Generation of Artificial Halo Orbits in Near-Moon Space Using Low-Thrust Engines

Author:

Du Chongrui ,Starinova O. L.

Publisher

Pleiades Publishing Ltd

Subject

Space and Planetary Science,Astronomy and Astrophysics,Aerospace Engineering

Reference35 articles.

1. Aksenov, S.A. and Bober, S.A., Upravlenie dvizheniem kosmicheskogo apparata na galo-orbite pri nalichii ogranichenii na napravleniya korrektiruyushchikh manevrov. Nekotorye aspekty sovremennykh problem mekhaniki i informatiki (Controlling the Spacecraft Motion in a Halo Orbit in the Presence of Restrictions on the Directions of Corrective Maneuvers. Some Aspects of Modern Problems of Mechanics and Informatics), Moscow: Inst. Kosm. Issled. Ross. Akad. Nauk, 2018.

2. Il’in, I.S., Sazonov, V.V., and Tuchin, A.G., Transfer trajectories from low-Earth orbit to the manifold of bounded orbits in the vicinity of the libration point L_2 of the Sun–Earth system, Preprint of Keldysh Inst. of Applied Mathematics, Russ. Acad. Sci., Moscow, 2012.

3. Shaykhutdinov, A.R. and Kostenko, V.I., Prospects for using the halo-orbit in the vicinity of the L2 libration point of the Sun–Earth system for the ground-space millimetron radio interferometer, Cosmic Res., 2020, vol., 58, no. 5, pp. 393–401.

4. Fain, M.K. and Starinova, O.L., Ballistic optimization of the L1–L2 and L2–L1 low thrust transfers in the Earth–Moon system, 7th Int. Conf. on Recent Advances in Space Technologies (RAST), IEEE, 2015.

5. Farquhar, R.W. and Kamel, A.A., Quasi-periodic orbits about the translunar libration point, Celestial Mech., 1973, vol. 7, no. 4, pp. 458–473.

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