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Deep learning-based prediction approaches of binary star parameters 基于深度学习的双星参数预测方法
IF 2.7 3区 物理与天体物理 Q2 ASTRONOMY & ASTROPHYSICS Pub Date : 2024-12-19 DOI: 10.1007/s10686-024-09969-1
Islam Helmy, Mohamed Ismail, Doaa Eid

The precise computation of binary star parameters is crucial for understanding their formation, evolution, and dynamics. However, large datasets of available astronomical measurements require substantial effort for computing using classic astronomical methods. Deep learning (DL) is a promising approach that can provide a proper solution for estimating the parameters and reducing the burden of the lengthy procedures of astronomical computations. This study proposes two DL-based models for estimating binary star parameters. The first is the well-known multi-layer perceptron (MLP) model, whereas the second is based on long short-term memory (LSTM). We rely on databases, such as large sky multi-object fiber spectroscopic telescope area (LAMOST), to train the proposed models. In addition, we verify the training ratio showing that the performance of both models at a low training ratio of (30%), based on the mean square error (MSE), results in acceptable performance. Furthermore, the LSTM-based DL model outperforms the conventional MLP for different training ratios. Eventually, the two models have superiority compared to the benchmark methods.

双星参数的精确计算对于理解它们的形成、演化和动力学是至关重要的。然而,大量可用的天文测量数据集需要大量的工作来使用经典的天文方法进行计算。深度学习(Deep learning, DL)是一种很有前途的方法,它可以为估计参数和减少冗长的天文计算过程的负担提供适当的解决方案。本研究提出了两种基于dl的双星参数估计模型。第一个是众所周知的多层感知器(MLP)模型,而第二个是基于长短期记忆(LSTM)的模型。我们依靠数据库,如大型天空多目标光纤光谱望远镜区域(LAMOST),来训练所提出的模型。此外,我们验证了训练比,表明两个模型在基于均方误差(MSE)的低训练比(30%)下的性能都是可以接受的。此外,基于lstm的深度学习模型在不同的训练比率下都优于传统的MLP模型。最终,这两种模型与基准方法相比具有优势。
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引用次数: 0
Preliminary design and development of the module back-end electronics for the large area detector onboard the eXTP mission 初步设计和开发用于 eXTP 飞行任务搭载的大面积探测器的模块后端电子设备
IF 2.7 3区 物理与天体物理 Q2 ASTRONOMY & ASTROPHYSICS Pub Date : 2024-12-17 DOI: 10.1007/s10686-024-09974-4
Hao Xiong, Jörg Bayer, Andrea Santangelo, Marco Feroci, Ettore Del Monte, Alejandro Guzman, Paul Hedderman, Gabriele Minervini, Samuel Pliego, Andreas Putz, Chris Tenzer, Alessio Trois, Xianqi Wang

The Large Area Detector (LAD) is one of the science payloads of the enhanced X-ray Timing and Polarimetry (eXTP) mission. The LAD is a spectral-timing instrument with a broad energy response, covering a range from 2 to 30 keV, a good timing resolution of better than 10 µs, and an expected energy resolution of 260 eV at 6 keV. The LAD consists of 640 large-area multi-anode Silicon Drift Detectors (SDDs). Given the large number of detectors, the LAD uses a modular design. Each module comprises sixteen detectors, and each detector is equipped with dedicated Front-End Electronics (FEE), interfacing with two separate Module Back-End Electronics (MBEEs). Each MBEE is designed to process the data from 1,792 anode channels in 8 FEEs (224 anode channels per FEE), performing the energy reconstruction and time tagging for X-ray events. The MBEE uses the European Field Programmable Gate Array (FPGA) from NanoXplore™, based on a pipeline concept, which reduces dead time, making the LAD suitable for higher flux X-ray detection, and it can handle a sustained flux of >500 mCrab and a continuous flux of >15 Crab for up to 300 minutes (Feroci et al. 2018). Additionally, the MBEE serves as the central hub for configuring the module’s electronics, including the FEEs, the Power Supply Unit (PSU), and the MBEE itself, and it is also responsible for collecting housekeeping data to monitor the system’s status. The prototype MBEE was designed, manufactured, and programmed with FPGA firmware using VHDL. The basic functional test was conducted in this paper, and the results indicated that the MBEE could be operated in different modes to perform the functions mentioned above. Analysis and testing show that it can transmit event packets-containing timing tag, event type, position ID, and energy information-at a baud rate of 2 Mbps with an event loss fraction of 1.5%.

