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一种高精度全自主相对导航系统研究
引用本文:徐海刚.一种高精度全自主相对导航系统研究[J].弹箭与制导学报,2010,30(1).
作者姓名:徐海刚
作者单位:北京航空航天大学仪器科学与光电工程学院,北京,100191
基金项目:“985工程”(222105)资助
摘    要:基于陀螺寻北原理、旋转调制技术及惯导系统的误差特性,提出一种完全自主的导航系统,不需任何外界信息,可进行寻北、测定纬度和高精度的相对导航。给出了旋转调制寻北、测定纬度的原理,分析了旋转调制对导航性能的影响;计算机仿真结果表明,在没有任何初始信息的情况下,系统的方位精度可达1′,24h内的相对定位精度可达1n mile。

关 键 词:自主导航  寻北  旋转调制  

Research on an Autonomous High-accuracy Relative Navigation System
XU Haigang.Research on an Autonomous High-accuracy Relative Navigation System[J].Journal of Projectiles Rockets Missiles and Guidance,2010,30(1).
Authors:XU Haigang
Affiliation:School of Instrumentation Science and Opto-electronics Engineering;BUAA;Beijing 100191;China
Abstract:An autonomous inertial navigation system (INS) was put forwards based on theory of finding north by gyro, rotation-modulation technology and characteristics of INS's error, which can be used to find north, measure latitude and navigate with high precision without any aided information. Basic theory of finding north, measuring latitude was presented, and rotation-modulation's effect to navigation was analyzed. It's validated by computer simulation that the system can provide azimuth with error less than 1' and relative position with error less than 1n mile.
Keywords:autonomous navigation  finding north  rotation-modulation  
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