多群体合作型协进化方法的数学建模及分析

采用传统单群体GA中模式复制方程的分析方法 ,对一种多群体合作型协进化方法建模并进行数学分析 ,对于目前尚未解决的协进化过程中的关键问题 ,包括个体适应度的评价方法、群体间合作的回报信贷分配以及由此影响到群体中个体的增长规律等在理论方面进行分析。最后表明 ,数学建模与分析的结果与Potter的实验结论相吻合     

线性无阻尼半正定振动系统简明正定化方法

从线性无阻尼半正定振动系统运动微分方程出发,分析得出系统作自由振动时具有内部惯性力守恒、振动动量守恒以及质心守恒等3个基本物理属性.在此基础上,给出了简明的正定化方法,并证明了该方法的普适性,数值算例也验证了其正确性.与"物理约束"法相比,文中提出的正定化方法规则简单,计算量小,适用于理论推导、计算机编程和数值计算.     

具连续分布滞量的二阶中立型阻尼偏微分方程解的振动准则

研究一类具有阻尼项和连续分布滞量的二阶中立型偏微分方程解的振动性,通过利用Riccati变换,引入一类Φ(t,s,l)型的新函数,获得该类方程在Robin,Dirichlet边值条件下振动的充分判据.     

潜艇水下回转运动稳定性分析

水下回转运动是潜艇常用的运动形式之一,属于潜艇转向运动的重要研究内容。回转运动过程中,潜艇受力复杂,容易出现分岔等非线性现象,潜艇运动稳定性变差。运用同伦延拓法、分岔理论和李雅普诺夫运动稳定性理论分析了潜艇水下回转运动稳定性,并通过数值仿真试验验证了分析结果的正确性和分析方法的有效性,为潜艇运动稳定性的研究提供了思路。     

发动机冷却燃料超临界压力下做功潜力㶲分析

在高马赫数飞行下,超燃冲压发动机的燃料冷却量大于燃料燃烧量。为了降低燃料的冷却量以及实现燃料冷却量和燃烧量的匹配,采用分析法对超燃冲压发动机壁面燃料冷却工质在超临界压力下进行做功潜力分析。发动机壁面冷却燃料的特性决定其热量大小。根据发动机壁面温度分布、热流密度分布计算热量,建立稳定流动燃料工质的平衡方程。结果表明:在壁面最高温度为1200 K时,传入壁面的热量为562.4 k W,其中理论热量为541.3 k W;冷却燃料工质流量增加,最大输出功减小;燃料工质出口温度增加,输出功减小;燃料工质出口压力增加,输出功基本不变。     

基于兰切斯特方程的网络中心战模型

为了更全面、客观地评价信息优势和决策优势对网络中心战进程的影响,在分析经典兰切斯特方程的基础上,引入信息?决策概率,提出了基于兰切斯特方程的网络中心战模型,仿真实验表明该模型能够有效地描述信息?决策概率在网络中心战进程中发挥的作用,为研究分析网络中心作战过程提供了理论参考。     

A novel gradient approach for optimal design and sensitivity analysis of EWMA control charts

Conventional control charts are often designed to optimize out‐of‐control average run length (ARL), while constraining in‐control ARL to a desired value. The widely employed grid search approach in statistical process control (SPC) is time‐consuming with unsatisfactory accuracy. Although the simulation‐based ARL gradient estimators proposed by Fu and Hu [Manag Sci 45 (1999), 395–413] can alleviate this issue, it still requires a large number of simulation runs to significantly reduce the variance of gradient estimators. This article proposes a novel ARL gradient estimation approach based on integral equation for efficient analysis and design of control charts. Although this article compares with the results of Fu and Hu [Manag Sci 45 (1999), 395–413] based on the exponentially weighted moving average (EWMA) control chart, the proposed approach has wide applicability as it can generally fit into any control chart with Markovian property under any distributions. It is shown that the proposed method is able to provide a fast, accurate, and easy‐to‐implement algorithm for the design and analysis of EWMA charts, as compared to the simulation‐based gradient estimation method. Moreover, the proposed gradient estimation method facilitates the computation of high‐order derivatives that are valuable in sensitivity analysis. The code is written in Matlab, which is available on request. © 2014 Wiley Periodicals, Inc. Naval Research Logistics 61: 223–237, 2014     

Stochastic framework for partially degradation systems with continuous component degradation‐rate‐interactions

Many conventional models that characterize the reliability of multicomponent systems are developed on the premise that for a given system, the failures of its components are independent. Although this facilitates mathematical tractability, it may constitute a significant departure from what really takes place. In many real‐world applications, system components exhibit various degrees of interdependencies, which present significant challenges in predicting degradation performance and the remaining lifetimes of the individual components as well as the system at large. We focus on modeling the performance of interdependent components of networked systems that exhibit interactive degradation processes. Specifically, we focus on how the performance level of one component affects the degradation rates of other dependent components. This is achieved by using stochastic models to characterize how degradation‐based sensor signals associated with the components evolve over time. We consider “Continuous‐Type” component interactions that occur continuously over time. This type of degradation interaction exists in many applications, in which interdependencies occur on a continuum. We use a system of stochastic differential equations to capture such “Continuous‐Type” interaction. In addition, we utilize a Bayesian approach to update the proposed model using real‐time sensor signals observed in the field and provide more accurate estimation of component residual lifetimes. © 2014 Wiley Periodicals, Inc. Naval Research Logistics 61: 286–303, 2014     

高超声速钝锥体俯仰阻尼导数影响因素分析

采用非定常双时间步长方法、刚性旋转动网格技术,结合空间隐式格式数值分析了高超声速钝锥体定常与非定常流场特征,并运用最小二乘法辨识出钝锥体的俯仰阻尼导数。通过与相应的实验数据、工程估算值进行比较,分析并验证了壁面网格雷诺数、钝头比、攻角与质心位置对钝锥体俯仰阻尼导数的影响。同时采用五种差分格式,其中包含五阶精度WENO与高精度WNND格式,对钝锥体俯仰阻尼导数进行了计算,结果表明不同无粘差分格式对俯仰静导数影响较小,但不同格式之间俯仰动导数结果存在差异,分析认为差分格式之间不同的粘性分辨率应是差异的主要来源。     

高超声速横向喷流的三维数值模拟

采用有限体积法,结合半隐的Harten TVD格式和Baldwin Lomax代数湍流模型,求解了三维全N S方程,计算了超声速气流干扰流场,并与实验数据进行了比较,模拟清晰地捕捉到喷流附近复杂波系结构和旋涡结构,并且显示出了弹体表面受到喷流影响的区域,说明横向喷流干扰对弹体影响非常大。