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“天链一号01星”对三类卫星中继性能仿真分析
引用本文:蒋虎.“天链一号01星”对三类卫星中继性能仿真分析[J].全球定位系统,2008,33(6):25-26.
作者姓名:蒋虎
作者单位:上海微小卫星工程中心,上海,200050;中国科学院上海微系统与信息技术研究所,上海,200050
摘    要:以三类卫星轨道为例,利用STK分析软件就“天链一号01星”对三类轨道卫星的中继能力进行仿真,其中仿真参数包括一天内可中继次数、最短中继时间、最长中继时间、平均中继时间和可中继时间百分比等关键指标。仿真结果表明:“天链一号01星”对400~800km轨道高度的低轨道卫星的中继时间百分比可达55%以上;对20000-24000km中轨道卫星的中继时间百分比可达90%以上;对倾斜地球同步轨道卫星的中继时间百分比可达100%。

关 键 词:倾斜地球同步卫星  低轨道卫星  中轨道卫星  中继  仿真

Analysis of Relay Capabilities for First Sino-TDRS Satellite
JIANG Hu.Analysis of Relay Capabilities for First Sino-TDRS Satellite[J].Gnss World of China,2008,33(6):25-26.
Authors:JIANG Hu
Institution:JIANG Hu1,2 (1.Shanghai Engineering Center for Micro-Satellites,Shanghai 200050,China,2.Shanghai Institute of Micro-system , Information Technology,the Chinese Academy of Sciences,China)
Abstract:Taking three types of orbits for examples,data relay capabilities for the first Sino-TDRS satellite are simulated and assessed via STK software.Such indexes are presented as daily relay frequency,shortest relaying interval,longest relaying interval,mean relaying interval and temporal percentage of availability of data relay.Simulations reveals that the first Sino-TDRS satellite can provide 55% relaying opportunity for low Earth orbiting satellites,and more than 90% for middle altitude satellites,and 100% fo...
Keywords:Inclined geosynchronous satellite  low earth orbiter  middle altitude satellite  relay  simulation  
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