Decoupling of the longitudinal modes of advanced aircraft

Skarpetis, MG; Koumboulis, FN

dc.contributor.author	Skarpetis, MG	en
dc.contributor.author	Koumboulis, FN	en
dc.date.accessioned	2014-03-01T01:11:51Z
dc.date.available	2014-03-01T01:11:51Z
dc.date.issued	1996	en
dc.identifier.issn	0731-5090	en
dc.identifier.uri	https://dspace.lib.ntua.gr/xmlui/handle/123456789/11831
dc.relation.uri	http://www.scopus.com/inward/record.url?eid=2-s2.0-0030241322&partnerID=40&md5=669e46ec8ff78495203b1e9c931e5187	en
dc.subject.classification	Engineering, Aerospace	en
dc.subject.classification	Instruments & Instrumentation	en
dc.subject.other	Aircraft	en
dc.subject.other	Closed loop control systems	en
dc.subject.other	Computer simulation	en
dc.subject.other	Control theory	en
dc.subject.other	Damping	en
dc.subject.other	Feedback control	en
dc.subject.other	Mathematical models	en
dc.subject.other	Mechanical variables control	en
dc.subject.other	Nonlinear equations	en
dc.subject.other	Transfer functions	en
dc.subject.other	Advanced aircraft	en
dc.subject.other	Decoupling	en
dc.subject.other	Eigenstructure assignment	en
dc.subject.other	Flight path angle	en
dc.subject.other	Longitudinal modes	en
dc.subject.other	Flight dynamics	en
dc.title	Decoupling of the longitudinal modes of advanced aircraft	en
heal.type	journalArticle	en
heal.language	English	en
heal.publicationDate	1996	en
heal.abstract	In this study, the pitch and flight-path angle of a multimode aircraft have been independently controlled, via static state feedback, using the input-output decoupling with simultaneous arbitrary pole assignment technique. The satisfactory closed-loop performance is illustrated by simulation for an AFTI F-16 aircraft. However, the present technique basically differs from that of eigenstructure assignment on the starting point. Based on this difference several results have been obtained which enabled the desirable damping and settling time to be achieved.	en
heal.publisher	AIAA, Washington, DC, United States	en
heal.journalName	Journal of Guidance, Control, and Dynamics	en
dc.identifier.isi	ISI:A1996VE51300029	en
dc.identifier.volume	19	en
dc.identifier.issue	5	en
dc.identifier.spage	1184	en
dc.identifier.epage	1186	en