Orbital maneuvers for asteroids using genetic algorithm

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dc.contributor.authorNeves, Guilherme Marcos [UNESP]
dc.contributor.authorSantos, Denilson P. S. [UNESP]
dc.contributor.authorDomingos, Rita de C. [UNESP]
dc.contributor.authorFormiga, Jorge K. S. [UNESP]
dc.contributor.institutionUniversidade Estadual Paulista (Unesp)
dc.date.accessioned2020-11-25T12:11:58Z
dc.date.available2020-11-25T12:11:58Z
dc.date.issued2019-10-01
dc.description.abstractNear Earth objects (NEOs) are comets and asteroids that orbit the vicinity of the Earth. The scientific interest in comets and asteroids is due in large part to their status as remnants remaining relatively unchanged from the process of forming the solar system some 4.6 billion years ago, and some asteroids are made of precious metals such as platinum. Genetic algorithms are a particular class of evolutionary algorithms that use techniques inspired by evolutionary biology such as heredity, mutation, natural selection, and recombination. They can also be defined as global optimization algorithms and model a solution to a specific problem. This method provides a way to find solutions to problems that would be unlikely to be analytically feasible. The present work aims to use this method to optimize the consumption of fuel in Rendezvous maneuvers in interplanetary missions in a context where one wishes to send a probe to an asteroid to study it.pt
dc.description.affiliationUniversidade Estadual Paulista (Unesp), Câmpus Experimental de São João da Boa Vista
dc.description.affiliationUniversidade Estadual Paulista (Unesp), Instituto de Ciência e Tecnologia, São José dos Campos
dc.description.sponsorshipFundação de Amparo à Pesquisa do Estado de São Paulo (FAPESP)
dc.description.sponsorshipIdFAPESP: 2018/18811-9
dc.description.sponsorshipIdFAPESP: 2017/04643-4
dc.description.sponsorshipIdFAPESP: 2016/15675-1
dc.description.versionVersão final do editorpt
dc.identifier.citationJ. Phys.: Conf. Ser., v. 1365, 2019.
dc.identifier.doi10.1088/1742-6596/1365/1/012019
dc.identifier.issn1742-6596
dc.identifier.lattes3269469964323365
dc.identifier.lattes5351862393409206
dc.identifier.lattes6652169083464327
dc.identifier.lattes3638759062433933
dc.identifier.orcid0000-0003-2682-4043
dc.identifier.orcid0000-0002-0516-0420
dc.identifier.orcid0000-0002-0004-7496
dc.identifier.urihttp://hdl.handle.net/11449/194400
dc.language.isoeng
dc.publisherIOP Publishing
dc.relationhttp://hdl.handle.net/11449/192410
dc.relationhttp://hdl.handle.net/11449/235737
dc.relation.ispartofJournal of physics: conference seriespt
dc.rights.accessRightsAcesso aberto
dc.subjectAlgoritmos genéticospt
dc.subjectAsteróides Órbitaspt
dc.subjectAstrodinâmicapt
dc.titleOrbital maneuvers for asteroids using genetic algorithmpt
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