大面积探测器(LAD)是增强型x射线定时和偏振测量(eXTP)任务的科学有效载荷之一。LAD是一种具有广泛能量响应的光谱定时仪器,覆盖范围从2到30 keV,定时分辨率优于10µs,预期能量分辨率为260 eV在6 keV。LAD由640个大面积多阳极硅漂移检测器(sdd)组成。考虑到大量的探测器,LAD采用模块化设计。每个模块包括16个探测器,每个探测器配备专用前端电子设备(FEE),与两个独立的模块后端电子设备(MBEEs)接口。每个MBEE设计用于处理来自8个FEE(每个FEE 224个阳极通道)的1,792个阳极通道的数据,执行x射线事件的能量重建和时间标记。MBEE使用NanoXplore™的欧洲现场可编程门阵列(FPGA),基于管道概念,减少了死区时间,使LAD适用于更高通量的x射线检测,并且它可以处理>;500 mcab的持续通量和>;15 Crab的连续通量长达300分钟(Feroci et al. 2018)。此外,MBEE还充当配置模块电子设备(包括FEEs、电源供应单元(PSU)和MBEE本身)的中心集线器,它还负责收集管理数据以监控系统状态。MBEE原型机的设计、制造和编程采用FPGA固件,使用VHDL进行。本文进行了基本功能测试,结果表明MBEE可以在不同的模式下运行,以实现上述功能。分析和测试表明,它可以以2mbps的波特率传输包含时间标签、事件类型、位置ID和能量信息的事件数据包,事件丢失率为1.5%。
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引用次数: 0
Galaxy formation and symbiotic evolution with the inter-galactic medium in the age of ELT-ANDES ELT-ANDES时代星系形成与星系间介质共生演化
IF 2.7 3区 物理与天体物理 Q2 ASTRONOMY & ASTROPHYSICS Pub Date : 2024-12-09 DOI: 10.1007/s10686-024-09967-3
Valentina D’Odorico, James S. Bolton, Lise Christensen, Annalisa De Cia, Erik Zackrisson, Aron Kordt, Luca Izzo, Jiangtao Li, Roberto Maiolino, Alessandro Marconi, Philipp Richter, Andrea Saccardi, Stefania Salvadori, Irene Vanni, Chiara Feruglio, Michele Fumagalli, Johan P. U. Fynbo, Pasquier Noterdaeme, Polychronis Papaderos, Céline Péroux, Aprajita Verma, Paolo Di Marcantonio, Livia Origlia, Alessio Zanutta

High-resolution absorption spectroscopy toward bright background sources has had a paramount role in understanding early galaxy formation, the evolution of the intergalactic medium and the reionisation of the Universe. However, these studies are now approaching the boundaries of what can be achieved at ground-based 8-10m class telescopes. The identification of primeval systems at the highest redshifts, within the reionisation epoch and even into the dark ages, and of the products of the first generation of stars and the chemical enrichment of the early Universe, requires observing very faint targets with a signal-to-noise ratio high enough to detect very weak spectral signatures. In this paper, we describe the giant leap forward that will be enabled by ANDES, the high-resolution spectrograph for the ELT, in these key science fields, together with a brief, non-exhaustive overview of other extragalactic research topics that will be pursued by this instrument, and its synergistic use with other facilities that will become available in the early 2030s.

对明亮背景源的高分辨率吸收光谱在理解早期星系形成、星系间介质的演化和宇宙的再电离方面起着至关重要的作用。然而,这些研究现在正在接近地面8-10米级望远镜所能达到的极限。在再电离时期甚至进入黑暗时代的最高红移的原始系统的识别,以及第一代恒星的产物和早期宇宙的化学富集,需要观察非常微弱的目标,其信噪比足够高,可以探测到非常微弱的光谱特征。在本文中,我们描述了ELT的高分辨率光谱仪ANDES将在这些关键科学领域实现的巨大飞跃,并简要概述了该仪器将追求的其他河外研究主题,以及它与将在2030年代初可用的其他设施的协同使用。
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引用次数: 0
High strehl and high contrast for the ELT instrument METIS ELT 仪器 METIS 的高条纹和高对比度
IF 2.7 3区 物理与天体物理 Q2 ASTRONOMY & ASTROPHYSICS Pub Date : 2024-11-29 DOI: 10.1007/s10686-024-09968-2
Markus Feldt, Thomas Bertram, Carlos Correia, Olivier Absil, M. Concepción Cárdenas Vázquez, Hugo Coppejans, Martin Kulas, Andreas Obereder, Gilles Orban de Xivry, Silvia Scheithauer, Horst Steuer

