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dc.contributor.authorCaetano, MAL-
dc.contributor.authorYoneyama, T.-
dc.date.accessioned2014-05-20T15:25:05Z-
dc.date.accessioned2016-10-25T17:59:27Z-
dc.date.available2014-05-20T15:25:05Z-
dc.date.available2016-10-25T17:59:27Z-
dc.date.issued1996-01-01-
dc.identifierhttp://dx.doi.org/10.2514/3.21613-
dc.identifier.citationJournal of Guidance Control and Dynamics. Reston: Amer Inst Aeronaut Astronaut, v. 19, n. 1, p. 262-264, 1996.-
dc.identifier.issn0731-5090-
dc.identifier.urihttp://hdl.handle.net/11449/35562-
dc.identifier.urihttp://acervodigital.unesp.br/handle/11449/35562-
dc.format.extent262-264-
dc.language.isoeng-
dc.publisherAmer Inst Aeronaut Astronaut-
dc.sourceWeb of Science-
dc.titleNew iterative method to solve optimal control problems with terminal constraintsen
dc.typeoutro-
dc.contributor.institutionInstituto Tecnológico de Aeronáutica (ITA)-
dc.contributor.institutionUniversidade Estadual Paulista (UNESP)-
dc.description.affiliationINST TECNOL AERONAUT,DEPT ELECTR ENGN,BR-12228900 S JOSE CAMPOS,BRAZIL-
dc.identifier.doi10.2514/3.21613-
dc.identifier.wosWOS:A1996TQ53100042-
dc.rights.accessRightsAcesso restrito-
dc.relation.ispartofJournal of Guidance Control and Dynamics-
Appears in Collections:Artigos, TCCs, Teses e Dissertações da Unesp

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