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New iterative method to solve optimal control problems with terminal constraints

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dc.contributor.authorCaetano, MAL
dc.contributor.authorYoneyama, T.
dc.contributor.institutionInstituto Tecnológico de Aeronáutica (ITA)
dc.contributor.institutionUniversidade Estadual Paulista (Unesp)
dc.date.accessioned2014-05-20T15:25:05Z
dc.date.available2014-05-20T15:25:05Z
dc.date.issued1996-01-01
dc.description.affiliationINST TECNOL AERONAUT,DEPT ELECTR ENGN,BR-12228900 S JOSE CAMPOS,BRAZIL
dc.format.extent262-264
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.doi10.2514/3.21613
dc.identifier.issn0731-5090
dc.identifier.urihttp://hdl.handle.net/11449/35562
dc.identifier.wosWOS:A1996TQ53100042
dc.language.isoeng
dc.publisherAmer Inst Aeronaut Astronaut
dc.relation.ispartofJournal of Guidance Control and Dynamics
dc.relation.ispartofjcr2.024
dc.relation.ispartofsjr1,104
dc.rights.accessRightsAcesso restrito
dc.sourceWeb of Science
dc.titleNew iterative method to solve optimal control problems with terminal constraintsen
dc.typeArtigo
dcterms.licensehttp://arc.aiaa.org/page/authorrights
dcterms.rightsHolderAmer Inst Aeronaut Astronaut
dspace.entity.typePublication
unesp.author.orcid0000-0001-5375-1076[2]

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