Pub Date : 2025-06-16DOI: 10.1007/s10686-025-10013-z
Srivani K.S., Girish B.S., Mayuri S. Rao, Saurabh Singh, Adarsh Kumar Dash, Narendra S., Yash Agrawal, Keerthipriya S., Somashekar R., Madhavi S., Jacob Rajan, Udaya Shankar N., Seetha S.
Probing ReionizATion of the Universe using Signal from Hydrogen (PRATUSH) is a proposed space-based radiometer that aims to detect the sky-averaged 21-cm signal from Cosmic Dawn – a crucial phase in the cosmic evolution of the Universe. PRATUSH will operate in the frequency range of 55-110 MHz. PRATUSH will conduct observations in low earth orbit in its first phase, followed by lunar orbit in the second phase. Digital correlation spectrometer is an integral subsystem of PRATUSH radiometer, enabling phase switching, digitization and generation of sky spectrum. The digital correlation spectrometer for PRATUSH laboratory model features 10-bit analog-to-digital converters (ADCs) and a Virtex-6 Field Programmable Gate Array (FPGA). A Raspberry Pi 4 Model B-based single-board computer (SBC) serves as the master controller, real-time processor and data recorder, to minimize the power, mass and volume requirement of the laboratory model. This paper presents the implementation of the PRATUSH laboratory model digital receiver, challenges arising from the use of an SBC in place of a conventional computer, and demonstrates the performance of the spectrometer when integrated with the PRATUSH laboratory model analog receiver.
利用来自氢的信号探测宇宙再电离(PRATUSH)是一种拟议的天基辐射计,旨在探测来自宇宙黎明的平均21厘米的天空信号——宇宙演化的关键阶段。PRATUSH将在55-110 MHz的频率范围内工作。PRATUSH将在第一阶段进行近地轨道观测,然后在第二阶段进行月球轨道观测。数字相关光谱仪是PRATUSH辐射计不可或缺的子系统,可实现相位切换、天空光谱数字化和生成。PRATUSH实验室模型的数字相关光谱仪具有10位模数转换器(adc)和Virtex-6现场可编程门阵列(FPGA)。基于Raspberry Pi 4 Model b的单板计算机(SBC)作为主控制器,实时处理器和数据记录器,以最大限度地减少实验室模型的功率,质量和体积要求。本文介绍了PRATUSH实验室模型数字接收机的实现,使用SBC代替传统计算机所带来的挑战,并演示了与PRATUSH实验室模型模拟接收机集成时光谱仪的性能。
{"title":"An SBC-based controller and processor for the laboratory model of PRATUSH digital receiver","authors":"Srivani K.S., Girish B.S., Mayuri S. Rao, Saurabh Singh, Adarsh Kumar Dash, Narendra S., Yash Agrawal, Keerthipriya S., Somashekar R., Madhavi S., Jacob Rajan, Udaya Shankar N., Seetha S.","doi":"10.1007/s10686-025-10013-z","DOIUrl":"10.1007/s10686-025-10013-z","url":null,"abstract":"<div><p>Probing ReionizATion of the Universe using Signal from Hydrogen (PRATUSH) is a proposed space-based radiometer that aims to detect the sky-averaged 21-cm signal from Cosmic Dawn – a crucial phase in the cosmic evolution of the Universe. PRATUSH will operate in the frequency range of 55-110 MHz. PRATUSH will conduct observations in low earth orbit in its first phase, followed by lunar orbit in the second phase. Digital correlation spectrometer is an integral subsystem of PRATUSH radiometer, enabling phase switching, digitization and generation of sky spectrum. The digital correlation spectrometer for PRATUSH laboratory model features 10-bit analog-to-digital converters (ADCs) and a Virtex-6 Field Programmable Gate Array (FPGA). A Raspberry Pi 4 Model B-based single-board computer (SBC) serves as the master controller, real-time processor and data recorder, to minimize the power, mass and volume requirement of the laboratory model. This paper presents the implementation of the PRATUSH laboratory model digital receiver, challenges arising from the use of an SBC in place of a conventional computer, and demonstrates the performance of the spectrometer when integrated with the PRATUSH laboratory model analog receiver.</p></div>","PeriodicalId":551,"journal":{"name":"Experimental Astronomy","volume":"60 1","pages":""},"PeriodicalIF":2.2,"publicationDate":"2025-06-16","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"145143711","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":3,"RegionCategory":"物理与天体物理","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Pub Date : 2025-06-14DOI: 10.1007/s10686-025-10011-1
Drew M. Miles, Ross McCurdy, Michael Labella, Randall L. McEntaffer, Fabien Grisé, Jake McCoy, James H. Tutt
