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Volume 32 Issue 06
Jun.  2006
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Journal of Beijing University of Aeronautics and Astronautics  > 2006  >  32(06): 675-679.
Zhang Jinbai, Zheng Zhaohu. Direct numerical simulation of turbulent channel flow of polymer solution[J]. Journal of Beijing University of Aeronautics and Astronautics, 2009, 35(12): 1417-1420. (in Chinese)
Citation: Zhou Shengqiang, Xiang Jinwu. Hopfield network based approach to aircraft design[J]. Journal of Beijing University of Aeronautics and Astronautics, 2006, 32(06): 675-679. (in Chinese)
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Hopfield network based approach to aircraft design

  • School of Aeronautic Science and Technology, Beijing University of Aeronautics and Astronautics, Beijing 100083, China

  • Received Date: 20 Jun 2005
  • Publish Date: 30 Jun 2006
    Abstract
  • Combining augmented lagrange multiplier(ALM) method to Hopfield neural network(HNN), was proposed to solve nonlinear constrained optimization. HNNis taken as a dynamic approach for minimization subproblem in ALM method, only needing the first derivative of the Lagrange function. The random neural network was extended by adding Gaussian noise gradually reducing with the temperature, whose ablity escapeing from the attraction of the localminimum points was limitedby the initial temperature. Combined with the simulated annealing, an improved algorithm for Euler method was presented for numerical implementation of the network. The approach was applied to jet trainer aircraft preliminary optimization. The results show that the computing process is stable and the optimal result is enough precise. The trade-off of design requirements was studied through the Lagrange multipliers. An aerodynamic/structural design optimization for the wing of a trunkeliner was studied.

     

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  • [1] Tsirukis A G, Reklaitis G V. Nonlinear optimization using generalized Hopfield networks[J].Neural Computing and Applications, 1989,1:511-521 [2] Dhingra A K, Rao S S. A neural network based approach to mechanical design optimization[J].Engineering Optimization, 1992,20:187-203 [3] 吴剑国,赵丽萍．工程结构优化的神经网络方法[J]．计算力学学报 ,1998,15(1):69-74 Wu Jianguo,Zhao Liping. Neural network method for structural engineering optimization[J].Chinese Journal of Computational Mechnaics, 1998,15(1):69-74(in Chinese) [4] 丛爽,王怡雯.随机神经网络发展现状综述[J].控制理论与应用,2004,21(6):975-980 Cong Shuang, Wang Yiwen. Survey of current progress in random neural network .Control Theory & Applications, 2004, 21(6) :975-980(in Chinese) [5] 石晓荣,张明廉.一种基于混沌神经网络的拟人智能控制方法[J].北京航空航天大学学报,2004, 30(9):879-892 Shi Xiaorong,Zhang Minglian. Human-imitating control based on chaotic neural networks[J]. Journal of Beijing University of Aeronautics and Astronautics, 2004,30(9):879-892(in Chinese) [6] 叶世伟,郑宏伟,王文杰,等.连续时间Hopfield网络模型数值实现分析 .软件学报,2004,15(6):881-890 Ye Shiwei,Zheng Hongwei,Wang Wenjie, et al. Analysis for numerical implementation of continuous time Hopfield network model[J]. Journal of Software, 2004,15(6):881-890(in Chinese) [7] 方卫国,郦正能．基于全局敏度方程方法的飞机方案优化设计[J]．航空学报,1998,19(3):293-298 Fang Weiguo,Li Zhengneng. Aircraft scheme optimization design based on global sensitivity equation method[J]. Acta Aeronautica et Astronautica Sinica,1998,19(3):293-298(in Chinese) [8] 董波,张晓东,郦正能.干线客机机翼气动/结构综合设计研究[J].北京航空航天大学学报,2002, 28(4):435-437 Dong Bo, Zhang Xiaodong, Li Zhengneng. Integrated aerodynamic/structural design optimization for wing of trunkliner[J]. Journal of Beijing University of Aeronautics and Astronautics,2002, 28(4):435-437(in Chinese)
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