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ELVES Measurements in the “UV Atmosphere” (Mini-EUSO) Experiment Onboard the ISS and Their Reconstruction 国际空间站上 "紫外线大气层"(迷你 EUSO)实验中的 ELVES 测量及其重构
IF 0.6 4区 物理与天体物理 Q4 ASTRONOMY & ASTROPHYSICS Pub Date : 2024-06-17 DOI: 10.1134/s0010952524600379
S. Sharakin, D. Barghini, M. Battisti, A. Belov, M. Bertaina, M. Bianciotto, F. Bisconti, C. Blaksley, S. Blin, G. Cambiè, F. Capel, M. Casolino, T. Ebisuzaki, J. Eser, F. Fenu, M. A. Franceschi, A. Golzio, P. Gorodetsky, F. Kajino, H. Kasuga, P. Klimov, M. Manfrin, L. Marcelli, W. Marszal, H. Miyamoto, M. Mignone, A. Murashov, T. Napolitano, H. Ohmori, A. Olinto, E. Parizot, P. Picozza, L. W. Piotrowski, Z. Plebaniak, G. Prévôt, E. Reali, M. Ricci, G. Romoli, N. Sakaki, K. Shinozaki, J. Szabelski, C. De La Taille, Y. Takizawa, M. Vrábel, L. Wiencke, M. Zotov

Abstract

More than three dozen submillisecond events of ELVES type (“elves”), which are the result of the interaction of the front of an electromagnetic pulse from a lightning discharge and the lower layer of the ionosphere, have been identified in the data of a UV Atmosphere orbital multichannel detector (Mini-EUSO). Each event has a characteristic annular glow pattern and occupies a significant part of the detector’s field of view, and the signal in a separate channel has an asymmetric profile with a pronounced peak. The distribution of peak times contains information about both the localization of the discharge and the altitude of the glow. In this paper, we propose a Bayesian (probabilistic) model for reconstructing ELVES events, implemented using probabilistic programming methods in PyMC-5. The capabilities of the model for determining the position of the discharge are shown using the example of several events. Methods for modifying the model to restore the discharge orientation and refine the glow height are outlined.

摘要 在紫外大气层轨道多通道探测器(Mini-EUSO)的数据中发现了三十多个 ELVES 类型的亚毫秒事件("精灵"),它们是闪电放电电磁脉冲前端与电离层下层相互作用的结果。每个事件都有一个特征性的环形辉光模式,并占据了探测器视野的很大一部分,而且单独通道中的信号具有一个明显峰值的不对称轮廓。峰值时间的分布包含放电定位和辉光高度的信息。在本文中,我们提出了一个用于重建 ELVES 事件的贝叶斯(概率)模型,该模型是在 PyMC-5 中使用概率编程方法实现的。以几个事件为例,展示了该模型确定放电位置的能力。概述了修改模型以恢复放电方向和完善辉光高度的方法。
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引用次数: 0
Modeling the Impact of Atomic Oxygen on Materials of Artificial Earth Satellites 模拟原子氧对人造地球卫星材料的影响
IF 0.6 4区 物理与天体物理 Q4 ASTRONOMY & ASTROPHYSICS Pub Date : 2024-06-17 DOI: 10.1134/s0010952524600409
L. S. Novikov, V. N. Chernik, E. N. Voronina, N. P. Chirskaya

Abstract

The paper describes a magnetoplasmodynamic accelerator and the laboratory facility based on it that have been developed at the Skobeltsyn Institute of Nuclear Physics of Moscow State University to simulate the impact of atomic oxygen in the Earth’s upper atmosphere on materials of low-orbit satellites. The simulation methodology for accelerated ground-based testing of spacecraft materials is described in detail. Some results of laboratory research and numerical modelling of polymeric materials destruction by atomic oxygen are presented.

摘要本文介绍了莫斯科国立大学斯科别尔琴核物理研究所开发的磁浆动力学加速器和基于该加速器的实验室设施,用于模拟地球高层大气中的原子氧对低轨道卫星材料的影响。详细介绍了航天器材料地面加速测试的模拟方法。介绍了实验室研究和原子氧破坏聚合材料的数值建模的一些结果。
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引用次数: 0
UV Microbursts in the Auroral Zone Measured by a Multichannel Imaging Photometer 用多通道成像光度计测量极光带的紫外线微爆
IF 0.6 4区 物理与天体物理 Q4 ASTRONOMY & ASTROPHYSICS Pub Date : 2024-06-17 DOI: 10.1134/s0010952524600367
K. D. Shchelkanov, A. A. Belov, P. A. Klimov, V. D. Nikolaeva, R. E. Saraev, S. A. Sharakin