The Rockets for Extended-source X-ray Spectroscopy (tREXS) grating spectrograph uses modules of reflection gratings to collect spectroscopic data from extended astronomical sources of soft X-rays. Two blazed master gratings were produced on silicon substrates with electron-beam lithography (EBL) and complementary nanofabrication processes that include KOH etching. Substrate-conformal imprint lithography (SCIL) was then used to create 191 replicas of the two grating masters for use in the flight instrument. Diffraction efficiency was measured for several replica gratings, which achieve a peak of ( varvec{>} )70% absolute efficiency near 0.22 keV and an average of ( varvec{approx } )50% absolute efficiency across the measured band, from 0.18 – 0.8 keV. Here we detail the nanofabrication of the grating masters, including the EBL parameters and tREXS-specific fabrication considerations, and the SCIL replication process used to generate the final instrument gratings. A discussion of grating characterization and areas for future improvement is also presented.
{"title":"Reflection grating fabrication for the Rockets for Extended-source X-ray Spectroscopy","authors":"Drew M. Miles, Ross McCurdy, Michael Labella, Randall L. McEntaffer, Fabien Grisé, Jake McCoy, James H. Tutt","doi":"10.1007/s10686-025-10011-1","DOIUrl":"10.1007/s10686-025-10011-1","url":null,"abstract":"<div><p>The Rockets for Extended-source X-ray Spectroscopy (tREXS) grating spectrograph uses modules of reflection gratings to collect spectroscopic data from extended astronomical sources of soft X-rays. Two blazed master gratings were produced on silicon substrates with electron-beam lithography (EBL) and complementary nanofabrication processes that include KOH etching. Substrate-conformal imprint lithography (SCIL) was then used to create 191 replicas of the two grating masters for use in the flight instrument. Diffraction efficiency was measured for several replica gratings, which achieve a peak of <span>( varvec{>} )</span>70% absolute efficiency near 0.22 keV and an average of <span>( varvec{approx } )</span>50% absolute efficiency across the measured band, from 0.18 – 0.8 keV. Here we detail the nanofabrication of the grating masters, including the EBL parameters and tREXS-specific fabrication considerations, and the SCIL replication process used to generate the final instrument gratings. A discussion of grating characterization and areas for future improvement is also presented.</p></div>","PeriodicalId":551,"journal":{"name":"Experimental Astronomy","volume":"59 3","pages":""},"PeriodicalIF":2.2,"publicationDate":"2025-06-14","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"https://www.ncbi.nlm.nih.gov/pmc/articles/PMC12165994/pdf/","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"144300894","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":3,"RegionCategory":"物理与天体物理","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"OA","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Pub Date : 2025-06-13DOI: 10.1007/s10686-025-10014-y
Alexey Uliyanov, Cuán de Barra, David Murphy, Derek O’Callaghan, Padraig McDermott, Joseph Thompson, Lorraine Hanlon, Sheila McBreen
GIFTS is a 6U CubeSat designed to detect and localise gamma-ray bursts (GRBs). Its main goal is to improve the sky coverage of existing GRB observatories and contribute to the search of electromagnetic counterparts to gravitational-wave events. GIFTS will use six CeBr( _3 ) scintillator detectors oriented at different angles to localise GRBs based on the difference in the observed count rates. Each detector employs an array of 24 SiPMs for scintillator readout. A full-size prototype of one GIFTS detector was built and tested with gamma rays with energies ranging from 31 keV to 1.3 MeV. It showed an energy resolution of 5.4% at 662 keV. Monte-Carlo simulations were used to estimate the GRB detection and localisation performance of the full instrument. GIFTS was able to detect about 50% of the GRBs from the Fermi GBM catalogue, provided they were not occulted by Earth. Assuming a 60% duty factor for GRB observations, GIFTS is expected to detect about 80 GRBs/year including 12 short GRBs/year. For 90% of the detected GRBs with positive elevations, the true localisation error is less than 32( ^{circ } ). The localisation error is mainly defined by statistical fluctuations in the observed count rates and becomes smaller for brighter events. Systematic localisation errors are expected to depend mainly on the accuracy of the instrument response model used by the localisation procedure. GIFTS is under development and expected to be launch ready for the next gravitational-wave observing run (O5).
