基于渐消因子的双机协同机动目标定位

传统的双机协同组网目标定位模型中,滤波方法大多为交互式多模型算法。交互式多模型算法的缺陷为需要目标机动先验模型,且模型个数的选择难以同时满足工程上关于跟踪精度和算法复杂性的要求。通过引入渐消因子,实时自适应校正机动目标的状态估计偏差,有效降低了目标运动先验模型对滤波的影响,提高了系统的机动处理能力和模型的工程实用性。     

New results on a stochastic duel game with each force consisting of heterogeneous units

Two forces engage in a duel, with each force initially consisting of several heterogeneous units. Each unit can be assigned to fire at any opposing unit, but the kill rate depends on the assignment. As the duel proceeds, each force—knowing which units are still alive in real time—decides dynamically how to assign its fire, in order to maximize the probability of wiping out the opposing force before getting wiped out. It has been shown in the literature that an optimal pure strategy exists for this two‐person zero‐sum game, but computing the optimal strategy remained cumbersome because of the game's huge payoff matrix. This article gives an iterative algorithm to compute the optimal strategy without having to enumerate the entire payoff matrix, and offers some insights into the special case, where one force has only one unit. © 2013 Wiley Periodicals, Inc. Naval Research Logistics 61: 56–65, 2014     

基于紧支径向基函数的固体域耦合数据传递方法

针对热-电场耦合仿真计算中非匹配网格之间的数据插值问题,提出了一种基于紧支径向基函数点插值的数据传递方法。推导了数据传递矩阵,根据所提出的数据传递方法编制了非匹配网格之间数据传递计算程序,以若干组非匹配网格之间的温度插值为例对本文所提方法进行了验证,并分析了不同参数对计算时间及精度的影响,结果表明,本文算法效率较高,计算误差较小,适用于以热-电场耦合为代表的固体域耦合非匹配网格间的数据传递计算。     

用紧支径向基函数传递固体域耦合数据的方法

针对热-电场耦合仿真计算中非匹配网格之间的数据插值问题,提出了一种基于紧支径向基函数点插值的数据传递方法。推导了数据传递矩阵,根据所提出的数据传递方法编制了非匹配网格之间数据传递计算程序,以若干组非匹配网格之间的温度插值为例进行了验证,并分析了不同参数对计算时间及精度的影响,结果表明,算法效率较高,计算误差较小,适用于以热-电场耦合为代表的固体域耦合非匹配网格间的数据传递计算。     

新世纪牢记“两个务必”的现实意义和基本要求

毛泽东在党的七届二中全会上提出“两个务必”,告诫全党在中国革命即将取得全国胜利的形势下务必继续保持谦虚谨慎、不骄不躁的作风,务必继续保持艰苦奋斗的作风。在新世纪,党要带领人民实现全面建设小康社会的宏伟目标,不断提高党的抵御风险能力、拒腐防变能力和执政为民能力,克服党所面临的四大危险,始终坚持牢记“两个务必”,仍具有非常重要的现实意义。     

人机工程学领域人体建模技术发展综述

随着数字化技术在现代人机工程学研究领域的普及,人体模型在人机工程研究方面具有重大的应用空间。文中指出了人体建模的重要性,对人体数据采集方法进行了阐述。划分了人体建模技术发展的阶段,并对国内外建模技术发展进行了总结,最后提到人体模型的应用范围十分广泛,有良好的应用前景。     

双轴平台动力调谐陀螺漂移补偿技术

在双轴平台动力调谐陀螺惯导系统中,动力调谐陀螺仪漂移与测量轴重力分量密切相关.根据动力调谐陀螺与重力相关漂移项的特点,提出了双轴平台陀螺漂移误差的补偿方法.通过安装在双轴平台上的加速度计测量载体姿态,并计算重力在陀螺两个测量轴的分量,建立了陀螺漂移模型,对方位漂移进行补偿.实验证明,该方法有效地提高了双轴平台方位漂移精度.     

公安消防机构办理失火案和消防责任事故案法理探讨

办理“两案”案件对公安消防机构来说是一个全新的概念,如何正确充分履行法律赋予的侦查职能,已成为各级公安消防机构面临的重要课题。从法理和实践角度对“两案”办理工作进行探讨。     

An inspection game: Taking account of fulfillment probabilities of players' aims

This paper deals with an inspection game of customs and a smuggler. The customs can take two options of assigning a patrol or not. The smuggler has two strategies of shipping its cargo of contraband or not. Two players have several opportunities to take actions during a limited number of days. When both players do, there are some possibilities that the customs captures the smuggler and, simultaneously, the smuggler possibly makes a success of the smuggling. If the smuggler is captured or there remain no days for playing the game, the game ends. In this paper, we formulate the problem into a multi‐stage two‐person zero‐sum stochastic game and investigate some characteristics of the equilibrium solution, some of which are given in a closed form in a special case. There have been some studies so far on the inspection game. However, some consider the case that the smuggler has only one opportunity of smuggling or the perfect‐capture case that the customs can certainly arrest the smuggler on patrol, and others think of a recursive game without the probabilities of fulfilling the players' purposes. In this paper, we consider the inspection game taking account of the fulfillment probabilities of the players' aims. © 2006 Wiley Periodicals, Inc. Naval Research Logistics, 2006     

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.