杨东凯, 王峰, 李伟强, 张彦仲. 基于低轨卫星的北斗反射事件仿真分析[J]. 电波科学学报, 2015, 30(3): 409-416. doi: 10.13443/j.cjors.2014072001
      引用本文: 杨东凯, 王峰, 李伟强, 张彦仲. 基于低轨卫星的北斗反射事件仿真分析[J]. 电波科学学报, 2015, 30(3): 409-416. doi: 10.13443/j.cjors.2014072001
      YANG Dongkai, WANG Feng, LI Weiqiang, ZHANG Yanzhong. Simulation analysis of BeiDou reflection events based on LEO satellites[J]. CHINESE JOURNAL OF RADIO SCIENCE, 2015, 30(3): 409-416. doi: 10.13443/j.cjors.2014072001
      Citation: YANG Dongkai, WANG Feng, LI Weiqiang, ZHANG Yanzhong. Simulation analysis of BeiDou reflection events based on LEO satellites[J]. CHINESE JOURNAL OF RADIO SCIENCE, 2015, 30(3): 409-416. doi: 10.13443/j.cjors.2014072001

      基于低轨卫星的北斗反射事件仿真分析

      Simulation analysis of BeiDou reflection events based on LEO satellites

      • 摘要: 导航卫星反射事件的空间分布和数量是星载反射信号应用的综合评估指标之一, 北斗系统作为我国独立研发的导航系统, 与其他系统相比, 其反射事件的空间分布和数量具有独特性.针对上述问题, 通过研究北斗系统空间星座的特征, 模拟生成了完整的北斗系统空间星座, 给出了反射事件空间分布和数量的分析步骤, 利用导航卫星反射信号的基本几何关系推导了镜面反射点存在性判决条件.从机理上分析了北斗反射事件的影响因素, 在此基础上仿真分析了低轨卫星轨道高度、倾角、升交点赤经以及近地点角距对北斗系统同步地球轨道、倾斜地球轨道和中地球轨道卫星反射事件空间分布和数量的影响.结果表明:低轨卫星高度、升交点赤经只影响北斗反射事件数量, 而不影响分布, 轨道倾角对数量和分布都有显著影响, 轨道近地点角距无显著影响.最后, 总结给出了对地观测需合理设计低轨卫星轨道参数的指导性结论.

         

        Abstract: Spatial distribution and number of GNSS reflection events is one of evaluation standard in spaceborne GNSS-R, and BeiDou system is developed by China independently, whose spatial distribution and number of reflection events is distinct with other navigation system. To analyze above-mentioned distinction, in this paper the complete BeiDou Navigation Satellite System constellation was simulated based on its space segment parameters. BeiDou reflection events spatial distribution calculation procedure was given through the specular reflection point visibility judgment. Its effects on the number and spatial distribution were studied including the orbit height, inclination, argument of perigee and right ascension of ascending node. And BeiDou satellites such as GEO (Geostationary Earth Orbit), IGSO (Inclined Geosynchronous Satellite Orbit) and MEO (Middle Erath Orbit) could provide different reflection events. Simulation results show that the orbit height and right ascension of ascending node affect only the events number, however, the inclination affect both the number and distribution in latitude or longitude, and the argument of perigee has no any influence on the events. The final conclusion was given on the low earth orbit parameters design with the different requirements for the earth observation.

         

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