The Mid-infrared ELT Imager and Spectrograph (METIS) is a first-generation instrument for the Extremely Large Telescope (ELT), Europe’s next-generation 39 m ground-based telescope for optical and infrared wavelengths, which is currently under construction at the European Southern Observatory (ESO) site at Cerro Armazones in Chile. METIS will offer diffraction-limited imaging, low- and medium-resolution slit spectroscopy, and coronagraphy for high-contrast imaging between 3 and 13 microns, as well as high-resolution integral field spectroscopy between 3 and 5 microns. The main METIS science goals are the detection and characterisation of exoplanets, the investigation of proto-planetary disks, and the formation of planets. The Single-Conjugate Adaptive Optics (SCAO) system corrects atmospheric distortions and is thus essential for diffraction-limited observations with METIS. SCAO will be used for all observing modes, with high-contrast imaging imposing the most demanding requirements on its performance. The Final Design Review (FDR) of METIS took place in the fall of 2022; the development of the instrument, including its SCAO system, has since entered the Manufacturing, Assembly, Integration and Testing (MAIT) phase. Numerous challenging aspects of an ELT Adaptive Optics (AO) system are addressed in the mature designs for the SCAO control system and the SCAO hardware module: the complex interaction with the telescope entities that participate in the AO control, wavefront reconstruction with a fragmented and moving pupil, secondary control tasks to deal with differential image motion, non-common path aberrations and mis-registration. A K-band pyramid wavefront sensor and a GPU-based Real-Time Computer (RTC), tailored to the needs of METIS at the ELT, are core components. This current paper serves as a natural sequel to our previous work presented in Hippler et al. (2018). It reflects all the updates that were implemented between the Preliminary Design Review (PDR) and FDR, and includes updated performance estimations in terms of several key performance indicators, including achieved contrast curves. We outline all important design decisions that were taken, and present the major challenges we faced and the main analyses carried out to arrive at these decisions and eventually the final design. We also elaborate on our testing and verification strategy, and, last not least, comprehensively present the full design, hardware and software in this paper to provide a single source of reference which will remain valid at least until commissioning.

中红外 ELT 成像仪和摄谱仪(METIS)是超大望远镜(ELT)的第一代仪器,ELT 是欧洲下一代 39 米地基光学和红外望远镜,目前正在智利 Cerro Armazones 的欧洲南方天文台(ESO)建造。METIS 将提供衍射极限成像、低分辨率和中分辨率狭缝光谱分析、用于 3 至 13 微米高对比度成像的日冕仪以及 3 至 5 微米高分辨率积分场光谱分析。METIS 的主要科学目标是探测系外行星并确定其特征,研究原行星盘和行星的形成。单共轭自适应光学系统(SCAO)可纠正大气畸变,因此对 METIS 的衍射极限观测至关重要。SCAO 将用于所有观测模式,其中高对比度成像对其性能要求最高。METIS 的最终设计审查(FDR)于 2022 年秋季进行;此后,包括 SCAO 系统在内的仪器开发进入了制造、组装、集成和测试(MAIT)阶段。ELT自适应光学(AO)系统的许多挑战性方面都在SCAO控制系统和SCAO硬件模块的成熟设计中得到了解决:与参与AO控制的望远镜实体之间的复杂交互、碎片和移动瞳孔的波前重建、处理差分图像运动的辅助控制任务、非共同路径像差和错误配准。根据 ELT METIS 的需要定制的 K 波段金字塔波前传感器和基于 GPU 的实时计算机(RTC)是核心组件。本文是我们在 Hippler 等人(2018 年)中介绍的先前工作的自然续篇。它反映了在初步设计审查(PDR)和最终设计审查(FDR)之间实施的所有更新,并包括几个关键性能指标的最新性能估计,包括实现的对比曲线。我们概述了做出的所有重要设计决定,并介绍了我们面临的主要挑战以及为做出这些决定和最终设计而进行的主要分析。我们还阐述了我们的测试和验证策略,最后也是最重要的一点是,我们在本文中全面介绍了完整的设计、硬件和软件,以提供一个单一的参考源,至少在试运行之前一直有效。
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引用次数: 0
A machine learning method for predicting telescope cycle time applied to the Cerro Murphy Observatory 应用于 Cerro Murphy 天文台的预测望远镜周期时间的机器学习方法
IF 2.7 3区 物理与天体物理 Q2 ASTRONOMY & ASTROPHYSICS Pub Date : 2024-11-28 DOI: 10.1007/s10686-024-09970-8
Mirosław Kicia, Mikołaj Kałuszyński, Marek Górski, Rolf Chini, Grzegorz Pietrzyński

