武警部队开进路线问题的蚂蚁算法研究

部队开进路线问题是类似于TSP的NP问题。本文将蚂蚁算法应用于部队开进路线问题中,在综合考量每条路径的通行条件、隐蔽性、迂回道路数量基础上,通过层次分析法求出每条路径的权值,进而运用蚂蚁算法原理对问题设计算法。算法用Delphi实现,通过对实际部队开进路线问题的测试,得到较好结果。相对于传统的经验选择路径方法,此方法更少依赖选择主体的主观性,从而更具客观性与可重复性。     

基于AT89C51和DS18B20温度的测量系统的实现

本系统为以AT89C51单片机作为主控芯片的温度测量系统,采用一线温度传感器DS18820实现温度的检测,结合128×64点阵式液晶显示模块OCM12864作为显示器,形象直观地显示测得的温度值。主要介绍了该系统的硬件结构和软件编程实现的方法,数字温度传感器DS18820的基本特性,阐述了DDRAM寻址与液晶点阵的对应关系及中文字符、中文菜单在液晶模块上的显示规则。     

基于最小隶属度偏差的作战通道模糊优选

作战通道的优选对于充分发挥武器装备的效能,提高水面舰艇的作战能力具有十分重要的意义.通过分析作战通道效能评估的指标因素,确定指标相对优属度,应用最小隶属度偏差法,建立了作战通道的模糊优选模型,求解后得出了在该原则下的通道评估结论,为作战通道的优选提供了一种比较科学的定量分析方法.最后通过实例仿真计算得出了多条作战通道的优劣排序,为海战指挥员的科学决策提供参考.     

利用詹森不等式推广几个数学问题

詹森（Jensen）不等式是解决不等式问题的一个重要方法,也是发现数学问题的重要手段。运用詹森不等式的关键是通过观察所给代数式的函数特征,构造一个凹或凸的函数,以利解题。     

矩阵开关技术在通用ATS电源模块自检中的应用

针对通用ATS中电源模块检查过程中存在检查时间长、劳动量大、工作效率低且易出错等问题,将矩阵开关技术引入通用ATS中电源模块的自检过程中,选取电压信号的均值和均方差作为评价电源模块性能的特征参数,并利用矩阵开关的多路复用功能设计了电源模块自检的拓扑结构,实现了自检过程中多通道的自动配置。仿真验证试验说明了该方法具有多通道自动配置、自检时间短、故障定位准确等优点。     

线性方程组迭代解法的另类矩阵形式

改进了线性方程组迭代解法的矩阵形式．以最简单的Jacobi迭代法的迭代矩阵为基础,只需经过简单的加减和数乘运算就可得到Seidel和SOR的迭代过程,使得算法新形式的求解过程数学意义非常明确,表达形式也非常简洁,这样不仅便于理解记忆,还非常有利于编程实现。改进后的矩阵迭代形式求解计算量为:Seidel需要大约n2次乘除法．SOR约为2n2次乘除法,且改进后的Seidel迭代法和SOR方法存储空间也较传统形式为少。     

指派问题的降阶优化算法

指派问题是运筹学中特殊线性规划中的一类问题。在现实生活中,指派问题非常普遍,常常可以见到各种各样的指派问题。通过对指派问题的数学模型进行分析,提出了与以往方法不同的求解指派问题的一种新的思路,通过对几个定理的研究,给出了一种新的求解方法——降阶优化算法。对求解指派问题提供了一种新的途径,在运筹学等领域有着较好的应用前景。     

防空导弹制导雷达综合抗干扰能力评估

分析了地空导弹武器系统制导雷达面临的主要干扰及其所采取的主要抗干扰措施,一般层次分析法(AHP)在评估某些模糊概念时存在缺陷。基于模糊层次分析法(FAHP),构造了模糊一致判断矩阵,建立了防空导弹制导雷达综合抗干扰能力评估模型,该模型具有快速、易于操作等优点,解决了在评价制导雷达综合抗干扰能力时难以定量分析的问题。     

Repairable consecutive‐k‐out‐of‐n: F system with Markov dependence

In this article, a model for a repairable consecutive‐k‐out‐of‐n: F system with Markov dependence is studied. A binary vector is used to represent the system state. The failure rate of a component in the system depends on the state of the preceding component. The failure risk of a system state is then introduced. On the basis of the failure risk, a priority repair rule is adopted. Then the transition density matrix can be determined, and the analysis of the system reliability can be conducted accordingly. One example each of a linear and a circular system is then studied in detail to explain the model and methodology developed in this paper. © 2000 John Wiley & Sons, Inc. Naval Research Logistics 47: 18–39, 2000     

Effect of tool rotational speed on the particle distribution in friction stir welding of AA6092/17.5 SiCp-T6 composite plates and its consequences on the mechanical property of the joint

This study investigates the effect of tool rotational speed (TRS) on particle distribution in nugget zone (NZ) through quantitative approach and its consequences on the mechanical property of friction stir welded joints of AA6092/17.5 SiC_p-T6 composite. 6 mm thick plates are welded at a constant tool tilt angle of 2° and tool traverse speed of 1 mm/s by varying the TRS at 1000 rpm, 1500 rpm and 2000 rpm with a taper pin profiled tool. Microstructure analysis shows large quantity of uniformly shaped smaller size SiC particle with lower average particle area which are homogeneously distributed in the NZ. The fragmentation of bigger size particles has been observed because of abrading action of the hard tool and resulting shearing effect and severe stress generation due to the rotation of tool. The particles occupy maximum area in the matrix compared to that of the base material (BM) due to the redistribution of broken particles as an effect of TRS. The migration of particles towards the TMAZ-NZ transition zone has been also encountered at higher TRS (2000 rpm). The microhardness analysis depicts variation in average hardness from top to bottom of the NZ, minimum for 1500 rpm and maximum for 2000 rpm. The impact strength at 1000 rpm and 1500 rpm remains close to that of BM (21.6 J) while 2000 rpm shows the accountable reduction. The maximum joint efficiency has been achieved at 1500 rpm (84%) and minimum at 1000 rpm (68%) under tensile loading. Fractographic analysis shows mixed mode of failure for BM, 1000 rpm and 1500 rpm, whereas 2000 rpm shows the brittle mode of failure.