首页 | 本学科首页   官方微博 | 高级检索  
     检索      

面向时间应用的可驯服铷钟
引用本文:陈智勇,韩蒂,庆毅,董柯,汤超,盛荣武.面向时间应用的可驯服铷钟[J].宇航计测技术,2013,33(1):31-34.
作者姓名:陈智勇  韩蒂  庆毅  董柯  汤超  盛荣武
作者单位:1、中国科学院武汉物理与数学研究所,湖北武汉,430071;; 2、西南电子设备研究所,四川成都,610036
摘    要:研制一种面向时间应用的GPS可驯服铷钟。当铷钟被GPS驯服后,它输出的秒信号实时同步于GPS接收机的秒信号。同时,铷钟和GPS接收机之间的时间差的数据通过一个比例积分控制器去校正铷钟的频率准确度。驯服后,两台GPS驯服铷钟之间的时间差小于20ns、频率差小于1E-12/d。使用一台专用的GPS信号处理板和特定的GPS接收机,时间差可小于5ns。

关 键 词:时间    频率    铷钟    GPS

A Disciplined Rubidium Oscillator for Timing Application
CHEN Zhi-yong,HAN Di,QING Yi,DONG Ke,TANG Chao,SHENG Rong-wu.A Disciplined Rubidium Oscillator for Timing Application[J].Journal of Astronautic Metrology and Measurement,2013,33(1):31-34.
Authors:CHEN Zhi-yong  HAN Di  QING Yi  DONG Ke  TANG Chao  SHENG Rong-wu
Institution:1、Wuhan Institute of Physics and Mathematics, Chinese Academy of Science, Wuhan,Hubei 430071; 2.、Southwest China Research Institute of Electronic Equipment, Chengdu,Sichuan 610036
Abstract:A GPS disciplined rubidium oscillator is designed for timing application. After disciplined, the rubidium oscillator outputs a second signal which is real-time synchronized to the second signal of the GPS receiver. In the same time, the time difference between the rubidium oscillator and the GPS receiver is processed to calibrate the frequency of the rubidium oscillator through a PI controller. The time difference is less than 10ns,the frequency difference is less than 1E-12/day between two GPS disciplined rubidium oscillator.After a dedicated GPS signal processing board and a particular GPS receiver is used, the time difference can be limited to 5ns.
Keywords:Time                                                                                                                        Frequency                                                                                                                        Rubidium oscillator                                                                                                                        GPS
本文献已被 CNKI 等数据库收录!
点击此处可从《宇航计测技术》浏览原始摘要信息
点击此处可从《宇航计测技术》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号