Influence of the resonance in a gravity-gradient stabilized satellite


Autoria(s): Moraes, R. Vilhena de; Silva, P. A. F. da
Contribuinte(s)

Universidade Estadual Paulista (UNESP)

Data(s)

27/05/2014

27/05/2014

01/09/1989

Resumo

Fundação de Amparo à Pesquisa do Estado de São Paulo (FAPESP)

Processo FAPESP: 85/2699-0

Using 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.

Formato

225-243

Identificador

http://dx.doi.org/10.1007/BF00053453

Celestial Mechanics and Dynamical Astronomy, v. 47, n. 3, p. 225-243, 1989.

0923-2958

1572-9478

http://hdl.handle.net/11449/63909

10.1007/BF00053453

WOS:000207114300001

2-s2.0-34249958718

Idioma(s)

eng

Relação

Celestial Mechanics and Dynamical Astronomy

Direitos

closedAccess

Tipo

info:eu-repo/semantics/article