Computer Science
Scientific paper
Mar 1984
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1984cemec..32..217v&link_type=abstract
Celestial Mechanics (ISSN 0008-8714), vol. 32, March 1984, p. 217-230. NATO-supported research.
Computer Science
12
Eccentricity, Hill Method, Numerical Stability, Orbit Perturbation, Orbital Mechanics, Three Body Problem, Circular Orbits, Elliptical Orbits, Natural Satellites, Planets, Solar System, Sun, Tables (Data)
Scientific paper
Hill-type stability surfaces are computed for the general hierarchical three-body problem for non-zero eccentricities of the initial osculating orbits. Significant differences are found between them and the one obtained for initial zero eccentricities. Application is made to the triple subgroups of the Solar System; in particular it is found that no analytical guarantee of Hill-type stability can be given to any of the satellites against solar perturbations.
Carusi Andrea
Roy Archie E.
Valsecchi Giovanni B.
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