基于BLISS和PMA的多学科可靠性设计优化

doi:10.7527/S1000-6893.2013.0377

固体力学与飞行器总体设计

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基于BLISS和PMA的多学科可靠性设计优化

刘云平¹, 张俊², 张冰², 孙瑾³

1. 南京信息工程大学信息与控制学院, 江苏南京 210044;
2. 山东水利职业学院机电工程系, 山东日照 276826;
3. 中信建设有限责任公司, 北京 100027

收稿日期:2012-10-29 修回日期:2012-12-25 出版日期:2013-10-25 发布日期:2012-12-29
通讯作者: 刘云平,Tel.: 025-58731276 E-mail: liuyunping2010@163.com E-mail:liuyunping2010@163.com
作者简介:刘云平男, 博士, 讲师。主要研究方向: 多学科可靠性设计, 机器人动力学与控制。 Tel: 025-58731276 E-mail: liuyunping2010@163.com;张俊女, 学士, 讲师。主要研究方向: 机械设计与模具创新设计。 Tel: 0633-8170099 E-mail: zhangjun_dw@163.com;张冰男, 硕士, 讲师。主要研究方向: 模具设计与优化。 Tel: 0633-8170099 E-mail: zhangbing@vip.163.com;孙瑾女, 硕士, 工程师。主要研究方向: 结构设计与多学科优化、自动控制。 Tel: 010-59327930 E-mail: sunjin1028@163.com
基金资助:
国家自然科学基金 (51175019,51205238);江苏省自然科学基金(BK20130999);江苏省普通高校自然科学研究资助项目(13KJB460012);中国博士后科学基金(230210235)

Multidisciplinary Reliability Design and Optimization Based on BLISS and PMA

LIU Yunping¹, ZHANG Jun², ZHANG Bing², SUN Jin³

1. College of Information and Control, Nanjing University of Information Science & Technology, Nanjing 210044, China;
2. Department of Mechanical & Electrical Engineering, Shandong Water Polytechnic, Rizhao 276826, China;
3. CITIC Construction Co., Ltd., Beijing 100027, China

Received:2012-10-29 Revised:2012-12-25 Online:2013-10-25 Published:2012-12-29
Supported by:
National Natural Science Foundation of China (51175019,51205238);Natural Science Foundation of Jiangsu Province (BK20130999);Natural Science Foundation of Colleges and Universities in Jiangsu Province (13KJB460012);Postdoctoral Science Foundation of China (230210235)

摘要/Abstract

摘要：

针对多学科设计优化(MDO)中考虑不确定性而带来的计算复杂性问题,采用序列优化与可靠性评估(SORA)法的解耦思想,提出了基于两级集成系统综合(BLISS)策略和性能测量法(PMA)的多学科可靠性设计优化(RBMDO)方法。该方法将传统的3层嵌套循环的RBMDO方法过程解耦为顺序执行的确定性多学科设计优化(DMDO)和多学科可靠性分析(MRA),DMDO和MRA均采用BLISS策略进行计算,避免了每次多学科设计优化对完整可靠性分析模型的反复调用。飞机起落架缓冲器算例结果表明,文中方法的计算效率较其他两种方法分别提高了52.01%和26.51%,验证了方法的有效性。

关键词: 两级集成系统综合, 性能测量法, 多学科可靠性设计优化, 可靠性, 缓冲器

Abstract:

In order to solve the computational complexity caused by the consideration of uncertainties in multidisciplinary design optimization (MDO), an efficient method for reliability-based MDO (RBMDO) based on the bi-level integrated system synthesis (BLISS) and performance measure approach (PMA) is proposed. With the decoupling idea of sequential optimization and reliability assessment (SORA) method, the conventional triple nested loop of RBMDO is decoupled into a series of sequential execution of deterministic multidisciplinary design optimization (DMDO) and multidisciplinary reliability analysis (MRA). Both the DMDO and MRA are implemented by BLISS, which avoids the total computation of the whole multidisciplinary reliability analysis model iteratively in each RBMDO cycle. Finally, a shock absorber of landing gear example has been demonstrated to verify the efficiency of the proposed method, which shows that the efficiency of the proposed method has been improved by 52.01% and 26.51% respectively compared to the other two methods.

Key words: bi-level integrated system synthesis, performance measure approach, reliability-based multidisciplinary design optimization, reliability, absorber

中图分类号:

V222

刘云平, 张俊, 张冰, 孙瑾. 基于BLISS和PMA的多学科可靠性设计优化[J]. 航空学报, 2013, 34(10): 2349-2356.

