首页> 外文会议>AAS/AIAA Space Flight Mechanics Meeting; 20050123-27; Copper Mountain,CO(US) >Atmosphere Variability at Mars Reconnaissance Orbiter Science Orbit Altitudes Based on Mars Express Reconstructions
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Atmosphere Variability at Mars Reconnaissance Orbiter Science Orbit Altitudes Based on Mars Express Reconstructions

机译:基于火星快速重构的火星侦察轨道科学轨道高度的大气变率

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摘要

This paper describes the orbit reconstruction of Mars Express (MEX) with the specific goal of estimating the atmospheric density near periapsis and evaluating its variability and predictability. The desired outcome is to validate the covariance analysis assumption of atmospheric variability for the 2005 NASA Mars Reconnaissance Orbiter (MRO), as well as evaluate the accuracy of the density estimates output from the atmosphere model used by MRO. Topics covered include the MRO atmosphere model, MEX orbit determination and post-fit Doppler residuals, and atmosphere trending statistics gleaned from the orbit reconstructions.
机译:本文描述了火星快车(MEX)的轨道重建,其具体目标是估算围根周围的大气密度,并评估其可变性和可预测性。理想的结果是验证2005 NASA火星侦察轨道器(MRO)的大气变化的协方差分析假设,以及评估MRO所使用的大气模型输出的密度估算值的准确性。涵盖的主题包括MRO大气模型,MEX轨道确定和拟合后的多普勒残差,以及从轨道重建中收集到的大气趋势统计数据。

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