|Table of Contents|

Simulation on Attack Angle Motion for Controlled Projectile with Canard

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

Issue:
2009年02期
Page:
242-246
Research Field:
Publishing date:

Info

Title:
Simulation on Attack Angle Motion for Controlled Projectile with Canard
Author(s):
LI Yan1WANG Zhong-yuan1YI Wen-jun2CHEN Yang2
1.School of Power Engineering;2.National Key Laboratory of Transient Physics,NUST,Nanjing 210094,China
Keywords:
canards ballistics models attack angle motion transfer function average force in period
PACS:
TJ413.6
DOI:
-
Abstract:
In order to research dynamic process of the attack angle for controlled projectile under canard control,and seek the better control mode of the canard,taking the shell with a pair of canards for example,a 6-DOF(degree of freedom) rigid trajectory model with canard control is built to research the effect control progress of the attack angle.The control transfer function is deduced for predigesting analysis in feature points.The numerical calculation and simulation by MATLAB show that the maximal average force in period can not only improve manipulative efficiency but also lead to intensive swing of the angle.This is not suit for the shell demand with high stability.

References:

[ 1] 王中原, 丁松滨, 王良明. 弹道修正弹在脉冲力矩作用下的飞行稳定性条件[ J] . 南京理工大学学报, 2000, 24( 4): 322- 325.
[ 2] 宋丕极. 枪炮与火箭外弹道学[M ] . 北京: 兵器工业出版社, 1993. 115- 122.
[ 3] 王中原, 周卫平. 外弹道设计理论与方法[M ]. 北京: 科学出版社, 2004. 44- 46.
[ 4] 袁子怀, 钱杏芳. 有控飞行力学与计算机仿真[M ]. 北京: 国防工业出版社, 2001. 183- 257.
[ 5] Curtis P M, B re tt R D. Optim a l contro l solution for dua l( ta il and canard) controlled m iss iles[ R]. AIAA, 2006- 6569.

Memo

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Last Update: 2012-11-19