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[1]王鹏,李旭昌,徐颖军,等.固体火箭发动机总体优化设计[J].火箭推进,2007,33(04):16-19.
　Wang Peng,Li Xuchang,Xu Yingjun.The optimal design of solid rocket motors[J].Journal of Rocket Propulsion,2007,33(04):16-19.
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固体火箭发动机总体优化设计

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V] 卷: 33 期数: 2007年04期 页码: 16-19 栏目: 研究与设计 出版日期: 2007-08-30
Title:
The optimal design of solid rocket motors
作者:
王鹏；李旭昌；徐颖军；
空军工程大学导弹学院；空军工程大学导弹学院陕西西安713800；陕西西安713800；
Author(s):
Wang Peng; Li Xuchang; Xu Yingjun
Missile Institute of Air Force Engineering University,Xi’an 713800,China
关键词:
固体火箭发动机; 遗传算法; 惩罚函数
分类号:
V435
文献标志码:
A
摘要:
通过遗传算法与惩罚函数相结合对固体火箭发动机总体进行优化设计,令体积比冲IV为目标函数,并采用交叉概率和变异概率的自适应调整性,有效地加快了搜索。用此方法对算例发动机各参数和目标函数优化,避免了设计变量之间较为复杂的相互关系,得到固体火箭发动机体积比冲的全局最优解,提高了整体性能。

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更新日期/Last Update: 1900-01-01