Pitch and flight path control with simultaneous forward gust rejection

dc.creator	Skarpetis, M. G.	en
dc.creator	Koumboulis, F. N.	en
dc.creator	Koussiouris, T. G.	en
dc.date.accessioned	2015-11-23T10:47:26Z
dc.date.available	2015-11-23T10:47:26Z
dc.date.issued	1999
dc.identifier.isbn	9608052122
dc.identifier.uri	http://hdl.handle.net/11615/33068
dc.description.abstract	The problem of rejecting atmospheric disturbances with simultaneous input-output decoupling of the pitch angle and the flight path angle of an aircraft, is studied. The problem is proven to be solvable for almost all flight conditions via static state controllers. All static controllers solving the problem are explicitly characterized. Stability requirements are fulfilled. The present results are illustrated via simulation.	en
dc.source.uri	http://www.scopus.com/inward/record.url?eid=2-s2.0-4944247419&partnerID=40&md5=3a1a54e7a03bc921b002c511178dbc10
dc.subject	Aircraft control	en
dc.subject	Disturbance decoupling	en
dc.subject	Feedback	en
dc.subject	Input-output decoupling	en
dc.subject	Linear systems	en
dc.subject	Stability	en
dc.subject	Approximation theory	en
dc.subject	Control equipment	en
dc.subject	Laplace transforms	en
dc.subject	Parameter estimation	en
dc.subject	Performance	en
dc.subject	Problem solving	en
dc.subject	Transfer functions	en
dc.subject	Vectors	en
dc.subject	Aerodynamic propulsion	en
dc.title	Pitch and flight path control with simultaneous forward gust rejection	en
dc.type	journalArticle	en

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