A semi-analytical approach to study resonances effects on the orbital motion of artificial satellites

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MetadadosDescriçãoIdioma
Autor(es): dc.contributorUniversidade Federal de São Paulo (UNIFESP)-
Autor(es): dc.contributorUniversidade Estadual Paulista (UNESP)-
Autor(es): dc.contributorIEF-
Autor(es): dc.contributorFATEC-
Autor(es): dc.creatorVilhena De Moraes, R.-
Autor(es): dc.creatorSampaio, J. C. [UNESP]-
Autor(es): dc.creatorDa Silva Fernandes, S.-
Autor(es): dc.creatorFormiga, J. K.-
Data de aceite: dc.date.accessioned2022-08-04T22:03:57Z-
Data de disponibilização: dc.date.available2022-08-04T22:03:57Z-
Data de envio: dc.date.issued2022-04-28-
Data de envio: dc.date.issued2022-04-28-
Data de envio: dc.date.issued2013-01-01-
Fonte completa do material: dc.identifierhttp://hdl.handle.net/11449/220132-
Fonte: dc.identifier.urihttp://educapes.capes.gov.br/handle/11449/220132-
Descrição: dc.descriptionA semi-analytical approach is proposed to study resonances effects on the orbital motion of artificial satellites or space debris orbiting the Earth. Applying successive Mathieu transformations, the order of dynamical system is reduced and the final system is solved by numerical integration. In the simplified dynamical model, we can choose the resonance to be considered as critical angle. Simulations are presented showing the variations of the orbital elements of bodies orbiting in the neighbourhood of the 2:1, 14:1 and 15:1 resonance condition. The half-width of the separatrix is calculated through a linearized model which describes the behavior of the dynamical system in a neighborhood of each critical angle. A semi-analytical approach is proposed to study resonances effects on the orbital motion of artificial satellites or space debris orbiting the Earth. Applying successive Mathieu transformations, the order of dynamical system is reduced and the final system is solved by numerical integration. In the simplified dynamical model, we can choose the resonance to be considered as critical angle. Simulations are presented showing the variations of the orbital elements of bodies orbiting in the neighbourhood of the 2:1, 14:1 and 15:1 resonance condition. The half-width of the separatrix is calculated through a linearized model which describes the behavior of the dynamical system in a neighborhood of each critical angle. © 2013 2013 California Institute of Technology.-
Descrição: dc.descriptionICT, UNIFESP-
Descrição: dc.descriptionDMA, UNESP-
Descrição: dc.descriptionIEF-
Descrição: dc.descriptionFATEC-
Descrição: dc.descriptionDMA, UNESP-
Formato: dc.format2773-2786-
Idioma: dc.languageen-
Relação: dc.relationAdvances in the Astronautical Sciences-
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Título: dc.titleA semi-analytical approach to study resonances effects on the orbital motion of artificial satellites-
Aparece nas coleções:Repositório Institucional - Unesp

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