Telescope cycle time estimation is one of the basic issues of observational astronomy. There are not many tools that help to calulate the cycle time for multiple telescopes with multiple instruments. This work presents a new tool for determing the observation time; it was applied at the Cerro Murphy Observatory (OCM) but can be used at any other observatory. The Machine Learning (ML) method was implied, resulting in a fully automatic software module that works without any user intervention. We propose a polynomial multiple regression method and demonstrate all steps to build a reliable ML model like data collecting, data cleaning, model training and error evaluation in relation to the implementation in the observatory software. The method was designed to work for different telescopes with several instruments. Accuracy analysis and the assessment of model errors were based on real data from telescopes, proving the usefulness of the presented method. Error evaluation shows that for 84.2 % of nights, the prediction error in operation time prediction does not exceed 2 %. Converted into a 10-hour observation night, 2 % corresponds to an error of no more than 12 minutes. The described model is already working at the OCM and optimizes the efficiency of the observations.

望远镜周期时间估算是观测天文学的基本问题之一。目前还没有很多工具可以帮助计算带有多种仪器的多台望远镜的周期时间。这项工作提出了一种确定观测时间的新工具;它应用于 Cerro Murphy 天文台(OCM),但也可用于任何其他天文台。我们采用了机器学习(ML)方法,从而开发出一个无需用户干预的全自动软件模块。我们提出了一种多项式多元回归方法,并演示了建立可靠的 ML 模型的所有步骤,如数据收集、数据清理、模型训练和与天文台软件实施相关的误差评估。该方法适用于配备多种仪器的不同望远镜。精度分析和模型误差评估以望远镜的真实数据为基础,证明了该方法的实用性。误差评估显示,在 84.2% 的夜晚,运行时间预测误差不超过 2%。换算成每晚 10 小时的观测时间,2% 相当于误差不超过 12 分钟。所述模型已在光学测量中心投入使用,并优化了观测效率。
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引用次数: 0
CNNCat: categorizing high-energy photons in a Compton/Pair telescope with convolutional neural networks CNNCat:利用卷积神经网络对康普顿/派尔望远镜中的高能光子进行分类
IF 2.7 3区 物理与天体物理 Q2 ASTRONOMY & ASTROPHYSICS Pub Date : 2024-11-04 DOI: 10.1007/s10686-024-09965-5
Jan Peter Lommler, Uwe Gerd Oberlack

A Compton/Pair telescope, designed to provide spectral resolved images of cosmic photons from sub-MeV to GeV energies, records a wealth of data in a combination of tracking detector and calorimeter. Onboard event classification can be required to decide on which data to down-link with priority, given limited data-transfer bandwidth. Event classification is also the first and one of the most crucial steps in reconstructing data. Its outcome determines the further handling of the event, i.e., the type of reconstruction (Compton, pair) or, possibly, the decision to discard it. Errors at this stage result in misreconstruction and loss of source information. We present a classification algorithm driven by a Convolutional Neural Network. It provides classification of the type of electromagnetic interaction, based solely on low-level detector data. We introduce the task, describe the architecture and the dataset used, and present the performance of this method in the context of the proposed (e-)ASTROGAM and similar telescopes.

