dc.contributorINPE: Instituto Nacional de Pesquisas Espaciais
dc.contributorUniversidade Estadual Paulista (Unesp)
dc.date.accessioned2019-10-06T15:23:14Z
dc.date.accessioned2022-12-19T18:26:02Z
dc.date.available2019-10-06T15:23:14Z
dc.date.available2022-12-19T18:26:02Z
dc.date.created2019-10-06T15:23:14Z
dc.date.issued2019-01-30
dc.identifierNonlinear Dynamics, v. 95, n. 2, p. 919-942, 2019.
dc.identifier1573-269X
dc.identifier0924-090X
dc.identifierhttp://hdl.handle.net/11449/187026
dc.identifier10.1007/s11071-018-4605-3
dc.identifier2-s2.0-85055951018
dc.identifier.urihttps://repositorioslatinoamericanos.uchile.cl/handle/2250/5368064
dc.description.abstractIn this work, the artificial equilibrium points for a general two-body system are derived, visualized, and summarized as functions of the direction of the thrust, for several directions. The results for the Sun-Earth system are also presented. Planar solar sail applications are also considered.
dc.languageeng
dc.relationNonlinear Dynamics
dc.rightsAcesso aberto
dc.sourceScopus
dc.subjectArtificial equilibrium point
dc.subjectAstrodynamics
dc.subjectNonlinear systems
dc.subjectRestricted three-body problem
dc.subjectSolar sail
dc.titleDetermination of thrusts to generate artificial equilibrium points in binary systems with applications to a planar solar sail
dc.typeArtículos de revistas


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