S.C. Lee, R. Nichols, R. L. Yuan, W. Blackert, M.P. Blair
{"title":"A LEO satellite concept for the advanced narrowband system","authors":"S.C. Lee, R. Nichols, R. L. Yuan, W. Blackert, M.P. Blair","doi":"10.1109/MILCOM.1999.821380","DOIUrl":null,"url":null,"abstract":"This paper examines the feasibility of deploying a low Earth orbit (LEO) satellite system to support the mobile user objective system requirements. The primary goal of the study was to develop a LEO constellation that could support continuous global voice and data communications to cellular telephone-like handsets while minimizing the use of high-cost/high-risk technology. Various system trade-offs are presented that address issues such as the user-to-spacecraft link performance, spacecraft and constellation design, and ground segment characteristic.","PeriodicalId":334957,"journal":{"name":"MILCOM 1999. IEEE Military Communications. Conference Proceedings (Cat. No.99CH36341)","volume":"11 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"1999-10-31","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"2","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"MILCOM 1999. IEEE Military Communications. Conference Proceedings (Cat. No.99CH36341)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/MILCOM.1999.821380","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 2
Abstract
This paper examines the feasibility of deploying a low Earth orbit (LEO) satellite system to support the mobile user objective system requirements. The primary goal of the study was to develop a LEO constellation that could support continuous global voice and data communications to cellular telephone-like handsets while minimizing the use of high-cost/high-risk technology. Various system trade-offs are presented that address issues such as the user-to-spacecraft link performance, spacecraft and constellation design, and ground segment characteristic.