Control and stabilization of a flexible beam attached to a rigid body
| dc.citation.epage | 31 | en_US |
| dc.citation.issueNumber | 1 | en_US |
| dc.citation.spage | 11 | en_US |
| dc.citation.volumeNumber | 51 | en_US |
| dc.contributor.author | Morgül, Ö. | en_US |
| dc.date.accessioned | 2016-02-08T10:56:29Z | en_US |
| dc.date.available | 2016-02-08T10:56:29Z | |
| dc.date.issued | 1990 | en_US |
| dc.department | Department of Electrical and Electronics Engineering | en_US |
| dc.description.abstract | We consider a flexible spacecraft modelled as a rigid body rotating in inertial space; a light flexible beam is clamped to the rigid body at one end and is free at the other. The equations of motion are obtained by using free-body diagrams. 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 the energy of the system as a Lyapunov functional. © 1990 Taylor and Francis Group, LLC. | en_US |
| dc.identifier.doi | 10.1080/00207179008934048 | en_US |
| dc.identifier.issn | 0020-7179 | |
| dc.identifier.uri | http://hdl.handle.net/11693/26209 | |
| dc.language.iso | English | en_US |
| dc.publisher | Taylor & Francis | en_US |
| dc.relation.isversionof | http://dx.doi.org/10.1080/00207179008934048 | en_US |
| dc.source.title | International Journal of Control | en_US |
| dc.title | Control and stabilization of a flexible beam attached to a rigid body | en_US |
| dc.type | Article | en_US |
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