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On the determination and investigation of the terrestrial ionospheric refractive indices using GEOS-3/ATS-6 satellite-to-satellite tracking data

机译:利用GEOS-3 / ATS-6卫星到卫星跟踪数据确定和研究地面电离层折射率

摘要

When the radio link between two satellites (GEOS-3/ATS-6) is intercepted by the earth's ionosphere and neutral atmosphere, a change in the Doppler frequency results. Travel through the atmosphere causes the Doppler phase to be advanced in the ionosphere's portion and retarded in the neutral portion of the atmosphere. Analysis of the shortening and lengthening of the phase of the Satellite-to-Satellite Tracking (SST) data that passed within 40-700 km above the earth's surface during its ATS-6 to GEOS-3 to ATS-6 path, caused by the atmosphere, results in refractivity versus height profiles. The SST Doppler data were used directly to adjust the GEOS-3 orbit. Perturbation from the Moon, Sun and a 15th order/degree earth gravity field were included in the orbit solution. This orbit was continued through the occultation period and a model ionosphere was estimated by a least-square adjustment of the Chapman ionosphere parameters from the SST data residuals. The refractivity profile obtained by this model ionosphere was compared to a refractivity profile obtained by a direct integral inversion of the SST data residuals. Systematic differences between the 2 methods were caused by orbital errors, which propagated into the solution. The SST data yielded refractive index profiles in a novel economical manner because no additional or special on-board equipment were required.
机译:当两颗卫星(GEOS-3 / ATS-6)之间的无线电链路被地球的电离层和中性大气所拦截时,会导致多普勒频率发生变化。穿过大气层会导致多普勒相在电离层部分超前,并在大气的中性部分受阻。由ATS-6到GEOS-3到ATS-6路径引起的卫星到卫星跟踪(SST)数据在地球表面上方40-700 km内通过的阶段的缩短和延长的分析。大气,导致折射率相对于高度的分布。 SST多普勒数据直接用于调整GEOS-3轨道。月球,太阳和15阶/度地球重力场的摄动被包括在轨道解中。该轨道持续了整个潜伏期,并根据SST数据残差对查普曼电离层参数进行了最小二乘调整,从而估算了电离层模型。将通过该模型电离层获得的折射率分布与通过SST数据残差的直接积分反演获得的折射率分布进行比较。两种方法之间的系统差异是由轨道误差引起的,这些误差传播到解中。 SST数据以一种新颖的经济方式产生了折射率分布,因为不需要额外的或特殊的车载设备。

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    Liu A. S.;

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  • 年度 1978
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