[an error occurred while processing this directive] [an error occurred while processing this directive]
[an error occurred while processing this directive]Journal of Projectiles, Rockets, Missiles and Guidance >
Solution of Reentry Trajectory of Ballistic Missile Using Genetic Algorithm
Received date: 2009-10-10
Online published: 2025-05-28
Based on the mathematic model of reentry movement of ballistic missile, the method of adopting preprogram trajectory to penetrate was established and solution of the penetration trajectory using genetic algorithm was studied. The genetic algorithm model which took the angle of attack changing along with reentry time increasing as the object of coding was introduced and the simulation was continued. The simulation result shows genetic algorithm can carry out the accuracy result of reentry trajectory solution with high speed, this algorithm can make the choice for application.
Key words: ballistic missile; reentry trajectory; genetic algorithm
FAN Ruirui , WANG Minghai . Solution of Reentry Trajectory of Ballistic Missile Using Genetic Algorithm[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2010 , 30(5) : 156 -158 . DOI: 10.15892/j.cnki.djzdxb.2010.05.020
| [1] | 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, 1990. |
| [2] | 邢文训, 谢金星. 现代优化计算方法[M]. 北京: 清华大学出版社, 2005. |
| [3] | 钱杏芳, 林瑞雄, 赵亚男. 导弹飞行力学[M]. 北京: 北京理工大学出版社, 2000. |
/
| 〈 |
|
〉 |