A general timing condition for consecutive collision orbits in the limiting case � = 0 of the elliptic restricted problem-Reference-Cited by-同舟云学术

A general timing condition for consecutive collision orbits in the limiting case � = 0 of the elliptic restricted problem

Published:1991 Issue:2 Volume:52 Page:167-194
ISSN:0923-2958
Container-title:Celestial Mechanics and Dynamical Astronomy
language:en
Short-container-title:Celestial Mech Dyn Astr

Author:

Howell K. C.,Marsh S. M.

Publisher

Springer Science and Business Media LLC

Subject

Space and Planetary Science,Astronomy and Astrophysics,Applied Mathematics,Computational Mathematics,Mathematical Physics,Modeling and Simulation

Link

http://link.springer.com/content/pdf/10.1007/BF00049448.pdf

Reference15 articles.

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2. Bruno, A.D.: 1981, ?On periodic flybys of the Moon?. Celest. Mech. 24, 255?268.

3. Egorov, V.A.: 1957, ?Certain problems of Moon flight dynamics. Dokl. Akad. Nauk SSSR(N.S.) 113, 46?49.

4. G�mez, G. and Oll�, M.: 1986, ?A note on the elliptic restricted three-body problem?. Celest. Mech. 39,33?55.

5. Guillaume, P.: 1969, ?Families of Symmetric Periodic Orbits of the Restricted Three-Body Problem, when the Perturbing Mass is Small?, Astron. Astrophys. 3, 57?76.

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