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双星定位系统/SINS深组合导航系统研究
引用本文:林雪原, 张立民, 刘建业, 李玉光. 双星定位系统/SINS深组合导航系统研究[J]. 空间科学学报, 2003, 23(5): 388-395.
作者姓名:林雪原  张立民  刘建业  李玉光
作者单位:海军航空工程学院电子工程系,烟台,264001;南京航空航天大学导航研究中心;海军航空工程学院电子工程系,烟台,264001;南京航空航天大学导航研究中心
基金项目:国防预研重点项目的资助
摘    要:以卫星模拟器为基础,介绍了一种双星定位系统定姿的基本原理,解决了双星定位系统存在的位置滞后即定位实时性较差的缺陷,把双星定位系统的位置与姿态信息和捷联惯导系统的位置、姿态信息进行组合后,可有效地提高系统的精度.

关 键 词:定姿  双星定位系统  位置补偿  组合导航
收稿时间:2002-11-28
修稿时间:2002-11-28

THE STUDY ON A DEEPLY INTEGRATED NAVIGATION SYSTEM OF DOUBLE-STAR POSITIONING SYSTEM/SINS
LIN Xueyuan, ZHANG Limin, LIU Jianye, LI Yuguang. THE STUDY ON A DEEPLY INTEGRATED NAVIGATION SYSTEM OF DOUBLE-STAR POSITIONING SYSTEM/SINS[J]. Chinese Journal of Space Science, 2003, 23(5): 388-395.
Authors:LIN Xueyuan ZHANG Limin LIU Jianye LI Yuguang
Affiliation:1. Electronic Department, Naval Aeronautics Engineering Academy, Yantai 264001;;;2. Navigation research center, Nanjing University of Aeronautics and Astronautics
Abstract:Double-Star positioning system is one kind of regional satellite positioning system built up in China, it's aim is to provide more accurate position information for the user, but it's shortcoming is that the real-time positioning is dufficulty to get. It is one new concept to use the Double-Star positioning system to measure the attitude. This paper introduces one kind of the basic principles of attitude determination with Double-Star positioning system on the basis of the satellite simulator and gives the mathematic model of the attitude measurement. Thus the shortcoming mentioned above can be overcome. When the position and attitude information of Double-Star positioning system and strap-down inertial system are integrated, the state and measurement functions are built up, the simulation is made under specific orbit. The simulation results show that the system's accuracy can be improved effectively.
Keywords:Attitude determination   Double-Star position system   Position compensation   Integrated navigation.
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