Secular perturbations of fictitious satellites of Uranus

Details Secular perturbations of fictitious satellites of Uranus Secular perturbations of fictitious satellites of Uranus

Sep 1991

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1991cemda..52..293k&link_type=abstract

Celestial Mechanics and Dynamical Astronomy (ISSN 0923-2958), vol. 52, no. 3, 1991, p. 293-303.

Statistics

Computation

13

Orbital Mechanics, Perturbation Theory, Secular Variations, Three Body Problem, Uranus Satellites, Computational Astrophysics, Hamiltonian Functions, Orbit Calculation

Scientific paper

Secular perturbations of fictitious satellites that are initially circular and in the equatorial plane of Uranus are discussed. Satellites located in the region where the solar perturbation is dominant become highly eccentric and inclined with respect to the equator, and have a possibility to collide with Uranus. Satellites located in the region where the oblateness perturbation is dominant keep the original eccentricity and the inclination. A scenario of a possible extinction of outer satellites of Uranus is also discussed.

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