{"title":"地球人造卫星运动的二阶解","authors":"Liu Lin, Zhao De-zi","doi":"10.1016/0146-6364(80)90024-9","DOIUrl":null,"url":null,"abstract":"<div><p>This paper gives a second-order, analytical solution for the motion of an artificial satellite of the Earth as perturbed by various factors, and the formula for a combined analytical and numerical method. The solution is valid for all eccentricities.</p></div>","PeriodicalId":100241,"journal":{"name":"Chinese Astronomy","volume":"4 4","pages":"Pages 343-353"},"PeriodicalIF":0.0000,"publicationDate":"1980-12-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"https://sci-hub-pdf.com/10.1016/0146-6364(80)90024-9","citationCount":"1","resultStr":"{\"title\":\"A second-order solution of the motion of artificial satellites of the Earth\",\"authors\":\"Liu Lin, Zhao De-zi\",\"doi\":\"10.1016/0146-6364(80)90024-9\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"<div><p>This paper gives a second-order, analytical solution for the motion of an artificial satellite of the Earth as perturbed by various factors, and the formula for a combined analytical and numerical method. The solution is valid for all eccentricities.</p></div>\",\"PeriodicalId\":100241,\"journal\":{\"name\":\"Chinese Astronomy\",\"volume\":\"4 4\",\"pages\":\"Pages 343-353\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"1980-12-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"https://sci-hub-pdf.com/10.1016/0146-6364(80)90024-9\",\"citationCount\":\"1\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Chinese Astronomy\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://www.sciencedirect.com/science/article/pii/0146636480900249\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Chinese Astronomy","FirstCategoryId":"1085","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/0146636480900249","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
A second-order solution of the motion of artificial satellites of the Earth
This paper gives a second-order, analytical solution for the motion of an artificial satellite of the Earth as perturbed by various factors, and the formula for a combined analytical and numerical method. The solution is valid for all eccentricities.
京公网安备 11010802042870号
京ICP备2023020795号-1
分享
求助内容：
应助结果提醒方式：
扫码关注我们
