Robust manoeuvres for the lateral motion of an aircraft

Skarpetis, MG; Koumboulis, FN

dc.contributor.author	Skarpetis, MG	en
dc.contributor.author	Koumboulis, FN	en
dc.date.accessioned	2014-03-01T02:48:27Z
dc.date.available	2014-03-01T02:48:27Z
dc.date.issued	1996	en
dc.identifier.issn	05379989	en
dc.identifier.uri	https://dspace.lib.ntua.gr/xmlui/handle/123456789/33811
dc.relation.uri	http://www.scopus.com/inward/record.url?eid=2-s2.0-0030392432&partnerID=40&md5=21fa88735f9b845b405f3d9e60e10c20	en
dc.subject.other	Aerospace engineering	en
dc.subject.other	Aircraft models	en
dc.subject.other	Closed loop control systems	en
dc.subject.other	Feedback control	en
dc.subject.other	Flight dynamics	en
dc.subject.other	Linear control systems	en
dc.subject.other	Maneuverability	en
dc.subject.other	Multivariable control systems	en
dc.subject.other	Robustness (control systems)	en
dc.subject.other	System stability	en
dc.subject.other	Aerospace	en
dc.subject.other	Lateral motion	en
dc.subject.other	Robust input output decoupling technique	en
dc.subject.other	Aircraft	en
dc.title	Robust manoeuvres for the lateral motion of an aircraft	en
heal.type	conferenceItem	en
heal.publicationDate	1996	en
heal.abstract	A Robust controller, facilitating yaw aircraft manoeuvres without affecting the respective roll modes, is designed for the case of uncertain air density, aircraft's mass and inertia. To handle the issue the robust input output decoupling technique is applied to the lateral motion dynamics of the aircraft. The condition under which the problem is solvable via state feedback appears to be generically true. The general form of the robust static decoupling controllers, as well as the general form of the resulting decoupled closed loop system, are derived. The conditions for robust decoupling with simultaneous robust stability are also established in terms of the lateral stability derivatives.	en
heal.publisher	IEE, Stevenage, United Kingdom	en
heal.journalName	IEE Conference Publication	en
dc.identifier.issue	427 /1	en
dc.identifier.spage	638	en
dc.identifier.epage	643	en