Analytical theory of a lunar artificial satellite with third body perturbations
-
Published:2006
Issue:
Volume:
Page:407-423
-
ISSN:
-
Container-title:Periodic, Quasi-Periodic and Chaotic Motions in Celestial Mechanics: Theory and Applications
-
language:
-
Short-container-title:
Author:
De Saedeleer Bernard
Publisher
Springer Netherlands
Reference23 articles.
1. Brouwer, D.: Solution of the problem of artificial satellite theory without air drag. Astron. J. 64, 378–397 (1959)
2. Chapront-Touzé, M., Chapront, J.: Lunar Tables and Programs 4000 BC to AD 8000. Willmann-Bell. (1991)
3. De Saedeleer, B., Henrard, J.: Orbit of a lunar artificial satellite: analytical theory of perturbations. IAU Colloq. 196: Transits of Venus: New Views of the Solar System and Galaxy. pp. 254–262 (2005)
4. De Saedeleer, B., Henrard, J.: The combined effect of J 2 and C 22 on the critical inclination of a lunar orbiter’. Adv. Space Res. 37(1): 80–87 (2006). The Moon and Near-Earth Objects. Also available as http://dx.doi.org/10.1016/j.asr.2005.06.052
5. De Saedeleer, B.: Analytical theory of an artificial satellite of the Moon. In: Belbruno, E., Gurfil, P. (eds.) Astrodynamics, Space Missions, and Chaos, of the Annals of the New York Academy of Sciences. Proceedings of the Conference New Trends in Astrodynamics and Applications, January 20–22, 2003, Vol. 1017, pp. 434–449. Washington (2004)