• 更多栏目

    王博

    • 教授     博士生导师   硕士生导师
    • 主要任职:党委常委、副校长
    • 其他任职:工业装备结构分析国家重点实验室副主任
    • 性别:男
    • 毕业院校:大连理工大学
    • 学位:博士
    • 所在单位:力学与航空航天学院
    • 学科:工程力学. 计算力学
    • 办公地点:工程力学系系楼304房间
    • 联系方式:办公电话: 0411-84706608; 手机: 壹叁玖肆贰捌伍玖捌伍伍
    • 电子邮箱:wangbo@dlut.edu.cn

    访问量:

    开通时间:..

    最后更新时间:..

    A novel non-probabilistic reliability-based design optimization algorithm using enhanced chaos control method

    点击次数:

    论文类型:期刊论文

    发表时间:2017-05-01

    发表刊物:COMPUTER METHODS IN APPLIED MECHANICS AND ENGINEERING

    收录刊物:SCIE、EI、ESI高被引论文

    卷号:318

    页面范围:572-593

    ISSN号:0045-7825

    关键字:Non-probabilistic reliability-based optimization; Enhanced chaos control method; Target performance approach; Convex model; Complex engineering problem

    摘要:In this study, an efficient and robust algorithm of non-probabilistic reliability-based design optimization (NRBDO) is proposed based on convex model. In this double-nested optimization model, the inner loop concerns a Min-max problem for the evaluation of reliability index, where the target performance approach is applied to substitute the Min-max problem. To improve the convergence rate, an enhanced chaos control (ECC) method is developed on the basis of chaotic dynamics theory, which can check and re-update the control factor by the Wolfe-Powell criterion. To further enhance the optimization efficiency, a novel NRBDO algorithm is developed based on the proposed ECC, where HL-RF algorithm is applied at the initial stage of this algorithm, while ECC is used to improve the robustness once the oscillation or chaotic behavior is identified. Three mathematical examples, one numerical example and one complex engineering problem, i. e. axially compressed stiffened shells in launch vehicles, are utilized to demonstrate the robustness and efficiency of the proposed method by comparison with other existing methods. Results indicate that the proposed method is particularly suitable for complicated engineering problems without prior knowledge of uncertainty distributions, which is expected to be utilized in the structural design of future launch vehicles. (C) 2017 Elsevier B. V. All rights reserved.