The Perturbing Effects on the Planetary Satellite
Abstract
The problem triaxial satellite having a plane of dynamical symmetry in the restricted problem of three bodies has been studied. The first integrals are established and the general solution of the problem can be written in quadratures. The results show that the semimajor axis of the satellite orbit and its rotational angular momentum remain unchanged. The singular solution of this problem has been considered and the elements of satellite orbit can be determined.
 Publication:

Earth Moon and Planets
 Pub Date:
 May 1991
 DOI:
 10.1007/BF00057427
 Bibcode:
 1991EM&P...53..117E
 Keywords:

 Natural Satellites;
 Orbit Perturbation;
 Planetary Orbits;
 Three Body Problem;
 Angular Momentum;
 Differential Equations;
 Equations Of Motion;
 Orbital Elements;
 Singularity (Mathematics);
 Astronomy