{"title":"受限三体问题的逃逸判据","authors":"Shuyue Fu , Shengping Gong","doi":"10.1016/j.asr.2025.02.017","DOIUrl":null,"url":null,"abstract":"<div><div>In this study, we investigate escape criterion suitable for the restricted three-body problem. First, the Earth-Moon planar circular restricted three-body problem is used as an example, and the escape criteria developed in previous works are presented and analyzed. Next, the energy of a test body is introduced as a key indicator for escape. A condition for identifying escape trajectories in the Earth-Moon planar circular restricted three-body problem is theoretically derived, based on an approximate relationship between the energy of the test body and the two-body energy with respect to the Earth-Moon barycenter. The proposed criterion is then transformed into numerical conditions for trajectory simulations. Numerical simulations verify that the proposed criterion can identify escape trajectories more accurately than those developed in previous works. Finally, the application of this criterion in identifying the natural and artificial escape trajectories is presented.</div></div>","PeriodicalId":50850,"journal":{"name":"Advances in Space Research","volume":"75 8","pages":"Pages 6376-6393"},"PeriodicalIF":2.8000,"publicationDate":"2025-02-13","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Escape criterion for restricted three-body problem\",\"authors\":\"Shuyue Fu , Shengping Gong\",\"doi\":\"10.1016/j.asr.2025.02.017\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"<div><div>In this study, we investigate escape criterion suitable for the restricted three-body problem. First, the Earth-Moon planar circular restricted three-body problem is used as an example, and the escape criteria developed in previous works are presented and analyzed. Next, the energy of a test body is introduced as a key indicator for escape. A condition for identifying escape trajectories in the Earth-Moon planar circular restricted three-body problem is theoretically derived, based on an approximate relationship between the energy of the test body and the two-body energy with respect to the Earth-Moon barycenter. The proposed criterion is then transformed into numerical conditions for trajectory simulations. Numerical simulations verify that the proposed criterion can identify escape trajectories more accurately than those developed in previous works. Finally, the application of this criterion in identifying the natural and artificial escape trajectories is presented.</div></div>\",\"PeriodicalId\":50850,\"journal\":{\"name\":\"Advances in Space Research\",\"volume\":\"75 8\",\"pages\":\"Pages 6376-6393\"},\"PeriodicalIF\":2.8000,\"publicationDate\":\"2025-02-13\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Advances in Space Research\",\"FirstCategoryId\":\"89\",\"ListUrlMain\":\"https://www.sciencedirect.com/science/article/pii/S027311772500136X\",\"RegionNum\":3,\"RegionCategory\":\"地球科学\",\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"Q2\",\"JCRName\":\"ASTRONOMY & ASTROPHYSICS\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Advances in Space Research","FirstCategoryId":"89","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S027311772500136X","RegionNum":3,"RegionCategory":"地球科学","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q2","JCRName":"ASTRONOMY & ASTROPHYSICS","Score":null,"Total":0}
Escape criterion for restricted three-body problem
In this study, we investigate escape criterion suitable for the restricted three-body problem. First, the Earth-Moon planar circular restricted three-body problem is used as an example, and the escape criteria developed in previous works are presented and analyzed. Next, the energy of a test body is introduced as a key indicator for escape. A condition for identifying escape trajectories in the Earth-Moon planar circular restricted three-body problem is theoretically derived, based on an approximate relationship between the energy of the test body and the two-body energy with respect to the Earth-Moon barycenter. The proposed criterion is then transformed into numerical conditions for trajectory simulations. Numerical simulations verify that the proposed criterion can identify escape trajectories more accurately than those developed in previous works. Finally, the application of this criterion in identifying the natural and artificial escape trajectories is presented.
期刊介绍:
The COSPAR publication Advances in Space Research (ASR) is an open journal covering all areas of space research including: space studies of the Earth''s surface, meteorology, climate, the Earth-Moon system, planets and small bodies of the solar system, upper atmospheres, ionospheres and magnetospheres of the Earth and planets including reference atmospheres, space plasmas in the solar system, astrophysics from space, materials sciences in space, fundamental physics in space, space debris, space weather, Earth observations of space phenomena, etc.
NB: Please note that manuscripts related to life sciences as related to space are no more accepted for submission to Advances in Space Research. Such manuscripts should now be submitted to the new COSPAR Journal Life Sciences in Space Research (LSSR).
All submissions are reviewed by two scientists in the field. COSPAR is an interdisciplinary scientific organization concerned with the progress of space research on an international scale. Operating under the rules of ICSU, COSPAR ignores political considerations and considers all questions solely from the scientific viewpoint.