gift是一颗6U立方体卫星,设计用于探测和定位伽马射线暴(GRBs)。它的主要目标是提高现有GRB天文台的天空覆盖范围,并为寻找引力波事件的电磁对应体做出贡献。gift将使用六个CeBr ( _3 )闪烁体探测器,以不同的角度定向,根据观测到的计数率的差异来定位grb。每个探测器采用24个sipm阵列进行闪烁体读出。建立了一个全尺寸的gift探测器原型,并对能量从31 keV到1.3 MeV的伽马射线进行了测试。它的能量分辨率为5.4% at 662 keV. Monte-Carlo simulations were used to estimate the GRB detection and localisation performance of the full instrument. GIFTS was able to detect about 50% of the GRBs from the Fermi GBM catalogue, provided they were not occulted by Earth. Assuming a 60% duty factor for GRB observations, GIFTS is expected to detect about 80 GRBs/year including 12 short GRBs/year. For 90% of the detected GRBs with positive elevations, the true localisation error is less than 32( ^{circ } ). The localisation error is mainly defined by statistical fluctuations in the observed count rates and becomes smaller for brighter events. Systematic localisation errors are expected to depend mainly on the accuracy of the instrument response model used by the localisation procedure. GIFTS is under development and expected to be launch ready for the next gravitational-wave observing run (O5).
{"title":"GIFTS: A 6U CubeSat for the detection and localisation of gamma-ray bursts","authors":"Alexey Uliyanov, Cuán de Barra, David Murphy, Derek O’Callaghan, Padraig McDermott, Joseph Thompson, Lorraine Hanlon, Sheila McBreen","doi":"10.1007/s10686-025-10014-y","DOIUrl":"10.1007/s10686-025-10014-y","url":null,"abstract":"<div><p>GIFTS is a 6U CubeSat designed to detect and localise gamma-ray bursts (GRBs). Its main goal is to improve the sky coverage of existing GRB observatories and contribute to the search of electromagnetic counterparts to gravitational-wave events. GIFTS will use six CeBr<span>( _3 )</span> scintillator detectors oriented at different angles to localise GRBs based on the difference in the observed count rates. Each detector employs an array of 24 SiPMs for scintillator readout. A full-size prototype of one GIFTS detector was built and tested with gamma rays with energies ranging from 31 keV to 1.3 MeV. It showed an energy resolution of 5.4% at 662 keV. Monte-Carlo simulations were used to estimate the GRB detection and localisation performance of the full instrument. GIFTS was able to detect about 50% of the GRBs from the Fermi GBM catalogue, provided they were not occulted by Earth. Assuming a 60% duty factor for GRB observations, GIFTS is expected to detect about 80 GRBs/year including 12 short GRBs/year. For 90% of the detected GRBs with positive elevations, the true localisation error is less than 32<span>( ^{circ } )</span>. The localisation error is mainly defined by statistical fluctuations in the observed count rates and becomes smaller for brighter events. Systematic localisation errors are expected to depend mainly on the accuracy of the instrument response model used by the localisation procedure. GIFTS is under development and expected to be launch ready for the next gravitational-wave observing run (O5).</p></div>","PeriodicalId":551,"journal":{"name":"Experimental Astronomy","volume":"59 3","pages":""},"PeriodicalIF":2.2,"publicationDate":"2025-06-13","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"https://link.springer.com/content/pdf/10.1007/s10686-025-10014-y.pdf","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"145143361","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":3,"RegionCategory":"物理与天体物理","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"OA","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
The High Altitude Detection of Astronomical Radiation (HADAR) experiment employs an innovative Cherenkov observation technique, boasting an expansive Field-of-View (FOV), and is specifically designed to capture the prompt emissions from Gamma Ray Bursts (GRBs).We propose a novel method for energy reconstruction of Very-high-energy (VHE) γ-rays in the HADAR experiment, based on the Boosted Decision Trees (BDTs) model in machine learning algorithms, referred to as BDTs-Erec. We discuss this energy reconstruction method in detail. A training dataset is generated through Monte Carlo simulation, and the TMVA tool in the ROOT framework is utilized to implement the BDTs model. This model minimizes prediction errors by incrementally adding decision trees and finally constructs 3000 BDTs, thus optimizing the accuracy of energy reconstruction. Performance comparisons are made against the traditional energy reconstruction method based on Look-Up-Tables (denoted as LUTs-Erec), indicating that BDTs-Erec significantly outperforms LUTs-Erec in prediction performance with increasing energy, while it exhibits poorer performance in the low-energy range.
