Formation Dynamics under a Class of Control Laws

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dc.contributor.advisorKrishnaprasad, Perinkulam S.en_US
dc.contributor.authorZhang, Fuminen_US
dc.contributor.authorKrishnaprasad, Perinkulam S.en_US
dc.contributor.departmentISRen_US
dc.contributor.departmentCDCSSen_US
dc.date.accessioned2007-05-23T10:13:23Z
dc.date.available2007-05-23T10:13:23Z
dc.date.issued2002en_US
dc.description.abstractA system of two earth satellites is analyzed as a controlled mechanical system. The orbit of an earth satellite can be represented by a point inthe vector space of ordered pairs of angular momentum and Laplace vectors. Control laws are obtained by introducing a Lyapunov function on this space. Formations of two satellites are achieved asymptotically by the controlled dynamics.en_US
dc.format.extent158640 bytes
dc.format.mimetypeapplication/pdf
dc.identifier.urihttp://hdl.handle.net/1903/6339
dc.language.isoen_USen_US
dc.relation.ispartofseriesISR; TR 2002-25en_US
dc.relation.ispartofseriesCDCSS; TR 2002-4en_US
dc.subjectGlobal Communication Systemsen_US
dc.titleFormation Dynamics under a Class of Control Lawsen_US
dc.typeTechnical Reporten_US

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