脉冲式末端修正弹的修正能力及控制精度分析
Analysis of Correction Capability and Control Accuracy for Impulse Terminal Correcting Ammunition
谢金 , 王朋飞 . 脉冲式末端修正弹的修正能力及控制精度分析[J]. 弹箭与制导学报, 2014 , 34(6) : 83 -86 . DOI: 10.15892/j.cnki.djzdxb.2014.06.022
In view of the problem that ballistic characteristics of low speed rolling ammunition would be influenced when impulse engine working, simulation of ballistic characteristics was implemented. The influence of impulse engine position and ignition phase on the terminal correct ammunition's correction capability was analyzed and impulse engine ignition time and position error on the control precision was calculated. Thus it can provide a basis for the design of terminal correcting ammunition. The result shows that the requirement of correction capability can be achieved through adjusting the impulse engine position and ignition phase. The error of control caused by ignition time and position is less than 5.1%.
| [1] | 王涛. 脉冲式弹道修正弹的修正方法研究[D]. 南京: 南京理工大学, 2005. |
| [2] | 王朋飞, 曹红松, 刘务平, 等. 引信头锥摆动角对火箭弹气动特性及控制能力影响[J]. 弹箭与制导学报, 2013, 33(1): 152-154. |
| [3] | 李新国, 方群. 有翼导弹飞行动力学[M]. 西安: 西北工业大学出版社, 2005. |
| [4] | 姚文进, 王晓鸣, 高旭东, 等. 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): 19-21. |
| [5] | 赵捍东, 郭锡福, 王芳, 等. 侧推矢量在提高火箭弹射击精度的技术研究[J]. 弹箭与制导学报, 2005, 25(2): 72-74. |
/
| 〈 |
|
〉 |