{"title":"A novel energy reconstruction method for wide-field-of-view imaging atmospheric Cherenkov technique experiments","authors":"Qingqian Zhou, Qingyuan Hou, Youliang Feng, Tianlu Chen, Hengjiao Liu, Yiqing Guo, Cheng Liu, Zihao Zhang, Qi Gao, Maoyuan Liu, Xiangli Qian, Yuanqi Liu, Jiadan Xie, Shanjie Shu, Zhiqiang Zhu, Weiqi Han, Qijiao Fang, Yanan Wang, Baozhen Liu, Shaohua Zhang","doi":"10.1007/s10686-025-10007-x","DOIUrl":"10.1007/s10686-025-10007-x","url":null,"abstract":"<div><p>The High Altitude Detection of Astronomical Radiation (HADAR) experiment employs an innovative Cherenkov observation technique, boasting an expansive Field-of-View (FOV), and is specifically designed to capture the prompt emissions from Gamma Ray Bursts (GRBs).We propose a novel method for energy reconstruction of Very-high-energy (VHE) γ-rays in the HADAR experiment, based on the Boosted Decision Trees (BDTs) model in machine learning algorithms, referred to as BDTs-Erec. We discuss this energy reconstruction method in detail. A training dataset is generated through Monte Carlo simulation, and the TMVA tool in the ROOT framework is utilized to implement the BDTs model. This model minimizes prediction errors by incrementally adding decision trees and finally constructs 3000 BDTs, thus optimizing the accuracy of energy reconstruction. Performance comparisons are made against the traditional energy reconstruction method based on Look-Up-Tables (denoted as LUTs-Erec), indicating that BDTs-Erec significantly outperforms LUTs-Erec in prediction performance with increasing energy, while it exhibits poorer performance in the low-energy range.</p></div>","PeriodicalId":551,"journal":{"name":"Experimental Astronomy","volume":"59 3","pages":""},"PeriodicalIF":2.2,"publicationDate":"2025-06-12","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"145143474","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":3,"RegionCategory":"物理与天体物理","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Pub Date : 2025-06-04DOI: 10.1007/s10686-025-10010-2
Federico Sabbatini, Catia Grimani
In this work we study the potentialities of machine learning models in reconstructing the solar wind speed observations gathered in the first Lagrangian point by the ACE satellite in 2016–2017. We leverage a supervised model trained with the ACE observations and the galactic cosmic-ray flux variation data measured with particle detectors hosted on board the LISA Pathfinder mission also orbiting around L1 during the same years. Missing data in galactic cosmic-ray time series have been filled with the benefit of other machine learning models developed in previous work. The model presented here will be used for the European Space Agency Laser Interferometer Space Antenna (LISA) after its launch in 2035 to estimate the solar wind speed, that will not be measured on board, with the only benefit of galactic cosmic-ray variation measurements. We show that ensemble models composed of heterogeneous weak regressors are able to outperform weak regressors in terms of predictive accuracy. Machine learning and other powerful predictive algorithms open a window on the possibility of substituting dedicated instrumentation with software models acting as surrogates for diagnostics of space missions such as the LISA mission and space weather science.
