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导弹与制导技术

高精度平台式惯导系统的实现

  • 张东荣 ,
  • 叶斌 ,
  • 党进
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  • 西北工业大学自动化学院,西安 710072

张东荣(1966-),男,陕西户县人,研究员,博士研究生,研究方向:导航、制导与控制。

收稿日期: 2010-09-09

  网络出版日期: 2025-05-30

The Realization of High Precision Platform Inertial Navigation System

  • ZHANG Dongrong ,
  • YE Bin ,
  • DANG Jin
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  • School of Automation, Northwestern Polytechnical University, Xi'an 710072, China

Received date: 2010-09-09

  Online published: 2025-05-30

摘要

惯导系统的导航精度随着导航时间的增加而增加,其中惯性测量元件是影响惯导系统的主要因素。旋转调制技术能够在现有惯性元件精度的条件下大幅提高系统导航性能,是提高惯导系统长时间导航精度的主要方法之一。文中在国产平台式标准惯导系统的基础上,通过改进算法和方位施矩回路,将由惯性测量元件水平方向上随时间发散误差量调制为常值误差,并通过阻尼进行消除,从而实现系统的高精度性能。仿真和试验验证结果表明,文中所设计的系统达到了预期的目的,具有较好的实用价值。

本文引用格式

张东荣 , 叶斌 , 党进 . 高精度平台式惯导系统的实现[J]. 弹箭与制导学报, 2011 , 31(3) : 59 -62 . DOI: 10.15892/j.cnki.djzdxb.2011.03.015

Abstract

The error of the inertial navigation system increases with navigation time, and inertial sensor is the main factor affecting the system precision. The revolution modulating technology can greatly improve the system precision under the condition that the inertial sensor keeps its original precision, and it is the main method for improving long time navigation precision of the inertial navigation system. On the basis of the domestic standard platform inertial navigation system, in the paper, the system algorithm and the azimuth matrix loop were improved, the errors diverging with time caused by the horizontal inertial measure unit were modulated as the constant errors. These constant errors can be eliminated by damping, and the precision of the inertial navigation system will be improved. The result of the simulation and experiment shows that the system designed by the authors meets the desired destination and have a good practice value.

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参考文献

[1]
秦永元. 惯性导航[M]. 北京: 科学出版社, 2006.
[2]
徐海刚. 旋转调制式捷联惯导系统研究[D]. 北京: 北京航空航天大学, 2006.
[3]
练军想, 吴文启, 吴美平,等. 机载惯导系统动态误差分析及旋转抑制研究[C]// 中国航空学会学术年会, 2007.
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