首页 | 本学科首页   官方微博 | 高级检索  
     

基于阻尼系数控制算法的时间驾驭方法研究
引用本文:赵赟,;周明翔,;潘峰,;赵景斐,;肖胜红. 基于阻尼系数控制算法的时间驾驭方法研究[J]. 宇航计测技术, 2014, 34(3): 13-17. DOI: 10.12060/j.issn.1000-7202.2014.03.03
作者姓名:赵赟,  周明翔,  潘峰,  赵景斐,  肖胜红
作者单位:1、北京卫星导航中心,北京 100094;2、中国科学院上海天文台,上海 200030
摘    要:在实现本地时间与参考时标精确同步的过程中,被驾驭对象频率稳定度和时间同步精度存在平衡矛盾。本文提出了一种基于阻尼系数控制算法的时间驾驭方法。首先利用Kalman滤波算法对历史数据的多项式模型进行拟合,得到被驾驭对象与参考源时标的相位差、频差及频漂,然后利用阻尼系数控制算法建立仿真模型进行分析,得到时间驾驭策略。仿真结果表明,本文提出的基于阻尼系数控制算法的时间驾驭方法在一定的时间偏差控制要求下,确保了被驾驭对象的频率稳定度。

关 键 词:时间驾驭方法  时间偏差  频率稳定度  同步精度  

Research on the Time Control Method based on the Damping Coefficient Control Algorithm
ZHAO Yun,ZHOU Ming-xiang,PAN Feng,ZHAO Jing-fei,XIAO Sheng-hong. Research on the Time Control Method based on the Damping Coefficient Control Algorithm[J]. Journal of Astronautic Metrology and Measurement, 2014, 34(3): 13-17. DOI: 10.12060/j.issn.1000-7202.2014.03.03
Authors:ZHAO Yun  ZHOU Ming-xiang  PAN Feng  ZHAO Jing-fei  XIAO Sheng-hong
Affiliation:1、Beijing Satellite Navigation Center, Beijing 100094; ;2、Shanghai Observatory of CAS, Shanghai 200030
Abstract:In the process of accurate synchronizing the local time with the reference time standard,there is always a trade-off between the synchronization accuracy and the frequency stability of the steered target. A time steer method based on the damping coefficient control algorithm is presented in this paper.Firstly,the history data is fitted by using Kalman filtering algorithm and the phase difference,frequency difference,frequency drift between steered target and the reference time standard can be obtained. Then,the time steer strategy is obtained by analyzing simulation model which is built on damping coefficient control algorithm. The simulation result shows that the time steer method based on the Damping Coefficient Control Algorithm can ensure frequency stability of the steered target under certain time deviation constraint.
Keywords:Time control method Time difference Frequency stability Aynchronization accuracy
本文献已被 维普 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