Control design for longitudinal flight dynamics

完整後設資料紀錄

DC 欄位	值	語言
dc.contributor.author	Liaw, Der-Cherng	en_US
dc.contributor.author	Chung, Wen-Ching	en_US
dc.contributor.author	Hsieh, Chien-Shu	en_US
dc.date.accessioned	2014-12-08T15:24:58Z	-
dc.date.available	2014-12-08T15:24:58Z	-
dc.date.issued	2006	en_US
dc.identifier.isbn	0-7695-2616-0	en_US
dc.identifier.uri	http://hdl.handle.net/11536/17347	-
dc.description.abstract	In this paper, the control issues of longitudinal flight dynamics is presented. System controllability with respect to the variation of the elevator deflection angle is first discussed Stabilization controllers using washout filter-aided feedback control law is then proposed Case study for F-8 aircraft is explicitly derived for constructing a feasible set of controllers. Numerical simulations for bifurcation scenarios are also given to compare the performance of the designs.	en_US
dc.language.iso	en_US	en_US
dc.title	Control design for longitudinal flight dynamics	en_US
dc.type	Proceedings Paper	en_US
dc.identifier.journal	ICICIC 2006: First International Conference on Innovative Computing, Information and Control, Vol 2, Proceedings	en_US
dc.citation.spage	150	en_US
dc.citation.epage	153	en_US
dc.contributor.department	電控工程研究所	zh_TW
dc.contributor.department	Institute of Electrical and Control Engineering	en_US
dc.identifier.wosnumber	WOS:000240868000037	-
顯示於類別：	會議論文