Overview of Earth-Moon Transfer Trajectory Modeling and Design  

作　　者：Jiye Zhang Huichang Yu Honghua Dai 

机构地区：[1]School of Astronautics,Northwestern Polytechnical University,Xi’an,710072,China

出　　处：《Computer Modeling in Engineering & Sciences》2023年第4期5-43,共39页工程与科学中的计算机建模（英文）

基　　金：supported by the National Key Research and Development Program of China(No.2021YFA0717100);the National Natural Science Foundation of China(Nos.12072270 and U2013206).

摘　　要：TheMoon is the only celestial body that human beings have visited.The design of the Earth-Moon transfer orbits is a critical issue in lunar exploration missions.In the 21st century,new lunar missions including the construction of the lunar space station,the permanent lunar base,and the Earth-Moon transportation network have been proposed,requiring low-cost,expansive launch windows and a fixed arrival epoch for any launch date within the launch window.The low-energy and low-thrust transfers are promising strategies to satisfy the demands.This review provides a detailed landscape of Earth-Moon transfer trajectory design processes,from the traditional patched conic to the state-of-the-art low-energy and low-thrust methods.Essential mechanisms of the various utilized dynamic models and the characteristics of the different design methods are discussed in hopes of helping readers grasp thebasic overviewof the current Earth-Moon transfer orbitdesignmethods anda deep academic background is unnecessary for the context understanding.

关 键 词：Earth-Moon transfer traditional direct transfer low-energy transfer manifold theory weak stability boundary theory low-thrust transfer 

分 类 号：V41[航空宇航科学与技术—航空宇航推进理论与工程]