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机译:太阳地球系统L_2点附近从人造卫星地球轨道到晕轨道的转移轨迹的弹道设计
Keldysh Institute of Applied Mathematics of the Russian Academy of Sciences, Miusskaya pl. 4, Moscow, 125047 Russia;
Keldysh Institute of Applied Mathematics of the Russian Academy of Sciences, Miusskaya pl. 4, Moscow, 125047 Russia;
National Research University Higher School of Economics, Moscow, Russia;
Keldysh Institute of Applied Mathematics of the Russian Academy of Sciences, Miusskaya pl. 4, Moscow, 125047 Russia;
Keldysh Institute of Applied Mathematics of the Russian Academy of Sciences, Miusskaya pl. 4, Moscow, 125047 Russia;
Keldysh Institute of Applied Mathematics of the Russian Academy of Sciences, Miusskaya pl. 4, Moscow, 125047 Russia;
Keldysh Institute of Applied Mathematics of the Russian Academy of Sciences, Miusskaya pl. 4, Moscow, 125047 Russia;
Keldysh Institute of Applied Mathematics of the Russian Academy of Sciences, Miusskaya pl. 4, Moscow, 125047 Russia;
机译:光环轨道传输轨迹设计在太阳地球系统中使用不变歧管,辐射压力和尺寸
机译:日地系统L_2交联点附近的晕轮
机译:将轨道从月球转移到太阳地球晕轨道
机译:在日地循环问题中将轨迹从低地球轨道转移到以L_1为中心的大型I类晕轨道
机译:从地球到月球L2点光晕轨道的最佳低推力转移轨迹。
机译:晕针穿透继发眶顶骨折和眶蜂窝组织炎:病例报告
机译:从地球到晕轨道的转移过程中的轨迹和校正动作
机译:太阳地球L1区域Halo-To-Halo轨道和Halo-to-Lissajous轨道转移