降落伞主充气阶段数值模拟

建立了降落伞主充气模型。前体、伞绳及伞衣离散为一系列弹性连接的质量节点,伞衣内部流场为二维无粘、不可压流。利用模型计算了主充气阶段伞衣形状变化、伞衣投影面积变化及伞绳张力。计算结果与试验结果进行了比较,相当吻合。     

A unified model incorporating yield,burn‐in,and reliability

The correlated improvement in yield and reliability has been observed in the case studies on integrated circuits and electronic assemblies. This paper presents a model that incorporates yield and reliability with the addition of a burn‐in step to explain their correlated improvement. The proposed model includes as special cases several yield and reliability models that have been previously published and thus provides a unifying framework. The model is used to derive a condition for which yield functions can be multiplied to obtain the overall yield. Yield and reliability are compared as a function of operation time, and an analytical condition for burn‐in to be effective is also obtained. Finally, Poisson and negative binomial defects models are further considered to investigate how reliability is based on yield. © 2004 Wiley Periodicals, Inc. Naval Research Logistics, 2004.     

Stochastic scheduling subject to machine breakdowns: The preemptive‐repeat model with discounted reward and other criteria

We consider the problem of scheduling a set of jobs on a single machine subject to random breakdowns. We focus on the preemptive‐repeat model, which addresses the situation where, if a machine breaks down during the processing of a job, the work done on the job prior to the breakdown is lost and the job will have to be started from the beginning again when the machine resumes its work. We allow that (i) the uptimes and downtimes of the machine follow general probability distributions, (ii) the breakdown process of the machine depends upon the job being processed, (iii) the processing times of the jobs are random variables following arbitrary distributions, and (iv) after a breakdown, the processing time of a job may either remain a same but unknown amount, or be resampled according to its probability distribution. We first derive the optimal policy for a class of problems under the criterion to maximize the expected discounted reward earned from completing all jobs. The result is then applied to further obtain the optimal policies for other due date‐related criteria. We also discuss a method to compute the moments and probability distributions of job completion times by using their Laplace transforms, which can convert a general stochastic scheduling problem to its deterministic equivalent. The weighted squared flowtime problem and the maintenance checkup and repair problem are analyzed as applications. © 2004 Wiley Periodicals, Inc. Naval Research Logistics, 2004     

一种新的数组逻辑结构猜想方法

许多编译优化技术都依赖于数组的逻辑结构,然而在实际的应用中,有相当多的数组是无结构的一维数组,从而妨碍了编译器的优化工作。提出了一种新的数组逻辑结构猜想算法,它能将无结构的一维数组自动变换成具有多维逻辑结构的数组,从而使编译器的优化工作成为可能。首先给出一个引理,指出猜想后的多维数组应满足的基本性质,然后基于该引理给出了猜想数组的逻辑结构应遵循的两条基本规则,最后基于这两条基本规则给出了猜想数组逻辑结构的算法。实验结果验证了所提出的数组逻辑结构猜想算法的有效性。     

一种新的高分辨率ADC有效位数测试方法

谱分析法和正弦拟合法是ADC动态特性测试的两种常用方法。但在测试信号源信噪比较低的情况下,两种方法的测试结果都存在较大的偏差。提出了一种新的ADC动态性能测试方法,该方法能较好消除信号源对测量结果的影响,使得在普通信号源下可以测试高分辨率的ADC。仿真分析证明了这一测试方法的正确性。最后给出了采用该方法对一ADC系统的实测结果。     

Walker星座自主定轨误差分析

通过对Walker星座中卫星间的相对运动进行分析,给出星间相对距离的解析表达式及其对轨道根数的偏导数,直观地描述在同轨道面和异轨道面的星间观测对轨道根数变化的体现情况;根据星座中卫星的相对位置,提出合理的约束条件和平差方法,利用星间测距网实现星座的整网定位;通过仿真算例,比较在不同情况下,采用合适的整网定位方法对轨道根数的系统误差和随机误差修正的情况。     

基于模糊理论的武器系统可靠性分析和评价

武器系统可靠性是指在规定条件下和规定时间内完成规定功能的能力。传统的可靠性计算方法是基于概率论的,其失效概率通常应根据第一手的数据。然而,实际上不可能收集到足够的数据,一般是依靠专家的经验来判断估计,这类判断通常与模糊性密切相关。本文基于可靠性理论和模糊数学的原则和方法,建立了一套计算串联系统和并联系统的模糊可靠度的计算公式。应用模糊数对武器装备系统单元可靠性予以模糊评价,并采用模糊可靠性计算模型,对武器系统可靠性进行模糊分析和计算。通过对一高炮武器系统的应用分析,证明了该方法的可行性。     

电磁发射超高速弹丸气动特性数值分析

采用数值计算方法研究了超高速弹丸的气动流场特性,重点分析了弹丸再入段的气动流场特性.利用风洞试验数据验证了S-A和k-ωSST湍流模型的预测精度,计算结果表明,在法向力预测上,两种湍流模型的预测精度较高,均在2％以内.在轴向力预测上,S-A湍流模型的预测精度较高,误差约为4.6％.当弹丸以大攻角再入时,弹丸横流效应较为...     

对当前消防部队信息化建设的思考

目前消防部队信息化建设取得了初步成效,但与部队需求还存在一定差距,存在着对信息化建设认识不够高、信息化应用不深入、专业人才偏少、人员素质偏低、投入资金不足等问题,并针对存在的问题提出了解决对策。     

浅析《孙子兵法》中的战机思想

《孙子兵法》中蕴含着丰富而深刻的战机思想。不战全胜的“胜机”思想、立足不败的“待机”思想、变中求胜的“创机”思想、兵贵神速的“夺机”思想和因情用势的“握机”思想等内容,是《孙子兵法》战机思想的核心与精华。