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4-GNSS radio occultation satellite constellation design based on Dual-gate uniformity evaluation index

机译:基于双门一致性评估指标的4-GNSS无线电掩星卫星星座设计

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A brand-new area of low earth orbit satellite constellation research has been expanded by global navigation satellite system (GNSS) radio occultation (RO) atmosphere sounding technology in the last decade. The possibility of reducing the sounding satellites while keeping the amount of atmosphere soundings increasing to produce low-cost meteorological data product is investigated, and a constellation capable of receiving the RO signals from all the 4-GNSS, such as GPS, GLONASS, Galileo, and Compass, is proposed in this paper. This paper focuses on the mathematical problems on the design of 4-GNSS RO satellite constellation. A forward GNSS RO sounding simulation algorithm based on ideal atmosphere model and two-dimensional radial tracing algorithm is presented for a rapidly and accurately sounding performance prediction of 4-GNSS RO satellite constellations. Then, an improved uniformity evaluation factor named Dual-gate is established for 4-GNSS RO satellite constellation optimization design, which is a combination of the uniformity evaluation factors for the latitudinal distribution of RO soundings and those for the gridding uniformity. On the basis of low earth orbit satellite orbit dynamics and spherical geometry, the impacts of partial constellation parameters on the amount and coverage performance accorded with Dual-gate uniformity evaluation index are derived, and a series of design criteria of 4-GNSS RO satellite constellation are summarized. A simplified 4-GNSS RO satellite constellation model is built on the basis of the design criteria, and an improved ant colony algorithm is used to optimize the parameters of a 4-GNSS RO constellation including as many satellites as COSMIC-2. The simulation result shows that this 4-GNSS RO constellation is capable of obtaining near 3000 atmosphere soundings per 3 h. It obtains 13% more soundings than COSMIC-2 with the same 4-GNSS RO sounding devices, and the uniformity of soundings is increased by 9%.
机译:近十年来,全球导航卫星系统(GNSS)无线电掩星(RO)大气探测技术扩展了一个崭新的低地球轨道卫星星座研究领域。研究了减少探空卫星同时保持不断增加的大气探测量以产生低成本气象数据产品的可能性,并研究了一种能够接收来自所有4-GNSS(例如GPS,GLONASS,Galileo,和指南针,在本文中提出。本文重点研究了4-GNSS RO卫星星座设计中的数学问题。提出了一种基于理想大气模型和二维径向跟踪算法的前向GNSS RO探测模拟算法,用于快速,准确地预测4-GNSS RO卫星星座的探测性能。然后,为4-GNSS RO卫星星座优化设计建立了一个改进的均匀度评价因子Dual-gate,该因子是RO测深的纬度分布和网格均匀度的均匀性评价因子的组合。在低地球轨道卫星轨道动力学和球形几何的基础上,推导了部分星座参数对双门均匀性评价指标所要求的数量和覆盖性能的影响,并提出了一系列4-GNSS RO卫星星座的设计准则总结。在设计准则的基础上建立了简化的4-GNSS RO卫星星座模型,并使用改进的蚁群算法来优化4-GNSS RO星座的参数,包括与COSMIC-2一样多的卫星。仿真结果表明,该4-GNSS RO星座图每3 h可获得近3000个大气探测。使用相同的4-GNSS RO测深装置,与COSMIC-2相比,它的测深高出13%,并且测深均匀度提高了9%。

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