Mathematics
Scientific paper
Oct 1982
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1982cemec..28..189s&link_type=abstract
(Conference on Mathematical Methods in Celestial Mechanics, 7th, Oberwolfach, West Germany, Aug. 24-28, 1981.) Celestial Mechani
Mathematics
3
Asteroids, Eccentric Orbits, Numerical Integration, Orbit Perturbation, Orbital Mechanics, Four Body Problem, Inclination, Secular Variations, Three Body Problem
Scientific paper
Because it is based on simplified differential equations, the theory of secular perturbations of an asteroid, in which proper inclination and proper eccentricity are constants of integration, are not applicable to Hilda-type motion. Such motion is a case of 3/2 resonance with respect to Jupiter, and numerical integration is necessary for an analogous study of the eccentric Hilda-type orbits. The procedure in which actual conditions are approximated by stepwise progression from a simplified model to the rigorous sun Jupiter-Saturn-asteroid problem leads to a way of determining proper Hilda inclinations. Long term integrations show no variations of these characteristic values.
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