LIU Yunping, ZHANG Jun, ZHANG Bing, SUN Jin. Multidisciplinary Reliability Design and Optimization Based on BLISS and PMA[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2013, 34(10): 2349-2356.

参考文献

[1] Sobieski J S, Haftka R T. Multidisciplinary aerospace design optimization: survey of recent developments. Structural and Multidisciplinary Optimization, 1997, 14(1): 1-23.
[2] Wu B B, Huang H, Wu W R. Multidisciplinary design optimization of main parameter of spacecraft with subvehicles. Acta Aeronautica et Astronautica Sinica, 2011, 32(4): 682-635.(in Chinese) 吴蓓蓓, 黄海, 吴文瑞. 带子星航天器总体参数多学科设计优化. 航空学报, 2011, 32(4): 682-635.
[3] Kang Z, Luo Y. Reliability-based structural optimization with probability and convex set hybrid models. Structural and Multidisciplinary Optimization, 2010, 42(1): 89-102.
[4] Yu M, Liu Y S, Li L R, et al. Reliability-based multidisciplinary design optimization of centrifugal impeller with double-loop strategy. Acta Aeronautica et Astronautica Sinica, 2012, 33(4): 650-657.(in Chinese) 于明, 刘永寿, 李磊瑞, 等. 基于双循环的离心叶轮多学科可靠性优化设计. 航空学报, 2012, 33(4): 650-657.
[5] Yao W, Chen X Q, Zhao Y, et al. A fractionated spacecraft system assessment tool based on lifecycle simulation under uncertainty. Chinese Journal of Aeronautics, 2012, 25(1): 71-82.
[6] Sues R H, Cesare M A. An innovative framework for reliability-based MDO. AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. Atlanta: American Society of Mechanical Engineers, 2000: 1-8.
[7] Padmanabhan D, Batill S M. Decomposition strategies for reliability based optimization in multidisciplinary system design.AIAA/USAF/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization. Atlanta: American Society of Mechanical Engineers, 2002: 1-15.
[8] Agarwal H, Renaund J E, Mark J D. A decomposition approach for reliability-based optimization in multidisciplinary system design. Proceedings of the 44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. Norfolk: American Society of Mechanical Engineers, 2000: 3439-3448.
[9] Ahn J, Kwon J H. An efficient strategy for reliability-based multidisciplinary design optimization using BLISS. Structure and Multidisciplinary Optimization, 2006, 31(5): 363-372.
[10] Du X, Guo J, Harish B. Sequential optimization and reliability assessment for multidisciplinary systems design. Structural and Multidisciplinary Optimization, 2008, 35(2): 117-130.
[11] Huang H Z, Yu H, Yuan Y H, et al. Individual disciplinary feasible method for reliability based multidisciplinary design optimization. Acta Aeronautica et Astronautica Sinica, 2009, 30(10): 1871-1876. (in Chinese) 黄洪钟, 余辉, 袁亚辉, 等. 基于单学科可行法的多学科可靠性设计优化. 航空学报, 2009, 30(10): 1871-1876.
[12] Fan H, Li W J. An efficient method for reliability-based multidisciplinary design optimization. Chinese Journal of Aeronautics, 2008, 21(4): 335-340.
[13] Tong L S, Shi B Q, Shen Y H, et al. First-order reliability method based multidisciplinary design optimization on gear transmission. Journal of Mechanical Engineering, 2010, 46(3): 42-46. (in Chinese) 仝令胜, 石博强, 申焱华, 等. 基于FORM的齿轮传动多学科优化. 机械工程学报, 2010, 46(3): 42-46.
[14] Sun J X, Zhang L Q, Chen J J, et al. Reliability-based multidisciplinary design optimization integrating collaborative optimization strategy and performance measurement approach. Journal of Computer-Aided Design & Computer Graphics, 2011, 23(8): 1373-1379. (in Chinese) 孙建勋, 张立强, 陈建江, 等. 集成协同优化策略与性能测量法的多学科可靠性设计优化. 计算机辅助设计与图形学学报, 2011, 23(8): 1373-1379.
[15] Norman S C. Aircraft landing gear design: principles and practices. Washington D.C.: America Institute of Aeronautics and Astronautics Press, 1988: 105-227.

E-mail：hkxb@buaa.edu.cn

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主管单位：中国科学技术协会主办单位：中国航空学会北京航空航天大学

基于BLISS和PMA的多学科可靠性设计优化

Multidisciplinary Reliability Design and Optimization Based on BLISS and PMA

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