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导弹与制导技术

一种高精度全自主相对导航系统研究

  • 徐海刚
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  • 北京航空航天大学仪器科学与光电工程学院,北京 100191

徐海刚(1979-),男,河北邯郸人,博士研究生,研究方向:旋转调制式惯性导航系统、组合导航、惯性导航理论。

收稿日期: 2008-12-14

  网络出版日期: 2025-05-19

基金资助

“985工程”(222105)资助

Research on an Autonomous High-accuracy Relative Navigation System

  • XU Haigang
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  • School of Instrumentation Science and Opto-electronics Engineering, BUAA, Beijing 100191, China

Received date: 2008-12-14

  Online published: 2025-05-19

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1nmile。

本文引用格式

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) : 1 -3 . DOI: 10.15892/j.cnki.djzdxb.2010.01.003

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.

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参考文献

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