{"title":"Solar wind speed estimate with machine learning ensemble models for LISA","authors":"Federico Sabbatini, Catia Grimani","doi":"10.1007/s10686-025-10010-2","DOIUrl":"10.1007/s10686-025-10010-2","url":null,"abstract":"<div><p>In this work we study the potentialities of machine learning models in reconstructing the solar wind speed observations gathered in the first Lagrangian point by the ACE satellite in 2016–2017. We leverage a supervised model trained with the ACE observations and the galactic cosmic-ray flux variation data measured with particle detectors hosted on board the LISA Pathfinder mission also orbiting around L1 during the same years. Missing data in galactic cosmic-ray time series have been filled with the benefit of other machine learning models developed in previous work. The model presented here will be used for the European Space Agency Laser Interferometer Space Antenna (LISA) after its launch in 2035 to estimate the solar wind speed, that will not be measured on board, with the only benefit of galactic cosmic-ray variation measurements. We show that ensemble models composed of heterogeneous weak regressors are able to outperform weak regressors in terms of predictive accuracy. Machine learning and other powerful predictive algorithms open a window on the possibility of substituting dedicated instrumentation with software models acting as surrogates for diagnostics of space missions such as the LISA mission and space weather science.</p></div>","PeriodicalId":551,"journal":{"name":"Experimental Astronomy","volume":"59 3","pages":""},"PeriodicalIF":2.2,"publicationDate":"2025-06-04","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"145142359","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":3,"RegionCategory":"物理与天体物理","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Pub Date : 2025-06-03DOI: 10.1007/s10686-025-10008-w
R. Krivonos, R. Burenin, E. Filippova, I. Lapshov, A. Tkachenko, A. Semena, I. Mereminskiy, V. Arefiev, A. Lutovinov, B. D. Ramsey, J. J. Kolodziejczak, D. A. Swartz, C.-T. Chen, S. R. Ehlert, A. Vikhlinin
The knowledge of the point spread function (PSF) of the Mikhail Pavlinsky Astronomical Roentgen Telescope–X-ray Concentrator (ART-XC) telescope aboard the Spectrum-Roentgen-Gamma (SRG) observatory plays an especially crucial role in the detection of point X-ray sources in the all-sky survey and the studies of extended X-ray objects with low surface brightness. In this work, we calibrate the far off-axis shape of the ART-XC PSF using in-flight data of Sco X-1 and the Crab Nebula, in all-sky survey or scan mode, respectively. We demonstrate that the so-called “slewing” ART-XC PSF (in contrast to the on-axis PSF), in convolution with the detector pixels, is consistent with ground calibration performed at the Marshall Space Flight Center, and can be used to model the PSF up to large off-axis distances in all-sky survey or scan modes. The radial profile of the Crab Nebula in the 4−12 keV band shows an extended structure out to ( sim )150” and is consistent with Sco X-1 at larger off-axis angles. Finally, we performed an analytic parametrization of the slewing ART-XC PSF as a function of energy.
{"title":"Inflight calibration of SRG/ART-XC point spread function at large off-axis angles","authors":"R. Krivonos, R. Burenin, E. Filippova, I. Lapshov, A. Tkachenko, A. Semena, I. Mereminskiy, V. Arefiev, A. Lutovinov, B. D. Ramsey, J. J. Kolodziejczak, D. A. Swartz, C.-T. Chen, S. R. Ehlert, A. Vikhlinin","doi":"10.1007/s10686-025-10008-w","DOIUrl":"10.1007/s10686-025-10008-w","url":null,"abstract":"<div><p>The knowledge of the point spread function (PSF) of the Mikhail Pavlinsky Astronomical Roentgen Telescope–X-ray Concentrator (ART-XC) telescope aboard the Spectrum-Roentgen-Gamma (<i>SRG</i>) observatory plays an especially crucial role in the detection of point X-ray sources in the all-sky survey and the studies of extended X-ray objects with low surface brightness. In this work, we calibrate the far off-axis shape of the ART-XC PSF using in-flight data of Sco X-1 and the Crab Nebula, in all-sky survey or scan mode, respectively. We demonstrate that the so-called “slewing” ART-XC PSF (in contrast to the on-axis PSF), in convolution with the detector pixels, is consistent with ground calibration performed at the Marshall Space Flight Center, and can be used to model the PSF up to large off-axis distances in all-sky survey or scan modes. The radial profile of the Crab Nebula in the 4−12 keV band shows an extended structure out to <span>( sim )</span>150” and is consistent with Sco X-1 at larger off-axis angles. Finally, we performed an analytic parametrization of the slewing ART-XC PSF as a function of energy.</p></div>","PeriodicalId":551,"journal":{"name":"Experimental Astronomy","volume":"59 3","pages":""},"PeriodicalIF":2.2,"publicationDate":"2025-06-03","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"145142097","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":3,"RegionCategory":"物理与天体物理","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
The Follow-up X-ray Telescope (FXT) is a primary scientific instrument on board the Einstein Probe (EP) astronomical satellite, which was launched in January 2024. FXT consists of two nested Wolter I-type telescopes (FXT-A and FXT-B) with a focal length of 1600 mm. The focal plane detector utilizes a PNCCD with a resolution of 384(times )384 pixels. One of the key functions of FXT is to perform the real-time triggering and localization of transients and burst sources. We have developed specialized real-time trigger software that operates within the Payload Data Processing Unit of EP. This onboard software can effectively search for and locate sources, while transmitting source information in real time via the Beidou short message unit and the Very High Frequency (VHF) unit. This paper provides a comprehensive description of the design and development of the onboard software, covering software requirements, module design, and workflow. Additionally, the paper introduces both ground-based and in-orbit testing of this software, and the test results demonstrate that the software meets all design requirements.
