Artificial satellites dynamics: Resonant effects

dc.contributorUniversidade Estadual Paulista (Unesp)
dc.contributorUniversidade Federal de São Paulo (UNIFESP)
dc.contributorInstituto Tecnológico de Aeronáutica (ITA)
dc.date.accessioned2014-05-27T11:26:26Z
dc.date.accessioned2022-10-05T18:33:33Z
dc.date.available2014-05-27T11:26:26Z
dc.date.available2022-10-05T18:33:33Z
dc.date.created2014-05-27T11:26:26Z
dc.date.issued2012-04-01
dc.identifierJournal of Aerospace Engineering, Sciences and Applications, v. 4, n. 2, p. 1-14, 2012.
dc.identifier2236-577X
dc.identifierhttp://hdl.handle.net/11449/73264
dc.identifier10.7446/jaesa.0402.01
dc.identifier2-s2.0-84871066512
dc.identifier2-s2.0-84871066512.pdf
dc.identifier7740917144757410
dc.identifier0000-0003-1289-8332
dc.identifier.urihttp://repositorioslatinoamericanos.uchile.cl/handle/2250/3922276
dc.description.abstractIn this work, the resonance problem in the artificial satellites motion is studied. The development of the geopotential includes the zonal harmonics J20 and J40 and the tesseral harmonics J22 and J42. Through successive Mathieu transformations, the order of dynamical system is reduced and the final system is solved by numerical integration. In the simplified dynamical model, two critical angles are studied, 2201 and 4211. Numerical results show the time behavior of the semi-major axis and 2 angle.
dc.languageeng
dc.relationJournal of Aerospace Engineering, Sciences and Applications
dc.rightsAcesso aberto
dc.sourceScopus
dc.subjectArtificial Satellites
dc.subjectOrbits
dc.subjectResonance
dc.titleArtificial satellites dynamics: Resonant effects
dc.typeTrabalho apresentado em evento


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