双球破片冲击柱壳装药的临界起爆条件

为了研究导弹战斗部(柱壳装药)在破片场中的累积毁伤问题,在现有单破片起爆平板装药的Jacobs-Roslund经验准则的基础上,分别建立了考虑破片尺寸、破片撞击角度、柱壳装药的装药半径和壳体厚度的单球破片、双球破片冲击柱壳装药临界起爆条件的工程分析模型.该模型计算结果与数值模拟结果和现有试验结果相吻,证明利用该模型能较...     

航迹关联算法仿真中的几个假定

航迹关联是多传感器信息融合的前提和基础,来自不同传感器的航迹数据只有在确定相互关联之后,才能进行目标运动状态信息和属性信息的融合处理。航迹关联仿真分析时往往人为地设定一些假定条件,导致算法的仿真结果出现比较大的偏差。对航迹关联算法仿真分析中的一些常见假定进行分析,结合实际应用情景,探讨航迹关联率的定义,明确了关联正确率、关联错误率和漏关联率的计算方法。     

空舰导弹航路规划攻击角度与发射距离选择仿真分析

如何使用空舰导弹突击具有区域防空能力水面战斗舰艇是对海突击战斗的重点、难点问题之一,从分析使用空舰导弹突击水面舰艇战斗过程入手,归纳了导弹航路规划中需要考虑的各种关键要素,并对各要素进行简要的分析,根据分析建立舰空导弹拦截过程的数学模型,并使用matlab编制仿真程序进行计算,根据计算结果对航路规划问题中空舰导弹进入方向与发射距离之间的关系进行探讨。     

基于粗糙集理论的飞行轨迹识别

针对飞行轨迹人工识别对专家经验依赖性强,识别准确率不稳定的问题,提出一种基于粗糙集理论的飞行轨迹识别方法。首先,对飞行轨迹进行特征提取,获取用于轨迹类别判定的条件属性和决策属性;其次,利用模糊自组织神经网络对飞行轨迹决策表离散化,采用启发式遗传约简算法对条件属性约简,消除了冗余属性对识别结果的影响;最后,利用实际飞参数据进行轨迹识别,结果证明该方法准确有效。     

A melt-cast Duan-Zhang-Kim mesoscopic reaction rate model and experiment for shock initiation of melt-cast explosives

A melt-cast Duan-Zhang-Kim (DZK) mesoscopic reaction rate model is developed for the shock initiation of melt-cast explosives based on the pore collapse hot-spot ignition mechanism. A series of shock initiation experiments was performed for the Comp B melt-cast explosive to estimate effects of the loading pressure and the particle size of granular explosive component, and the mesoscopic model is validated against the experimental data. Further numerical simulations indicate that the initial density and formula proportion greatly affect the hot-spot ignition of melt-cast explosives.     

基于Dijkstra算法的水平航迹规划

战术飞行任务的航迹规划是依靠地形信息和敌情信息,在某些约束条件下,找出作战飞机从起飞点到目标突防生存概率最大、航程最短的飞行轨迹的过程。采用简易方法建立了威胁模型,用Dijkstra算法实现了作战飞机整体最优水平航迹解算,并给出了具体算例,验证了算法的有效性和实用性。     

Effect of microstructure on short pulse duration shock initiation of TATB and initial response mechanism

Micro-TATB particles with different sizes and 3D nanoporous TATB architectures with different specific surface areas were prepared through recrystallization to study short pulse duration shock initiation properties by electric gun technology. For micro-TATB, the initiation threshold significantly decreases with TATB average size ranging from 79.7 μm to 0.5 μm. For 3D nanoporous TATB architecture, the initiation threshold decreases and then increases with specific surface areas increased from 9.6 m²/g to 36.2 m²/g. The lowest initiation thresholds are obtained for the micro-TATB with average sizes of 1.3 μm and 0.5 μm, and 3D nanoporous TATB architecture with specific surface area of 22.4 m²/g. The shock initiation thresholds of micro-TATB and 3D nanoporous TATB architectures show significantly decreases with the porosity increased. The decomposition reaction and thermal conductivity properties were further investigated to understand the initial response mechanism. High porosity provides more collapse sites to generate high temperature for formation of hot spots. The low thermal conductivity and decomposition temperature could enhance the formation and ignition of the hot spots, and initial decomposition reaction of TATB. The effect of the decomposition temperature is higher than that of the thermal conductivity on the shock initiation properties. The enhanced decomposition reaction could promote energy release and transfer process from the ignition to the combustion. This work offers a new insight to understand the effects of microstructure on the shock initiation properties and the initial response mechanism of TATB.     

基于一步延时的航迹起始改进算法

针对现有多目标航迹起始算法工程实践性不强的特点,研究了一种基于一步延时的航迹起始算法,并在分析该算法的基础上,针对该算法计算量随目标数目增加而成指数增长的不足,对其算法进行了改进,提出了一种双重滤波的一步延时的航迹起始算法。仿真结果表明,该算法提高了航迹的正确起始概率,减少了计算量,具有较好的工程应用前景。     

一种多普勒雷达修正逻辑起始算法

针对一类具有多普勒量测的航迹起始问题,首先推导了目标任意三个时刻的斜距量测与多普勒量测乘积线性组合的统计特性,进而提出了一种修正逻辑起始算法.该算法通过在传统逻辑起始算法的航迹扩展阶段加入点迹关联的假设检验环节,来降低虚假航迹的数目.仿真结果表明,该算法的航迹起始概率与传统逻辑起始算法相当,而其虚假航迹数远远小于传统逻辑起始算法,并且运算量略有降低.     

基于投票分布积累的Hough变换航迹起始法?

针对密集杂波下匀加速运动的低可观测目标的航迹起始问题,提出了一种基于投票分布积累的Hough变换航迹起始法。该方法利用单元投票数以及该单元附近投票数的密集程度定义了投票密度和投票均值,构造了两级门限来滤除部分杂波,快速给出目标航迹参数在参数空间的大概位置,最后由直观法给出起始航迹的数目以及参数。仿真结果表明,该方法不仅能提高正确航迹起始概率、降低错误起始概率,而且所用时间短,尤其适用于复杂环境中的目标检测。