Artigo
Influence of the resonance in a gravity-gradient stabilized satellite
Fecha
1989-09-01Registro en:
Celestial Mechanics and Dynamical Astronomy, v. 47, n. 3, p. 225-243, 1989.
0923-2958
1572-9478
10.1007/BF00053453
WOS:000207114300001
2-s2.0-34249958718
Autor
Instituto Tecnológico de Aeronáutica
Universidade Estadual Paulista (Unesp)
Resumen
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.