康普顿/Pair 望远镜的设计目的是提供从亚兆电子伏到 GeV 能量的宇宙光子的光谱分辨图像,它在跟踪探测器和热量计的组合中记录了大量数据。在数据传输带宽有限的情况下,需要进行星载事件分类,以决定优先下链哪些数据。事件分类也是重建数据的第一步,也是最关键的一步。它的结果决定了对事件的进一步处理,即重建类型(康普顿,对),或可能决定丢弃事件。这一阶段的错误会导致重建错误和源信息丢失。我们提出了一种由卷积神经网络驱动的分类算法。它完全基于低级探测器数据,对电磁相互作用的类型进行分类。我们介绍了任务,描述了所使用的架构和数据集,并在拟议的 (e-)ASTROGAM 和类似望远镜的背景下展示了该方法的性能。
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引用次数: 0
Reflectivity test method of x-ray optics at the 100-m x-ray test facility 100 米 X 射线测试设备的 X 射线光学器件反射率测试方法
IF 2.7 3区 物理与天体物理 Q2 ASTRONOMY & ASTROPHYSICS Pub Date : 2024-11-01 DOI: 10.1007/s10686-024-09964-6
Yuxuan Zhu, Zijian Zhao, Dongjie Hou, Yanji Yang, Xiongtao Yang, Yifan Zhang, Kaiji Wu, Fei Ding, Dong Xie, Yupeng Xu, Bo Wang, Langping Wang, Yusa Wang

Reflectivity is a key topic in soft X-ray optics research and serves as the foundation for studying the performance of the optics for X-ray astronomical satellites. Since its establishment, the 100-m X-ray Test Facility (100XF) has been continuously developing various testing functionalities, including calibration of timing, imaging, and energy response. This paper provides a detailed description of the X-ray optics reflectivity test method based on the 100XF, which can be applied to various grazing incident X-ray optics, including Wolter-I and lobster-eye types, significantly expanding the application scope of the 100XF. A flat mirror sample (SiO(_{text{2 }}) coated on a Si wafer) is tested. Results of the variation of reflectivity with angle @ C-K(alpha ) (0.28 keV), Al-K(alpha )(1.49 keV), and Ti-K(alpha )(4.50 keV) are presented in the description. The reflectivity test method has also been applied to the coating reflectivity study of the enhanced X-ray Timing and Polarimetry Mission (eXTP) mirror. At the same time, a new method utilizing the continuum spectrum of bremsstrahlung was carried out to study the continuous variation of reflectivity with energy, greatly improving efficiency compared to traditional methods, and all the results show a good agreement with the theoretical values. The deviation between the test and theoretical values in the low-energy range (1.5-8.0 keV) is less than 10%.

反射率是软 X 射线光学研究的关键课题,也是研究 X 射线天文卫星光学性能的基础。自建立以来,100 米 X 射线测试设备(100XF)一直在不断开发各种测试功能,包括定时校准、成像和能量响应。本文详细介绍了基于 100XF 的 X 射线光学器件反射率测试方法,该方法可应用于各种掠入射 X 射线光学器件,包括 Wolter-I 和龙虾眼类型,大大扩展了 100XF 的应用范围。测试了一个平面镜样品(在硅晶片上镀有 SiO(_{text{2 }}/)。描述中给出了反射率随角度变化的结果@ C-K(α ) (0.28 keV)、Al-K/(α ) (1.49 keV)和Ti-K/(α ) (4.50 keV)。该反射率测试方法还被应用于增强型 X 射线定时和偏振探测任务(eXTP)反射镜的涂层反射率研究。同时,利用轫致辐射连续谱的新方法研究了反射率随能量的连续变化,与传统方法相比大大提高了效率,所有结果均与理论值吻合。在低能量范围(1.5-8.0 keV)内,测试值与理论值的偏差小于 10%。
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引用次数: 0
Ground calibration and network of the first CATCH pathfinder 第一个 CATCH 探路者的地面校准和网络
IF 2.7 3区 物理与天体物理 Q2 ASTRONOMY & ASTROPHYSICS Pub Date : 2024-10-31 DOI: 10.1007/s10686-024-09963-7
Yiming Huang, Jingyu Xiao, Lian Tao, Shuang-Nan Zhang, Qian-Qing Yin, Yusa Wang, Zijian Zhao, Chen Zhang, Qingchang Zhao, Xiang Ma, Shujie Zhao, Heng Zhou, Xiangyang Wen, Zhengwei Li, Shaolin Xiong, Juan Zhang, Qingcui Bu, Jirong Cang, Dezhi Cao, Wen Chen, Siran Ding, Yanfeng Dai, Min Gao, Yang Gao, Huilin He, Shujin Hou, Dongjie Hou, Tai Hu, Guoli Huang, Yue Huang, Liping Jia, Ge Jin, Dalin Li, Jinsong Li, Panping Li, Yajun Li, Xiaojing Liu, Ruican Ma, Lingling Men, Xingyu Pan, Liqiang Qi, Liming Song, Xianfei Sun, Qingwen Tang, Liyuan Xiong, Yibo Xu, Sheng Yang, Yanji Yang, Yong Yang, Aimei Zhang, Wei Zhang, Yifan Zhang, Yueting Zhang, Donghua Zhao, Kang Zhao, Yuxuan Zhu

