, CCen_US
dc.contributor.authorChung, WCen_US
dc.date.accessioned2014-12-08T15:26:03Z-
dc.date.available2014-12-08T15:26:03Z-
dc.date.issued2003en_US
dc.identifier.isbn0-7803-7896-2en_US
dc.identifier.issn0743-1619en_US
dc.identifier.urihttp://hdl.handle.net/11536/18466-
dc.description.abstractThis paper presents the nonlinear analysis and control of a third-order model for longitudinal flight dynamics. Bifurcation analysis using numerical study for F-8 aircraft reveals that Hopf bifurcations may occur at some critical values of the elevator commands. These results agree with the well-known nonlinear phenomena existed in longitudinal flight dynamics. Furthermore, bifurcation control using both washout filter and direct state feedback are applied to develop the stabilizing laws for system equilibria and periodic solutions emerged from bifurcation points. Numerical simulations are provided to demonstrate these main results.en_US
dc.language.isoen_USen_US
dc.titleNonlinear control of longitudinal flight dynamicsen_US
dc.typeProceedings Paperen_US
dc.identifier.journalPROCEEDINGS OF THE 2003 AMERICAN CONTROL CONFERENCE, VOLS 1-6en_US
dc.citation.spage1637en_US
dc.citation.epage1642en_US
dc.contributor.department電控工程研究所zh_TW
dc.contributor.departmentInstitute of Electrical and Control Engineeringen_US
dc.identifier.wosnumberWOS:000186706200277-
Appears in Collections:Conferences Paper