DOES MILITARY EXPENDITURE MATTER FOR INFLATION AND ECONOMIC GROWTH?

This paper sets up a monetary endogenous growth model, and uses it to explain the ambiguous linkage between the military burden and the inflation rate observed in existing empirical studies. It is found that an expansion in the military burden has an ambiguous effect on the inflation rate depending upon the relative extent of two conflicting forces. More specifically, if the increase in the marginal benefit from holding money exceeds (falls short of) the increase in the marginal product of private capital, the inflation rate will rise (fall) in response. Moreover, it is found that an increase in the military burden will stimulate the balanced growth rate, confirming Benoit’s famous empirical findings.     

基于EMD的改进小波阈值降噪法在超声信号处理中的应用

针对超声检测回波信号中的大量噪声,分析了超声检测回波信号的特性,考虑经验模式分解（EMD）和小波哗噪的优点,在改进阈值函数基础上提出一种基于EMD的小波阈值降噪方法．该方法利用EMD对超声信号进行分解,对高频分量用改进小波阈值函数方法进行处理,再结合低频分量重构得到降噪信号．仿真实验结果表明,该方法降噪效果优于小波软、硬阂值降噪,进一步提高了重建信号的信噪比,降低了其均方根误差,是一种可行的超声信号降噪方法．     

Comparison between constant‐stress and step‐stress accelerated life tests under Time Constraint

By running life tests at higher stress levels than normal operating conditions, accelerated life testing (ALT) quickly yields information on the lifetime distribution of a test unit. The lifetime at the design stress is then estimated through extrapolation using a regression model. In constant‐stress testing, a unit is tested at a fixed stress level until failure or the termination time point of test, whereas step‐stress testing allows the experimenter to gradually increase the stress levels at some prefixed time points during the test. In this work, the optimal k‐level constant‐stress and step‐stress ALTs are compared for the exponential failure data under complete sampling and Type‐I censoring. The objective is to quantify the advantage of using the step‐stress testing relative to the constant‐stress one. Assuming a log‐linear life–stress relationship with the cumulative exposure model for the effect of changing stress in step‐stress testing, the optimal design points are determined under C/D/A‐optimality criteria. The efficiency of step‐stress testing to constant‐stress one is then discussed in terms of the ratio of optimal objective functions based on the information matrix. © 2013 Wiley Periodicals, Inc. Naval Research Logistics 00: 000–000, 2013     

目标识别中的传感器管理方法

基于假设检验的方法,研究了目标识别中的传感器管理方法。分别以用于假设检验问题中的最大后验概率、最小代价函数和最大正确检测概率为目标函数,给出了用于目标识别问题的多传感器管理方法,并针对目标识别问题的特点,对其进行了相应的改进。通过对一定场景的仿真,比较了三种不同方法的识别正确率和平均采样次数,分析了各种方法的特点。     

基于信息论的C3I系统决策性能的评价

信息熵是描述信息系统的一种比较成功的方法.采用信息论的方法对决策系统进行描述,在考虑了决策者的有界合理性限制和达到满意性能指标的要求下,分析了单人指挥决策系统的系统性能,并在此基础上分析了多人指挥决策系统的系统性能,最后得出采用决策系统的误差概率P和相互一致性度量Q作为评价C3I系统决策性能标准的结论.     

航空电子总线测试系统的设计与实现

现代航空电子综合化系统通常建立在M IL-STD-1533B多路传输数据总线通信网络基础之上,总线控制器(BC)和各个远程终端(RT)必须满足M IL-STD-1553B规定的各项协议指标要求,才能正确地联网通讯。讨论了某型航空电子总线测试系统的设计与实现,主要探讨了此系统的软、硬件开发,系统组成及其BC和RT有效性测试的主要内容和要求。在实际应用中收到了很好的效果。     

基于DIFHA算子的动态直觉模糊多属性群决策方法

动态决策问题是现实中的一类常见问题。在提出动态直觉模糊混合平均(D IFHA)算子的基础之上,提供一种动态直觉模糊多属性群决策方法。该方法能同时考虑决策过程的阶段性和属性值位置对决策结果的影响,并较好地处理决策过程中的定性指标。分析和算例证实该方法的可行性和实用性。     

军用软件的测试与实践方法

首先分析了民用软件存在的问题,然后结合军用软件的特点,对影响军用软件可靠性的因素进行分析,最后提出提高军用软件质量的几种测试与实践方法.     

基于假设检验的编队组织决策设计

从集中式和分散式组织结构分析出发,采用假设检验的方法,探讨了分布式结构假设检验在海军舰艇编队环境评估中的组织决策设计,并从决策设计和算法上对其进行了复杂性分析.研究结果表明,基于假设检验的组织决策是一个NP问题,就存在的问题提出算法和组织设计研究的思路.     

Fabrication of AA7005/TiB2-B4C surface composite by friction stir processing: Evaluation of ballistic behaviour

The present work aims to enhance the ballistic resistance of AA7005 alloy by incorporating the TiB₂ and B₄C ceramic reinforcement particles. Surface composites with different weight fractions of TiB₂ and B₄C particles were processed by friction stir processing. Micro-hardness and depth of penetration tests were carried out to evaluate the ballistic properties of the surface composites. The surface hardness of the composite was found to be nearly 70 HV higher than base alloy. The depth of penetration of the steel projectile was 20–26 mm in the composites as compared to 37 mm in the base alloy. Ballistic mass efficiency factor of the surface composite was found to be 1.6 times higher than base alloy. This is mainly attributed to the dispersion strengthening from the reinforcement particles.