Accuracy Error and Correction of Reentry Ballistic Missile Based on Stat Wind Field Model

YANG  Tao; CAO  Rui; LI  Liujian

doi:10.15892/j.cnki.djzdxb.2011.03.057

Journal of Projectiles, Rockets, Missiles and Guidance >

2011 , Vol. 31 >Issue 3: 180 - 182

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2011.03.057

BALLISTIC AND AIRDYNAMICS

Accuracy Error and Correction of Reentry Ballistic Missile Based on Stat Wind Field Model

YANG Tao ,
CAO Rui ,
LI Liujian

Expand

¹ The Second Artillery Engineering College, Xi'an 710025, China
² No. 96167 Unit, Fujian Yong'an 366000, China

Received date: 2010-03-16

Online published: 2025-05-30

Fold

Abstract

On the base of analyzing the affection of wind field that used in the ballistic computation and the method by changing the parameter of missile to correct of warhead wind field was put forward. The actual wind field parameter got by measurement was used to build a wind field error correction model. The ballistic simulation computation shows that the correction pattern created can effectively improve the accuracy of the reentry warhead, and the model is correct.

Key words： wind field; ballistic simulation; reentry warhead; accuracy error

Cite this article

YANG Tao , CAO Rui , LI Liujian . Accuracy Error and Correction of Reentry Ballistic Missile Based on Stat Wind Field Model[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2011 , 31(3) : 180 -182 . DOI: 10.15892/j.cnki.djzdxb.2011.03.057

[an error occurred while processing this directive]

References

[1]	张毅, 肖龙旭, 王顺宏. 弹道导弹弹道学[M]. 长沙: 国防科技大学出版社, 2005.
[2]	肖龙旭. 地地导弹弹道与制导[M]. 北京: 中国宇航出版社, 2003.
[3]	曲延禄. 外弹道气象学概论[M]. 北京: 气象出版社, 1987.
[4]	国家气象局卫星气象中心. 中国高空气象记录月报[R]. 北京: 1985-1990.
[5]	严佳民, 李智, 董利强. 弹道导弹再入气象修正[J]. 航天发射技术, 2001(2): 1-5.
[6]	程开甲, 李元正, 胡世祥等. 航天气象学[M]. 北京: 国防工业出版社, 2002.
[7]	张金槐. 远程火箭精度分析与评估[M]. 长沙: 国防科技大学出版社, 1995.
[8]	李洪儒, 叶鹏. 再入段风场对弹道导弹射击精度影响的仿真试验研究[J]. 战术导弹控制技术, 2006(4): 45-49.

Options

Outlines