首页 | 本学科首页   官方微博 | 高级检索  
     检索      

求解航空发动机数学模型的混合智能方法
引用本文:杨伟,冯雷星,彭靖波,王海涛.求解航空发动机数学模型的混合智能方法[J].推进技术,2008,29(5):614-616.
作者姓名:杨伟  冯雷星  彭靖波  王海涛
作者单位:空军工程大学,工程学院,陕西,西安,710038
摘    要:针对传统求解方法收敛性不强而遗传算法求解效率较低的问题,利用BP神经网络逼近发动机平衡方程的反函数,将求解结果作为Newton-Raphson法的初值,提出了求解模型的混合智能方法。仿真结果表明,该方法可以保证非线性数学模型在整个飞行包线范围内收敛,与遗传算法相比又提高了求解效率。

关 键 词:航空发动机  数学模型  平衡方程  神经网络

An intelligent algorithm for solution of nonlinear mathematical model for aeroengine
YANG Wei,FENG Lei-xing,PENG Jing-bo and WANG Hai-tao.An intelligent algorithm for solution of nonlinear mathematical model for aeroengine[J].Journal of Propulsion Technology,2008,29(5):614-616.
Authors:YANG Wei  FENG Lei-xing  PENG Jing-bo and WANG Hai-tao
Institution:(Engineering Inst.,Air Force Engineering Univ.,Xi’an 710038,China)
Abstract:Current solutions are not always convergent while genetic algorithm is inefficient.Because of this,BP neural networks was used to approach the inverse function of balance equations,and the approximate solution was used as the initial value of Newton-Raphson algorithm,thus an intelligent algorithm is proposed.Simulation results show that this algorithm can make nonlinear mathematical model for aeroengine convergent in the entire flight envelope,and also has higher efficiency compared with genetic algorithm.
Keywords:Aeroengine  Mathematical model  Balance equations  Neural networks
本文献已被 CNKI 万方数据 等数据库收录!
点击此处可从《推进技术》浏览原始摘要信息
点击此处可从《推进技术》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号