{"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}
引用次数: 1
Abstract
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.
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