Abstract

In the autumn of 2021, a multichannel imaging photometer of the Pulsating Aurora Imaging Photometer System was installed at the Verkhnetulomsky Observatory. During the first season of operation (2021/2022), measurements were made over the course of 163 nights in three modes of temporal resolution: 2.5 μs, 320 μs, and 41 ms. The high temporal resolution makes it possible to investigate the fine temporal structure of the emission, which are short (less than 1 s) bursts of UV radiation, so-called “microbursts” that can be single or follow in series. The long-term series of microbursts registered on November 27–29, 2021, were analyzed. It is shown that the series of bursts have a complex temporal structure, individual bursts have several peaks with intervals of 100–400 ms, the intervals between bursts are of the order of 1 s, and they appear in packs lasting from several seconds to minutes. The series appear both in quiet geomagnetic conditions and during substorms; the frequency and amplitude of bursts in the second case are significantly larger.

摘要 2021 年秋季,在上努洛姆斯基天文台安装了脉冲极光成像光度计系统的多通道成像光度计。在第一个运行季节(2021/2022 年),共进行了 163 个夜晚的测量,有三种时间分辨率模式:2.5 μs、320 μs 和 41 ms。高时间分辨率使得研究发射的精细时间结构成为可能,这些发射是紫外线辐射的短脉冲(小于 1 秒),即所谓的 "微爆",可以是单个的,也可以是串联的。我们分析了 2021 年 11 月 27-29 日记录的长期系列微暴。结果表明,微暴系列具有复杂的时间结构,单个微暴有几个间隔为 100-400 毫秒的峰值,微暴之间的间隔为 1 秒,它们成群出现,持续时间从几秒到几分钟不等。这些脉冲串既出现在安静的地磁条件下,也出现在亚暴期间;在第二种情况下,脉冲串的频率和振幅要大得多。
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引用次数: 0
Geomagnetic Pulsations in the 1–4 mHz Frequency Range (Pc5/Pi3) in the Magnetotail. Internal and Extramagnetospheric Sources 磁尾 1-4 mHz 频率范围 (Pc5/Pi3) 内的地磁脉冲。磁层内部和外部来源
IF 0.6 4区 物理与天体物理 Q4 ASTRONOMY & ASTROPHYSICS Pub Date : 2024-06-17 DOI: 10.1134/s0010952524600355
N. V. Yagova, N. S. Evsina

Abstract

Spectral and spatial parameters of nonstorm Pc5/Pi3 geomagnetic pulsations in the geomagnetic tail are studied based on magnetic measurements on Cluster satellites under different conditions in the interplanetary medium. Both the average values of the magnetic field components in front of the bow shock and fluctuations in the pulsations’ frequency range are considered. Special attention is paid to the conditions of small amplitudes of fluctuations (“zero” perturbation) in order to localize the source of pulsations starting under these conditions. For this purpose, simultaneous data from two satellites located on one or different sides of the magnetopause are used. It is shown that, along with a decrease in the amplitude of fluctuations in front of the bow shock, the amplitude and spatial scale of fluctuations in the magnetosheath change and the coherence between fluctuations on different sides of the magnetopause decreases sharply. This allows us to conclude that the pulsations occurring in the geomagnetic tail under “zero” level fluctuations in front of the bow shock are an intramagnetospheric phenomenon weakly related to the processes beyond the magnetopause.

摘要 根据星簇卫星在行星际介质中不同条件下的磁测量结果,研究了地磁尾部非风暴 Pc5/Pi3 地磁脉动的光谱和空间参数。既考虑了弓形冲击前磁场分量的平均值,也考虑了脉动频率范围内的波动。特别关注了小振幅波动("零 "扰动)的条件,以便定位在这些条件下开始的脉冲源。为此,使用了位于磁层顶一侧或不同侧的两颗卫星的同步数据。结果表明,随着弓形冲击前波动振幅的减小,磁鞘中波动的振幅和空间尺度也发生了变化,磁极线不同侧波动之间的一致性急剧下降。由此我们可以得出结论,在弓形冲击前的 "零 "级波动下,地磁尾部出现的脉动是一种磁层内现象,与磁极面以外的过程关系不大。
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引用次数: 0
Estimating Expected Radiation Doses in a Flight to the Moon Using Low-Thrust Engines 估算使用低推力发动机飞往月球的预期辐射剂量
IF 0.6 4区 物理与天体物理 Q4 ASTRONOMY & ASTROPHYSICS Pub Date : 2024-06-17 DOI: 10.1134/s0010952524600380
A. N. Turundaevskiy, N. I. Nikolaeva, A. D. Panov, M. V. Podzolko, D. M. Podorozhny, K. R. Rakhimchanova

Abstract

Estimates of doses inside the spacecraft were carried out for flights to the Moon using low-thrust engines. The characteristics of the trajectory, which is significantly different from the Hohmann trajectory, are taken into account. Such a trajectory causes a long stay inside the radiation belts, which can cause disruptions in the operation of onboard equipment. It turned out that, during long-term transportation of food products, they may be damaged under the influence of radiation. This is extremely important in the case of the creation of habitable stations on the Moon surface or near-Moon orbit. The presented results can be used in the preparation of future space experiments.