{"title":"The real-time trigger software of the follow-up X-ray telescope on board the EP satellite","authors":"Xiaofan Zhao, Hanyu Ban, Hongbo Cai, Jingjing Xu, Fei Li, Zijian Zhao, Ye Zhang, Weiwei Cui, Hao Wang, Laidan Luo, Wei Li, Yong Chen","doi":"10.1007/s10686-025-10006-y","DOIUrl":"10.1007/s10686-025-10006-y","url":null,"abstract":"<div><p>The Follow-up X-ray Telescope (FXT) is a primary scientific instrument on board the Einstein Probe (EP) astronomical satellite, which was launched in January 2024. FXT consists of two nested Wolter I-type telescopes (FXT-A and FXT-B) with a focal length of 1600 mm. The focal plane detector utilizes a PNCCD with a resolution of 384<span>(times )</span>384 pixels. One of the key functions of FXT is to perform the real-time triggering and localization of transients and burst sources. We have developed specialized real-time trigger software that operates within the Payload Data Processing Unit of EP. This onboard software can effectively search for and locate sources, while transmitting source information in real time via the Beidou short message unit and the Very High Frequency (VHF) unit. This paper provides a comprehensive description of the design and development of the onboard software, covering software requirements, module design, and workflow. Additionally, the paper introduces both ground-based and in-orbit testing of this software, and the test results demonstrate that the software meets all design requirements.</p></div>","PeriodicalId":551,"journal":{"name":"Experimental Astronomy","volume":"59 3","pages":""},"PeriodicalIF":2.7,"publicationDate":"2025-05-27","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"144140125","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":3,"RegionCategory":"物理与天体物理","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Pub Date : 2025-05-15DOI: 10.1007/s10686-025-10005-z
Jiamin Sun, Lin Zhu, Ye Chai, He Gao, Zhouhui Liu, Shibo Shu, Yaqiong Li, Yifei Zhang, Zhengwei Li, Yudong Gu, Mengqi Jiang, Qinglei Xiu, Zhijia Sun, Daikang Yan, Congzhan Liu
Transition-edge sensor (TES) as a type of low-temperature superconducting bolometers offers excellent signal-to-noise-ratio, and is one of the most up-to-date technologies used for cosmic microwave background (CMB) observations. The Ali CMB polarization telescope (AliCPT) project in China uses TES bolometers as the focal plane detector through an international collaborative effort. To increase collecting efficiency of the telescope, and include bolometers of different frequency bands, large-scale production of TES bolometer arrays needs to be accomplished in the future. In this work, we developed single pixel TES bolometers, the saturation power and noise equivalent power (NEP) of which satisfy the requirements of 90 GHz and 150 GHz CMB applications. Each of the bolometers consist of a 1200 ppm AlMn alloy TES for CMB science observation and an Al TES for laboratory optical tests. Dark characterization is applied on these bolometers. Their heat capacities are in the range of 0.7(sim )1.6 pJ/K and the NEP values are below 30 aW/(sqrt{Hz}). The T(_{c}) values are about 360 mK and can be adjusted to about 410 mK by additional annealing.
