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Chance-Constrained Optimization Approach Based on Density Matching and Active Subspaces

机译:基于密度匹配和主动子空间的机会约束优化方法

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摘要

Chance-constrained optimization has recently been receiving much attention from the engineering community. Uncertainties are being incorporated in increasingly large numbers to ensure reliability and robustness. However, the efficiency and accuracy of chance-constrained optimization under multiple uncertainties remains challenging. In this study, a constrained density-matching optimization methodology is established to address these pressing issues in chance-constrained optimization. The methodology employs an alternative objective metric between a designer-given target and system response, enables more uncertainties in design variables and random parameters to be handled, and accommodates multiple chance constraints with an adaptive penalty function. An active subspace identification strategy and a dynamic response surface are given to overcome the curse of uncertainty dimensionality and to guarantee sufficient samples for kernel density estimation in an uncertainty analysis. The efficacy is demonstrated on three optimization examples: a response function problem, a standard NASA test, and a practical application in the conceptual design of a satellite system. Different quadrature points, penalty functions, and target forms are discussed, respectively. The methodology exhibits high accuracy and strong adaptability at considerably reduced computational cost, thus providing a potential template for tackling a wide variety of chance-constrained optimization problems.
机译:机会约束的优化最近已引起工程界的广泛关注。为了确保可靠性和鲁棒性,越来越多地引入不确定性。但是,在多个不确定性下机会受限的优化的效率和准确性仍然具有挑战性。在这项研究中,建立了约束密度匹配优化方法,以解决机会约束优化中的这些紧迫问题。该方法在设计者给定的目标和系统响应之间采用了替代的客观度量,使设计变量和随机参数的更多不确定性得以处理,并通过自适应惩罚函数适应了多个机会约束。提出了一种主动子空间识别策略和一个动态响应面,以克服不确定性维数的诅咒,并保证在不确定性分析中有足够的样本用于核密度估计。通过三个优化示例证明了其有效性:一个响应函数问题,一个标准的NASA测试以及在卫星系统概念设计中的实际应用。分别讨论了不同的正交点,罚函数和目标形式。该方法具有很高的准确性和很强的适应性,并且大大降低了计算成本,因此为解决各种机会受限的优化问题提供了一个潜在的模板。

著录项

  • 来源
    《AIAA Journal》 |2018年第3期|1158-1169|共12页
  • 作者单位

    China Aerodynam Res & Dev Ctr, Computat Aerodynam Inst, Mianyang 621000, Peoples R China;

    China Aerodynam Res & Dev Ctr, Computat Aerodynam Inst, Mianyang 621000, Peoples R China;

    Natl Univ Def Technol, Coll Aerosp Sci & Engn, Changsha 410073, Hunan, Peoples R China;

    Univ Cambridge, Dept Engn, Cambridge CB2 1PZ, England;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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