估算故障可能性的新型定向模拟方法

IF 5 1区 工程技术 Q1 ENGINEERING, AEROSPACE
Xia Jiang , Zhenzhou Lu , Michael Beer
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引用次数: 0

摘要

在模糊不确定性条件下,失效可能性对评估结构的安全等级起着至关重要的作用。然而,传统的模糊模拟方法需要大量样本才能进行精确估算,因此存在计算效率低的问题。针对这一问题,我们提出了一种定向模拟方法,以提高失效可能性估算的效率。方向模拟法将失效可能性估计重新划分为两个关键步骤:生成方向样本和在标准模糊空间的极坐标系中估计每个方向样本下的条件失效可能性。为确保方向一致性,这些方向样本是通过在单位超立方体上分层抽样的基础上采用良好的网格点集生成的。通过求解非线性方程的最小根来估计每个方向样本下的条件故障可能性。所提出的方法有效降低了模糊输入的维度,大大提高了计算效率。为进一步提高效率,在方向模拟方法中嵌入了自适应克里金模型,以减少性能函数评估的次数。通过四个实例说明了所提方法的准确性和效率。结果表明,定向模拟法优于传统的模糊模拟法,在保持较高估计精度的同时大幅提高了计算效率。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
A novel directional simulation method for estimating failure possibility
Failure possibility plays a crucial role in assessing the safety level of structures under fuzzy uncertainty. However, the traditional fuzzy simulation method suffers from computational inefficiency as it requires a large number of samples for accurate estimation. To address this issue, a directional simulation method is proposed to improve the efficiency of estimating failure possibility. The directional simulation method reformulates the failure possibility estimation into two key steps: the generation of direction samples and the estimation of conditional failure possibility under each direction sample in the polar coordinate system of the standard fuzzy space. To ensure direction uniformity, these direction samples are generated by adopting a good lattice point set based on stratified sampling on the unit hypercube. The conditional failure possibility under each direction sample is estimated by solving the minimum root of a nonlinear equation. The proposed method effectively reduces the dimensionality of the fuzzy input and greatly improves the computational efficiency. To further enhance efficiency, an adaptive Kriging model is embedded into the directional simulation method to reduce the number of performance function evaluations. Four examples are performed to illustrate the accuracy and efficiency of the proposed method. The results highlight the superiority of the directional simulation method over the traditional fuzzy simulation method, offering substantial improvements in computational efficiency while maintaining high estimation accuracy.
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来源期刊
Aerospace Science and Technology
Aerospace Science and Technology 工程技术-工程:宇航
CiteScore
10.30
自引率
28.60%
发文量
654
审稿时长
54 days
期刊介绍: Aerospace Science and Technology publishes articles of outstanding scientific quality. Each article is reviewed by two referees. The journal welcomes papers from a wide range of countries. This journal publishes original papers, review articles and short communications related to all fields of aerospace research, fundamental and applied, potential applications of which are clearly related to: • The design and the manufacture of aircraft, helicopters, missiles, launchers and satellites • The control of their environment • The study of various systems they are involved in, as supports or as targets. Authors are invited to submit papers on new advances in the following topics to aerospace applications: • Fluid dynamics • Energetics and propulsion • Materials and structures • Flight mechanics • Navigation, guidance and control • Acoustics • Optics • Electromagnetism and radar • Signal and image processing • Information processing • Data fusion • Decision aid • Human behaviour • Robotics and intelligent systems • Complex system engineering. Etc.
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