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

导航星座自主导航的守时算法研究
引用本文:易航,仲崇霞.导航星座自主导航的守时算法研究[J].宇航计测技术,2012,32(5):22.
作者姓名:易航  仲崇霞
作者单位:1、北京无线电计量测试研究所,北京 100039; 2、计量与校准技术国防科技重点实验室,北京 100039
摘    要:导航星座自主导航是提高卫星导航系统生存能力的一个重要方面,而实现导航星座自主导航的前提在于自主守时,星上综合原子时的计算则是自主守时的关键技术之一。本文分别研究了星上综合原子时计算的传统加权平均算法与卡尔曼滤波算法,并分别做了仿真实验,结果表明,通过合理设置,两种方法均可保持60d内自主守时25ns。

关 键 词:导航星座  时间尺度  自主守时  加权平均  卡尔曼滤波  

Research on Time Keeping Algorithm of the Autonomous Navigating of Navigation Constellation
YI Hang,ZHONG Chong-xia.Research on Time Keeping Algorithm of the Autonomous Navigating of Navigation Constellation[J].Journal of Astronautic Metrology and Measurement,2012,32(5):22.
Authors:YI Hang  ZHONG Chong-xia
Institution:1、.Beijing Institute of Radio Metrology and Measurement, Beijing 100039; 2、Science and Technology on Metrology and Calibration Laboratory, Beijing 100039
Abstract:Autonomous time keeping is one of the key techniques for the autonomous navigation of navigation constellation which plays an important role in improving the viability of the navigation constellation, while the algorithm of jointed atomic time scale on board is the key of autonomous time-keeping. In this paper, both the two algorithms based on weighted average and EKF are used in the calculation of jointed atomic time scale on board. The simulation results prove that both the two algorithms can keep the clock error within 25ns in a period of 240 days.
Keywords:Navigation constellation  Time scale  Autonomous time-keeping  Weighted average  
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