Journal of Projectiles, Rockets, Missiles and Guidance >
An Effective Trajectory Fitting Method Based on NN
Received date: 2013-05-19
Online published: 2025-05-30
As for large-scale ballistic simulation, traditional data solution costs much time and calculation, can hardly satisfy the requirement of fast operation response. In this article, an effective curve coefficient fitting method was put forward based on BP NN via constructing equation of main factors of ballistic curve and time, studying the relationship between equation coefficient and launching parameter, the missile curve was fit quickly. The simulation result shows that this method is more effective than the method of traditional data solution for calculating multiple trajectories.
Key words: NN; ballistic curve; coefficient fitting
DONG Xiongfeng , LIU Xinxue , WANG Datong , MENG Shaofei . An Effective Trajectory Fitting Method Based on NN[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2014 , 34(2) : 135 -138 . DOI: 10.15892/j.cnki.djzdxb.2014.02.036
| [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, 1999. |
| [2] | 高洪月. 弹道导弹的弹道设计与仿真[D]. 哈尔滨: 哈尔滨工业大学, 2010. |
| [3] | 王辉, 田劲松, 张莉英. 基于飞行时间的弹道导弹火力控制[J]. 火力指挥与控制, 2005, 30(2): 85-87. |
| [4] | 马莉. MATLAB 语言实用教程[M]. 北京: 清华大学出版社, 2010. |
| [5] | MATLAB中文论坛. MATLAB 神经网络30个案例分析[M]. 北京: 北京航空航天大学出版社, 2010. |
| [6] | 杨磊, 李擎. MATLAB 在弹道仿真中的应用[J]. 计算机仿真, 2008, 25(1): 58-61. |
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