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机译:由部署在地球Halo轨道中的CubeSat系统启用了旧的远程定位
Chinese Acad Sci Technol & Engn Ctr Space Utilizat Key Lab Space Utilizat 9 Dengzhuang S Rd Beijing 100094 Peoples R China|Univ PSL CNRS Observ Paris IMCCE 77 Av Denfert Rochereau F-75014 Paris France;
Chinese Acad Sci Technol & Engn Ctr Space Utilizat Key Lab Space Utilizat 9 Dengzhuang S Rd Beijing 100094 Peoples R China|Univ Chinese Acad Sci 9 Dengzhuang S Rd Beijing 100094 Peoples R China;
Chinese Acad Sci Technol & Engn Ctr Space Utilizat Key Lab Space Utilizat 9 Dengzhuang S Rd Beijing 100094 Peoples R China|Univ Chinese Acad Sci 9 Dengzhuang S Rd Beijing 100094 Peoples R China;
Chinese Acad Sci Technol & Engn Ctr Space Utilizat Key Lab Space Utilizat 9 Dengzhuang S Rd Beijing 100094 Peoples R China|Univ Chinese Acad Sci 9 Dengzhuang S Rd Beijing 100094 Peoples R China;
Chinese Acad Sci Technol & Engn Ctr Space Utilizat Key Lab Space Utilizat 9 Dengzhuang S Rd Beijing 100094 Peoples R China|Univ Chinese Acad Sci 9 Dengzhuang S Rd Beijing 100094 Peoples R China;
Chinese Acad Sci Technol & Engn Ctr Space Utilizat Key Lab Space Utilizat 9 Dengzhuang S Rd Beijing 100094 Peoples R China;
Lunar far side; Positioning constellations; Lunar CubeSats; Trajectory optimization; Inter-sat tracking;
机译:通过部署在月球晕圈中的CubeSat系统实现的月球远端定位
机译:从月球远端到地球月球L_2晕轨道的上升轨迹
机译:使用L1和L2平面Lyapunov轨道的垂直不稳定性用于从近直线卤素轨道转移到地球系统中的平面遥远的逆行轨道
机译:在月球L2南部近直线光晕和蝴蝶轨道上演的人类着陆系统上实现全球登月访问
机译:月球系统内近直线晕轨道的特性和设计策略
机译:月球轨道激光测高仪探测月潮
机译:HALO轨道动态和月球全球定位系统设计的性能