电磁轨道发射器动态发射过程的数值模拟

针对电磁轨道发射器动态发射过程的数值模拟问题,基于矢量磁位A和时间积分标量电位V,采用节点单元法,并选择运动坐标系描述运动问题,推导出动态发射下的电磁轨道发射器三维涡流场有限元离散方程。结合温度场控制方程,建立电磁轨道发射器的三维电磁-温度耦合有限元模型。针对一个电磁轨道发射器动态发射问题,对模型进行数值模拟,得到了动态发射下轨道及电枢的温度场分布特点及发射器电感梯度随时间的变化规律。计算结果表明,模型计算出的脉冲电流峰值、出口电流大小、出口速度等参数均与试验结果吻合较好,验证了所开发的有限元程序代码的正确性。     

空中多飞行器飞行轨迹优化数值仿真

针对空中多飞行器在复杂环境中飞行轨迹的多目标最优问题，分析了多飞行器飞行过程中各种可视和不可视约束条件。基于在回避威胁区前提下燃料消耗最少、飞行时间最短的综合性能指标，采用“多方法组合”思路，提出了改进动态规划法和多点边值法组合算法，并进行了仿真验证，大量C＋＋数值飞行仿真结果表明该算法能够在考虑外界复杂环境和飞行器各种约束条件下快速规划出空中多飞行器的最优飞行轨迹，该组合算法具有一定的实用性和创新性。     

一致光滑Banach空间中一类非线性算子方程的解

证明了一个新的锐角原理,在不使用连续性条件的情况下,给出了在一致光滑Banach空间中一类非线性算子方程的可解性定理。     

Dynamic signatures and their use in comparing the reliability of new and used systems

The signature of a system with independent and identically distributed (i.i.d.) component lifetimes is a vector whose ith element is the probability that the ith component failure is fatal to the system. System signatures have been found to be quite useful tools in the study and comparison of engineered systems. In this article, the theory of system signatures is extended to versions of signatures applicable in dynamic reliability settings. It is shown that, when a working used system is inspected at time t and it is noted that precisely k failures have occurred, the vector s [0,1]^n‐k whose jth element is the probability that the (k + j)th component failure is fatal to the system, for j = 1,2,2026;,n ‐ k, is a distribution‐free measure of the design of the residual system. Next, known representation and preservation theorems for system signatures are generalized to dynamic versions. Two additional applications of dynamic signatures are studied in detail. The well‐known “new better than used” (NBU) property of aging systems is extended to a uniform (UNBU) version, which compares systems when new and when used, conditional on the known number of failures. Sufficient conditions are given for a system to have the UNBU property. The application of dynamic signatures to the engineering practice of “burn‐in” is also treated. Specifically, we consider the comparison of new systems with working used systems burned‐in to a given ordered component failure time. In a reliability economics framework, we illustrate how one might compare a new system to one successfully burned‐in to the kth component failure, and we identify circumstances in which burn‐in is inferior (or is superior) to the fielding of a new system. © 2009 Wiley Periodicals, Inc. Naval Research Logistics, 2009     

机载视觉自主着陆过程中的跑道提取方法

跑道直线参数的准确提取,是机载视觉完成自主着陆过程的重要条件.首先在边缘图像的基础上利用相位编组算法,得到当前边缘图像中大量的线段,根据线段之间的角度,端点距离,以及线段两边的灰度均值,设计了一套规则来定量描述线段之间的亲近性,根据亲近值,将处于同一直线上的短线段首尾连接成长线段.取最长的若干条线段待选,再利用跑道区域的先验知识,主要是跑道内外的灰度对比信息,将位于同一条跑道的两条边缘上的线段识别出来.大量的实际图像结果验证了算法的有效性.     

舰船汽力装置变工况性能的图形化处理

应用现代计算机图形处理方法动态地描述舰用蒸汽动力装置及其设备的变工况性能数据，包括用图形交互的方式输入、显示和保存数据等关键内容．该方法已用于实际工程分析．     

船用电缆绝缘电阻自动检测精度的分析与研究

提出了一种实际的船用电缆绝缘电阻检测方案 ,包括信号变换电路和方案的硬件与软件结构 .分析了检测误差产生的主要原因 ,并提出了两种提高检测精度的措施     

基于CSCW的机关业务协同办公系统协作多用户界面研究

简要阐述了研究CSCW系统协作多用户界面的必要性,介绍了协作多用户界面的基本概念,分析并评价了几种传统的协作多用户界面体系结构,最后以某机关业务协同办公系统的协作多用户界面的设计为例,提出了一种协同混合式体系结构及具体的实现。     

型号研制与产品数据管理

介绍了产品数据管理(PDM)的概念和基本功能,结合当前型号研制的特点和计算机信息技术应用的状况、发展,研究了型号研制产品数据管理的需求、功能及实施,为当前型号研制依靠CIMS技术实现产品数据管理提出了8条基本原则。     

Does Military Spending Nonlinearly Affect Economic Growth in South Africa?

Using annual data collected from 1988 to 2015, this study provides evidence of a non-linear relationship between military spending, economic growth and other growth determinants for the South African economy. The empirical study is based on estimates of a logistic smooth transition regression (LSTR) model and our empirical results point to an inverted U-shaped relationship between military spending and economic growth for the data. Furthermore, our empirical results suggest that the current levels of military spending, as a component of total government expenditure, are too high in the South African economy and need to be transferred towards more productive non-military expenditure in order to improve the performance of economic growth and other growth determinants.