The Chasing All Transients Constellation Hunters (CATCH) space mission is focused on exploring the dynamic universe via X-ray follow-up observations of various transients. The first pathfinder of the CATCH mission, CATCH-1, was launched on June 22, 2024, alongside the Space-based multiband astronomical Variable Objects Monitor (SVOM) mission. CATCH-1 is equipped with narrow-field optimized Micro Pore Optics (MPOs) featuring a large effective area and incorporates four Silicon Drift Detectors (SDDs) in its focal plane. This paper presents the system calibration results conducted before the satellite integration. Utilizing the data on the performance of the mirror and detectors obtained through the system calibration, combined with simulated data, the ground calibration database can be established. Measuring the relative positions of the mirror and detector system, which were adjusted during system calibration, allows for accurate installation of the entire satellite. Furthermore, the paper outlines the operational workflow of the ground network post-satellite launch.

追逐所有瞬变天体星座猎手(CATCH)空间任务的重点是通过对各种瞬变天体进行X射线跟踪观测来探索动态宇宙。CATCH 任务的第一个探路者 CATCH-1 于 2024 年 6 月 22 日与天基多波段天文变星监测器(SVOM)任务同时发射。CATCH-1 配备了具有大有效面积的窄场优化微孔光学器件(MPO),并在焦平面上安装了四个硅漂移探测器(SDD)。本文介绍了卫星集成前进行的系统校准结果。利用系统校准获得的反射镜和探测器性能数据,结合模拟数据,可以建立地面校准数据库。通过测量在系统校准过程中调整的反射镜和探测器系统的相对位置,可以准确安装整个卫星。此外,论文还概述了卫星发射后地面网络的运行工作流程。
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引用次数: 0
Simulations and machine learning models for cosmic-ray short-term variations and test-mass charging on board LISA 宇宙射线短期变化模拟和机器学习模型以及 LISA 上的测试质量充电
IF 2.7 3区 物理与天体物理 Q2 ASTRONOMY & ASTROPHYSICS Pub Date : 2024-10-30 DOI: 10.1007/s10686-024-09962-8
Mattia Villani, Federico Sabbatini, Andrea Cesarini, Michele Fabi, Catia Grimani

Energetic particles of galactic and solar origin charge the metal free-falling test masses (TMs) of the interferometers for gravitational wave detection in space. The deposited charge couples with stray electric fields thus generating spurious Coulomb forces between the TMs and the electrode housing that limit the interferometer sensitivity. Long-term and short-term galactic cosmic-ray variations are strongly energy-dependent and the TM charging varies with particle energy distribution. We propose three different approaches involving Monte Carlo simulations and machine learning models in comparison to particle transport with the Parker equation to study the recurrent modulation of energy spectra of galactic particles ascribable to the passage of high-speed solar wind streams. The transit of interplanetary counterparts of coronal mass ejections modifies the effects of high-speed streams. This work aims at better understanding the energy-dependence of galactic cosmic-ray short-term variations for the Laser Interferometer Space Antenna (LISA), the first interferometer for gravitational wave detection in space, starting from lessons learned with LISA Pathfinder. The outcomes of our models will be used to assess the TM charging during the time LISA will remain in orbit around the Sun.

