首页 | 官方网站   微博 | 高级检索  
     

单通道测量条件下DORIS实时定轨方法研究
引用本文:刘俊宏,谷德峰,赖育网,易东云.单通道测量条件下DORIS实时定轨方法研究[J].飞行器测控学报,2011(5):50-54.
作者姓名:刘俊宏  谷德峰  赖育网  易东云
作者单位:国防科学技术大学理学院;
基金项目:国家自然科学基金(61002033)
摘    要:重点研究了单通道测量条件下的DORIS实时定轨方法。推导了实时定轨的扩展卡尔曼滤波(EKF)公式,仿真生成了47个测站的观测数据文件,分析了单通道测量条件下EKF滤波器的收敛性及其精度。仿真实验表明,仅有单个测站的观测数据时,滤波难以收敛;但在不同测站的观测数据切换时,滤波收敛效果显著。对于轨道高度为800km的卫星,初轨各轴位置误差小于500m、速度误差小于5m/s时,滤波平均收敛时间约55min;若各项系统误差能准确建模,实时轨道的位置精度将优于40cm。

关 键 词:DORIS  平均径向速度  单通道  扩展卡尔曼滤波  实时定轨

DORIS Real-time Orbit Determination Method under the Condition of a Single Channel
LIU Junhong,GU Defeng,LAI Yuwang,YI Dongyun.DORIS Real-time Orbit Determination Method under the Condition of a Single Channel[J].Journal of Spacecraft TT&C Technology,2011(5):50-54.
Authors:LIU Junhong  GU Defeng  LAI Yuwang  YI Dongyun
Affiliation:LIU Junhong,GU Defeng,LAI Yuwang,YI Dongyun (College of Science,National University of Defense Technology,Changsha 410073)
Abstract:DORIS is an advanced ground-based satellite orbit tracking system.This paper studies DORIS real-time orbit determination method under the condition of a single channel.Extended Kalman Filter formulations are derived for real-time orbit determination.Observation data files of 47 permanent beacons are generated.The convergence and accuracy of the filter is analyzed.Simulation and experiments show that,with a single channel,it is difficult for the filter to converge with the measurements of only one beacon whi...
Keywords:DORIS  Average Range Rate  Single Channel  Extended Kalman Filter(EKF)  Real-Time Orbit Determination  
本文献已被 CNKI 维普 等数据库收录!
点击此处可从《飞行器测控学报》浏览原始摘要信息
点击此处可从《飞行器测控学报》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-23

京公网安备 11010802026262号