摘要 对使用低推力发动机飞往月球的航天器内的剂量进行了估计。考虑到了与霍曼轨迹明显不同的轨迹特点。这种轨迹会导致在辐射带内长时间停留,从而可能导致机载设备运行中断。事实证明,在长期运输食品的过程中,食品可能会在辐射的影响下受损。这对于在月球表面或近月轨道上建立宜居站极为重要。所提供的结果可用于准备未来的空间实验。
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引用次数: 0
Solar Activity in the Last 20 Years and a Forecast of the 25th Solar Cycle 过去 20 年的太阳活动和第 25 个太阳周期的预测
IF 0.6 4区 物理与天体物理 Q4 ASTRONOMY & ASTROPHYSICS Pub Date : 2024-06-17 DOI: 10.1134/s0010952524600392
Y. I. Stozhkov, V. P. Okhlopkov

Abstract

Experimental data on solar activity (sunspot number, induction of solar polar magnetic field Bp, and others), characteristics of interplanetary space, and cosmic ray fluxes testify that the Sun has entered a deep minimum of its activity similar to the Dalton minimum. An almost functional relationship was found between maximum values of Bpmax observed in the solar activity minimum of the 11-year cycle and the next sunspot maximum. Based on this relationship, a simple method of forecasting maximum number of sunspots Rzmax and time course Rz(t) was developed. A forecast of the 25th solar cycle is given.

摘要有关太阳活动(太阳黑子数、太阳极磁场感应Bp等)、行星际空间特征和宇宙射线通量的实验数据证明,太阳已进入其活动的深度极小期,类似于道尔顿极小期。在 11 年周期的太阳活动最低点观测到的 Bpmax 最大值与下一个太阳黑子最大值之间几乎存在函数关系。根据这种关系,开发了一种预测太阳黑子最大数量 Rzmax 和时间过程 Rz(t) 的简单方法。给出了第 25 个太阳周期的预报。
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引用次数: 0
Modeling Arrival Time of Coronal Mass Ejections to Near-Earth Orbit Using Coronal Dimming Parameters 利用日冕调暗参数模拟日冕物质抛射到达近地轨道的时间
IF 0.6 4区 物理与天体物理 Q4 ASTRONOMY & ASTROPHYSICS Pub Date : 2024-06-17 DOI: 10.1134/s0010952524600422
A. A. Vakhrusheva, K. B. Kaportseva, Yu. S. Shugay, V. E. Eremeev, V. V. Kalegaev

Abstract

The paper demonstrates results of modeling arrival time of coronal mass ejections (CME) to near-Earth space with parameters of coronal dimmings in 2010–2018. We use drag-based model (DBM) for CME propagation and empirical model for quasi-stationary solar wind streams. We compared the ICME arrival time and speed forecast for events with coronal source in the central region of the solar disk based on the CME initial speed using (1) CACTus database; (2) dimming maximum intensity drop from Solar Demon database to calculate the initial speed of the CME. Results show that the methods result in similar errors. To study the possibility of predicting ICME, for which a CME may not be observed in the coronagraph for some reason, modeling of ICME was carried out using dimming parameters. In 43% of cases, ICME arrival time were forecasted with an accuracy of 24 h using parameters of dimmings in the central region of solar disk that could not be associated with any CMEs.

摘要 本文展示了 2010-2018 年日冕物质抛射(CME)到达近地空间时间的建模结果以及日冕暗淡参数。我们使用基于阻力的模型(DBM)来计算日冕物质抛射的传播,并使用经验模型来计算准静止太阳风流。我们使用(1)CACTus 数据库;(2)Solar Demon 数据库中的日冕最大强度下降来计算 CME 的初始速度,并根据 CME 的初始速度对日冕源位于太阳圆盘中心区域的事件的 ICME 到达时间和速度预测进行了比较。结果表明,这两种方法产生的误差相似。为了研究是否有可能预测因某些原因而无法在日冕仪中观测到的偶极体,利用调光参数对偶极体进行了建模。在43%的情况下,利用太阳圆盘中心区域的调光参数预报集成流到达时间的精确度为24小时,而这些太阳圆盘中心区域与任何CME都不相关。
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引用次数: 0
On Consistent Dynamics of the Magnetic Field and Relativistic Electron Fluxes in the Geostationary Orbit Region 论地球静止轨道区域磁场和相对论电子通量的一致动力学
IF 0.6 4区 物理与天体物理 Q4 ASTRONOMY & ASTROPHYSICS Pub Date : 2024-06-17 DOI: 10.1134/s0010952524600410
N. A. Vlasova, V. V. Kalegaev

