Mapping stable direct and retrograde orbits around the triple system of asteroids (45) Eugenia

dc.contributor.authorAraujo, R. A.N. [UNESP]
dc.contributor.authorMoraes, R. V.
dc.contributor.authorPrado, A. F.B.A.
dc.contributor.authorWinter, O. C. [UNESP]
dc.contributor.institutionNational Institute for Space Research (INPE)
dc.contributor.institutionUniversidade Federal de São Paulo (UNIFESP)
dc.contributor.institutionUniversidade Estadual Paulista (Unesp)
dc.date.accessioned2018-12-11T17:34:24Z
dc.date.available2018-12-11T17:34:24Z
dc.date.issued2017-12-01
dc.description.abstractIt is widely accepted that knowing the composition and the orbital evolution of asteroids might help us to understand the process of formation of the Solar system. It is also known that asteroids can represent a threat to our planet. Such an important role has made space missions to asteroids a very popular topic in current astrodynamics and astronomy studies. Taking into account the increasing interest in space missions to asteroids, especially to multiple systems, we present a study that aims to characterize the stable and unstable regions around the triple system of asteroids (45) Eugenia. The goal is to characterize the unstable and stable regions of this system and to make a comparison with the system 2001 SN263, which is the target of the Advanced Spaceborne Thermal Emission and Reflection Radiometer (ASTER) mission. A new concept was used for mapping orbits, by considering the disturbance received by the spacecraft from all perturbing forces individually. This method has also been applied to (45) Eugenia. We present the stable and unstable regions for particles with relative inclination between 0° and 180°. We found that (45) Eugenia presents larger stable regions for both prograde and retrograde cases. This is mainly because the satellites of this system are small when compared to the primary body, and because they are not close to each other. We also present a comparison between these two triple systems, and we discuss how these results can guide us in the planning of future missions.en
dc.description.affiliationNational Institute for Space Research (INPE)
dc.description.affiliationInstituto de Ciência e Tecnologia (ICT) Federal University de São Paulo (UNIFESP)
dc.description.affiliationUniversidade Estadual Paulista (UNESP) Grupo de Dinâmica Orbital e Planetologia
dc.description.affiliationUnespUniversidade Estadual Paulista (UNESP) Grupo de Dinâmica Orbital e Planetologia
dc.description.sponsorshipConselho Nacional de Desenvolvimento Científico e Tecnológico (CNPq)
dc.description.sponsorshipIdCNPq: 150378/2015-7
dc.format.extent3999-4006
dc.identifierhttp://dx.doi.org/10.1093/mnras/stx2230
dc.identifier.citationMonthly Notices of the Royal Astronomical Society, v. 472, n. 4, p. 3999-4006, 2017.
dc.identifier.doi10.1093/mnras/stx2230
dc.identifier.file2-s2.0-85030667441.pdf
dc.identifier.issn1365-2966
dc.identifier.issn0035-8711
dc.identifier.scopus2-s2.0-85030667441
dc.identifier.urihttp://hdl.handle.net/11449/179256
dc.language.isoeng
dc.relation.ispartofMonthly Notices of the Royal Astronomical Society
dc.relation.ispartofsjr2,346
dc.relation.ispartofsjr2,346
dc.rights.accessRightsAcesso aberto
dc.sourceScopus
dc.subjectCelestial mechanics
dc.subjectMethods: numerical
dc.subjectMinor planets, asteroids: individual: (45) Eugenia
dc.subjectPlanets and satellites: dynamical evolution and stability
dc.titleMapping stable direct and retrograde orbits around the triple system of asteroids (45) Eugeniaen
dc.typeArtigo
unesp.departmentMatemática - FEGpt

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