Tension force in nanosatellite tethers systems

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dc.contributor.authorMoia, Guilherme Parreira [UNESP]
dc.contributor.authorSantos, Denilson P. S. [UNESP]
dc.contributor.authorFormiga, Jorge K. S. [UNESP]
dc.contributor.institutionUniversidade Estadual Paulista (Unesp)
dc.date.accessioned2020-04-30T14:28:52Z
dc.date.available2020-04-30T14:28:52Z
dc.date.issued2019-11
dc.description.abstractThe use of innovative technologies in space missions has evolved considerably in the last decade. The use of large cables in space structures to connect spacecrafts and satellites with the goal to minimize cost of missions created a new field to be explored. A brief explanation will be considered about papers related to the equilibrium and stability of the movement of space systems connected by cables, known as Tether Systems. It will be presented the mathematical formulation for the system formed by two point masses connected by a tether in the central force field, in a Keplerian movement. The Lagrangian formulation was used to describe the rotational movement of the dumbbell-like system. Results of system behavior, tension and kinetic energy will be presented for two different situations, considering equal masses and different masses.en
dc.description.affiliationSão Paulo State University (Unesp), São João da Boa Vista
dc.description.sponsorshipFundação de Amparo à Pesquisa do Estado de São Paulo (FAPESP)
dc.description.sponsorshipPró-Reitoria de Pesquisa (PROPe UNESP)
dc.description.sponsorshipIdFAPESP: 2018/18811-9
dc.description.sponsorshipIdFAPESP: 2017/04643-4
dc.description.sponsorshipIdFAPESP: 2016/15675-1
dc.description.sponsorshipIdPROPe UNESP: 46421
dc.description.versionVersão final do editorpt
dc.identifier.citationJ. Phys.: Conf. Ser., v. 1365, 2019.
dc.identifier.doi10.1088/1742-6596/1365/1/012010
dc.identifier.issn1742-6596
dc.identifier.lattes4619733986441108
dc.identifier.lattes5351862393409206
dc.identifier.lattes3638759062433933
dc.identifier.orcid0000-0003-2682-4043
dc.identifier.orcid0000-0002-0004-7496
dc.identifier.urihttp://hdl.handle.net/11449/192410
dc.language.isoeng
dc.publisherIOP Publishing
dc.relationhttp://hdl.handle.net/11449/194400
dc.relation.ispartofJournal of physics: conference seriespt
dc.rights.accessRightsAcesso aberto
dc.subjectAstrodinâmicapt
dc.subjectSatélites artificiaispt
dc.subjectSistemas espaciaispt
dc.titleTension force in nanosatellite tethers systemsen
dc.typeArtigo
unesp.campusUniversidade Estadual Paulista (Unesp), Faculdade de Engenharia, São João da Boa Vistapt

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Artigos - Engenharia Aeronáutica - São João da Boa Vista