精密坐标镗床CNC系统研究

介绍了作者研制的通用ＣＮＣ系统,该系统以ＡＳＴ３８６作为控制器,采用ＰＷＭ驱动直流伺服电机,并配以软、硬件接口;文中对该系统的主要组成部分作了分析,在此基础上应用传统的ＰＩＤ控制方法设计数字控制器;最后通过实验验证了该系统的输出响应和控制器的性能。     

细长压杆临界载荷的图乘法近似求解

从细长压杆的挠曲线方程出发,采用图乘法,近似计算了两种不同支承细长压杆的临界载荷,并将其结果与欧拉法的精确解作了比较。     

基于B-样条分形插值的垂直尺度因子的计算方法

将线性分形插值推广到B-样条上,可避免线性分形插值局限性,进一步扩大分形理论的应用范围。分形插值应用的关键问题,是如何合理地确定垂直尺度因子di的值,而它的计算却没有一种很有效的方法。通过解析方法,获得了均匀B-样条分形插值“S”点的代数解,从而,可准确计算出垂直尺度因子,解决了影响B-样条分形插值应用的难题。     

战车火控仿真评估系统仿真控制与测试分系统设计

战车火控仿真评估系统是为适应新装备的预研与研制、现装备的技术改造、部队的技术保障需要而产生的,这一系统是综合有火控系统、指控系统和电子综合化系统的半实物仿真与性能评估试验平台,而其中的仿真控制与测试分系统又是重要组成部分,起着仿真控制、数据处理、传输等重要作用.在分析仿真控制与测试分系统功能的基础上,确定了仿真控制与测试分系统基于CAN总线的分布式设计方案.     

基于B样条的螺旋桨升力面设计

为了改善螺旋桨的空泡性能,从效率和空泡性能2个方面的权衡来确定环量分布.在升力面理论设计中计及桨毂的影响.桨叶几何用较少的B样条控制角点来表示.将升力面理论计算的控制点处法向速度的平方和作为优化目标函数,并通过最小化目标函数得到桨叶几何.     

军用系统间歇可用度及其战时计算模型研究

根据我军训练和作战的实际情况,对间歇可用度（AP）的概念进行了分析,说明了它在一次作战任务周期内计算精度要优于使用可用度,推导出了它的战时计算模型,界定了其使用条件与限制要求。最后通过仿真计算,证明了间歇可用度战时计算模型的可行性。     

Signature based analysis of m‐Consecutive‐k‐out‐of‐n: F systems with exchangeable components

In this article, we study reliability properties of m‐consecutive‐k‐out‐of‐n: F systems with exchangeable components. We deduce exact formulae and recurrence relations for the signature of the system. Closed form expressions for the survival function and the lifetime distribution as a mixture of the distribution of order statistics are established as well. These representations facilitate the computation of several reliability characteristics of the system for a given exchangeable joint distribution or survival function. Finally, we provide signature‐based stochastic ordering results for the system's lifetime and investigate the IFR preservation property under the formulation of m‐consecutive‐k‐out‐of‐n: F systems. © 2011 Wiley Periodicals, Inc. Naval Research Logistics, 2011     

Investigating optimal replacement of aging air force systems

An availability‐oriented approach has been developed to decide when to replace an aging system. For an existing system, it is optimal to operate another year if and only if the incremental cost per available year is less than the lifetime average cost per available year of a new aircraft. We illustrate our approach using United States Air Force KC‐135 tanker data. In demonstrating our approach, we find it will be optimal to replace the KC‐135 by the end of the decade.     

Military Spending and Income Inequality:Evidence on Cointegration and Causality for Turkey,1963–2007

This paper investigates a series of unit root, cointegration and causality tests to ascertain the direction of causality between the growth of GNP and defence expenditure in Turkey for the years 1955–2000. The main conclusion is that there is a long‐run equilibrium relationship between GNP and defence expenditures. Furthermore, the short run causality test indicates that there is a unidirectional causality between variables, from defence expenditure to economic growth. In order to see the effect of a shock, we employed impulse response analyses. The results show that GNP decreased during the period then output finally recovered from the initial shock to defence expenditures.