来自银河系和太阳的高能粒子会给用于空间引力波探测的干涉仪的金属自由落体测试块(TMs)充电。沉积电荷与杂散电场耦合,从而在 TM 和电极外壳之间产生虚假的库仑力,限制了干涉仪的灵敏度。银河宇宙射线的长期和短期变化与能量密切相关,TM 电荷随粒子能量分布而变化。我们提出了三种不同的方法,包括蒙特卡罗模拟和机器学习模型,并与帕克方程的粒子传输进行比较,以研究高速太阳风流通过时银河系粒子能谱的反复调制。日冕物质抛射的行星际对应物的过境会改变高速流的影响。这项工作的目的是更好地理解银河宇宙射线短期变化的能量依赖性,为激光干涉仪空间天线(LISA)--第一个在空间探测引力波的干涉仪--服务,从 LISA 探路者吸取经验教训。我们的模型结果将用于评估 LISA 在绕太阳运行期间的 TM 充电情况。
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引用次数: 0
The ground calibration of the HERMES-Pathfinder payload flight models HERMES 探路者有效载荷飞行模型的地面校准
IF 2.7 3区 物理与天体物理 Q2 ASTRONOMY & ASTROPHYSICS Pub Date : 2024-10-26 DOI: 10.1007/s10686-024-09958-4
G. Dilillo, E. J. Marchesini, G. Baroni, G. Della Casa, R. Campana, Y. Evangelista, A. Guzmán, P. Hedderman, P. Bellutti, G. Bertuccio, F. Ceraudo, M. Citossi, D. Cirrincione, I. Dedolli, E. Demenev, M. Feroci, F. Ficorella, M. Fiorini, M. Gandola, M. Grassi, G. La Rosa, G. Lombardi, P. Malcovati, F. Mele, P. Nogara, A. Nuti, M. Perri, S. Pliego-Caballero, S. Pirrotta, S. Puccetti, I. Rashevskaya, F. Russo, G. Sottile, C. Tenzer, M. Trenti, S. Trevisan, A. Vacchi, G. Zampa, N. Zampa, F. Fiore

HERMES-Pathfinder is a space-borne mission based on a constellation of six nano-satellites flying in a low-Earth orbit. The 3U CubeSats, to be launched in early 2025, host miniaturized instruments with a hybrid Silicon Drift Detector/scintillator photodetector system, sensitive to both X-rays and gamma-rays. A seventh payload unit is installed onboard SpIRIT, an Australian-Italian nano-satellite developed by a consortium led by the University of Melbourne and launched in December 2023. The project aims at demonstrating the feasibility of Gamma-Ray Burst detection and localization using miniaturized instruments onboard nano-satellites. The HERMES flight model payloads were exposed to multiple well-known radioactive sources for spectroscopic calibration under controlled laboratory conditions. The analysis of the calibration data allows both to determine the detector parameters, necessary to map instrumental units to accurate energy measurements, and to assess the performance of the instruments. We report on these efforts and quantify features such as spectroscopic resolution and energy thresholds, at different temperatures and for all payloads of the constellation. Finally we review the performance of the HERMES payload as a photon counter, and discuss the strengths and the limitations of the architecture.

HERMES-Pathfinder 是一项空间飞行任务,由六颗在低地球轨道上飞行的超小型卫星组成。这些将于 2025 年初发射的 3U 立方体卫星载有小型化仪器,配备了混合硅漂移探测器/闪烁体光电探测器系统,对 X 射线和伽马射线都很敏感。第七个有效载荷单元安装在 SpIRIT 上,这是一颗澳大利亚和意大利联合研制的超小型卫星,由墨尔本大学牵头,将于 2023 年 12 月发射。该项目旨在证明利用纳卫星上的微型仪器进行伽马射线暴探测和定位的可行性。在受控实验室条件下,HERMES 飞行模型有效载荷暴露于多个知名放射源,以进行光谱校准。通过对校准数据的分析,既可以确定探测器参数(这是将仪器单位映射到精确能量测量所必需的),也可以评估仪器的性能。我们报告了这些工作,并量化了不同温度下和星座所有有效载荷的光谱分辨率和能量阈值等特征。最后,我们回顾了作为光子计数器的 HERMES 有效载荷的性能,并讨论了该结构的优势和局限性。
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Experimental Astronomy
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