Transfer Trajectories from the Moon to Sun–Earth Halo Orbits
2014; American Institute of Aeronautics and Astronautics; Volume: 37; Issue: 3 Linguagem: Inglês
10.2514/1.62059
ISSN1533-3884
AutoresMasaki Nakamiya, Yasuhiro Kawakatsu,
Tópico(s)Space Satellite Systems and Control
ResumoNo AccessEngineering NoteTransfer Trajectories from the Moon to Sun–Earth Halo OrbitsMasaki Nakamiya and Yasuhiro KawakatsuMasaki NakamiyaResearch Institute for Sustainable Humanosphere, Kyoto University, Kyoto 611-0011, Japan and Yasuhiro KawakatsuDepartment of Space Systems and Astronautics, Japan Aerospace Exploration Agency, Kanagawa 252-5210, JapanPublished Online:25 Apr 2014https://doi.org/10.2514/1.62059SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Breakwell J. V. and Brown J. V., "The 'Halo' Family of 3-Dimensional Periodic Orbits in the Earth–Moon' Restricted 3-Body Problem," Celestial Mechanics, Vol. 20, No. 4, Nov. 1979, pp. 389–404. doi:https://doi.org/10.1007/BF01230405 CLMCAV 0008-8714 CrossrefGoogle Scholar[2] Farquhar R. W., "The Control and Use of Libration-Point Satellites," NASA Tech. Rept. R-346, 1970. Google Scholar[3] Richardson D. 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