航天动力学（英文）2025，Vol.9Issue(5)：785-805,21.DOI:10.1007/s42064-024-0250-4
Leveraging the Hill restricted four-body problem to investigate the ephemeris transition characteristics in the Earth-Moon L2 halo orbit region
Leveraging the Hill restricted four-body problem to investigate the ephemeris transition characteristics in the Earth-Moon L2 halo orbit region
摘要
关键词
Earth-Moon L2 halo family/Hill restricted four-body problem(HR4BP)/bifurcations/ephemeris transitionKey words
Earth-Moon L2 halo family/Hill restricted four-body problem(HR4BP)/bifurcations/ephemeris transition引用本文复制引用
Rohith Reddy Sanaga,Kathleen C.Howell..Leveraging the Hill restricted four-body problem to investigate the ephemeris transition characteristics in the Earth-Moon L2 halo orbit region[J].航天动力学（英文）,2025,9(5):785-805,21.基金项目
The authors appreciate the support of Purdue University,the School of Aeronautics and Astronautics as well as the Department of Computer Science.The authors also thank Beom Park and the rest of the members(current and previous)of the Multi-Body Dynamics Research Group at Purdue University for useful discussions. （current and previous）
