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首页> 外文期刊>Advances in space research >High-fidelity geometry models for improving the consistency of CHAMP, GRACE, GOCE and Swarm thermospheric density data sets
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High-fidelity geometry models for improving the consistency of CHAMP, GRACE, GOCE and Swarm thermospheric density data sets

机译:高保真几何模型,可改善CHAMP,GRACE,GOCE和Swarm热球密度数据集的一致性

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During the last two decades, accelerometers on board of the CHAMP, GRACE, GOCE and Swarm satellites have provided high-resolution thermosphere density data to improve our knowledge on atmospheric dynamics and coupling processes in the thermosphere-ionosphere region. Most users of the data have focused on relative density variations. Scale differences between datasets and models have been largely neglected or removed using ad hoc scale factors. The origin of these scale differences arises from errors in the aerodynamic modelling, specifically in the modelling of the satellite outer surface geometry and of the gas-surface interactions. Therefore, the first step to remove the scale differences is to enhance the geometry modelling. This work forms the foundation for the future improvement of characterization of satellite aerodynamics and gas-surface interactions models at TU Delft, as well as for extending the use of sideways and angular accelerations in the aerodynamic analysis of accelerations and derivation of thermosphere datasets. Although work to improve geometry and aerodynamic force models by other authors has focused on CHAMP and GRACE, this paper includes the GOCE and Swarm satellites as well. In addition, it uses a density determination algorithm that is valid for arbitrary attitude orientations, enabling a validation making use of attitude manoeuvres. The results show an improvement in the consistency of density data between these four missions, and of data obtained before, during and after attitude manoeuvres of CHAMP and Swarm. The new models result in larger densities, compared to the previously used panel method. The largest average rescaling of density, by switching to the new geometry models is reached for Swarm at 32%, the smallest for GRACE at 5%. For CHAMP and GOCE, mean differences of 11% and 9% are obtained respectively. In this paper, an overview of the improvements and comparisons of data sets is provided together with an introduction to the next research phase on the gas-surface interactions.
机译:在过去的二十年中,CHAMP,GRACE,GOCE和Swarm卫星上的加速度计提供了高分辨率的热圈密度数据,以提高我们对热圈-电离层区域大气动力学和耦合过程的了解。数据的大多数用户都专注于相对密度变化。数据集和模型之间的比例差异已使用临时比例因子在很大程度上被忽略或消除。这些尺度差异的根源来自于空气动力学建模中的误差,特别是卫星外表面几何形状和气-气表面相互作用的建模误差。因此,消除比例差异的第一步是增强几何模型。这项工作为将来改进TU Delft的卫星空气动力学特性和气面相互作用模型奠定了基础,并为在对加速和派生热层数据集进行空气动力学分析中扩展了侧向加速度和角加速度的使用奠定了基础。尽管其他作者改善几何和空气动力模型的工作主要集中在CHAMP和GRACE,但本文还包括GOCE和Swarm卫星。另外,它使用对任意姿态定向均有效的密度确定算法,从而可以利用姿态操纵进行验证。结果表明,这四个任务之间的密度数据以及CHAMP和Swarm的姿态演习之前,之中和之后获得的数据的一致性都得到了改善。与以前使用的面板方法相比,新模型具有更大的密度。通过切换到新的几何模型,Swarm的密度平均最大缩放比例达到了32%,而GRACE的最小平均缩放比例达到了5%。对于CHAMP和GOCE,平均差异分别为11%和9%。在本文中,提供了对数据集的改进和比较的概述,并介绍了有关气体-表面相互作用的下一个研究阶段。

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