Low-Energy Sub-Optimal Low-Thrust Trajectories to Libration Points and Halo-Orbits-Reference-Cited by-同舟云学术

Low-Energy Sub-Optimal Low-Thrust Trajectories to Libration Points and Halo-Orbits

Published:2019-09 Issue:5 Volume:57 Page:378-388
ISSN:0010-9525
Container-title:Cosmic Research
language:en
Short-container-title:Cosmic Res

Author:

Ivanyukhin A. V.,Petukhov V. G.

Publisher

Pleiades Publishing Ltd

Subject

Space and Planetary Science,Astronomy and Astrophysics,Aerospace Engineering

Link

http://link.springer.com/content/pdf/10.1134/S0010952519050022.pdf

Reference35 articles.

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2. Egorov, V.A., Prostranstvennaya zadacha dostizheniya Luny (The Spatial Problem of Reaching the Moon), Moscow: Nauka, 1965.

3. Egorov, V.A. and Gusev, L.I., Dinamika pereletov mezhdu Zemlei i Lunoi (Dynamics of Flights between the Earth and the Moon), Moscow: Nauka, 1980.

4. Wu, W., Tang, Y., Zhang, L., and Qiao, D., Design of communication relay mission for supporting lunar-farside soft landing, Sci. China Inf. Sci., 2018, vol. 61, no. 4, id 040305.

5. McGuire, M.L., Burke, L.M., McCarty, S.L., et al., Low thrust cis-lunar transfers using a 40 kW-class solar electric propulsion spacecraft, AAS/AIAA Astrodynamics Specialist Conference, Washington, 2017, AAS 17-583.

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