多核处理器验证中存储数据错误快速定位机制

提出并实现的一种数据错误快速定位机制(Fast Fault Location Mechanism,FFLM)面向多核处理器存储系统的功能验证,FFLM基于硬件仿真器构建多端口存储器黄金模型,通过在仿真过程中实时监控存储系统与处理器核之间的访存报文,在线比较被测系统访问真实存储器的数据与黄金模型中的对应数据是否一致,在错误数据从存储系统送入处理器核的时刻就能够发现数据错误。与传统方法相比,FFLM具有仿真速度快、硬件资源代价低以及定位错误时间短的优点。对自主设计的CMP-16多核处理器进行仿真时的统计数据表明:使用FFLM后定位数据错误的速度能够比未使用FFLM时平均提高6.5倍。     

基于网络雷达的目标定位跟踪

网络雷达实现了有源与无源探测一体化及雷达情报与电子对抗情报一体化,具有良好的目标定位跟踪性能。首先分析了网络雷达工作在有源无源一体模式的目标定位原理及定位的CRLB,并通过仿真说明了网络雷达的定位优势。然后根据网络雷达的特点,提出了一种基于目标状态和属性联合最近邻的数据关联算法,该算法合理地利用了目标的电子属性信息(如载频、重频、脉宽和脉内特征等)。对小角度交叉运动目标进行了跟踪仿真试验,该算法得到了很好的关联跟踪效果。     

多径环境下平面时差定位精度分析

从多径环境下时差测量误差的概率分布模型入手,研究了该环境下基于测量误差概率分布的时差定位精度模型,给出了时差定位误差椭圆的位置与大小的计算方法.通过计算机仿真,分别得出了等腰三角形布站和直角三角形布站情况下的定位误差椭圆分布,结果表明:该模型能较为直观准确地反映出多径效应对时差定位精度的影响.     

Facility location for an extraterrestrial production/distribution system

This paper extends traditional production/distribution system analysis to address raw material, factories, and markets located beyond Earth. It explains the eventual advantages of such operations and discusses likely sites in the solar system. It furnishes a typology for production/distribution systems, assessing the fit of each type to space operations. It briefly reviews the physics of orbits. It develops transportation and inventory cost functions for the simplest case of Hohmann trajectories, and for transportation between circular orbits of similar radii using higher‐energy trajectories. These cost functions are used to derive a model of production/distribution system cost, the minimization of which selects an optimal factory location. The paper suggests potential extensions to this work, and concludes with ideas for location research on the novel reaches of extraterrestrial space. © 2005 Wiley Periodicals, Inc. Naval Research Logistics, 2005.     

A branch and bound algorithm for sector allocation of a naval task group

A naval task group (TG) is a collection of naval combatants and auxiliaries that are grouped together for the accomplishment of one or more missions. Ships forming a TG are located in predefined sectors. We define determination of ship sector locations to provide a robust air defense formation as the sector allocation problem (SAP). A robust formation is one that is very effective against a variety of attack scenarios but not necessarily the most effective against any scenario. We propose a 0‐1 integer linear programming formulation for SAP. The model takes the size and the direction of threat into account as well as the defensive weapons of the naval TG. We develop tight lower and upper bounds by incorporating some valid inequalities and use a branch and bound algorithm to exactly solve SAP. We report computational results that demonstrate the effectiveness of the proposed solution approach. © 2011 Wiley Periodicals, Inc. Naval Research Logistics, 2011     

一种基于球坐标系的四站三维时差定位算法

提出了一种在球坐标系下的无源时差定位算法,该算法解决了参变量法中难于解决的模糊和无解问题,计算量小,定位结果可信。当布站接近平面时,本算法可独立进行定位,当站址高度差较大时本算法可以与参变量法相配合解决模糊和无解问题,适合于工程应用。     

基于混沌特征的高分辨雷达目标识别

根据高分辨导弹制导雷达的基本工作原则和舰船目标的散射特性,利用现有雷达回波的仿真技术,在合理的战术想定下,计算了三类典型舰船的雷达回波.在此基础上,研究了利用雷达回波功率谱的方法来识别目标类型的有效性,并基于混沌理论提出了一种比功率谱方法更加有效的新的识别方法,从而为进一步利用混沌理论来开发雷达目标识别技术奠定了初步的理论基础.     

Aircraft routing under the risk of detection

The deterministic problem for finding an aircraft's optimal risk trajectory in a threat environment has been formulated. The threat is associated with the risk of aircraft detection by radars or similar sensors. The model considers an aircraft's trajectory in three‐dimensional (3‐D) space and represents the aircraft by a symmetrical ellipsoid with the axis of symmetry directing the trajectory. Analytical and discrete optimization approaches for routing an aircraft with variable radar cross‐section (RCS) subject to a constraint on the trajectory length have been developed. Through techniques of Calculus of Variations, the analytical approach reduces the original risk optimization problem to a vectorial nonlinear differential equation. In the case of a single detecting installation, a solution to this equation is expressed by a quadrature. A network optimization approach reduces the original problem to the Constrained Shortest Path Problem (CSPP) for a 3‐D network. The CSPP has been solved for various ellipsoid shapes and different length constraints in cases with several radars. The impact of ellipsoid shape on the geometry of an optimal trajectory as well as the impact of variable RCS on the performance of a network optimization algorithm have been analyzed and illustrated by several numerical examples. © 2006 Wiley Periodicals, Inc. Naval Research Logistics, 2006     

无人机对地目标多帧融合定位与误差收敛特性分析

对地目标高精度定位是无人机开展目标侦察、火力引导、效能评估等的重要前提,然而无人机对地目标定位精度受到误差因素多、传递链长等因素的制约。采用基于卡尔曼滤波的图像多帧配准对地面目标定位的方法,通过融合无人机获取的多帧目标图像,基于卡尔曼滤波方法,研究无人机对地目标高精度融合定位方法,并引入蒙特卡洛法进行仿真,分析基于卡尔曼滤波法多帧融合定位的误差收敛性、大小和分布,分析观测间隔、视线俯仰角等对误差收敛性的影响,形成若干提高定位精度的建议。     

海天背景下舰船可见光图像目标区域定位方法

针对行均值法用于海天背景下舰船目标区域定位可靠性不高、容易受到舰船目标大小和海天背景复杂程度影响的不足,提出一种基于图像行灰度熵的舰船目标区域定位方法。该方法在分析海天背景下舰船目标可见光图像成像特点基础上,结合信息熵理论给出了图像灰度熵及行灰度熵的概念,利用图像行灰度熵描述图像在行方向上的灰度变化程度,选用滑动区间方差搜索策略得到图像行灰度熵曲线的突变区间,从而实现舰船目标区域定位,最后通过实际图像进行了实验验证。实验结果表明,该方法能对舰船目标所在区域有效定位,其准确性及鲁棒性均优于行均值法。