Abstract

The paper presents the results of studying the dynamics of the magnetic field and electron fluxes of the Earth’s outer radiation belt with an energy of >2 MeV according to the GOES-15 geostationary satellite during a fairly long period (October 16, 2016 to February 16, 2017) of moderate and weak magnetospheric activity caused by the arrival of a sequence of high-speed solar wind streams. The main variations in the electron flux in the geostationary orbit are caused by the movement, deceleration and acceleration of particles in the outer radiation belt of the Earth under the influence of geomagnetic activity. The results of a comparative analysis of variations in electron fluxes and components of the magnetospheric field testify to the predominant influence of the magnitude and structure of the magnetospheric field on the dynamics of relativistic electron fluxes in the outer radiation belt. Changes in the components of the magnetospheric magnetic field and in electron fluxes are results of a single process that occurs together with changes in the magnetosphere as a whole.

摘要本文介绍了在一连串高速太阳风流到来导致的中等和弱磁层活动的相当长时期(2016年10月16日至2017年2月16日),根据GOES-15静止卫星对地球外辐射带能量为2 MeV的磁场和电子通量的动态研究结果。地球静止轨道上电子通量的主要变化是由地磁活动影响下地球外辐射带中粒子的运动、减速和加速引起的。对电子通量的变化和磁层磁场成分进行比较分析的结果证明,磁层磁场的大小和结构对外辐射带中相对论电子通量的动态有主要影响。磁层磁场成分和电子通量的变化是与整个磁层的变化一起发生的单一过程的结果。
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引用次数: 0
A Multipole Representation for the Gravitational Field of Asteroid (433) Eros 小行星 (433) 爱神号引力场的多极表示法
IF 0.6 4区 物理与天体物理 Q4 ASTRONOMY & ASTROPHYSICS Pub Date : 2024-06-04 DOI: 10.1134/s0010952524600240
A. A. Burov, V. I. Nikonov

Abstract

For asteroid (433) Eros, a multipole representation of the gravitational potential is determined up to multipoles of the fourth order. The obtained expression for the potential is used in constructing the areas of possible motion of the spacecraft in the vicinity of the celestial body under consideration.

摘要 针对小行星(433)厄洛斯,确定了重力势能的多极表示法,最高可达四阶多极。得到的引力势表达式用于构建航天器在所考虑的天体附近的可能运动区域。
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引用次数: 0
A Model Problem of Motion along the Handrail Constraint by a Solar Sail 太阳帆沿扶手约束运动的模型问题
IF 0.6 4区 物理与天体物理 Q4 ASTRONOMY & ASTROPHYSICS Pub Date : 2024-06-04 DOI: 10.1134/s0010952524600276
V. S. Vaskova, A. V. Rodnikov

Abstract

The paper considers the possibility of cargo relocation without fuel costs along a tether connecting two heavy space stations by a spacecraft with a controlled solar sail. The spacecraft’s relative motion dynamics is studied within the context of a model problem that assumes that the stations describe one heliocentric orbit, the solar sail is a perfect reflective flat panel, and the tether realizes an ideal unilateral handrail constraint that restricts the spacecraft relative motion to an ellipsoid. It is noted that, if the distance between stations is sufficiently small and the ratio of the sail area to the spacecraft mass is on the same order of magnitude as in already-implemented space missions, solar radiation is the main factor that influences the spacecraft’s motion in the orbital frame of reference. The problem of searching a set of pairs of points, between which relocation with a permanently oriented sail is possible, is solved for the pairs that belong to the intersection of the ellipsoid boundary and the plane of the stations’ orbit. The duration of the spacecraft relocation between the ellipsoid poles is estimated for the case of the sail oriented orthogonally to the solar rays. Also, the duration of the fastest relocation between poles is computed using special sail orientation control laws, including the case of zero initial and final velocities.

摘要 本文考虑了通过带有可控太阳帆的航天器沿连接两个重型空间站的系绳进行无燃料成本的货物搬迁的可能性。该模型假定空间站描述一个日心轨道,太阳帆是一个完美的反射平板,系绳实现了一个理想的单边扶手约束,将航天器的相对运动限制在一个椭圆形内。据指出,如果站点之间的距离足够小,并且帆板面积与航天器质量的比例与已执行的空间飞行任务的比例相同,太阳辐射就是影响航天器在轨道参照系中运动的主要因素。在椭球边界和空间站轨道平面的交点上寻找一组点对,在这些点对之间用永久定向帆板进行重新定位是可能的,这个问题是针对这些点对解决的。在帆板方向与太阳光线正交的情况下,对航天器在椭球体两极之间重新定位的持续时间进行了估算。此外,还利用特殊的帆板定向控制法计算了两极之间最快重新定位的持续时间,包括初始速度和最终速度为零的情况。
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引用次数: 0
期刊
Cosmic Research
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