Astronomy and Astrophysics – Astronomy
Scientific paper
Aug 1976
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1976aaas.conf.....u&link_type=abstract
American Institute of Aeronautics and Astronautics and American Astronautical Society, Astrodynamics Conference, San Diego, Cali
Astronomy and Astrophysics
Astronomy
1
Gravitational Effects, Lunar Orbits, Orbital Mechanics, Polar Orbits, Spacecraft Stability, Three Body Problem, Astrodynamics, Lunar Orbiter, Numerical Integration, Perturbation Theory, Satellite Perturbation, Zonal Harmonics
Scientific paper
A class of highly inclined lunar orbits is discussed for which earth perturbations have significant influence on the orbit evolution and the usefulness of the orbit for scientific exploration. The theory of the long-term motion of particles under third-body and zonal harmonic perturbations is taken as a starting point for investigations of orbits with relatively long lifetimes and evolutionary patterns that enhance the effectiveness of the satellite as a lunar farside relay. An equilibrium solution in the doubly-averaged three-body problem with oblateness is identified and the results of some numerical integrations are presented.
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