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arXiv 2609.11605astro-ph.IM

基于RFSoC的球载甚长基线干涉测量实验后端与授时系统

An RFSoC-based Backend and Timing System for the Balloon-borne Very Long Baseline Interferometry Experiment

Mayukh Bagchi, Felix M. Thiel, Laura M. Fissel, Maggie Oxford, Lindy Blackburn, Rafael Costa, Vincent L. Fish, Daryl Haggard, Michael D. Johnson, Dominic W. Pes… 展开作者

Mayukh Bagchi, Felix M. Thiel, Laura M. Fissel, Maggie Oxford, Lindy Blackburn, Rafael Costa, Vincent L. Fish, Daryl Haggard, Michael D. Johnson, Dominic W. Pesce, Ganesh Rajagopalan, Javier L. Romualdez, Aarchi Shah, Adrian K. Sinclair, Stephanie St-Jean, Terry Yang

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中文总结 AI 辅助

本文介绍球载VLBI实验BVEX的RFSoC数字后端与授时系统,采用4.096 GSPS采样和8.2 Gbps记录,首次部署于平流层气球,地面测试通过,2025年飞行失败,计划2027年再飞。

中文摘要 AI 辅助

我们介绍了球载甚长基线干涉测量实验(BVEX)的数字后端与高精度授时系统的设计与性能表征,该实验是22 GHz平流层甚长基线干涉测量的探路者。后端使用AMD-Xilinx RFSoC 4x2上四个14位模数转换器输入之一。尽管转换器支持高达5 GSPS的采样率,飞行配置以4.096 GSPS对2-4 GHz中频进行数字化。CASPER固件提供用于指向和接收机验证的高分辨率光谱仪,以及具有两位重新量化的VLBI采集链,记录速率约为8.2 Gbps。带时间戳的数据包通过100千兆以太网(GbE)发送到存储计算机中的16 TB NVMe阵列,该计算机功耗约为70-80 W。授时链使用Rakon恒温晶振作为授时参考,而时间间隔计数器以约60 ps的分辨率测量其相对于GPS参考的漂移。这是RFSoC基VLBI后端与高精度授时系统首次部署在平流层气球上。地面测试验证了后端、光谱仪和授时链。2025年8月的CSA STRATOS飞行因气球故障而未达到目标浮空高度,因此未获得科学观测数据。对于计划中的2027年再飞行,我们正在开发一款传导冷却的数据存储计算机,具有24 TB NVMe容量,并提供从100 GbE接口到NVMe阵列的直接数据路径。

英文摘要

We present the design and performance characterization of the digital backend and precision-timing system for the Balloon-borne Very Long Baseline Interferometry Experiment (BVEX), a pathfinder for high-frequency stratospheric VLBI at 22 GHz. The backend uses one of the four 14-bit analog-to-digital converter inputs on an AMD-Xilinx RFSoC 4x2. Although the converters support sampling rates up to 5 GSPS, the flight configuration digitizes the 2-4 GHz intermediate frequency at 4.096 GSPS. CASPER firmware provides both a high-resolution spectrometer for pointing and receiver verification, and a VLBI acquisition chain with two-bit requantization that records at a rate of about 8.2 Gbps. The timestamped data packets are sent over 100 Gigabit Ethernet (GbE) to a 16 TB NVMe array in a storage computer that draws approximately 70-80 W. The timing chain uses a Rakon oven-controlled crystal oscillator as a timing reference while a time-interval counter measures its drift relative to a GPS reference with approximately 60 ps resolution. This is the first deployment of an RFSoC-based VLBI backend and precision-timing system on a stratospheric balloon. Ground tests validated the backend, spectrometer, and timing chain. The August 2025 CSA STRATOS flight ended before reaching the target float altitude because of a balloon failure, and as a result no science observations were obtained. For the planned 2027 reflight, we are developing a conduction-cooled data storage computer with 24 TB of NVMe capacity and a direct data path from the 100 GbE interface to the NVMe array.

发表机构

  • Queen’s University(女王大学)
  • Harvard University(哈佛大学)
  • Center for Astrophysics | Harvard & Smithsonian(天体物理中心 | 哈佛与史密森尼学会)
  • MIT Haystack Observatory(麻省理工学院海斯塔克天文台)
  • McGill University(麦吉尔大学)
  • Trottier Space Institute at McGill(麦吉尔大学特罗蒂尔太空研究所)
  • StarSpec Technologies Inc.(StarSpec科技有限公司)
  • Johns Hopkins University(约翰斯·霍普金斯大学)

机构由 AI 辅助整理,请以论文原文为准。

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