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.     

基于双自适应调节算子的装备作战效能评估方法

为解决某型装备作战效能评估客观性差问题,在分析作战任务基础上构建效能评估指标体系,通过构建改进的效能评估模型,引入双自适应调节算子灵敏反应指标数据波动,确保了指标权重精确度,并通过单个权重和双自适应调节算法权重衡量方法的实例对比,验证了本模型的科学性、准确性.该模型对基础数据要求低,计算相对简便;构建的指标体系全面,较好地反映了评估对象的作战特征;避免了人为因素对指标权重的影响,结论更加客观.研究结果对快速、科学制定作战方案和改进某型装备性能设计有一定的参考意义.     

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.     

基于模糊综合评判的装备软件可靠性分析

可靠性是衡量装备软件质量的重要参数,但由于软件可靠性的特点,在实际对装备软件可靠性定量分析往往很难,甚至不可能。从软件质量框架模型出发,结合装备软件的特点,分析了影响装备软件可靠性的几个参数,提出了一种运用模糊综合评判方法对装备软件可靠性进行定性分析的方法。该方法简单,可行性强。最后,给出了一个实例。     

火箭炮定向器电动操瞄性能检测系统研究

采用旋转编码器获得旋转角度信号,利用信号转接器提取电信号,并通过计算机进行处理,对火箭炮定向器的电动操瞄性能进行在线检测。研究表明,使用该检测系统既能离线检测以辅助安装电动操瞄系统,又能在线检测电动操瞄的各项性能指标,包括高低和方向各个限位点是否正确,各运动区域的速度是否正常。     

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。     

基于遗传算法的准维燃烧模型修正方法

针对目前准维燃烧模型不能客观反映高原柴油机工作过程的问题,提出了一种基于计算机智能仿真模型修正方法.采用正交试验的极差分析,计算并识别出准维燃烧模型的经验参数对柴油机性能影响的主次顺序,并确定为待修正参数.基于遗传算法,以试验数据为依据,对柴油机准维燃烧模型进行修正.修正后的柴油机工作过程模型误差在4％以内,为深入开展高原环境柴油机性能研究奠定了基础.