商务印书馆函授学校英文科学员来源地考察——基于《英语周刊》(1921-1922)记载的分析

商务印书馆函授学校英文科在中国近现代成人教育史、职业教育史上都占据着非常重要的位置.1921年至1922年期间的《英语周刊》对英文科学员来源地等信息均有着较为详细的记载,弥补了已发现的相关史料的不足,从而可以对其办学效果做出一个客观、精确的评价.通过《英语周刊》的相关记载,可以发现英文科学员来源地范围覆盖区域非常广泛,其学员来源地构成状况呈现出了多元化、多样化的特点.仅仅从学员来源地状况的角度去审视、考察,商务函授学校英文科取得了显著的办学效果,它在一定程度上弥补了普通学校教育资源的不足,有力促进了中国教育近代化事业的发展.     

基于模板的态势估计推理模型与算法

分析了态势估计的三级模型,给出了基于模板的计划识别推理框架,研究了态势估计推理算法,并提出一个通用的态势估计模板匹配算法,最后运用专家系统工具CLIPS实现了事件/活动、军事计划的模板表示及推理,结果表明使用模板匹配的方法实现态势估计是有效可行的。     

模糊偏序关系的一种信息集成方法

以模糊超过关系、模糊不协调关系为例,就模糊偏序关系给出了一种基于分组加权极大(极小)算子的信息集成方法,讨论了该方法的一致性、非独裁性等性质.     

The effects of model parameter deviations on the variance of a linearly filtered time series

We consider a general linear filtering operation on an autoregressive moving average (ARMA) time series. The variance of the filter output, which is an important quantity in many applications, is not known with certainty because it depends on the true ARMA parameters. We derive an expression for the sensitivity (i.e., the partial derivative) of the output variance with respect to deviations in the model parameters. The results provide insight into the robustness of many common statistical methods that are based on linear filtering and also yield approximate confidence intervals for the output variance. We discuss applications to time series forecasting, statistical process control, and automatic feedback control of industrial processes. © 2010 Wiley Periodicals, Inc. Naval Research Logistics, 2010     

攻角对双三角翼旋涡特性影响的数值模拟

采用数值方法研究了双三角翼上涡流运动随攻角的变化规律.计算取层流假设,研究了攻角在5°～30°,76°/40°后掠双三角翼绕流的流场结构随攻角的变化,并对双三角翼上涡破裂现象对流场结构及气动力性能的影响进行了分析.结果表明,双三角翼上的多涡结构存在强烈的相互影响,较大的攻角会导致涡破裂在翼面上发生,严重影响了双三角翼的气动力性能.     

一类广义延拓四元数矩阵的奇异值分解

从普通四元数矩阵的奇异值分解出发,给出了具有行或列对称结构的一类四元数矩阵(即广义四元数延拓矩阵)的奇异值、奇异向量与其母矩阵的奇异值、奇异向量之间的定量关系,推广了现有文献的结果。理论分析和数值实验的结果表明,就一大类广义四元数延拓矩阵而言,仅用母矩阵进行奇异值分解不但可以节省计算量和存储量,而且不影响任何数值精度。     

Exact algorithms for scheduling multiple families of jobs on parallel machines

In many practical manufacturing environments, jobs to be processed can be divided into different families such that a setup is required whenever there is a switch from processing a job of one family to another job of a different family. The time for setup could be sequence independent or sequence dependent. We consider two particular scheduling problems relevant to such situations. In both problems, we are given a set of jobs to be processed on a set of identical parallel machines. The objective of the first problem is to minimize total weighted completion time of jobs, and that of the second problem is to minimize weighted number of tardy jobs. We propose column generation based branch and bound exact solution algorithms for the problems. Computational experiments show that the algorithms are capable of solving both problems of medium size to optimality within reasonable computational time. © 2003 Wiley Periodicals, Inc. Naval Research Logistics 50: 823–840, 2003.     

采用瞬态球状热斗篷方法的浅层地下目标红外隐身技术

由于浅层地下目标与背景土壤的热物性不同,影响了整个区域表面的温度场分布,容易被敌方探测系统发现并击毁。针对这一问题,考虑太阳辐射、天空辐射以及风速的影响,建立了埋藏地下目标的区域温度分布传热模型,揭示了不同时段埋藏地下目标对区域表面温度场的影响。在变换热力学的基础上,通过坐标变换的方法,推导出球状瞬态热斗篷的导热系数的通解表达式。根据等效介质理论,对设计的热物性参数进行均质化,并通过数值实验方法验证了基于热斗篷地下目标红外隐身技术的可行性。     

New inequalities for finite and infinite group problems from approximate lifting

In this paper, we derive new families of facet‐defining inequalities for the finite group problem and extreme inequalities for the infinite group problem using approximate lifting. The new valid inequalities for the finite group problem include two‐ and three‐slope facet‐defining inequalities as well as the first family of four‐slope facet‐defining inequalities. The new valid inequalities for the infinite group problem include families of two‐ and three‐slope extreme inequalities. These new inequalities not only illustrate the diversity of strong inequalities for the finite and infinite group problems, but also provide a large variety of new cutting planes for solving integer and mixed‐integer programming problems. © 2008 Wiley Periodicals, Inc. Naval Research Logistics, 2008     

满足大动压模拟要求的试验弹道优化设计

为了解决弹道导弹在高海拔发射场进行飞行试验时的大动压检验问题,提出一种模拟大动压条件的试验弹道设计方法。针对发射场的实际特点,建立残骸再入的动力学模型与落区边界模型;将大动压模拟条件转化为过程约束,提出一种主动段联合优化策略。基于自适应模拟退火算法,分别设计了三组满足不同大动压模拟条件和各项约束的试验弹道,并给出了对应的落区调整方案,验证了该方法的可行性。设计结果表明,最大动压主要出现在一级,一级最大负攻角增加,则最大动压也明显提高;同时调整发射方位角和二、三级程序角可以保证试验弹道满足弹头落点约束条件。