A study of collision orbits with the moon by the method of surface of section

Details A study of collision orbits with the moon by the method of surface of section A study of collision orbits with the moon by the method of surface of section

Sep 1986

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1986em%26p...36...49g&link_type=abstract

Earth, Moon, and Planets (ISSN 0167-9295), vol. 36, Sept. 1986, p. 49-61.

Physics

Celestial Mechanics, Collision Parameters, Lunar Orbits, Natural Satellites, Orbit Calculation, Three Body Problem, Cartesian Coordinates, Equations Of Motion, Lunar Surface, Particle Trajectories

Scientific paper

The surface of section method is used to study the nonperiodic orbits of a lunar satellite. The plane circular restricted three-body problem, where q1 and q2 are the Cartesian coordinates of a particle with infinitesimal mass, is used as an example. It is concluded that the present surface of section method can be used to study orbits which collide with the moon's surface following a large number of revolutions.

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