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弹道修正弹脉冲修正机构简易控制方法
引用本文:姚文进,王晓鸣,高旭东,李文彬. 弹道修正弹脉冲修正机构简易控制方法[J]. 弹道学报, 2007, 19(3): 19-22
作者姓名:姚文进  王晓鸣  高旭东  李文彬
作者单位:南京理工大学,机械工程学院,南京,210094
摘    要:建立了采用脉冲力控制的弹道修正弹飞行弹道模型.利用均匀设计方法,通过回归分析研究了脉冲修正起始时间、脉冲力级数、弹丸射角以及作用角度对修正效果的影响,推导出关系模型,利用该模型提出了一种简易的脉冲力控制方法.仿真结果证实该简易方法控制脉冲发动机工作能够有效提高弹丸的命中精度,对脉冲发动机在弹道修正弹上的工程应用有一定的参考意义.

关 键 词:弹道修正弹  脉冲修正  均匀设计  简易控制
文章编号:1004-499X(2007)03-0019-04
修稿时间:2006-10-11

A Simple Control Method for Impulse Correction Device in Trajectory Correction Projectile
YAO Wen-jin,WANG Xiao-ming,GAO Xu-dong,LI Wen-bin. A Simple Control Method for Impulse Correction Device in Trajectory Correction Projectile[J]. Journal of Ballistics, 2007, 19(3): 19-22
Authors:YAO Wen-jin  WANG Xiao-ming  GAO Xu-dong  LI Wen-bin
Affiliation:College of Mechanical Engineering, NUST, Nanjing 210094, China
Abstract:The trajectory correction projectile model using impulse was established. Based on the theory of equality design and method of regression analysis, effect of the starting time, impulse number, elevation angle and acting angle on the correction ability was studied. The relationship model was deduced. According to this model, one simple control method was put forward. The simulation results show this method can improve the hitting precision effectively. This method is useful in the engineering application of impulse engine in trajectory correction projectile.
Keywords:trajectory correction projectile   impulse correction   design of equality   simple control
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