dc.contributorInstituto Nacional de Pesquisas Espaciais (INPE)
dc.contributorUniversidade Federal do ABC (UFABC)
dc.contributorUniversidade Estadual Paulista (Unesp)
dc.date.accessioned2014-05-27T11:27:23Z
dc.date.accessioned2022-10-05T18:39:13Z
dc.date.available2014-05-27T11:27:23Z
dc.date.available2022-10-05T18:39:13Z
dc.date.created2014-05-27T11:27:23Z
dc.date.issued2012-12-01
dc.identifierProceedings of the International Astronautical Congress, IAC, v. 7, p. 5919-5924.
dc.identifier0074-1795
dc.identifierhttp://hdl.handle.net/11449/73985
dc.identifier2-s2.0-84883516636
dc.identifier0960024575647258
dc.identifier0000-0002-4901-3289
dc.identifier.urihttp://repositorioslatinoamericanos.uchile.cl/handle/2250/3922955
dc.description.abstractAn alternative transfer strategy to send spacecrafts to stable orbits around the Lagrangian equilibrium points L4 and L5 based in trajectories derived from the periodic orbits around LI is presented in this work. The trajectories derived, called Trajectories G, are described and studied in terms of the initial generation requirements and their energy variations relative to the Earth through the passage by the lunar sphere of influence. Missions for insertion of spacecrafts in elliptic orbits around L4 and L5 are analysed considering the Restricted Three-Body Problem Earth- Moon-particle and the results are discussed starting from the thrust, time of flight and energy variation relative to the Earth. Copyright© (2012) by the International Astronautical Federation.
dc.languageeng
dc.relationProceedings of the International Astronautical Congress, IAC
dc.relation0,116
dc.rightsAcesso aberto
dc.sourceScopus
dc.subjectEnergy variations
dc.subjectEquilibrium point
dc.subjectGeneration requirements
dc.subjectLagrangian points
dc.subjectPeriodic orbits
dc.subjectRestricted three-body problem
dc.subjectSphere of influences
dc.subjectTransfer strategies
dc.subjectLagrange multipliers
dc.subjectSpacecraft
dc.subjectTrajectories
dc.subjectMoon
dc.titleOptimal low-cost transfer to L4 and L5 lagrangian points based on G-family of periodic orbits
dc.typeTrabalho apresentado em evento


Este ítem pertenece a la siguiente institución