{"title":"AlMn-Al dual TES bolometer development for CMB telescopes","authors":"Jiamin Sun, Lin Zhu, Ye Chai, He Gao, Zhouhui Liu, Shibo Shu, Yaqiong Li, Yifei Zhang, Zhengwei Li, Yudong Gu, Mengqi Jiang, Qinglei Xiu, Zhijia Sun, Daikang Yan, Congzhan Liu","doi":"10.1007/s10686-025-10005-z","DOIUrl":"10.1007/s10686-025-10005-z","url":null,"abstract":"<div><p>Transition-edge sensor (TES) as a type of low-temperature superconducting bolometers offers excellent signal-to-noise-ratio, and is one of the most up-to-date technologies used for cosmic microwave background (CMB) observations. The Ali CMB polarization telescope (AliCPT) project in China uses TES bolometers as the focal plane detector through an international collaborative effort. To increase collecting efficiency of the telescope, and include bolometers of different frequency bands, large-scale production of TES bolometer arrays needs to be accomplished in the future. In this work, we developed single pixel TES bolometers, the saturation power and noise equivalent power (NEP) of which satisfy the requirements of 90 GHz and 150 GHz CMB applications. Each of the bolometers consist of a 1200 ppm AlMn alloy TES for CMB science observation and an Al TES for laboratory optical tests. Dark characterization is applied on these bolometers. Their heat capacities are in the range of 0.7<span>(sim )</span>1.6 pJ/K and the NEP values are below 30 aW/<span>(sqrt{Hz})</span>. The T<span>(_{c})</span> values are about 360 mK and can be adjusted to about 410 mK by additional annealing.</p></div>","PeriodicalId":551,"journal":{"name":"Experimental Astronomy","volume":"59 3","pages":""},"PeriodicalIF":2.7,"publicationDate":"2025-05-15","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"143949636","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":3,"RegionCategory":"物理与天体物理","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
The first pathfinder of the CATCH mission, CATCH-1, was launched in June 2024. It is equipped with a light-weight, narrow-field optimized Lobster Eye X-ray Optics. By sacrificing a portion of the field of view to achieve a large effective area, the telescope’s sensitivity is enhanced. This paper presents the equipment and procedures employed for calibrating the optics assembly. A comprehensive on-ground calibration for the Lobster Eye X-ray Optics is conducted before its launch using multi-target X-ray sources and the pnCCD Color X-Ray Camera in the 100 m X-Ray Test Facility. The results are derived from calibration measurements taken before and after the mechanical testing and mainly include measurements of the focal length, point spread function, angular resolution, and the effective area for incident X-rays at 0.28 keV, 0.93 keV, 1.49 keV, 2.98 keV, and 4.51 keV. The results indicate that the mirror’s performance remains stable and no observable variation before and after the mechanical testing. At 0.93 keV, the mirror’s angular resolution is (6.11^{prime }) (FWHM), and the effective area is 40.75 (textrm{cm}^{2}), meeting the expected performance of CATCH-1 X-ray optics.
