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Comparison analyses on the 150 x 150 lunar gravity field models by gravity/topography admittance, correlation and precision orbit determination

机译:通过重力/地形导纳,相关性和精确轨道确定对150 x 150月球重力场模型进行比较分析

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摘要

We analyzed the 150 × 150 lunar gravity field models, LP150Q, GLGM-3 and SGM150, using the power spectrum on the lunar nearside and farside, the lunar global and localized gravity/topography admittance and correlation, and Chang'E-2 precision orbit determination to investigate which model is a more effective tool to estimate geophysical parameters and determine the lunar satellite precision orbit. Results indicate that all gravity field models can be used to estimate the lunar geophysical parameters of the nearside of the Moon. However, SGM150 is better in such computation of the farside. Additionally, SGM150 is shown to be the most useful model for determining the lunar satellite orbit.
机译:我们使用月球近端和远端的功率谱,月球全球和局部重力/地形的导纳率和相关性以及Chang娥二号精确轨道分析了150×150月球重力场模型LP150Q,GLGM-3和SGM150确定调查哪种模型是估计地球物理参数和确定月球卫星精确轨道的更有效工具。结果表明,所有重力场模型都可用于估算月球附近的月球地球物理参数。但是,SGM150在这种远端计算方面更好。此外,SGM150被证明是确定月球卫星轨道的最有用的模型。

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  • 来源
    《Advances in space research》 |2013年第3期|512-520|共9页
  • 作者单位

    State Key Laboratory of Information Engineering in Surveying, Mapping and Remote Sensing, Wuhan University, Wuhan 430070, China,Space Research Institute, Austrian Academy of Science, Graz 8042, Austria;

    State Key Laboratory of Information Engineering in Surveying, Mapping and Remote Sensing, Wuhan University, Wuhan 430070, China,School of Physics and Electronic Science, Guizhou Normal University, Guiyang, 550001, China;

    State Key Laboratory of Information Engineering in Surveying, Mapping and Remote Sensing, Wuhan University, Wuhan 430070, China;

    Department of Hydrology and Water Resources, University of Arizona, Tucson, AZ 85721, USA;

    National Astronomical Observatories, Chinese Academy of Science, Beijing 100012, China;

    Space Flight Dynamics Laboratory, Beijing Aerospace Command and Control Center, Beijing 100094, China;

    Space Flight Dynamics Laboratory, Beijing Aerospace Command and Control Center, Beijing 100094, China;

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  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Lunar gravity field models; Admittance spectrum; Correlation spectrum; Chang'E-2; Precision orbit determination;

    机译:月球重力场模型;导纳谱相关频谱E娥二号;精密轨道确定;

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