Perturbed motion of the artificial satellite of the Moon in the project «UkrSelena»

1Aleksandrov, Yu.V
1V.N. Karazin National University of Kharkiv, Kharkiv, Ukraine
Kosm. nauka tehnol. 2009, 15 ;(1):05-08
https://doi.org/10.15407/knit2009.01.005
Publication Language: Russian
Abstract: 
We analyse the stability of the orbit of the artificial lunar satellite proposed in the «Ukrselena» project with respect to perturbing action of the Earth and the Sun. Some recommendations are made concerning the selection of the node longitude and time moment of the vehicle injection into the orbit relative to the mutual location of the Earth and the Moon.
Keywords: Moon, orbit stability, perturbing action
References: 
1. Aleksandrov Iu. V. Celestial Mechanics, 227 p. (KhNU, Kharkov, 2007) [in Russian].
2. Lidov M. L. Evolution of Orbits of Artificial Satellites of Planets under the Action of Gravitational Perturbations from External Bodies. Iskusstvennye Sputniki Zemli, Is. 8, 5—45 (1961) [in Russian].
3. Shkuratov Yu. G., Bondarenko N. V., Kachanov A. S. Objectives for a lunar polar sracecraft after the «Clementine» mission.
Kosm. nauka tehnol., 4 (1), 46—53 (1998) [in Russian].
https://doi.org/10.15407/knit1998.01.046
4. Shkuratov Yu. G., Lytvynenko L. N., Shulga V. M., et. al. Objectives of a Ukranian orbiter mission to the Moon. Adv. Space Res., 31 (11), 2341—2345 (2003).
https://doi.org/10.1016/S0273-1177(03)00534-9