金星大气中的太阳掩星实验:轨道参数对测量值时空分布的影响

Jayadev Pradeep, S. Sunilkumar
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引用次数: 0

摘要

太阳掩星是一种基于卫星的高分辨率行星大气垂直剖面技术。由于独特的观测几何结构,推断掩星测量的时空覆盖作为航天器轨道的函数是非平凡的。在这项工作中,我们为一个假设的太阳掩星实验(SOE)实现了基于python的掩星观测几何的3D模拟,以研究金星的大气。利用astropy和poliastro软件包进行行星运动和轨道传播模拟,并利用三维矢量代数计算瞬时视距切点。利用金星快车的SPICAV/SOIR数据验证了模拟结果,结果非常吻合。通过模拟,我们首次对不同航天器轨道元素对金星大气中掩星测量时空分布的影响进行了理论研究,证实了一种高度敏感的依赖性。发现航天器轨道的半长轴(a)和倾角(i)影响观测的纬度范围和掩星季节的性质/持续时间,而偏心率(e)和近日点角(ω)决定了稀疏观测的不同区域。发现单个SOE剖面的时空分布依赖于轨道参数和太阳β角。我们的研究结果表明,从实现特定科学目标的角度来看,可以设计具有适当参数的航天器轨道,以优化SOE测量的覆盖范围,为未来旨在实施太阳掩星技术的金星任务提供有价值的输入。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Solar Occultation Experiments (SOE) in the Venusian Atmosphere: effect of orbital parameters on the spatiotemporal distribution of measurements
Solar occultation is a satellite-based technique for high-resolution vertical profiling of planetary atmospheres. Owing to the distinctive observational geometry, the deduction of the spatiotemporal coverage of solar occultation measurements as a function of the spacecraft orbit is non-trivial. In this work, we have implemented python-based 3D simulations of the occultation-viewing geometry for a hypothetical Solar Occultation Experiment (SOE) to study the atmosphere of Venus. The simulations incorporate planetary motions and orbital propagation using the astropy and poliastro packages, and compute the instantaneous line-of-sight (LoS) tangent point using 3D vector algebra. SPICAV/SOIR data from Venus Express was used to validate the simulations, showing excellent agreement. Using the simulations, we conducted a first-of-its-kind theoretical study on the effect of varying different spacecraft orbital elements on the spatiotemporal distribution of solar occultation measurements in the Venusian atmosphere, confirming a highly sensitive dependence. The semimajor axis (a) and inclination (i) of the spacecraft orbit are found to influence the latitudinal extent of observations and the nature/duration of occultation seasons, while the eccentricity (e) and argument of periapsis (ω) determine the distinct regions of sparse observations. The spatiotemporal spread of individual SOE profiles is found to depend on the orbital parameters as well as the solar beta angle. Our results show that spacecraft orbits can be designed with appropriate parameters to optimize the coverage of SOE measurements in view of achieving specific science goals, providing valuable inputs for future missions to Venus that aim to implement the solar occultation technique.
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