Dynamics and Mission Design Near Libration Points
Dynamics and Mission Design Near Libration Points
复制标题
DOI：
10.1142/9789812810632
复制
发表时间：
2001
期刊：
影响因子：
--
通讯作者：
G. Gómez;À. Jorba;C. Simó;J. Masdemont
中科院分区：
文献类型：
--
作者：
G. Gómez;À. Jorba;C. Simó;J. Masdemont
本书研究了太阳系中平动点附近轨道的位置保持问题。主要关注的是（地球+月球）-太阳系统中晕轨道附近的轨道。以受限三体问题为出发点，整个太阳系的运动被视为该简化模型的摄动。所有研究都具有足够的通用性，可以作为分析和数值计算的简单扩展轻松应用于其他初级-次级系统。
In this book the problem of station keeping is studied for orbits near libration points in the solar system. The main focus is on orbits near halo ones in the (Earth+ Moon)-Sun system. Taking as starting point the restricted three-body problem, the motion in the full solar system is considered as a perturbation of this simplified model. All the study is done with enough generality to allow easy application to other primary-secondary systems as a simple extension of the analytical and numerical computations.