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Pitch and flight path control with simultaneous forward gust rejection

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dc.contributor.author Skarpetis, MG en
dc.contributor.author Koumboulis, FN en
dc.contributor.author Koussiouris, TG en
dc.date.accessioned 2014-03-01T01:48:42Z
dc.date.available 2014-03-01T01:48:42Z
dc.date.issued 1999 en
dc.identifier.uri https://dspace.lib.ntua.gr/xmlui/handle/123456789/25567
dc.relation.uri http://www.scopus.com/inward/record.url?eid=2-s2.0-4944247419&partnerID=40&md5=baefe7d665d3c1838c862fe845a3195b en
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.other Approximation theory en
dc.subject.other Control equipment en
dc.subject.other Feedback en
dc.subject.other Laplace transforms en
dc.subject.other Parameter estimation en
dc.subject.other Performance en
dc.subject.other Problem solving en
dc.subject.other Stability en
dc.subject.other Transfer functions en
dc.subject.other Vectors en
dc.subject.other Aerodynamic propulsion en
dc.subject.other Aircraft control en
dc.subject.other Disturbance decoupling en
dc.subject.other Input-output decoupling en
dc.subject.other Linear systems en
dc.title Pitch and flight path control with simultaneous forward gust rejection en
heal.type journalArticle en
heal.publicationDate 1999 en
heal.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
heal.publisher World Scientific and Engineering Academy and Society en
heal.journalName Computers and Computational Engineering in Control en
dc.identifier.spage 170 en
dc.identifier.epage 173 en


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