Influence of the resonance in a gravity-gradient stabilized satellite

dc.contributorUniversidade Estadual Paulista (UNESP)
dc.creatorMoraes, R. Vilhena de
dc.creatorSilva, P. A. F. da
dc.date2014-05-27T06:09:36Z
dc.date2016-10-25T18:12:19Z
dc.date2014-05-27T06:09:36Z
dc.date2016-10-25T18:12:19Z
dc.date1989-09-01
dc.date.accessioned2017-04-06T00:41:44Z
dc.date.available2017-04-06T00:41:44Z
dc.identifierCelestial Mechanics and Dynamical Astronomy, v. 47, n. 3, p. 225-243, 1989.
dc.identifier0923-2958
dc.identifier1572-9478
dc.identifierhttp://hdl.handle.net/11449/63909
dc.identifierhttp://acervodigital.unesp.br/handle/11449/63909
dc.identifier10.1007/BF00053453
dc.identifierWOS:000207114300001
dc.identifier2-s2.0-34249958718
dc.identifierhttp://dx.doi.org/10.1007/BF00053453
dc.identifier.urihttp://repositorioslatinoamericanos.uchile.cl/handle/2250/885857
dc.descriptionUsing Hamiltonian formalism the translational-rotational motion of a satellite is studied near a resonance considering the orbital and rotational motions. A first order perturbation theory is derived by Hori's transformation in order to eliminate short and long periodic terms, preserving in the new Hamiltonian secular and resonant terms. This theory is again applied to study the resonant system whose analysis lead us to a system of equations equivalent to the equations of a simple pendulum which is integrable in terms of elliptical integrals. © 1990 Kluwer Academic Publishers.
dc.descriptionFundação de Amparo à Pesquisa do Estado de São Paulo (FAPESP)
dc.languageeng
dc.relationCelestial Mechanics and Dynamical Astronomy
dc.rightsinfo:eu-repo/semantics/closedAccess
dc.titleInfluence of the resonance in a gravity-gradient stabilized satellite
dc.typeOtro


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