Influence of the resonance in a gravity-gradient stabilized satellite
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 |