最优化算法的收敛准则

收敛准则是最优化算法的重要组成部分，其选择得好与坏将直接影响到算法的成功与否以及收敛得快与慢。现有常用的收敛准则基本上是建立在前后迭代点的逼近和它们相应函数值的逼近是否达到一定的精度要求以及迭代点处函数梯度是否接近于零的基础上的。它们各自有自己的适用范围。但它们的共同特点是对迭代终止点的性质不能做出判断。本文在总结和分析现有算法收敛准则的基础上，借助于正定矩阵、一维优化方法中对分法和黄金分割法，提出了新的算法收敛准则。算例结果表明，这些收敛准则是有效实用的。     

吊车荷载作用下钢结构吊车梁的疲劳可靠寿命评估

从Miner累积损伤的定义出发，视累积损伤为随机过程，临界损伤为随机变量，基于疲劳动态可靠性理论，提出了在役钢结构吊车梁疲劳剩余寿命的可靠寿命评估法。之后与现行《钢结构检测评定与加固技术规程》(YB9257-96)中安全期限寿命评估法进行了分析比较，说明了安全寿命评估方法的概率意义。算例分析结果表明，本文提出的可靠寿命评估方法更加合理。     

Log-likelihood maximization and response surface in reliability assessment

Nonlinear dynamics problems can generally be solved only in a numerical way. This prevents from a direct application of standard reliability methods. A technique which makes use of iterated response-surface analytical approximations of the system performance function was therefore proposed in view of reliability assessment. The limitation of this technique was of working in a standard normalized space, so that appropriate space transformations are preliminarly required.This paper shows how this response-surface iterative scheme can also be used in the original space of the random variables, provided a maximum log-likelihood constrained optimization problem is solved. Moreover, asymptotic theory also provides a better estimate of the probability of failure of the dynamical system against any assigned limit state.     

机翼全尺寸延寿试验及可靠性分析

机翼全尺寸疲劳试验是老龄飞机延寿的科学依据。本文介绍了疲劳裂纹形成和扩展寿命的分散系数，以及可靠度和标准差的选取。针对延寿的可靠性分析，提出按疲劳／损伤容限设计概念或当量裂纹扩展寿命方法，以及机翼串联模型，确定整机延寿使用寿命的技术途径。最后给出应用实例。     

Eléments finis stochastiques en élasticité linéaireA stochastic finite element method in linear mechanics

The stochastic finite element method presented in this Note consists in representing in a probabilistic form the response of a linear mechanical system whose material properties and loading are random. Each input random variable is expanded into a Hermite polynomial series in standard normal random variables. The response (e.g., the nodal displacement vector) is expanded onto the so-called polynomial chaos. The coefficients of the expansion are obtained by a Galerkin-type method in the space of probability. To cite this article: B. Sudret et al., C. R. Mecanique 332 (2004).     

Quick assessment methodology for reliability of solder joints in ball grid array (BGA) assembly—Part I: Creep constitutive relation and fatigue model

In this study, a new unified creep constitutive relation and a modified energy-based fatigue model have been established respectively to describe the creep flow and predict the fatigue life of Sn−Pb solders. It is found that the relation successfully elucidates the creep mechanism related to current constitutive relations. The model can be used to describe the temperature and frequency dependent low cycle fatigue behavior of the solder. The relation and the model are further employed in part II to develop the numerical simulation approach for the long-term reliability assessment of the plastic ball grid array (BGA) assembly. The project supported by the National Natural Science Foundation of China (59705008)     

RESEARCH ON RELIABILITY GROWTH FOR SYNCHRONOUSLY DEVELOPED MULTI-SYSTEMS

IntroductionAMSAA model could evaluate reliability growth test for mono-system perfectly[1-8].Butfor multi-systems,especially for synchronously developed multi-systems,the model parametersneed to be estimated by developing some newmethods.AMSAA-BISE model…     

疲劳可靠性二维概率MINER准则

给出在裂纹起始阶段疲劳损伤演化规律的四个基本假设，即单调增、无耦合、可分高、不相交，由损伤力学原理得到等幅加载下个体Ｄ－Ｓ＿ａ－Ｓ＿ｍ－Ｎ等损伤曲面，推导出二维个体Ｍｉｎｅｒ准则，进而建立了母体在变幅以及随机时间历程加载下的二维概率Ｍｉｎｅｒ准则（Ｔｗｏ－ｄｉｍｅｎｓｉｏｎａｌＰｒｏｂａｂｉｌｉｓｔｉｃＭｉｎｅｒ’ｓＲｕｌｅ，即ＴＰＭＩＮＥＲ），并用测度论给予了证明．试验数据验证结果显示ＴＰＭＩＮＥＲ的预测值与试验值吻合良好，对工程结构疲劳可靠性分析有较好的应用价值．     

结构元件安全评估与监控的风险预测方法

提出了一种评估结构疲劳可靠性的方法－风险预测方法。该方法利用结构在服股过役过程中的信息,在考虑了工程结构承采载荷的各态历经性的基础上,结合了结构元件寿命机分布形式和Ｍｉｎｅｒ线性累积损伤理论,以风险值来评价并监控结构元件在不同时间失效的危险性,并用算例和试验结果进行对比分析。     

二维正态分布函数值的一个近似算法

二维正态分布函数值的计算是估算串联结构体系失效概率上、下限的一项重要内容。目前一般常采用两种方法，即数值积分和界限法。前者因计算量大，耗时多不便实用，后者使结构体系失效率的上、下界限进一步变宽。本文给出一个计算二维正态分布函数值的近似方法。实际计算表明，本方法计算效率高，精度完全能满足工程应用要求