Advanced Search
Volume 39 Issue 2
Feb.  2013
Turn off MathJax
Article Contents
Journal of Beijing University of Aeronautics and Astronautics  > 2013  >  39(2): 239-243.
Liang Haoquan, Zhu Ming, Jiang Guangtai, et al. Conceptual design optimization of stratosphere airship based on improved CO-RS[J]. Journal of Beijing University of Aeronautics and Astronautics, 2013, 39(2): 239-243. (in Chinese)
Citation: Liang Haoquan, Zhu Ming, Jiang Guangtai, et al. Conceptual design optimization of stratosphere airship based on improved CO-RS[J]. Journal of Beijing University of Aeronautics and Astronautics, 2013, 39(2): 239-243. (in Chinese)
shu

Conceptual design optimization of stratosphere airship based on improved CO-RS

  • School of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

  • Received Date: 22 Nov 2011
  • Publish Date: 28 Feb 2013
    Abstract
  • An improved collaborative optimization based on response surface(CO-RS) methodology was developed to be well applied to the engineering design. The response surface was constructed independent on gradient by augmented Lagrange and trust region optimization methods. System mission requirements and disciplinary coupling relations of stratosphere airship were analyzed in the framework of improved CO-RS.multidisciplinary design optimization(MDO) model coupled with dynamics and propulsion subsystem, structure subsystem, and energy subsystem analysis models was established with total mass as the objective for stratosphere airship conceptual design. Using the iSIGHT software to construct the solving architecture, the MDO model and analysis models were simulated and calculated with the improved CO-RS methodology. The results prove the rationality of the MDO model and the effectiveness of the improved CO-RS methodology in stratosphere airship conceptual design optimization.

     

    • FullText(HTML)
  • loading
    • References(19)
  • [1]
    Pant R S.Methodology for determination of baseline specifications of a nonrigid airship[J].Journal of Aircraft,2008,45(6):2177-2182
    [2]
    Ozoroski T A,Mas K G,Hahn A S.A PC-based design and analysis system for lighter-than-air unmanned vehicles [R].AIAA 2003-6566,2003
    [3]
    Kanikdale T S,Marathe A G,Pant R S.Multidisciplinary optimization of airship envelope shape[C]// 10th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference.Albany:AIAA,2004:1-21
    [4]
    Lutz T,Wagner S.Drag reduction and shape optimization of airship bodies[J].Journal of Aircraft,1998,35(3):345-351
    [5]
    Ram C V,Pant R S.An MDO approach to shape optimization of aerostat envelopes [R].AIAA 2006-1613,2006
    [6]
    Ram C V,Pant R S.Multidisciplinary shape optimization of aerostat envelopes[J].Journal of Aircraft,2010,47(3):1073-1076
    [7]
    Wang X,Shan X.Shape optimization of stratosphere airship[J].Journal of Aircraft,2006,43(1):283-287
    [8]
    Wang Q,Chen J,Fu G,et al.A methodology for optimization design and analysis of stratosphere airship[J].Aeronautical Journal,2009,113(1146):533-540
    [9]
    Sobieski I,Kroo I.Aircraft design using collaborative optimization[C]// 34th AIAA Aerospace Sciences Meeting and Exhibit.Reno:AIAA,1996
    [10]
    Roth B,Kroo I.Enhanced collaborative optimization:application to an analytic test problem and aircraft design[C]// 12th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference.Victoria:AIAA,2008
    [11]
    Braun R D,Moore A A,Kroo I M.Use of the collaborative optimization architecture for launch vehicle design[C]//6th AIAA/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization.Bellevue:AIAA,1996
    [12]
    Braun R D,Moore A A,Kroo I M.Collaborative approach to launch vehicle design[J].Journal of Spacecraft and Rockets,1997,34(4):478-486
    [13]
    Budianto I A,Olds J R.Design and deployment of a satellite constellation using collaborative optimization[J].Journal of Spacecraft and Rockets,2004,41(6):956-963
    [14]
    Sobieski I P,Manning V M,Kroo I M.Response surface estimation and refinement in collaborative optimization [R].AIAA 98-4753,1998
    [15]
    Sobieski I P,Kroo I M.Collaborative optimization using response surface estimation[J].AIAA Journal,2000,38(10):1931-1938
    [16]
    Rodriguez J F,Renaud J E,Watson L T.Trust region augmented Lagrangian methods for sequential response surface approximation and optimization[J].Journal of Mechanical Design,1998,120(1):58-66
    [17]
    王振国,陈小前,罗文彩,等.飞行器多学科设计优化理论与应用研究[M].北京:国防工业出版社,2006:268 Wang Zhenguo,Chen Xiaoqian,Luo Wencai,et al.Research on the theory and application of multidisciplinary design optimization of flight vehicles [M].Beijing:National Defense Industry Press,2006:268(in Chinese)
    [18]
    Liang H Q,Zhu M,Guo X,et al.Conceptual design optimization of high altitude airship in concurrent subspace optimization .AIAA 2012-1180,2012
    [19]
    李崇银,李琳,谭言科,等.平流层气候[M].北京:气象出版社,2008:79-89 Li Chongyin,Li Lin,Tan Yanke,et al.Stratospheric climate[M].Beijing:China Meteorological Press,2008:79-89(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(1924) PDF downloads(763) 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@cqjj8.com

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

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return