Averaged parabolic restricted three-body problem

Details Averaged parabolic restricted three-body problem Averaged parabolic restricted three-body problem

Apr 1989

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1989azh....66..377m&link_type=abstract

Astronomicheskii Zhurnal (ISSN 0004-6299), vol. 66, Mar.-Apr. 1989, p. 377-384. In Russian.

Statistics

Computation

1

Orbit Perturbation, Parabolic Flight, Three Body Problem, Computational Astrophysics, Numerical Integration

Scientific paper

The plane, singly averaged parabolic restricted three-body problem is
considered. The expansion of the perturbing function is obtained in the
case when the first two terms are taken. Results of the numerical
integration of the exact and singly averaged equations are presented.
Element variations are considered for the case of Mars.

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