[an error occurred while processing this directive] [an error occurred while processing this directive] [an error occurred while processing this directive]
[an error occurred while processing this directive]

Journal of Projectiles, Rockets, Missiles and Guidance >

2012 , Vol. 32 >Issue 4: 57 - 60

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2012.04.039

MISSILES AND GUIDANCETECHNOLOGY

The Using Method of IMU Testing Data Before Launching Based on the Best Guidance Precise

  • XIAO Zhenglin ,
  • MOU Jianhua ,
  • CHEN Fang ,
  • FU Min
Expand
  • The Second Artillery Equipment Academy, Beijing 100085, China

Received date: 2011-11-02

  Online published: 2025-05-29

Fold

Abstract

A method discussed to further improve strapdown inertial guidance by making full use of IMU data before launching. The deviation of impact point related with equations of IMU through estimating coefficient. he optimal estimating coefficients obtained by minimizing the (CEP) of the estimating error of the deviation of impact point. The application method presented and the simulation result its effectiveness.

Key words： inertial-measurement-unit(IMU); guidance precise; ballistic missile

Cite this article

XIAO Zhenglin , MOU Jianhua , CHEN Fang , FU Min . The Using Method of IMU Testing Data Before Launching Based on the Best Guidance Precise[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2012 , 32(4) : 57 -60 . DOI: 10.15892/j.cnki.djzdxb.2012.04.039

[an error occurred while processing this directive]

References

[1]
钟万登 液浮惯性器件[M]. 北京: 中国宇航出版社, 1994.
[2]
肖正林, 徐军辉, 钱培贤. 惯性组合误差射前标定方法研究. 弹箭与制导学报, 2004, 24 (4): 362- 366.
[3]
鲜勇, 钱培贤. 惯性组合误差射前等效补偿方法研究[]. 飞行力学, 2001, 19 (3): 77- 79.
[4]
陈世年. 控制系统设计[M]. 北京: 中国宇航出版社, 1996.
[5]
周小刚, 肖正林, 钱培贤. 惯性测量组合射前动态标定误差分析. 战术导弹控制技术, 2004 (4): 27- 29.
Options
Outlines

/

〈 〉

[an error occurred while processing this directive]