{"title":"Pre-flight calibration of the optics assembly for CATCH’s first pathfinder","authors":"Jingyu Xiao, Yiming Huang, Zijian Zhao, Yusa Wang, Qian-Qing Yin, Chen Zhang, Dongjie Hou, Yuxuan Zhu, Yifan Zhang, Donghua Zhao, Sheng Yang, Lingling Men, Ge Jin, Lian Tao, Shuang-Nan Zhang, Wen Chen, Yanfeng Dai, Min Gao, Huilin He, Guoli Huang, Zhengwei Li, Xiaojing Liu, Panping Li, Yajun Li, Ruican Ma, Liqiang Qi, Xiangyang Wen, Shaolin Xiong, Yibo Xu, Liyuan Xiong, Yong Yang, Juan Zhang, Aimei Zhang, Heng Zhou, Shujie Zhao, Kang Zhao, Qingchang Zhao","doi":"10.1007/s10686-025-10001-3","DOIUrl":"10.1007/s10686-025-10001-3","url":null,"abstract":"<div><p>The first pathfinder of the CATCH mission, CATCH-1, was launched in June 2024. It is equipped with a light-weight, narrow-field optimized Lobster Eye X-ray Optics. By sacrificing a portion of the field of view to achieve a large effective area, the telescope’s sensitivity is enhanced. This paper presents the equipment and procedures employed for calibrating the optics assembly. A comprehensive on-ground calibration for the Lobster Eye X-ray Optics is conducted before its launch using multi-target X-ray sources and the pnCCD Color X-Ray Camera in the 100 m X-Ray Test Facility. The results are derived from calibration measurements taken before and after the mechanical testing and mainly include measurements of the focal length, point spread function, angular resolution, and the effective area for incident X-rays at 0.28 keV, 0.93 keV, 1.49 keV, 2.98 keV, and 4.51 keV. The results indicate that the mirror’s performance remains stable and no observable variation before and after the mechanical testing. At 0.93 keV, the mirror’s angular resolution is <span>(6.11^{prime })</span> (FWHM), and the effective area is 40.75 <span>(textrm{cm}^{2})</span>, meeting the expected performance of CATCH-1 X-ray optics.</p></div>","PeriodicalId":551,"journal":{"name":"Experimental Astronomy","volume":"59 3","pages":""},"PeriodicalIF":2.7,"publicationDate":"2025-05-08","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"143918915","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":3,"RegionCategory":"物理与天体物理","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
The reconstruction of the photoelectron tracks in X-ray polarimetric detectors based on Gas Pixel Detectors (GPD) is crucial for polarization detection. In addition to traditional moment analysis methods, the convolutional neural network (CNN) is also a noteworthy approach. However, most existing CNN methods for polarization detection have only been effectively validated on simulated data, and the few methods validated on experimental data have not yielded satisfactory results. We have improved the CNN algorithm for reconstructing the emission direction of photoelectron tracks in X-ray polarimetric detectors. We tested this algorithm using calibration data from the detectors of the PolarLight mission and the Polarimetry Focusing Array (PFA) onboard the enhanced X-ray Timing and Polarimetry (eXTP) mission. The results indicate that the optimized deep learning model increased the modulation factor by approximately 0.02 over the 2-8 keV energy range and only introduced a small systematic error. This can enhance the sensitivity of polarization detector in the low-energy range. Additionally, the computational resources required for the model are much lower than the previous CNN models.
{"title":"Optimization of deep learning method on track reconstruction for X-ray polarimetry with gas pixel detectors","authors":"Yang Jiao, Weichun Jiang, Jiechen Jiang, Huilin He, Hua Feng, Xiaohua Liu, Hong Li, Liming Song, Yuanyuan Du, Liang Sun, Xiaojing Liu, Qiong Wu, Jiawei Yang, Zipeng Song, Hangyu Chen, Yongqi Zhao, Yupeng Xu, Congzhan Liu, Shuangnan Zhang","doi":"10.1007/s10686-025-10003-1","DOIUrl":"10.1007/s10686-025-10003-1","url":null,"abstract":"<div><p>The reconstruction of the photoelectron tracks in X-ray polarimetric detectors based on Gas Pixel Detectors (GPD) is crucial for polarization detection. In addition to traditional moment analysis methods, the convolutional neural network (CNN) is also a noteworthy approach. However, most existing CNN methods for polarization detection have only been effectively validated on simulated data, and the few methods validated on experimental data have not yielded satisfactory results. We have improved the CNN algorithm for reconstructing the emission direction of photoelectron tracks in X-ray polarimetric detectors. We tested this algorithm using calibration data from the detectors of the PolarLight mission and the Polarimetry Focusing Array (PFA) onboard the enhanced X-ray Timing and Polarimetry (eXTP) mission. The results indicate that the optimized deep learning model increased the modulation factor by approximately 0.02 over the 2-8 keV energy range and only introduced a small systematic error. This can enhance the sensitivity of polarization detector in the low-energy range. Additionally, the computational resources required for the model are much lower than the previous CNN models.</p></div>","PeriodicalId":551,"journal":{"name":"Experimental Astronomy","volume":"59 3","pages":""},"PeriodicalIF":2.7,"publicationDate":"2025-05-08","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"143918914","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":3,"RegionCategory":"物理与天体物理","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}