共查询到19条相似文献，搜索用时 296 毫秒
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《天文研究与技术》2020,(3)
星载氢原子钟具有频率稳定度高、频率漂移率低的优点,在卫星导航定位和频率计量中得到了广泛应用。星载氢原子钟的腔泡系统用于实现氢原子的量子跃迁及其信号采集,原子跃迁信号幅度直接决定了系统的信噪比,进而影响整机性能指标,所以腔泡系统是星载氢原子钟的核心组件。目前,星载氢原子钟腔泡系统主要采用直螺线管来产生原子跃迁所需的C场。由于星载氢原子钟物理部分的结构限制,直螺线管的磁场均匀度有进一步提高的空间。探讨使用多段线圈代替直螺线管用于产生C场的可行性。首先对多段线圈产生的磁场进行理论分析计算,同时使用ANSYS电磁场仿真软件对多段线圈的各项参数进行仿真和优化,包括各段长度、段数、间距以及匝数、内径和总长度等。然后优选磁场均匀度较好的线圈配置参数,可将C场的非均匀度由直螺线管约10%降低到多段线圈约1%。根据仿真优化结果建立了试验九段线圈,对比测试了原子跃迁信号增益,同时结合电路部分进行闭环测试,对频率稳定度指标进行了对比。实验结果表明,原子跃迁信号可有效提升,阿伦方差在中短稳(1～1 000 s)表现更好。此项工作为星载氢原子钟整机性能指标的进一步提升打下了基础。 相似文献
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目前利用激光来冷却和囚禁中性原子的技术已取得激动人心的进展。通过使用廉价的二极管激光器和蒸汽室收集器，有效地降低了囚禁原子的复杂性和高成本，在零点几μＫ温度下，可得到１０１１个原子／ｃｍ３的原子密度。本文介绍了有关激光冷却与囚禁技术，讨论了其现实应用：频率标准一基本物理性质研究。 相似文献
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根据全国自然科学学科发展规划,中国科学院陕西天文台主要从事高精度的时间频率工作及相应的理论和应用研究,在有关兄弟单位合作下建立独立的原子时间基准,确定世界时,并通过长波、短波电台发播我国标准时间与标准频率,同时利用电视网络和卫星系统开展多途径、高精度的时间频率服务工作,以适应我国国防、国民经济建设和科学研究的需要。目前,原子时间基准系统已经基本建立,长波授时实验台(呼号BPL)已经建成并开始发播,无源电视同步已工作多年,短波授时发 相似文献
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采用Ramsey分离振荡场方法,研究了紧束缚一维强相互作用的超冷玻色气体在Tonks-Girardeau区的Ramsey干涉。在等失谐情况下,干涉条纹宽度随着原子与分离场作用时间和拉比(Rabi)频率的增大而变窄。对量子投影噪声的研究表明,相比二能级Tonks-Girardeau气体,对于三能级模型,通过控制原子总数和调节外场可以降低量子噪声,有效地减少噪声对Tonks-Girardeau气体系统的干扰。原子干涉的探索对提高量子频率标准的精度具有重要理论指导意义。 相似文献
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目前利用激光来冷却和困禁中性原子的技术已取得激动人心的进展，通过使用廉价的二极管激光器和蒸汽室收集器，有效地降低了困禁原子的复杂性和高成本，在零点的μＮ温度下，可得到１０＾１１个原子／ｃｍ＾３的原子密度，本文介绍了有关激光冷却与困禁技术，讨论了其现实应用，频率标准→基本物理性质研究。 相似文献
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中国计划于2025年左右建立月球轨道VLBI (Very Long Baseline Interferometer)测站,将会搭载被动型星载氢钟作为时间频率标准.由于是首次在VLBI观测中使用星载氢钟,需要研究和验证其可行性.因此,利用星载氢钟作为频率基准开展了VLBI观测.实验时,分别使用主动型地面氢钟和被动型星载氢钟作为频率基准,利用上海天文台佘山25 m射电望远镜和其他测站对我国火星探测器天问一号进行了交替VLBI观测.数据处理分析结果表明,基于地面氢钟与星载氢钟的VLBI残余群时延标准差均在0.5 ns以内,表明星载氢钟可满足深空探测VLBI测定轨的精度要求,验证了其作为月球VLBI测站频率基准的可行性. 相似文献
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定量分析了原子钟的时间频率特性产生的守时时差,估算了原子时频标准的守时时差对有关物理量测量所产生的影响．给出了现代实用型原子钟的性能指标比较表,和用现代无线电手段传递、比对时频标准信号达到的指标．论述了高精度时间频率标准在大地、深空间探测、VLBI及毫秒脉冲星计时应用测量中的重要地位、作用．阐述了50 m射电望远镜的科学目标、“嫦娥”1号探月卫星任务对时间标准提出的高精度要求和选用原则．为了实现其科学目标和任务,必须建设与其研究目标相适宜的、标准尽可能高的原子时频标准,才能获得高质量的数据信息和高效能的研究成果．并对建设怎样的时间标准等问题进行讨论和提出具体建议． 相似文献
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国外原子时频最新进展 总被引：1，自引：0，他引：1
概述了传统原子频标的现状，以及新型原子频标和国际原子时的研究进展，介绍了为适应高精度新型频标和国际原子时的比对需要而开展的远程时频传递技术。 相似文献
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Hui-jie Song Shao-wu Dong Wei Li Ji-hai Zhang Yue-juan Jing 《Chinese Astronomy and Astrophysics》2018,42(2):279-290
The simulation methods of different kinds of noises of atomic clocks are given. The frequency flicker noise of atomic clocks is studied by using the Markov process theory. The method for estimating the maximum interval error of the frequency white noise is studied by using the Wiener process theory. Based on the operation of 9 cesium atomic clocks in the laboratory of time and frequency primary standards of NTSC (National Time Service Center), the noise factors of power-law spectrum models are estimated, and the simulations are carried out according to the corresponding noise models. Finally, the maximum interval error estimates of the frequency white noises generated by the 9 cesium atomic clocks are acquired. 相似文献
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A powerful and highly configurable simulator of generic clock frameworks is presented and evaluated. This software tool was
initially designed to test the reliability of clock data for the Gaia space mission. However, our application has been developed
as much parameterized as possible in order to easily adapt it to any other space mission. The main goals of our software tool
