阀门电动装置智能速度控制器研究与仿真

针对阀门电动装置难以实现阀门快速准确定位和柔性关断的问题,采用位置和速度双闭环调节控制方法,通过参数自调节控制策略,设计了基于模糊PID控制原理 的智能速度控制器.仿真结果表明,智能速度控制器可以实现阀门变速调节、快速准确定位和柔性关断.     

海战复杂性度量研究

为把握现代海战的发展规律,在分析海战复杂性概念的基础上将海战复杂性分为海战结构复杂性和海战行为复杂性进行度量。提出＂点权分布熵＂以度量海战的静态结构复杂性,并运用复杂网络建立模型;提出＂行为熵＂以度量动态的行为复杂性,并从信息质量和决策水平角度建立模型。给出了海战复杂性的度量公式,分析了影响海战复杂性的因素。     

纯固态聚氨基甲酸乙酯涂料的研制及其应用

为了解决两栖装甲车辆底盘、浮箱表面的磨损腐蚀问题,研制了新型的纯固态聚氨基甲酸乙酯涂料。试验应用表明该涂料施工性能优异,涂层的耐磨性能和防腐性能优越,满足两栖装甲车辆的使用要求。     

军事装备管理系统“四个机制”联合概念模型构建及分析

针对当前“四个机制”实施中存在的问题,在建立“四个机制”各自概念模型的基础上,提出了“四个机制”联合概念模型,以利于“四个机制”的有机结合和互相促进,以期达到促进军事装备管理系统的有序化和良性运行的目的。     

分布式拒绝服务攻击的网络跟踪算法

分布式拒绝服务攻击通过控制多台傀儡机对目标机进行攻击,该类型攻击的攻击路径隐蔽,对攻击者跟踪困难.在分析该类型攻击的特点,通过形式化的描述,分析该类型网络入侵规律,通过聚类分析技术描述出分布式拒绝服务攻击的攻击路径,定位网络入侵的实施者,有效地打击网络入侵行为.     

An efficient and modular modeling for launch dynamics of tubed rockets on a moving launcher

This paper develops a modular modeling and efficient formulation of launch dynamics with marching fire (LDMF) using a mixed formulation of the transfer matrix method for multibody systems (MSTMM) and Newton-Euler formulation. Taking a ground-borne multiple launch rocket systems (MLRS), the focus is on the launching subsystem comprising the rocket, flexible tube, and tube tail. The launching subsystem is treated as a coupled rigid-flexible multibody system, where the rocket and tube tail are treated as rigid bodies while the flexible tube as a beam with large motion. Firstly, the tube and tube tail can be elegantly handled by the MSTMM, a computationally efficient order-N formulation. Then, the equation of motion of the in-bore rocket with relative kinematics w.r.t. the tube using the Newton-Euler method is derived. Finally, the rocket, tube, and tube tail dynamics are coupled, yielding the equation of motion of the launching subsystem that can be regarded as a building block and further integrated with other subsystems. The deduced dynamics equation of the launching subsystem is not limited to ground-borne MLRS but also fits for tanks, self-propelled artilleries, and other air-borne and naval-borne weapons undergoing large motion. Numerical simulation results of LDMF are given and partially verified by the experiment.     

一种弹道外测数据的野值处理方法

为抑制弹道外测数据中异常值的影响,设计了一种基于最小二乘趋势项建模与一阶差分还原的联合野值处理方法.该方法基于最小二乘原理建立了外测数据趋势项多项式的一般模型;利用一阶差分处理化斑点型野值为孤立型野值,在简化野值类型的同时又降低了野值的处理难度;最后引入肖维涅准则进行野值检验剔除,并积分还原得到便于后续分析的外测数据.仿真算例结果对比表明,该方法简便易行,在不破坏原始数据有用信息前提下,可抑制复杂类型野值的影响,取得较好的处理效果.     

Quasi-steady aerodynamic characteristics of Terminal Sensitive Bullets with short cylindrical portion

The aerodynamic characteristics are vital for short cylindrical Terminal Sensitive Bullets(TSB)with low aspect ratio,especially in terminal trajectory.Currently,there is little research in terms of the TSB and short cylinder with two free ends,and particularly in this trajectory,where the scanning angle β and roll angle α vary over a broad range between 0° and 180°.In this work,wind tunnel experiments are first conducted to learn the effects of Reynolds number and scanning angle on aerodynamic parameters for short cylinder with aspect ratio L/D = 1.Similar to infinite cylinder,for the short cylinder with two free ends,the drag crisis phenomenon still exists in the critical regime 1.7 × 105 ≤ Re ≤ 6.8 × 105.Then 3D simulations are performed to demonstrate the aerodynamic characteristics of short cylinder and TSB over a broad range of Re,L/D,α and β.The sensitivity analysis of time step and grid are presented as well.When β=0°,for short cylinder,the drag crisis phenomenon was also observed in the simulation,but not as obvious as in the wind tunnel test.In some attitudes,there is an obvious Kármán vortex in the wake of short cylinder and TSB.The correlation between time-averaged aerodynamic coefficients and L/D,Re,α&β is discussed.The vortex shedding frequency and shear layer behavior are obtained for quasi-steady and unsteady flow.Finally,the effect of end's shape on drag reduction and vortex shedding frequency is analyzed.     

外光电效应中光电流的计算

根据金属中电子系统可假设为具有质量为m的粒子组成的理想费密气体,其在热平衡时服从费密-狄喇克分布规律,导出单位强度单色光束照射金属时所感生的光电流.     

大学计算机基础课程教材的建设与实践

面向21世纪计算机课程体系的核心是计算机层次教育.以1996～1998年出版的全军统编计算机教材和国家级"九五"重点计算机教材为基础,论述了计算机层次教育所包括的内容及具体的实施办法.