Low-Energy Lunar Trajectory Design: Parker/Low-Energy
Low-Energy Lunar Trajectory Design: Parker/Low-Energy
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DOI：
10.1002/9781118855065
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发表时间：
2014-06
期刊：
影响因子：
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通讯作者：
J. Parker;Rodney L. Anderson
中科院分区：
文献类型：
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作者：
J. Parker;Rodney L. Anderson
基于NASA喷气推进实验室多年的研究，低能月球轨道设计为使命管理者提供了高层次的信息，并为使命设计者提供了关于地球和月球之间低能传输的详细信息。这本书回答了关于在任何给定的月份和年份中这种传输的可用性和性能的高级问题。低能量月球转移与其他各种类型的转移进行了比较，并将其置于历史任务的背景下。使用这本书，设计者可以重建其中描述的任何转移，以及设计类似的转移与特定的设计参数。附录，“定位的拉格朗日点，”和一个有用的清单的条款和常数完成这一技术参考。调查可能用于在地球和月球之间转移航天器的数千种可能的轨道，包括转移到月球天平动轨道，低月球轨道和月球表面提供有关用于设计低能量月球转移的方法，模型和工具的信息，包括讨论这些转移从一个月到下一个月的变化，以及实施低能量月球转移的重要操作方面。另外，还讨论了导航、位置保持和航天器系统等问题
Based on years of research conducted at the NASA Jet Propulsion Laboratory, Low-Energy Lunar Trajectory Design provides high-level information to mission managers and detailed information to mission designers about low-energy transfers between Earth and the moon. The book answers high-level questions about the availability and performance of such transfers in any given month and year. Low-energy lunar transfers are compared with various other types of transfers, and placed within the context of historical missions. Using this book, designers may reconstruct any transfer described therein, as well as design similar transfers with particular design parameters. An Appendix,“Locating the Lagrange Points,” and a useful list of terms and constants completes this technical reference. Surveys thousands of possible trajectories that may be used to transfer spacecraft between Earth and the moon, including transfers to lunar libration orbits, low lunar orbits, and the lunar surface Provides information about the methods, models, and tools used to design low-energy lunar transfers Includes discussion about the variations of these transfers from one month to the next, and the important operational aspects of implementing a low-energy lunar transfer Additional discussions address navigation, station-keeping, and spacecraft systems issues