Advanced Search
Volume 33 Issue 02
Feb.  2007
Turn off MathJax
Article Contents
Journal of Beijing University of Aeronautics and Astronautics  > 2007  >  33(02): 176-179.
Li Zhongming, Jiao Zongxia, Wang Kejunet al. Optimum design of erecting system[J]. Journal of Beijing University of Aeronautics and Astronautics, 2007, 33(02): 176-179. (in Chinese)
Citation: Li Zhongming, Jiao Zongxia, Wang Kejunet al. Optimum design of erecting system[J]. Journal of Beijing University of Aeronautics and Astronautics, 2007, 33(02): 176-179. (in Chinese)
shu

Optimum design of erecting system

  • School of Automation Science and Electrical Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100083, China

  • Received Date: 22 Mar 2006
  • Publish Date: 28 Feb 2007
    Abstract
  • Optimum design of erecting system was analyzed from the points of view of rapidity and acting force, and the objective function of optimization wa s established. Each objective function was nondimensionalized, and the multiobje ctive optimization function was solved by conventional weighting method. Sample point was appointed by uniform design. The polynomial response surface model was set up based on sample experimental data of collaborative simulation. Multidisc iplinary design optimization of the position of key pivots on some erecting syst em was carried out. The polynomial response surface method was compared with con ventional multiobjective optimization method through the evaluation function con structed. It shows that the polynomial response surface method is effective by a nalyzing the difference between the two methods. This method is a favorable tool for further development and design of erecting system.

     

    • FullText(HTML)
  • loading
    • References(1)
  • [1] 黄先祥,高钦和,郭晓松. 大型装置起竖过程的动力学建模研究[J]. 系统仿真学报,2002,14(3):271-273 Huang Xianxiang,Gao Qinhe, Guo Xiaosong. Dynamic modeling of erected process f or large mechanism[J]. Journal of System Simulation,2002,14(3):271-273(in Chinese) [2] Golovidov O, Kodiyalam S, Marineau P. Flexible implementation of approximation concepts in an MDO framework . AIAA-98-4959,1998 [3] Timothy W S,Timothy M M, John J K. Kriging model for global approximatio n in simulation-based multidisciplinary design optimization[J]. AIAA Journal ,2001, 39(12):2233-2241 [4] Kodiyalam S, Yang R J, Gu L. High-performance computing and surrogate mo deling for rapid visualization with multidisciplinary optimization[J]. AIAA J ournal,2004, 42(11):2347-2354 [5] 王小妮,余雄庆. 大展弦比联结翼结构重量估算[J].北京航空航天大学学报,2005,31(12):1289-1292 Wang Xiaoni, Yu Xiongqing. Predictions of structural weight for high aspect rati o joined-wings[J]. Journal of Beijing University of Aeronautics and Astronaut ics, 2005,31(12):1289-1292(in Chinese) [6] Kodiyalam S, Lin J, Wujek B. Design of experiments based response surface models for design optimization . AIAA-98-2030, 1998 [7] 方开泰,马长兴. 正交与均匀试验设计[M]. 北京:北京科学出版社,200 1 Fang Kaitai, Ma Changxing. Orthogonal and uniform design of experiment[M].Beijing:Science Press, 2001(in Chinese) [8] 高钦和,黄先祥. 多级缸起竖系统运动过程的建模与仿真[J].系统仿真学报,2005,17(7):1563－1565 Gao Qinhe,Huang Xianxiang. Dynamic modelling and simulation of erecting system w ith multi-stage cylinder[J]. Journal of System Simulation,2005,17(7):1563 －1565(in Chinese)
    • Relative Articles
    • Supplements(0)
    • Cited By
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索
    Get Citation
    PDF
    XML

    Article Metrics

    Article views(2606) PDF downloads(1021) Cited by()
    Proportional views
    Related

    Copyright © Journal of Beijing University of Aeronautics and Astronautics

    Address: Editorial Department of Journal of Beijing University of Aeronautics and Astronautics, 37 Xueyuan Road, Haidian District, Beijing Post Code: 100191 Email: jbuaa@buaa.edu.cn

    Supported by: Beijing Renhe Information Technology Co., Ltd.    

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return