论文标题

电击参数估算的单飞机技术技术:一种系统的方法

Single-spacecraft techniques for shock parameters estimation: A systematic approach

论文作者

Trotta, Domenico, Vuorinen, Laura, Hietala, Heli, Horbury, Timothy, Dresing, Nina, Gieseler, Jan, Kouloumvakos, Athanasios, Price, Daniel James, Valentini, Francesco, Kilpua, Emilia, Vainio, Rami

论文摘要

航天器任务为研究利用原位测量的无碰撞冲击的特性提供了独特的机会。在过去的几年中,已经开发了几种诊断,以使用磁场的时间序列(和等离子体)数据来解决关键冲击参数,该数据通过单个航天器收集的横穿冲击阵线收集的数据。此类诊断的一个关键方面是评估上游下游数量的平均过程。在这项工作中,我们讨论了其中几种技术,特别关注冲击倾斜度(定义为上游磁场和休克正常矢量之间的角度)估计。我们引入了上游/下游平均窗口的系统变化,并产生了冲击参数的集合,这是一种有用的工具来解决其估计的稳健性。首先通过合成的休克对这种方法进行测试,并符合Rankine-Hugoniot跳跃条件的休克,包括噪声和干扰。然后,我们采用自洽的混合动力学休克模拟将诊断应用于虚拟航天器,在其进化的各个阶段越过冲击阵线,突出了冲击诱导的参数估计中的波动的作用。这种方法具有保留无碰撞冲击的一些重要特性的强大优势,同时能够设置已知的名义性冲击参数。最后,提出了两次来自太阳轨道航天器的星际冲击的两次观察结果,并在通过磁层多尺度(MMS)任务的四个航天器测量的行星际冲击测试中测试了该方法。所有用于诊断和使用的Python软件(SERPYSHOCK)均可公开开放,其中包括Solar Orbiter Spacecraft最近观察到的电击波的参数估计的示例。

Spacecraft missions provide the unique opportunity to study the properties of collisionless shocks utilising in situ measurements. In the past years, several diagnostics have been developed to address key shock parameters using time series of magnetic field (and plasma) data collected by a single spacecraft crossing a shock front. A critical aspect of such diagnostics is the averaging process involved in the evaluation of upstream-downstream quantities. In this work, we discuss several of these techniques, with a particular focus on the shock obliquity (defined as the angle between the upstream magnetic field and the shock normal vector) estimation. We introduce a systematic variation of the upstream/downstream averaging windows, yielding to an ensemble of shock parameters, a useful tool to address the robustness of their estimation. This approach is first tested with a synthetic shock, compliant with the Rankine-Hugoniot jump conditions for a shock, including the presence of noise and disturbances. We then employ self-consistent, hybrid kinetic shock simulations to apply the diagnostics to virtual spacecraft crossing the shock front at various stages of its evolution, highlighting the role of shock-induced fluctuations in the parameters estimation. This approach has the strong advantage of retaining some important properties of collisionless shock while being able to set a known, nominal set of shock parameters. Finally, two recent observations of interplanetary shocks from the Solar Orbiter spacecraft are presented, and the approach is also tested on an interplanetary shock measured by the four spacecraft of the Magnetospheric Multiscale (MMS) mission. All the Python software developed and used for the diagnostics (SerPyShock) is made available for the public, including an example of parameter estimation for a shock wave recently observed in-situ by the Solar Orbiter spacecraft.

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