Evolution on orbital resonance in restricted 3-body problem

Details Evolution on orbital resonance in restricted 3-body problem Evolution on orbital resonance in restricted 3-body problem

May 1988

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1988sssmp..31..585l&link_type=abstract

Scientia Sinica, Series A - Mathematical, Physical, Astronomical and Technical Sciences (ISSN 0253-5831), vol. 31, May 1988, p.

Statistics

Computation

Asteroid Belts, Jupiter (Planet), Mars (Planet), Orbital Resonances (Celestial Mechanics), Planetary Orbits, Three Body Problem, Computational Astrophysics, Perturbation Theory, Solar System

Scientific paper

In order to understand the orbital resonant action on the dynamic
evolution, it is necessary to investigate the resonant characteristics
present over a long period of time. The variation in the characteristics
is numerically studied for three kinds of orbital resonances, namely,
p/q = 2/1, 3/2, 3/1, and some beneficial results have been obtained.

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