| 防空导弹垂直发射转弯优化设计的新方法 |
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| 引用本文： | 李向林,于本水.防空导弹垂直发射转弯优化设计的新方法[J].现代防御技术,2000,28(5):44-50. |
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| 作者姓名： | 李向林 于本水 |
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| 作者单位： | 中国航天机电集团二院二部,北京,100854 |
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| 摘 要： | 防空导弹采用垂直发射方式时 ,最重要的要求就是导弹发射后在最短的时间内以最小转弯半径完成程序转弯 ,所以是一个快速最优控制问题 ,文章对连续系统的最优控制进行离散化 ,从而应用遗传算法对防空导弹垂直发射转弯程序进行了优化设计
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| 关 键 词： | 最优控制 遗传算法 离散化 防空导弹 垂直发射转弯 |
| 修稿时间： | 1999-12-06 |
A New Method of Optimal Design of Air-defense Missile's Vertical Launch and Turning |
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| LI Xiang-lin,YU Ben-shui.A New Method of Optimal Design of Air-defense Missile''s Vertical Launch and Turning[J].Modern Defence Technology,2000,28(5):44-50. |
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| Authors: | LI Xiang-lin YU Ben-shui |
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| Abstract: | As the antiaircraft missile adopts the vertical launch,the most important requirement is that the missile finishes the program turning with the least turning radius in the shortest time.This is a problem of quick optimal control.In this paper,the technique of discretization of optimal control of continuous system is used and genetic algorithm is also applied to optimize the vertical launch and turning program of antiaircraft missile. |
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| Keywords: | Optimal control Genetic algorithm Discretization Antiaircraft missile Vertical launch and turning |
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