Pseudo-range Differential Integrated Time Synchronizing Method for Anchor Nodesormalsize
-
摘要: 传统时频同步方法维持分布式节点之间同步的精度较高,但并不适用于空间非接触节点的时频同步问题.本文提出一种基于伪距差分增强的时间同步方法,给出了系统原理和基本组成,运用总体最小二乘法解算分布式节点的先验钟差信息,并利用卡尔曼滤波构建了主从节点间的时间同步算法模型.仿真校验与结果分析显示,相比独立GPS授时同步,本文提出的系统同步算法能够提高空间分布式节点同步精度,在基线距离平均为25km的条件下,可将节点同步精度控制在亚纳秒量级.Abstract: Traditional time synchronization method could reach a high precision for distributed nodes, but does not apply to the spatially non-contact nodes. In order to solve the above problems, a time synchronization method based on pseudorange differential GPS was proposed, and the system principle and synchronization scheme are given. Moreover, the clock model of the Anchor Nodes (ANs) is built to estimate synchronization parameter, which is solved by the Total Least Squares (TLS) method. The Kalman Filter (KF) method is derived from the theoretical time synchronization module, which can enhance the real timing and precision. The results of numerical simulating show that the proposed system synchronization and parameter estimation methods can control the synchronization accuracy of distributed node in sub-nanosecond level.
-
Key words:
- Time synchronization /
- Anchor nodes /
- Pseudo-range difference /
- Kalman Filter
-
[1] JONO T, TAKAYAMA Y, KURA N, et al. OICETS on-orbit laser communication experiments[C]//Proceedings of SPIE 2006, Free-Space Laser Communication Technologies X!V!I!I!I. San Jose, California, United States:SPIE, 2006:13-24 [2] COFFEY V C. First optical link between satellites uses lasers[J]. Laser Focus World, 2002, 3(1):15-16 [3] WU Haitao, LI Xiaohui, LU Xiaochun, et al. Time Basis of Satellite Navigation System[M]. Beijing:Press of Science, 2011(吴海涛, 李孝辉, 卢晓春, 等. 卫星导航系统时间基础[M]. 北京:科学出版社, 2011) [4] KOPPANG P, WHEELE P. Working application of TWSTT for high precision remote synchronization[C]//Proceedings of the 1998 IEEE International Frequency Control Symposium. Pasadena, CA, USA:IEEE, 1998:273-277 [5] SONG Xiaoyong, JIA Xiaolin, MAO Yue. Two steps time synchronizing method for autonav with crosslink ranging measurement[J]. Geomat. Inf. Sci. Wuhan Univ., 2009, 34(11):1297-1300 [6] LIU Rongfang, SU Shengyi, WANG Wenbin. Relative positioning based on kinematic method using single difference GPS observations[J]. Manned Spacecraft, 2015, 21(4):356-361(刘荣芳, 苏晟翊, 王文彬. GPS单差观测量的运动学相对定轨研究[J]. 载人航天, 2015, 21(4):356-361) [7] WANG Leyang. Research of properties of total least squares estimation[J]. J. Geod. Geodyn., 2012, 32(5):48-52, 57(王乐洋. 总体最小二乘解性质研究[J]. 大地测量与地球动力学, 2012, 32(5):48-52, 57) [8] ZHANG Xianda. Modern Signal Processing[M]. 2nd ed. Beijing:Tsinghua University Press, 2002(张贤达. 现代信号处理[M]. 2版. 北京:清华大学出版社, 2002) [9] GALLEANI L, TAVELLA P. Time and the kalman filter[J]. IEEE Control Sys., 2010, 30(2):44-65 [10] Navstar GPS. IS-GPS-200D Navstar GPS Space Segment/Navigation User Interfaces[S]. Fountain Valley, CA:ARING Research Corporation, 2004 [11] AUDOIN C, GUINOT B. The Measurement of Time:Time, Frequency and the Atomic Clock[M]. London:Cambridge University Press, 2001 [12] RILEY W J. Handbook of Frequency Stability Analysis, Hamilton Technical Services[R]. Washington:NIST, 2007 -
-
计量
- 文章访问数: 1719
- HTML全文浏览量: 244
- PDF下载量: 726
-
被引次数:
0(来源:Crossref)
0(来源:其他)
下载: