Citation: | Rong Xiaomin, Xu Yuanming, Wu Decaiet al. Computational intelligence technology for optimal design of grid-stiffened composite structure[J]. Journal of Beijing University of Aeronautics and Astronautics, 2006, 32(08): 926-929. (in Chinese) |
[1] 丁永生.计算智能:理论、技术与应用[M].北京:科学出版社,2004 Ding Yongsheng.Computational intelligence:theory,technology and application . Beijing:Science Press,2004(in Chinese) [2] Xu Yuanming,Li Shuo,Rong Xiaomin. Composite structural optimization by genetic algorithm and neural network response surface modeling[J].Chinese Journal of Aeronautics,2005,18(4):310-316 [3] Collier C, Yarrington P, Van West B. Composite,grid-stiffened panel design for post buckling using hypersizer Collect Tech Pap AIAA ASME ASCE AHS Struct Struct Dyn Mater. Alexandria,VA:AIAA,2002,1:157-172 [4] Stanley K O,Miikkulainen R. Efficient reinforcement learning through evolving neural network topologies Proceeding of the Genetic and Evolutionary Computation Conference(GECCO-2002). San Francisco:Morgan Kaufmann Publishers Inc,2002:569-577 [5] 潘正君,康立山,陈毓屏.演化计算[M],北京:清华大学出版社,1998 Pan Zhengjun,Kang Lishan,Chen Yuping. Evolutionary computation[M].Beijing:Tsinghua University Press,1998(in Chinese) [6] 李敏强,徐博艺.遗传算法与神经网络的结合[J].系统工程理论与实践,1999(2):65-69 Li Minqiang,Xu Boyi. On the combination of genetic algorithms and neural networks[J]. Journal Systems Science and Systems Engineering,1999(2):65-69(in Chinese) [7] Barbosa H J C, Lemonge A C C.A new adaptive penalty scheme for genetic algorithms[J].Information Sciences,2003,156(3-4):215-251 [8] Jaunky N,Knight N F Jr,Ambur D R.Optimal design of grid-stiffened composite panels using global and local buckling analyses[J].Journal of Aircraft,1998,35(3):478-486
|