Full-Text Search:
Home|Journal Papers|About CNKI|User Service|FAQ|Contact Us|中文
《Aircraft Design》 2006-02
Add to Favorite Get Latest Update

Optimization Design Based on Hopfield Neural Network & KS-Function

ZHOU Sheng-qiang~()(School of Aeronautic Science and Engineering,Beijing University of Aeronautics and Astronautics,Beijing 100083,China)  
The principle of Hopfield neural network for optimization is presented.The numerical implementation of the network is transformed into the initial value problem of non-linear differential equations,and the ODE solver of MATLAB can be used.For multi-constraint optimization problems,KS function can agglomerate these constraints,the smooth and differentiable feature of which is favorable for the solution.The results from the application of the method to a non-liner constrained optimization and a parameter optimization for the conceptual design of an aircraft indicate that the method is effective.
【CateGory Index】: TP183
Download(CAJ format) Download(PDF format)
CAJViewer7.0 supports all the CNKI file formats; AdobeReader only supports the PDF format.
【Citations】
Chinese Journal Full-text Database 3 Hits
1 Fang Weiguo , Li Zhengneng (Institute of Aircraft Design, Beijing University of Aeronautics and Astronautics, Beijing, 100083);AIRCRAFT SCHEME OPTIMIZATION DESIGN BASED ON GLOBAL SENSITIVITY EQUATION METHOD[J];ACTA AERONAUTICA ET ASTRONAUTICA SINICA;1998-03
2 WAN Chao yan,ZHAO Wen zhong,LI Xiao feng,Ma Si qun (Dept. of Mechanical Engineering, Dalian Railway Institute, Dalian 116028,China);Study on solving problems of multi-constraint optimization based on KS function[J];Journal of Machine Design;2003-09
3 CONG Shuang, WANG Yi-wen(Department of Automation,University of Science & Technology of China,Hefei Anhui 230027,China);Survey of current progress in random neural network[J];Control Theory & Applications;2004-06
【Co-citations】
Chinese Journal Full-text Database 10 Hits
1 Zhou Shengqiang Xiang Jinwu(School of Aeronautic Science and Technology,Beijing University of Aeronautics and Astronautics,Beijing 100083,China);Hopfield network based approach to aircraft design[J];Journal of Beijing University of Aeronautics and Astronautics;2006-06
2 Jiang Huan Zhou Hao Chen Wanchun(School of Astronautics,Beijing University of Aeronautics and Astronautics,Beijing 100191,China)Yang Baokui(The Third Academy,China Aerospace Science and Industry Corporation,Beijing 100074,China);Multilayer trajectory optimization design for surface-to-air missile based on global sensitivity equation method[J];Journal of Beijing University of Aeronautics and Astronautics;2009-12
3 CHEN Yong-liang1,ZHOU Bin2,LI Xue-bin1(1.Institute of Mineral Resources Prognosis on Synthetic Information,Jilin University,Changchun 130026,China 2.College of Computer Science and Technology,Jilin University,Changchun 130012,China);Mineral target prediction based on Boltzmann machines[J];Progress in Geophysics;2012-01
4 LIU Tong1,XU Yuan-ming1,LI Shuo2,ZHAO Wen2(1.School of Aeronautic Science and Engineering,Beijing University of Aeronautics and Astronautics,Beijing 100083,China)(2.China Academy of Launch Vehicle Technology,Beijing 100076,China);Development and Application of the Particle Swarm Optimization Plug-in Based on HyperDesign Platform[J];Aircraft Design;2009-06
5 ZHOU Sheng-qiang,XIANG Jin-wu(School of Aeronautic Science and Technology,Beijing University of Aeronautics andAstronautics,Beijing 100083,China);Multi-objective robust optimization method to aircraft conceptual design[J];Journal of Engineering Design;2006-06
6 SUI Yun-kang,WANG Xiao-guang(College of Mechanical Engineering and Applied Electronics Technology,Beijing University of Technology,Beijing 100124,China);A Solution Method on Condense Single Constraint by Using K-S Function for Nonlinear Programming[J];Journal of Beijing University of Technology;2013-07
7 ;Collaborative Optimization Based on KS Function and Its Application[J];Aeronautical Manufacturing Technology;2011-06
8 HE Lie tang, ZENG Qing hua (Institute of Aerospace and Material Engine,NUDT,Changsha 410073,China)$$$$;The Aerodynamic Figuration Optimize Design of Micro Air Vehicle[J];Aeronautical Computer Technique;2002-04
9 JIANG Ya-nan,WANG He-ping(School of Aeronautics,Northwestern Polytechnical University,Xi′an 710072,China);Robust Design Optimization Method to Aircraft Based on Sensitivity Analysis[J];Aeronautical Computing Technique;2009-05
10 GU Liang-xian,QIU Li-kuan,GONG Chun-lin(School of Aeronautics,Northwestern Polytechnical University,Xi′an 710072,China);Study on Global Sensitivity Analysis Method[J];Aeronautical Computing Technique;2011-01
【Secondary Citations】
Chinese Journal Full-text Database 2 Hits
1 WAN Chao-yan, LI Xiao-feng, ZHAO Wen-zhong (Dept. of Mechanical Engineering, Dalian Railway Institute, Dalian 116028, China);A New Method Solving Linear Programming Problem[J];Journal of Dalian Railway Institute;2003-01
2 Wan Chaoyan 1) Zhao Wenzhong 1) Cao Jialian 2) 1)(Department of Mechanical Engineering, Dalian Railway Institute, Dalian 116028) 2)(Department of Electrical Engineering, Dalian Railway Institute, Dalian 116028);Higher Order Smooth Fitting for SD Space Convex Body by Multiple Functions[J];Journal of Computer Aided Design & Computer Graphics;2003-03
©2006 Tsinghua Tongfang Knowledge Network Technology Co., Ltd.(Beijing)(TTKN) All rights reserved