Please use this identifier to cite or link to this item: http://repositorio.unitau.br/jspui/handle/20.500.11874/2316
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dc.contributor.authorSoares, Álvaro Manoel de Souzapt_BR
dc.contributor.authorGóes, Luiz Carlos Sandovalpt_BR
dc.contributor.authorGrandinetti, Francisco Josépt_BR
dc.date.accessioned2019-09-12T16:33:11Z-
dc.date.available2019-09-12T16:33:11Z-
dc.date.issued2003-
dc.citation.volume2pt_BR
dc.citation.spage75-
dc.citation.epage84-
dc.identifier.urihttps://www.scopus.com/inward/record.uri?eid=2-s2.0-22344447283&partnerID=40&md5=ede8231da3b1f0112ca14bcea72df8ff-
dc.identifier.urihttp://repositorio.unitau.br/jspui/handle/20.500.11874/2316-
dc.descriptionIAC-03-I.P.01pt_BR
dc.description.abstractThe objective of this work is to describe the design and the implementation of an experiment to study the dynamics and the active control of a slewing multi-link flexible structure. The experimental apparatus was designed to be representative of a flexible space structure such as a satellite with multiple flexible appendages. In this study we describe the design procedures, the analog and digital instrumentation, the analytical modeling together with model validation studies carried out through experimental modal testing and parametric system identification studies in the frequency domain. Preliminary results of a simple positional control with collocated sensor and actuator is also described. Copyright © 2003 by the International Astronautical Federation. All rights reserved.en
dc.description.provenanceMade available in DSpace on 2019-09-12T16:33:11Z (GMT). No. of bitstreams: 0 Previous issue date: 2003en
dc.languageInglêspt_BR
dc.publisher.countryAlemanhapt_BR
dc.relation.ispartof54th International Astronautical Congress of the International Astronautical Federation (IAF), the International Academy of Astronautics and the International Institute of Space Law-
dc.relation.haspart54th International Astronautical Congress of the International Astronautical Federation (IAF), the International Academy of Astronautics and the International Institute of Space Law-
dc.rightsAcesso Restritopt_BR
dc.sourceScopuspt_BR
dc.subject.otherFlexible Structuresen
dc.subject.otherIdentificationen
dc.subject.otherIdentification and Control of Structuresen
dc.subject.otherModal Analysisen
dc.subject.otherDigital instrumentationen
dc.subject.otherElastic deformationen
dc.subject.otherIdentification and control of structuresen
dc.subject.otherNon-linear effectsen
dc.subject.otherDC motorsen
dc.subject.otherIdentification (control systems)en
dc.subject.otherInterfaces (computer)en
dc.subject.otherMathematical modelsen
dc.subject.otherModal analysisen
dc.subject.otherPiezoelectric devicesen
dc.subject.otherRobustness (control systems)en
dc.subject.otherSensorsen
dc.subject.otherPosition controlen
dc.titleModeling and position control of multibody system with flexible appendagesen
dc.typeTrabalho apresentado em eventopt_BR
dc.description.affiliationDe Souza Scares, A.M., Depto of Mechanical Engineering, University, of Taubaté, Campus da Juta, Rua Daniel Danelli, s/n, 12060-440 - Taubaté - SP, Brazil-
dc.description.affiliationGóes, L.C.S., Mechanical and Aeronautical Engineering Division, Technological Institute of Aeronautical-HA-CTA, IEMP, 12228-900, Sao Jose dos Campos, SP, Germany-
dc.description.affiliationGrandinetti, F.J., Depto of Mechanical Engineering, University, of Taubaté, Campus da Juta, Rua Daniel Danelli, s/n, 12060-440 - Taubaté - SP, Brazil-
dc.identifier.scopus2-s2.0-22344447283-
dc.contributor.scopus8635186100pt_BR
dc.contributor.scopus8613267100pt_BR
dc.contributor.scopus56278896000pt_BR
Appears in Collections:Trabalhos Apresentados em Eventos
Artigos de Periódicos

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