Network Performance of pLEO Topologies in a High-Inclination Walker Delta Satellite Constellation

T. Royster, Jun Sun, A. Narula-Tam, T. Shake
{"title":"Network Performance of pLEO Topologies in a High-Inclination Walker Delta Satellite Constellation","authors":"T. Royster, Jun Sun, A. Narula-Tam, T. Shake","doi":"10.1109/AERO55745.2023.10115752","DOIUrl":null,"url":null,"abstract":"Low-earth-orbit satellite constellations with hundreds to thousands of satellites are emerging as practical alternatives for providing various types of data services such as global networking and large-scale sensing. The network performance of these satellite constellations is strongly dependent on the topology of the inter-satellite links (ISLs) in such systems. This paper studies the effects of six different ISL topologies, coupled with three configurations of ground relay terminals, on path failure rate, path latency, and link transmission efficiency in an example highly-inclined Walker Delta constellation with 360 satellites. These network performance parameters are calculated in the presence of satellite failures in the constellation. Trade-offs between ISL connection density and overall performance are examined and quantified. Topologies with 4 active ISLs per satellite are shown to perform significantly better than topologies requiring fewer, especially as the average number of active ISLs per satellite becomes significantly less than three. Latencies for a topology requiring 3 active ISLs per satellite are shown to be between 15 and 60 % higher than for a 4- ISL reference topology. Path availabilities for the 3- ISL topology are shown to be on the order of 30 % lower for a benchmark case of 10 satellite failures. The performance of near-minimal topologies (e.g., an average of 2.2 active ISLs per satellite) is much worse. Latency reductions of 10-30% and path failure rate improvements on the order of 45 % are shown to be obtainable by the inclusion of 2 to 5 strategically located ground relay stations. 11DISTRIBUTION STATEMENT A. Approved for public release. Distribution is unlimited. This material is based upon work supported by the Defense Advanced Research Projects Agency under Air Force Contract No. FA8702-15-D-0001. The views, opinions and/or findings expressed are those of the authors and should not be interpreted as representing the official views or policies of the Department of Defense or the U.S. Government.","PeriodicalId":344285,"journal":{"name":"2023 IEEE Aerospace Conference","volume":"62 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2023-03-04","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"2023 IEEE Aerospace Conference","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/AERO55745.2023.10115752","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 0

Abstract

Low-earth-orbit satellite constellations with hundreds to thousands of satellites are emerging as practical alternatives for providing various types of data services such as global networking and large-scale sensing. The network performance of these satellite constellations is strongly dependent on the topology of the inter-satellite links (ISLs) in such systems. This paper studies the effects of six different ISL topologies, coupled with three configurations of ground relay terminals, on path failure rate, path latency, and link transmission efficiency in an example highly-inclined Walker Delta constellation with 360 satellites. These network performance parameters are calculated in the presence of satellite failures in the constellation. Trade-offs between ISL connection density and overall performance are examined and quantified. Topologies with 4 active ISLs per satellite are shown to perform significantly better than topologies requiring fewer, especially as the average number of active ISLs per satellite becomes significantly less than three. Latencies for a topology requiring 3 active ISLs per satellite are shown to be between 15 and 60 % higher than for a 4- ISL reference topology. Path availabilities for the 3- ISL topology are shown to be on the order of 30 % lower for a benchmark case of 10 satellite failures. The performance of near-minimal topologies (e.g., an average of 2.2 active ISLs per satellite) is much worse. Latency reductions of 10-30% and path failure rate improvements on the order of 45 % are shown to be obtainable by the inclusion of 2 to 5 strategically located ground relay stations. 11DISTRIBUTION STATEMENT A. Approved for public release. Distribution is unlimited. This material is based upon work supported by the Defense Advanced Research Projects Agency under Air Force Contract No. FA8702-15-D-0001. The views, opinions and/or findings expressed are those of the authors and should not be interpreted as representing the official views or policies of the Department of Defense or the U.S. Government.
查看原文
分享 分享
微信好友 朋友圈 QQ好友 复制链接
本刊更多论文
高倾角Walker Delta卫星星座pLEO拓扑网络性能研究
拥有数百至数千颗卫星的低地球轨道卫星星座正在成为提供各种类型数据服务(如全球联网和大规模传感)的实际替代方案。这些卫星星座的网络性能强烈依赖于这些系统中卫星间链路(isl)的拓扑结构。以360颗高倾斜Walker Delta星座为例,研究了六种不同ISL拓扑结构和三种地面中继终端配置对路径故障率、路径延迟和链路传输效率的影响。这些网络性能参数是在星座中存在卫星故障的情况下计算的。ISL连接密度和整体性能之间的权衡进行了检查和量化。每颗卫星有4个活动isl的拓扑比需要更少活动isl的拓扑表现得好得多,特别是当每颗卫星的活动isl的平均数量明显少于3个时。每颗卫星需要3个活动ISL的拓扑的延迟比4个ISL参考拓扑高15%到60%。对于10颗卫星故障的基准情况,3- ISL拓扑的路径可用性显示为低30%左右。接近最小拓扑(例如,每颗卫星平均有2.2个有效isl)的性能要差得多。通过包含2至5个战略位置的地面中继站,可以将延迟减少10-30%,并将路径故障率提高45%。A.批准公开发行。分发是无限的。这份材料是基于美国空军合同第5号国防高级研究计划局支持的工作。fa8702 - 15 d - 0001。所表达的观点、意见和/或调查结果仅代表作者的观点,不应被解释为代表国防部或美国政府的官方观点或政策。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
求助全文
约1分钟内获得全文 去求助
来源期刊
自引率
0.00%
发文量
0
期刊最新文献
The Mission for Education and Multimedia Engagement: Breaking the Barriers to Satellite Education TID Testing of COTS-based, Two-Phase, Point-of-Load Converters for Aerospace Applications Point-Source Target Detection and Localization in Single-Frame Infrared Imagery Comparative Analysis of Different Profiles of Riblets on an Airfoil using Large Eddy Simulations A Receiver-Independent GNSS Smart Antenna for Simultaneous Jamming and Spoofing Protection
×
引用
GB/T 7714-2015
复制
MLA
复制
APA
复制
导出至
BibTeX EndNote RefMan NoteFirst NoteExpress
×
×
提示
您的信息不完整,为了账户安全,请先补充。
现在去补充
×
提示
您因"违规操作"
具体请查看互助需知
我知道了
×
提示
现在去查看 取消
×
提示
确定
0
微信
客服QQ
Book学术公众号 扫码关注我们
反馈
×
意见反馈
请填写您的意见或建议
请填写您的手机或邮箱
已复制链接
已复制链接
快去分享给好友吧!
我知道了
×
扫码分享
扫码分享
Book学术官方微信
Book学术文献互助
Book学术文献互助群
群 号:481959085
Book学术
文献互助 智能选刊 最新文献 互助须知 联系我们:info@booksci.cn
Book学术提供免费学术资源搜索服务,方便国内外学者检索中英文文献。致力于提供最便捷和优质的服务体验。
Copyright © 2023 Book学术 All rights reserved.
ghs 京公网安备 11010802042870号 京ICP备2023020795号-1