任务驱动的军事信息服务知识推理研究

根据任务需要敏捷组织信息服务活动,从海量信息资源中提取准确的信息,高效地为各级指挥员提供精准的信息服务,是提升我军信息服务能力的关键所在.以使命任务、信息服务活动和信息资源为核心概念,建立了军事信息服务本体模型,定义了模型中概念之间的语义关系和时序关系,提出了军事信息服务知识推理方法,为任务驱动的军事信息服务领域知识的推理提供了理论基础.以封堵河堤溃口突发事件应急处置信息服务模型构建和知识推理实例作为具体测试案例,验证了构建的本体模型和知识推理方法的有效性.     

基于奇异谱修正香农熵的雷达信号识别方法

针对当前雷达辐射源识别在低信噪比下识别率准确率不高,信号处理过程中难以很好保留有用信息的问题,提出了一种基于奇异谱修正香农熵(Singular Spectrum Modified Shannon Entropy,SSSE)的雷达调制信号识别方法.通过符号化聚合近似和奇异谱分析对雷达信号进行处理,求出信号的分类特征SSSE,通过分类器将处理后的信号进行分类.仿真结果显示,该方法在低信噪比范围下,仍有较高总体识别率,并且优于符号化聚合近似和奇异谱分析法.     

Theoretical and numerical simulation study on jet formation and penetration of different liner structures driven by electromagnetic pressure

The use of a shaped liner driven by electromagnetic force is a new means of forming jets. To study the mechanism of jet formation driven by electromagnetic force, we considered the current skin effect and the characteristics of electromagnetic loading and established a coupling model of"Electric—Magnetic—Force"and the theoretical model of jet formation under electromagnetic force. The jet formation and penetration of conical and trumpet liners have been calculated. Then, a numerical simulation of liner collapse under electromagnetic force, jet generation, and the stretching motion were performed using an ANSYS multiphysics processor. The calculated jet velocity, jet shape, and depth of penetration were consistent with the experimental results, with a relative error of less than 10％. In addition, we calculated the jet formation of different curvature trumpet liners driven by the same loading condition and ob-tained the influence rule of the curvature of the liner on jet formation. Results show that the theoretical model and the ANSYS multiphysics numerical method can effectively calculate the jet formation of liners driven by electromagnetic force, and in a certain range, the greater the curvature of the liner is, the greater the jet velocity is.     

Chain damage effects of multi-spaced plates by reactive jet impact

Chain damage is a new phenomenon that occurs when a reactive jet impacts and penetrates multi-spaced plates.The reactive jet produces mechanical perforations on the spaced plates by its kinetic energy(KE),and then results in unusual chain rupturing effects and excessive structural damage on the spaced plates by its deflagration reaction.In the present study,the chain damage behavior is initially demonstrated by experiments.The reactive liners,composed of 26 wt％Al and 74 wt％PTFE,are fabricated through a pressing and sintering process.Three reactive liner thicknesses of 0.08 CD,0.10 CD and 0.12 CD(charge diameter)are chosen to carry out the chain damage experiments.The results show a chain rupturing phenomenon caused by reactive jet.The constant reaction delay time and the different penetration velocities of reactive jets from liners with different thicknesses result in the variation of the deflagration position,which consequently determines the number of ruptured plates behind the armor.Then,the finite-element code AUTODYN-3D has been used to simulate the kinetic energy only-induced rupturing effects on plates,based on the mechanism of behind armor debris(BAD).The significant discrepancies between simulations and experiments indicate that one enhanced damage mechanism,the behind armor blast(BAB),has acted on the ruptured plates.Finally,a theoretical model is used to consider the BAB-induced enhancement,and the analysis shows that the rupturing area on aluminum plates depends strongly upon the KE only-induced pre-perforations,the mass of reactive materials,and the thickness of plates.     

仿生偏振光导航传感器量测模型研究

仿生偏振导航传感器仿照昆虫利用天空偏振光进行导航的原理,测量载体的姿态和方位,具有精度高、功耗低等优势,是一种新型的导航传感器．根据偏振导航的原理分析偏振导航传感器的测量参考矢量和导航能力,根据其参考矢量的数量及性质,对偏振导航传感器使用在不同性质载体上的测量进行建模,并提出其对载体进行定姿的条件．     

基于OLS算法的导弹气动系数模型优选

针对导弹控制系统中的气动力建模问题,将正交最小二乘法用于模型结构优选,并提出一种候选模型集预处理方法,用以剔除模型中的相关项在此基础上建立了导弹气动力模型优选方法。将其应用于一种导弹滚转力矩系数模型,进行了仿真计算,取得了与风洞试验数据一致的计算结果。结果显示该方法在导弹气动力建模中有效可行,为构建最优化的模型结构提供指导。     

多模调制遥测发射机的设计与实现

随着遥测信息量的增加和遥测形式的多样化,需要研制一种通用性强、码速率高、灵活性好的遥测发射机来代替目前所使用的模拟调制发射机.介绍了一种能够适应目前及未来遥测任务需求的S波段多模调制遥测发射机,给出了详细设计,并对其进行了系统性能测试分析,测试结果得到了良好的实际效果,可广泛应用于飞行器遥测系统.     

基于营区精、气、神文化表达的自然仿生设计

精、气、神文化是营区规划设计的核心.自然仿生设计为营区精、气、神文化的表达提供了独特而有效的方式.通过对营区精、气、神文化的解读,发掘出自然仿生的3个层面,即“形”之仿生,“意”之仿生和“结构”之仿生.在营区规划设计中,当自然仿生的这3个层面得到有效表达,实现有机统一,营区就会产生独特的文化气质与魅力,从而体现其精、气、神特色,展现部队的“军营魂”.     

一种设计八进六出“S”盒的方法

本文叙述了一种同时考虑扩散性和均匀性的设计86S-box的方法,并给出了程序流程图及非线性强度和随机性的论证。     

基于HLA的空战仿真应用

HLA技术是当前仿真的趋势.给出了基于HLA的空战仿真的体系结构、仿真对象模型和联邦对象模型的设计,分析了应用的HLA接口规范.HLA应用于人在回路的仿真要求具有实时性,当前RTI软件却一般不能满足要求,需要以某种方式去解决,给出了一种解决手段.优化了三维显示盟员/数据记录盟员在HLA的应用方法.