Ballistic optimization of the L1-L2 and L2-L1 low thrust transfers in the Earth-Moon system

Author:

Fain Maxim K.,Starinova Olga L.

Publisher

IEEE

Cited by 8 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Generation of Artificial Halo Orbits in Near-Moon Space Using Low-Thrust Engines;Cosmic Research;2022-04

2. Optimal Control of Transfer to Vertical Orbits from Lyapunov Orbits Using Low-Thrust Engine;Mekhatronika, Avtomatizatsiya, Upravlenie;2022-03-06

3. Methods of accounting for the shadow zones influence on low thrust spacecraft moving in the Earth – Moon system;XLIII ACADEMIC SPACE CONFERENCE: dedicated to the memory of academician S.P. Korolev and other outstanding Russian scientists – Pioneers of space exploration;2019

4. Spacecraft trajectory optimization: A review of models, objectives, approaches and solutions;Progress in Aerospace Sciences;2018-10

5. Halo-orbit formation in the Earth-Moon system by the electric propulsion spacecraft;AIP Conference Proceedings;2018

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