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Multiple tail models including inverse measures for structural design under uncertainties.

机译:多个尾部模型,包括不确定性下结构设计的逆向度量。

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摘要

Sampling-based reliability estimation with expensive computer models may be computationally prohibitive due to a large number of required simulations. One way to alleviate the computational expense is to extrapolate reliability estimates from observed levels to unobserved levels. Classical tail modeling techniques provide a class of models to enable this extrapolation using asymptotic theory by approximating the tail region of the cumulative distribution function (CDF). This work proposes three alternate tail extrapolation techniques including inverse measures that can complement classical tail modeling. The proposed approach, multiple tail models, applies the two classical and three alternate extrapolation techniques simultaneously to estimate inverse measures at the extrapolation regions and use the median as the best estimate. It is observed that the range of the five estimates can be used as a good approximation of the error associated with the median estimate. Accuracy and computational efficiency are competing factors in selecting sample size. Yet, as our numerical studies reveal, the accuracy lost to the reduction of computational power is very small in the proposed method. The method is demonstrated on standard statistical distributions and complex engineering examples.
机译:由于需要大量仿真,因此使用昂贵的计算机模型进行的基于采样的可靠性估计可能在计算上令人望而却步。减轻计算费用的一种方法是将可靠性估计值从观察到的水平外推到未观察到的水平。经典的尾部建模技术提供了一类模型,可通过渐近理论通过逼近累积分布函数(CDF)的尾部区域来进行这种外推。这项工作提出了三种替代的尾部外推技术,包括可以补充经典尾部建模的逆向度量。所提出的方法,多尾模型,同时应用了两种经典的和三种交替的外推技术,以估计外推区域的逆度量,并使用中位数作为最佳估计。可以看出,五个估计的范围可以用作与中值估计相关的误差的良好近似。准确性和计算效率是选择样本量的竞争因素。然而,正如我们的数值研究显示的那样,所提出的方法由于降低计算能力而损失的精度很小。该方法在标准统计分布和复杂的工程示例中得到了证明。

著录项

  • 作者

    Ramu, Palaniappan.;

  • 作者单位

    University of Florida.;

  • 授予单位 University of Florida.;
  • 学科 Engineering Aerospace.
  • 学位 Ph.D.
  • 年度 2007
  • 页码 126 p.
  • 总页数 126
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 航空、航天技术的研究与探索;
  • 关键词

  • 入库时间 2022-08-17 11:40:12

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