基于支持向量机的移动回归增强策略,用于复杂结构的响应预测和可靠性估算

IF 5 1区 工程技术 Q1 ENGINEERING, AEROSPACE
Hui Zhu , Hui-Kun Hao , Cheng Lu
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引用次数: 0

摘要

为了预测复杂结构的响应特性并估算其可靠性水平,我们在支持向量机(SVM)、启发式算法和移动最小平方(MLS)技术的基础上提出了基于支持向量机的增强移动回归(MR-ESVM)策略。在这一策略下,我们开发了四种不同的 SVM 模型,包括基于 SVM 的移动回归(MR-SVM)、基于 SVM 的改进移动回归(IMR-SVM)、基于 SVM 的改进移动回归(MR-ISVM)和基于 SVM 的双优化移动回归(BiOMR-SVM)方法。在这些已开发的 MR-ESVM 方法中,MR-SVM 方法是通过在 SVM 模型中引入 MLS 技术来进行探索的;IMR-SVM 方法是通过将 MR-SVM 方法与人工兔子优化(ARO)相融合来进行讨论的,ARO 用于搜索紧凑区域的最佳半径;通过将 ARO 融入 MR-SVM 方法,提出了 MR-ISVM 方法,并应用 ARO 寻找 SVM 模型中的最优值;通过合并 IMR-SVM 和 MR-ISVM 方法,提出了 BiOMR-SVM 方法。为了验证所开发的 MR-ESVM 策略的有效性,实现了多变量非线性函数逼近,从数学角度说明了其优势;得出了航空发动机涡轮叶盘径向变形可靠性分析和飞机液压系统低压可靠性分析,证明了其在工程实践中的适用性。分析结果表明,这四种 MR-ESVM 方法在建模特征和仿真特性方面都具有很好的优点。这些研究成果为复杂结构的响应预测提供了新的思路,丰富了复杂结构代用模型的可靠性估算原理。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Enhanced support vector machine-based moving regression strategy for response prediction and reliability estimation of complex structure
For predicting response property and estimating reliability level of complex structure, enhanced support vector machine-based moving regression (MR-ESVM) strategy is proposed based on support vector machine (SVM), heuristic algorithm and moving least square (MLS) technique. Under this strategy, we develop four different SVM models including SVM-based moving regression (MR-SVM), SVM-based improved moving regression (IMR-SVM), improved SVM-based moving regression (MR-ISVM) and bi-optimized SVM-based moving regression (BiOMR-SVM) methods. In these developed MR-ESVM approaches, the MR-SVM method is explored by introducing the MLS technique into the SVM model; the IMR-SVM method is discussed by fusing the MR-SVM method and artificial rabbits optimization (ARO), and the ARO is used to search the optimal radius of compact region; the MR-ISVM method is raised by integrating the ARO into the MR-SVM, and the ARO is applied to find the optimal values in the SVM model; The BiOMR-SVM method is emerged by merging the IMR-SVM and MR-ISVM methods. To verify the effectiveness of these developed MR-ESVM strategies, a multivariate nonlinear function approximation is implemented to illustrate the advantages from the mathematics perspective, an aeroengine turbine blisk radial deformation reliability analysis and an aircraft hydraulic system low pressure reliability analysis are derived to demonstrate the applicability in engineering practice. The analytical results show that these four MR-ESVM approaches hold excellent merits in modeling features and simulation characteristics. The efforts of this work provide a novel idea for the response prediction of complex structure, and enrich the reliability estimation principle of surrogate models of complex structure.
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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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