Distant satellite orbits in the restricted circular three-body problem

Details Distant satellite orbits in the restricted circular three-body problem Distant satellite orbits in the restricted circular three-body problem

Nov 1988

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1988kosis..26..813k&link_type=abstract

Kosmicheskie Issledovaniia (ISSN 0023-4206), vol. 26, Nov.-Dec. 1988, p. 813-818. In Russian.

Physics

1

Hill Method, Orbital Mechanics, Satellite Orbits, Three Body Problem, Celestial Mechanics, Gravitational Effects, Integral Equations, Orbit Perturbation

Scientific paper

Satellite orbits in the vicinity of a smaller gravitating body are examined that are removed from this body by a distance significantly greater than the Hill-sphere radius. A description of such orbits and their long-period evolution is given, and their stability condition is investigated. The analytical results are shown to agree well with results of the numerical integration of the three-body-problem equations.

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