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Compass Satellite Orbit Determination Based on Inter-satellite and Satellite-to-station Ranging

机译:基于星际和卫星到站测距的罗盘卫星轨道确定

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For those satellite navigation systems, whose groundstations distributed only in local area, such as Compass,satellite observation arcs are limited. Satellite orbitdetermination based on these satellite-to-station ranges islack of precision. Inter-satellite ranging based on Intersatellitelink is able to extend satellite observation arcsand enhance satellite orbit determination accuracy.Aiming at the inter-satellite link of narrow-beam antenna,a new TDMA frame structure is proposed. Orbitdetermination performance based on joint ranges of intersatelliteand satellite-to-station under the new TDMAframe structure is analyzed. The factors impacting orbitdetermination performance such as ranging error, ranginginterval and ranging link number are all analyzed.Simulation results show that after adding inter-satellitelink, the maximum improvement of orbit determinationaccuracy is 77.5%. Among the factors, ranging interval isthe predominate one.
机译:对于那些卫星导航系统,其地面 仅分布在本地的电台,例如指南针, 卫星观测弧是有限的。卫星轨道 基于这些卫星到站的范围的确定是 缺乏精确度。基于星际的星际测距 链接能够扩展卫星观测弧 并提高卫星轨道确定的准确性。 针对窄波束天线的星际链路, 提出了一种新的TDMA帧结构。轨道 星际联合范围的卫星确定性能 和新的TDMA下的卫星到站 框架结构进行了分析。影响轨道的因素 确定性能,例如测距误差,测距 间隔和测距链接号均已分析。 仿真结果表明,添加星际后 链接,最大程度提高轨道确定性 准确度是77.5%。在这些因素中,测距间隔为 占主导地位的一个。

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