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Utilize este identificador para citar ou criar um link para este item: http://acervodigital.unesp.br/handle/11449/38887
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Campo DCValorIdioma
dc.contributor.authorRosado, VOG-
dc.contributor.authorNeto, A. R.-
dc.date.accessioned2014-05-20T15:29:16Z-
dc.date.accessioned2016-10-25T18:04:30Z-
dc.date.available2014-05-20T15:29:16Z-
dc.date.available2016-10-25T18:04:30Z-
dc.date.issued1992-11-01-
dc.identifierhttp://dx.doi.org/10.1016/0094-5765(92)90059-R-
dc.identifier.citationActa Astronautica. Oxford: Pergamon-Elsevier B.V., v. 26, n. 11, p. 773-777, 1992.-
dc.identifier.issn0094-5765-
dc.identifier.urihttp://hdl.handle.net/11449/38887-
dc.identifier.urihttp://acervodigital.unesp.br/handle/11449/38887-
dc.description.abstractA formulation used to determine the time-optimal geomagnetic attitude maneuvers subject to dynamic and geometric constraints is proposed in this paper. This was obtained by a direct search procedure based on a control function parametrization method, using linear programming to obtain numerical suboptimal solutions by linear perturbation. Due to its characteristics it can be used in small computers and to generate computer programs of general application. The dynamic modeling, the magnetic torque model and the suboptimal control procedure are presented. Simulation runs have verified the feasibility of the formulation thus derived and have shown a notable improvement in performance.en
dc.format.extent773-777-
dc.language.isoeng-
dc.publisherElsevier B.V.-
dc.sourceWeb of Science-
dc.titleTIME-OPTIMAL GEOMAGNETIC ATTITUDE MANEUVERS OF AN AXISYMMETRICAL SPINNING SATELLITEen
dc.typeoutro-
dc.contributor.institutionUniversidade Estadual Paulista (UNESP)-
dc.description.affiliationUNESP,DEPT MECANICA,CAMPUS GUARATINGUETA,CP 205,BR-12500 GUARATINGUETA,SP,BRAZIL-
dc.description.affiliationUnespUNESP,DEPT MECANICA,CAMPUS GUARATINGUETA,CP 205,BR-12500 GUARATINGUETA,SP,BRAZIL-
dc.identifier.doi10.1016/0094-5765(92)90059-R-
dc.identifier.wosWOS:A1992KD17400003-
dc.rights.accessRightsAcesso restrito-
dc.relation.ispartofActa Astronautica-
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