are to simulate the real performance of an atomic master clock, including the typical noises present in this kind of devices,
and to check the reliability of the generation and distribution of clock sub-products. The latter, which are generated by
other devices such as frequency multipliers and dividers, are also implemented in the simulator, as well as the corresponding
transmission lines. In our simulator the clock outputs obtained from the several nodes of the framework can be displayed with
the appropriate graphical tools, therefore easing the task of validating several design issues. Also, the parameters of the
master clock and of all the framework devices, as well as the whole clock framework structure are entered using XML files,
which can also be graphically verified. Finally, the accuracy and stability of the atomic clock which is expected to fly on-board
of Gaia is assessed. We also discuss in depth the several issues regarding the time data products that Gaia will require and
we characterize the most important elements. 相似文献
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《Chinese Astronomy and Astrophysics》2022,46(3):297-308
China plans to establish a lunar orbital VLBI (Very Long Baseline Interferometer) station around 2025, which will carry a space passive hydrogen maser as the time and frequency reference. Since it is the first time to use a space passive hydrogen maser for VLBI observation, its feasibility needs to be studied and verified. Therefore, we carried out VLBI observations using the space passive hydrogen maser as the frequency reference. In the experiment, the active hydrogen atomic clock and space passive hydrogen maser were used as the frequency standard, and the alternate VLBI observations of China’s Mars probe TW1 (Tianwen 1) were carried out using the 25 m radio telescope at Sheshan, Shanghai, and other VLBI stations. The results of data processing and analysis show that the standard deviation of VLBI residual group delay based on both active hydrogen atomic clock and space passive hydrogen maser are within 0.5 ns, which indicates that the space passive hydrogen maser can meet the accuracy requirements of VLBI measurement for deep space exploration, and verify its feasibility as the frequency standard of lunar orbital VLBI stations. 相似文献
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高精度国际时间比对的进展 总被引：12，自引：0，他引：12
在过去的４５ｙｒ中原子频标的性能大约每７ｙｒ提高一个数量级,从国际标准时间和各国高精度守时的需要出发,远距离的高精度时间频率传递比对技术也有与之相适应的很大的发展。ＧＰＳ卫星在近２０ｙｒ中不仅成为导航定位不可缺少的工具,在时间、频率的方面也发挥出巨大威力;近年来多通道“全视接收”技术的发展钎时频传输比对的稳定性有了重大改善;ＧＬＯＮＡＳＳ卫星系统在高精度时间比对方面正在成为ＧＰＳ系统的重要补充手段 相似文献
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NTSC的双混频时差测量系统试运转结果分析 总被引：1，自引：1，他引：1
中国科学院国家授时中心(NTSC)新进口的由德国Timetech公司制造的双混频时差测量系统(dual mixer time difference system,DMTD)已经通过了试运行。介绍了DMTD的工作原理和设备结构。NTSC时频基准实验室的主钟(MC)信号作为DMTD的频率参考信号,5个氢钟和18个铯钟的频率信号作为被测信号与MC信号进行相位比对。用频率分配放大器输出的多路MC信号也作为被测信号用以监测DMTD本身的精度和稳定度。给出了DMTD和时间间隔计数器TIC实际测量结果的比较及误差分析。测量结果表明DMTD特别适用于频率短期稳定度非常高的氢原子钟这样的频标之间的频率和时间比对。该设备将用于NTSC的守时工作,不久的将来也将用于铯喷泉与氢钟的频率比对。 相似文献
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The design of detector systems for flight applications requires the consideration of a number of issues unique to space instrumentation. Flight detectors must endure hostile radiation environments and thermal extremes. Paramount importance is given to reliability since inflight replacement is at best difficult and usually impossible. Flight detectors are also significant cost and design drivers since they often determine key requirements for flight instruments such as volume, mass, power consumption, heat dissipation and communications budgets. In this paper we describe the primary concerns in developing flight detector systems, and review the challenges posed by future NASA and ESA space science missions for detector development. 相似文献