Disturbance rejection for an aircraft flying in atmospheric disturbances

Skarpetis, MG

dc.contributor.author	Skarpetis, MG	en
dc.date.accessioned	2014-03-01T01:10:56Z
dc.date.available	2014-03-01T01:10:56Z
dc.date.issued	1995	en
dc.identifier.issn	0925-4668	en
dc.identifier.uri	https://dspace.lib.ntua.gr/xmlui/handle/123456789/11503
dc.subject.classification	Automation & Control Systems	en
dc.subject.classification	Engineering, Mechanical	en
dc.subject.other	Aircraft	en
dc.subject.other	Closed loop control systems	en
dc.subject.other	Control system synthesis	en
dc.subject.other	System stability	en
dc.subject.other	Vectors	en
dc.subject.other	Velocity	en
dc.subject.other	Wind effects	en
dc.subject.other	Atmospheric disturbance	en
dc.subject.other	Disturbance rejection	en
dc.subject.other	Stabilizability	en
dc.subject.other	Feedback control	en
dc.title	Disturbance rejection for an aircraft flying in atmospheric disturbances	en
heal.type	journalArticle	en
heal.identifier.primary	10.1007/BF01968504	en
heal.identifier.secondary	http://dx.doi.org/10.1007/BF01968504	en
heal.language	English	en
heal.publicationDate	1995	en
heal.abstract	For an aircraft flying in atmospheric disturbances a static state feedback controller is designed. The design goal is that of rejecting the influence of a rotary gust disturbance to the vertical and forward velocity of the aircraft. The necessary and sufficient condition for this problem to have a solution is derived in terms of simple forms involving only the flight stability derivatives of the aircraft. The general analytical expression of the disturbance rejection controller matrix and the resulting closed, loop system, are derived in forms involving the aircraft parameters as well as arbitrary design parameters. The necessary and sufficient conditions for disturbance rejection with simultaneous stabilizability of the closed loop flight system are also established. © 1995 Kluwer Academic Publishers.	en
heal.publisher	Kluwer Academic Publishers	en
heal.journalName	Dynamics and Control	en
dc.identifier.doi	10.1007/BF01968504	en
dc.identifier.isi	ISI:A1995RY52300004	en
dc.identifier.volume	5	en
dc.identifier.issue	4	en
dc.identifier.spage	389	en
dc.identifier.epage	400	en