共查询到19条相似文献,搜索用时 125 毫秒
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设计并调试了闪光二号加速器气体主开关同步触发系统。该系统主要由同步控制部分和高压脉冲形成部分构成。整个触发过程包括同步信号的引出、整形滤波、快速比较电路传输、前级脉冲形成、高压脉冲产生。通过对同步信号的整形处理,解决了发生器电流上的高频信号干扰问题;经过快速比较电路和前级脉冲后,选取了同步信号开始工作的时间点,并形成十几V的触发信号;高压脉冲形成部分主开关采用场畸变结合预电离的方式,该结构的气体开关时间响应为50 ns,抖动小于5 ns,满足使用要求。调试结果表明:该系统输出脉冲电压幅值100 kV,前沿小于10 ns,系统的工作时延440 ns,抖动13.5 ns;可通过增加电缆长度来控制触发信号到达气体开关的时刻,实现气体主开关与Marx发生器的延时同步工作。 相似文献
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设计并调试了闪光二号加速器气体主开关同步触发系统。该系统主要由同步控制部分和高压脉冲形成部分构成。整个触发过程包括同步信号的引出、整形滤波、快速比较电路传输、前级脉冲形成、高压脉冲产生。通过对同步信号的整形处理,解决了发生器电流上的高频信号干扰问题;经过快速比较电路和前级脉冲后,选取了同步信号开始工作的时间点,并形成十几V的触发信号;高压脉冲形成部分主开关采用场畸变结合预电离的方式,该结构的气体开关时间响应为50 ns,抖动小于5 ns,满足使用要求。调试结果表明:该系统输出脉冲电压幅值100 kV,前沿小于10 ns,系统的工作时延440 ns,抖动13.5 ns;可通过增加电缆长度来控制触发信号到达气体开关的时刻,实现气体主开关与Marx发生器的延时同步工作。 相似文献
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在激光等离子体机理的研究中,为实现灵活的界面配置和多路脉冲激光器高精度的时序延时,设计了一种基于微控制器STM32和FPGA的多路时序延时控制系统。重点介绍了基于FPGA的多路ns级时序信号和基于ucGUI的触摸屏界面的设计。另外,采用高速光电隔离技术和高速FET开关电路技术,对驱动电路进行了设计,缩短了输出脉冲上升沿的时间,提高了系统延时精度、驱动能力和抗干扰性能。测试结果表明,该设计每路延时可调,调节范围为5 ns~10 ms,最小可调步进为5 ns,延时误差小于1 ns。 相似文献
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为实现s档条纹相机扫描非线性标定,建立了基于延时可调信号源和外触发激光器的条纹相机s档扫描非线性标定系统,弥补了标准具法的不足。系统通过延时值的递增,得到条纹相机扫描速度在全扫程的变化。系统中时间关系抖动来源主要是测试设备延时抖动和条纹相机触发延时抖动。时间抖动测试与分析显示,条纹相机延时抖动0.6 ns,测试设备延时抖动0.3 ns,系统总时间抖动0.7 ns。系统时间抖动会造成最终时间轴信息的起伏。大量数值模拟分析表明,时间轴起伏对系统时间抖动的影响2 ns,在可以接受的范围内。因此,该系统能够胜任条纹相机s扫程时间信息的测量标定。 相似文献
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为实现μs档条纹相机扫描非线性标定,建立了基于延时可调信号源和外触发激光器的条纹相机μs档扫描非线性标定系统,弥补了标准具法的不足。系统通过延时值的递增,得到条纹相机扫描速度在全扫程的变化。系统中时间关系抖动来源主要是测试设备延时抖动和条纹相机触发延时抖动。时间抖动测试与分析显示,条纹相机延时抖动±0.6ns,测试设备延时抖动±0.3ns,系统总时间抖动±0.7ns。系统时间抖动会造成最终时间轴信息的起伏。大量数值模拟分析表明,时间轴起伏对系统时间抖动的影响±2ns,在可以接受的范围内。因此,该系统能够胜任条纹相机μs扫程时间信息的测量标定。 相似文献
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The method and experiment analysis of two-way common-view satellite time transfer for compass system
《中国科学:物理学 力学 天文学(英文版)》2015,(8)
Time synchronization between ground and satellites is a key technology for satellite navigation system. With dual-channel satellite, a method called Two-Way Common-View(TWCV) satellite time transfer for Compass system is proposed, which combines both characteristics of satellite common-view and two-way satellite-ground time transfer. By satellite-ground two-way pseudo-range differencing and two stations common-view differencing, this TWCV method can completely eliminate the influence of common errors, such as satellite clock offset, ephemeris errors, troposphere delay and station coordinates errors. At the same time, ionosphere delay related to signal frequency is also weakened significantly. So the precision of time transfer is improved much more greatly than before. In this paper, the basic principle is introduced in detail, the effect of major errors is analyzed and the practical calculation model in the Earth-fixed coordinate system for this new method is provided. Finally, experiment analysis is conducted with actual Compass observing data. The results show that the deviation and the stability of the satellite dual channel can be better than 0.1 ns, and the accuracy of the two-way common-view satellite time transfer can achieve 0.4 ns. All these results have verified the correctness of this TWCV method and model. In addition, we compare this TWCV satellite time transfer with the independent C-band TWSTFT(Two-Way Satellite Time and Frequency Transfer). It shows that the result of the TWCV satellite time transfer is in accordance with the C-band TWSTFT result, which further suggests that the TWCV method is a remote high precision time transfer technique. The research results in this paper are very important references for the development and application of Compass satellite navigation system. 相似文献
