摘要: This paper presents a study of transfers between distant retrograde orbits (DROs) and L2 halo orbits in the Earth-Moon system that could be flown by a spacecraft with solar electric propulsion (SEP). Two collocation-based optimal ... 展开
作者 | Parrish, N. L. Parker, J. S. Hughes, S. P. Heiligers, J. | ||
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原报告号 | N160003314 | 总页数 | 9 |
主办者 | National Aeronautics and Space Administration | ||
报告分类号 | [ 84A - Astronautics, 84D - Spacecraft Trajectories &, Flight Mechanics] | ||
报告类别/文献类型 | DE / NTIS科技报告 | ||
关键词 | Low thrust Retrograde orbits Earth-moon system Solar electric propulsion Trajectories Transfer orbits Collocation Astrodynamics Earth-moon trajectories |