Ballistic optimization of the L1-L2 and L2-L1 low thrust transfers in the Earth-Moon system
Author:
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/7169399/7208298/07208322.pdf?arnumber=7208322
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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