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在多路并联运行的电容储能型脉冲功率源中,为实现初级储能气体开关和脉冲形成主开关的同步,需要多组延时可调、每组多路输出的快前沿高电压脉冲来分别触发,为此研制了一套快响应低抖动100 kV快前沿电脉冲触发系统。该系统由同步机DG535和多组电脉冲放大单元组成,各组放大单元输出脉冲的延迟时间可调,延时步长由DG535设定,每组最短延时时间约为305 ns,抖动2 ns,可同时输出多路触发脉冲,在高阻负载上幅值可达180 kV,当输出信号为4路时,上升时间10 ns,当输出信号为8路时,上升时间15 ns。 相似文献
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In this paper, we investigate the impact of interferometer delay time in a 5 Gb/s optical double sideband-suppressed carrier (ODSB-SC) RoF system transmitting two wavelength interleaved radio frequency (RF) signals at 10 and 15 GHz over an optical fiber. Here, an optical Mach–Zehnder modulator is used for both optical carrier suppression and signal modulation. At the receiver, delay interferometer is used for the separation of RF frequency signals. We analyze the performance of the RoF system by varying the value of delay time of interferometer from 0.02 to 0.14 ns. The result shows that the RoF system performance is optimum for the time delay of 0.1 ns. Further, the optical spectrums, RF spectrums and eye diagrams of two interleaved RF signals have been compared. 相似文献
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ShanShi Zhou XiaoGong Hu Li Liu Rui Guo LingFeng Zhu ZhiQiao Chang ChengPan Tang XiuQiang Gong Ran Li Yang Yu 《中国科学:物理学 力学 天文学(英文版)》2016,59(10):109511
A two-way satellite time and frequency transfer(TWSTFT) device equipped in the BeiDou navigation satellite system(BDS)can calculate clock error between satellite and ground master clock. TWSTFT is a real-time method with high accuracy because most system errors such as orbital error, station position error, and tropospheric and ionospheric delay error can be eliminated by calculating the two-way pseudorange difference. Another method, the multi-satellite precision orbit determination(MPOD)method, can be applied to estimate satellite clock errors. By comparison with MPOD clock estimations, this paper discusses the applications of the BDS TWSTFT clock observations in satellite clock measurement, satellite clock prediction, navigation system time monitor, and satellite clock performance assessment in orbit. The results show that with TWSTFT clock observations, the accuracy of satellite clock prediction is higher than MPOD. Five continuous weeks of comparisons with three international GNSS Service(IGS) analysis centers(ACs) show that the reference time difference between BeiDou time(BDT) and golbal positoning system(GPS) time(GPST) realized IGS ACs is in the tens of nanoseconds. Applying the TWSTFT clock error observations may obtain more accurate satellite clock performance evaluation in the 104 s interval because the accuracy of the MPOD clock estimation is not sufficiently high. By comparing the BDS and GPS satellite clock performance, we found that the BDS clock stability at the 103 s interval is approximately 10.12, which is similar to the GPS IIR. 相似文献
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