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dc.contributor.authorMorgül, Ö.en_US
dc.date.accessioned2016-02-08T10:56:09Z
dc.date.available2016-02-08T10:56:09Z
dc.date.issued1991en_US
dc.identifier.issn0020-7179
dc.identifier.urihttp://hdl.handle.net/11693/26182
dc.description.abstractA flexible spacecraft modelled as a rigid body which rotates in an inertial space is considered; a light flexible beam is clamped to the rigid body at one end and free at the other end. The equations of motion are obtained by using the geometrically exact beam model for the flexible beam, and it is then shown that under planar motion assumption, linearizationof this model yieldsthe Timoshenko beam model. It is shown that suitable boundary controls applied to the free end of the beam and a control torque applied to the rigid body stabilize the system. The proof is obtained by using a Lyapunov functional based on the energy of the system. © 1991 Taylor and Francis Ltd.en_US
dc.language.isoEnglishen_US
dc.source.titleInternational Journal of Controlen_US
dc.relation.isversionofhttp://dx.doi.org/10.1080/00207179108934185en_US
dc.subjectBeams And Girders--Controlen_US
dc.subjectControl Systems--Applicationsen_US
dc.subjectMathematical Techniques--Numerical Methodsen_US
dc.subjectBoundary Controlen_US
dc.subjectEquations of Motionen_US
dc.subjectInertial Space Rotationen_US
dc.subjectPlanar Motionen_US
dc.subjectRigid Bodiesen_US
dc.subjectTimoshenko Beamen_US
dc.subjectSpacecraften_US
dc.titleBoundary control of a Timoshenko beam attached to a rigid body: planar motionen_US
dc.typeArticleen_US
dc.departmentDepartment of Electrical and Electronics Engineering
dc.citation.spage763en_US
dc.citation.epage791en_US
dc.citation.volumeNumber54en_US
dc.citation.issueNumber4en_US
dc.identifier.doi10.1080/00207179108934185en_US
dc.publisherTaylor & Francisen_US


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