|Table of Contents|

Methods to Improve Firing Accuracy of Ballistic Missiles

《南京理工大学学报》(自然科学版)[ISSN:1005-9830/CN:32-1397/N]

Issue:
2007年01期
Page:
10-16
Research Field:
Publishing date:
2007-02-28

Info

Title:
Methods to Improve Firing Accuracy of Ballistic Missiles
Author(s):
YANG Fan 12RUI Xiao-ting 1WANG Guo-ping 1
1.School of Power Engineering,NUST,Nanjing 210094,China;2.General Armament Department of the Chinese People’s Liberation Army,Beijing 100034,China
Keywords:
ballisticmissiles firingaccuracy systemdynamics launch flight
PACS:
TJ761.3
DOI:
-
Abstract:
From the view point of the weapon system, some new theories in the launch dynam ics and transferm atrix method of multibody syste mare used to study the method to improve the firingaccura-cy of ballisticm issilesandto analyze thecauses of errors influencing the missile accuracy. Basedon the exact description of  the quantitative relations between the dynamics performance and wholepa-rameters of the weapon system, anewtho ught to improve the firing accuracyofmissiles is discussed in theory, computation and experimen.t These provide new measure ments for improving the firing accuracy of missiles.

References:

[ 1] 芮筱亭, 陆毓琪,王国平, 等. 多管火箭发射动力学仿真与试验测试方法[M]. 北京: 国防工业出版社, 2003.
[ 2] 芮筱亭, 王国平, 陆毓琪,等. 提高多管火箭射击密集度新技术[ J]. 兵工学报, 2006, 27(2): 301-305.
[ 3] 杨帆, 王国平,芮筱亭, 等. 射击间隔对多管火箭动态特性的影响[ J]. 南京理工大学学报, 2006, 30 (4): 400- 403.\
[ 4] 王国平, 芮筱亭,杨帆, 等. 多体系统传递矩阵法在多管火箭动力学中的应用[ J]. 南京理工大学学报, 2006, 30( 4): 434- 438.
[ 5] 芮筱亭, 贠来峰,陆毓琪, 等. 多管火箭发射动力学研究[ J]. 兵工学报, 2004, 25(5): 556- 561.
[ 6] 蔡洪, 张士峰, 张金槐. Bayes试验分析与评估 [M]. 长沙:国防科技大学出版社, 2004.
[ 7] 杨辉耀. 弹道导弹制导精度提高与再入误差分析 [D]. 西北工业大学航空学院, 1995.
[ 8] 费景高. 捷联式制导系统中四元数的保范递推计算[ J]. 航天控制, 2000, 18(3): 37-43.
[ 9] 张毅, 杨辉耀, 李俊莉. 弹道导弹弹道学[M]. 长沙: 国防科技大学出版社, 1999.
[ 10] 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[ J]. 战术导弹控制技术, 2004( 4): 27- 29.
[ 11] 杨辉耀,鲜勇. 环境温度对导弹精度、最大射程的影响分析与修正[ J]. 航天控制, 2000, 18( 1): 20-25.
[ 12] InnocentiM. Nonlinear guidance techniques for agile missiles [ J]. Control Engineering Practice, 2001, 9 ( 10): 1131- 1144.
[ 13] 魏伟波, 芮筱亭. 精确制导技术研究[ J]. 火力与指挥控制, 2006, 31( 2): 5-8.
[ 14] MalyavejV, SavkinAV. The problemof optimal ro-bustKalmanstate estimationvia limitedcapacitydigi-t al communication channels [ J]. Systems&Control Letters, 2005, 54( 12): 4283- 4292.
[ 15] KimSeung-Hwan, KimYoon-Sik, Song Chanho. A robust adaptive nonlinear control approach to missile autopilot design [ J]. Control Engineering Practice, 2004, 12( 2): 149- 154.

Memo

Memo:
-
Last Update: 2007-02-28