[an error occurred while processing this directive] [an error occurred while processing this directive] [an error occurred while processing this directive]
[an error occurred while processing this directive]
弹道与气动力技术

遗传算法解算弹道导弹再入弹道

  • 范锐锐 ,
  • 王明海
展开
  • 第二炮兵工程学院,西安 710025

范锐锐(1985-),男,安徽繁昌人,硕士研究生,研究方向:飞行动力学和制导理论。

收稿日期: 2009-10-10

  网络出版日期: 2025-05-28

Solution of Reentry Trajectory of Ballistic Missile Using Genetic Algorithm

  • FAN Ruirui ,
  • WANG Minghai
Expand
  • The Second Artillery Engineering College, Xi'an 710025, China

Received date: 2009-10-10

  Online published: 2025-05-28

摘要

基于弹道导弹再入段运动数学模型,提出了预定程序弹道再入突防的方法并进行了遗传算法解算突防弹道的研究。建立了以攻角随再入时间增长的变化量为编码对象的遗传算法模型并进行仿真计算。仿真结果表明,该算法能够实现预定程序再入弹道快速高精度的解算,具有工程的应用价值。

本文引用格式

范锐锐 , 王明海 . 遗传算法解算弹道导弹再入弹道[J]. 弹箭与制导学报, 2010 , 30(5) : 156 -158 . DOI: 10.15892/j.cnki.djzdxb.2010.05.020

Abstract

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.

[an error occurred while processing this directive]

参考文献

[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.
文章导航

/

[an error occurred while processing this directive]