Nonlinear decoupling control of a spacecraft

Tsirikos, AS; Mastorakis, NE

dc.contributor.author	Tsirikos, AS	en
dc.contributor.author	Mastorakis, NE	en
dc.date.accessioned	2014-03-01T01:48:41Z
dc.date.available	2014-03-01T01:48:41Z
dc.date.issued	1999	en
dc.identifier.uri	https://dspace.lib.ntua.gr/xmlui/handle/123456789/25549
dc.relation.uri	http://www.scopus.com/inward/record.url?eid=2-s2.0-19544364141&partnerID=40&md5=3980f1161e44d31c51bd7aef4587a8c6	en
dc.subject	Decoupling control problem	en
dc.subject	Nonlinear Systems	en
dc.subject	Partial differential equations	en
dc.subject.other	Closed loop control systems	en
dc.subject.other	Control systems	en
dc.subject.other	Eigenvalues and eigenfunctions	en
dc.subject.other	Gravitation	en
dc.subject.other	Mathematical models	en
dc.subject.other	Nonlinear systems	en
dc.subject.other	Problem solving	en
dc.subject.other	Trajectories	en
dc.subject.other	Control laws	en
dc.subject.other	Nonlinear decoupling	en
dc.subject.other	Yaw angles	en
dc.subject.other	Spacecraft	en
dc.title	Nonlinear decoupling control of a spacecraft	en
heal.type	journalArticle	en
heal.publicationDate	1999	en
heal.abstract	In this paper a new approach to the nonlinear decoupling control problem using static state feedback is applied to the model of a spacecraft. The general analytical expression for the control law, which leads to a decoupled closed-loop system, is derived. Moreover, it is proven that appropriate selection of the arbitrary parameters of the control law leads to a closed-loop system with linear input-output description and arbitrarily assignable eigenvalues.	en
heal.publisher	World Scientific and Engineering Academy and Society	en
heal.journalName	Advances in Intelligent Systems and Computer Science	en
dc.identifier.spage	388	en
dc.identifier.epage	399+xi	en