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Improvement in thermospheric neutral density estimations of the numerical TIE-GCM by incorporating helium data from the empirical NRLMSISE-00 model.

机译:通过合并来自经验性NRLMSISE-00模型的氦数据,改进了数值TIE-GCM的热层中性密度估计。

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摘要

The total atmospheric neutral densities derived from the CHAMP (CHAllenging Minisatellite Payload) and the GRACE (Gravity Recovery And Climate Experiment) accelerometer data are used to investigate the accuracy of the empirical as well as numerical thermospheric neutral density models during the solar maximum (year 2002) through the solar minimum (year 2007). The models used in this thesis include the empirical models of the Jacchia-Bowman models (JB2006 and JB2008) and the MSIS (Mass Spectrometer Incoherent Scatter)-class model, and the numerical model of the NCAR's TIE-GCM (National Center for Atmospheric Research's Thermosphere Ionosphere Electrodynamics General Circulation Model). The thermospheric neutral density models show good agreement to the variations of neutral densities from the accelerometer data, but still had uncertainties which should be taken into account for better prediction of satellites' position in orbit. The TIE-GCM shows larger uncertainties in the root mean square (RMS) in percent deviations at 400 km compared to the empirical models: 47.1% for the TIE-GCM compared to 15.7%, 10.3%, and 20.3% for the JB2006, JB2008, and NRLMSISE-00 models, respectively. The errors gradually increase with the decline in the solar activity. The partial pressures of helium obtained from the Naval Research Laboratory's MSIS Extension 2000 (NRLMSISE-00) model are incorporated into the TIE-GCM to reflect the helium effect in calculating the molecular viscosity, the thermal conductivity, and the specific heat. As a result, the secular increases of the percent deviations are eliminated and the RMS of the TIE-GCM is improved to 21.4% and 22.8% for the densities from the CHAMP and the GRACE-A accelerometer data, respectively, with the incorporation of 71% partial pressures of helium from the NRLMSISE-00 model.
机译:利用CHAMP(挑战性迷你卫星有效载荷)和GRACE(重力恢复和气候实验)加速度计数据得出的总大气中性密度用于研究太阳最大(2002年)期间经验性和数值性热层中性密度模型的准确性。 )到最低的太阳光(2007年)。本文使用的模型包括Jacchia-Bowman模型(JB2006和JB2008)和MSIS(质谱仪非相干散射)类模型的经验模型,以及NCAR TIE-GCM(国家大气研究中心)的数值模型。热层电离层电动力学通用循环模型)。热圈中性密度模型与加速度计数据的中性密度变化显示出很好的一致性,但仍存在不确定性,为更好地预测卫星在轨道上的位置应考虑这些不确定性。与经验模型相比,TIE-GCM在400 km处的均方根(RMS)偏差百分比具有更大的不确定性:TIE-GCM为47.1%,而JB2006,JB2008为15.7%,10.3%和20.3% ,和NRLMSISE-00型号。随着太阳活动的减少,误差逐渐增加。从海军研究实验室的MSIS Extension 2000(NRLMSISE-00)模型获得的氦分压被合并到TIE-GCM中,以反映氦在计算分子粘度,热导率和比热中的作用。结果,消除了偏差的长期增加,并且将CHAMP和GRACE-A加速度计数据的密度分别提高了TIE-GCM的RMS到21.4%和22.8%,并结合了71来自NRLMSISE-00模型的氦气分压的%。

著录项

  • 作者

    Kim, Jung Soo.;

  • 作者单位

    The Pennsylvania State University.;

  • 授予单位 The Pennsylvania State University.;
  • 学科 Engineering Aerospace.;Engineering Electronics and Electrical.
  • 学位 Ph.D.
  • 年度 2011
  • 页码 175 p.
  • 总页数 175
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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