Study of a Moon's artificial satellite dynamics valid for all eccentricities and inclinations

Details Study of a Moon's artificial satellite dynamics valid for all eccentricities and inclinations Study of a Moon's artificial satellite dynamics valid for all eccentricities and inclinations

Oct 1993

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1993cemda..57..245s&link_type=abstract

Celestial Mechanics and Dynamical Astronomy (ISSN 0923-2958), vol. 57, no. 1-2, p. 245-246

Astronomy and Astrophysics

Astronomy

Gravitational Effects, Lunar Orbits, Lunar Satellites, Orbit Perturbation, Orbital Elements, Satellite Orbits, Spacecraft Trajectories, Trajectory Analysis, Eccentricity, Geomagnetism, Inclination, Lunar Gravitation, Solar Gravitation

Scientific paper

This work deals with the study of trajectories of artificial satellites
around the Moon to the end of missions. It means to study all the
trajectories of lunar satellites below 10,000 km, only considering for
now actions that derive from a gravitational potential.

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