Field test and probabilistic analysis of irregular steel debris casualty risks from a person-borne improvised explosive device

Person-borne improvised explosive devices (PBIEDs) are often used in terrorist attacks in Western countries. This study aims to predict the trajectories of PBIED fragments and the subsequent safety risks for people exposed to this hazard. An explosive field test with a typical PBIED composed of a plastic explosive charge and steel nut enhancements was performed to record initial fragment behaviour, including positions, velocity, and trajectory angles. These data were used to predict the full trajectory of PBIED fragments using a probabilistic analysis. In the probabilistic analyses a probability of fatality or serious injury was computed. Based on the results presented, many practical conclusions can be drawn, for instance, regarding safe evacuation distances if a person were exposed to a suspected PBIED.     

基于虚拟目标的反舰导弹的最优制导律研究

为了对抗敌方预警系统的跟踪、预测以及远程防空导弹的拦截,反舰导弹的飞行弹道应采用大空域变轨弹道。将弹目相对运动分解为俯仰和航向两个平面内的运动,考虑了制导过程中能量消耗最小以及末端角度要求,分别设计了两个平面内的最优制导律。利用该制导律可以引导反舰导弹向大空域内任何虚拟目标进行变轨机动,从而实现了各种各样的大空域变轨弹道。只要虚拟目标参数设置合适,反舰导弹的各项性能指标均能满足要求。弹道仿真表明了所设计的最优制导律的有效性。     

自主驾驶衍生的安全技术在军车中的应用

自主驾驶技术许多相关技术可以应用到车辆主动安全中去.文章阐述了一些主动安全的基本概念,并讨论了主动安全技术在军车的应用展望.     

战斗机隐蔽接敌轨迹优化方法

针对空战对抗的隐蔽作战需求,对战斗机隐蔽接敌方法进行研究。基于战斗机雷达反射截面积的动态特性建立雷达探测威胁模型;以空战态势参数为状态建立接敌引导模型;以给定目标发现概率为暴露阈值进行威胁约束;以最小化接敌过程中累积被发现概率为性能指标;将战斗机隐蔽接敌问题建模为隐蔽性约束下的最优控制问题。为保证算法的实时性和有效性,引入滚动时域控制策略进行在线优化,并采用高斯伪谱法进行数值求解。仿真实验表明,通过路径约束和性能指标双重约束,能有效增强战斗机接敌的隐蔽性,算法实时性能满足战斗机控制的需求。     

文化安全视角下的新疆高校网络舆情管理探究

文化安全的关键在意识形态,意识形态领域中的关键问题是价值观掌控问题。作为文化传播的主要组成部分,网络舆情对文化安全的表层和深层结构都有重要影响。本文从文化安全视角下切入,结合新疆高校网络舆情调研,分析了文化安全面临的冲击与挑战,并提出了基于文化安全保障下的新疆高校网络舆情有效管理方式和路径。     

Thermal hazard assessment of TKX-50-based melt-cast explosive

In the present study, thermal hazards of TNT and DNAN used as the molten binder in TKX-50-based melt-cast explosives were comparatively studied through accelerating rate calorimeter (ARC) and Cook-off experiments. Two kinds of ARC operation modes were performed to investigate the thermal safety performance under adiabatic conditions (HWS mode) and constant heating (CHR mode). The obtained results demonstrated that at both heating modes, DNAN/TKX-50 outperformed TNT/TKX-50 from the thermal safety point of view. However, the sensitivity to heat of the samples was reverse because of the different heating modes. In addition, the results of thermal hazard assessment obtained from the cook-off experiment complied with ARC analysis which indicated the molten binder TNT replaced by DNAN would reduce the hazard of the TKX-50 melt cast explosive. Furthermore, the results of cook-off experiments also showed that DNAN/TKX-50 outperformed TNT/TKX-50 from the aspect of thermal stability, which was consistent with the result of CHR mode because of the similar heating process.     

Terrorism,crime and public spending: Panel VAR evidence from europe

Within a panel VAR framework and utilizing generalized impulse response and forecast error variance decomposition analysis, we explore the dynamic effects of terrorism and crime on public order and safety spending across European countries during the period 1994–2006. Our findings show that a ‘shock’ in terrorism and/or in crime, significantly increases the subsequent trajectory of public order and safety spending. As a by-product, we find that public spending is ineffective in reducing observed crime or terrorism.     

弹道导弹被动段最优脉冲变轨方法

弹道导弹大气层外飞行时间长且弹道固定,易被敌方预测和拦截。针对以上问题,本文提出一种最优脉冲式变轨方法,该方法设计的弹道由2条不同的椭圆弧段组成,成功命中目标的同时,增加了敌方的拦截难度。以机动变轨所需能量和变轨后飞行剩余时间的加权最优为性能指标,设计了利用遗传算法在初始弹道上寻求最优变轨点的方法。最后,将遗传算法搜索最优点结果与遍历搜索结果进行对比,其最大误差为 ,从而验证了遗传算法在应用于导弹变轨问题,用以寻求最优变轨点是准确有效的。     

翼伞精确空投系统归航轨迹规划与控制

翼伞归航轨迹规划与控制问题是翼伞系统在一定初始状态下,利用自身可操作性,完成从初始位置到目标位置的转移问题。针对翼伞空投系统不同归航要求,规划出满足精度要求为圆径概率误差（ CEP ）小于40m的归航轨迹并经过一定量的控制完成翼伞空投系统精确空投任务。首先建立翼伞系统状态空间六自由度模型,并在此基础上提出系统简化稳态模型,通过最优控制方法,规划出满足空投要求的最优归航轨迹后对翼伞进行不断控制直至目标点。最后通过Matlab仿真试验,绘出翼伞系统归航轨迹图与控制变化图。     

火箭助飞鱼雷发控及弹道仿真

针对水面舰艇反潜武器系统研制、火箭助飞鱼雷作战使用研究中对助飞鱼雷的仿真需求,重点研究了助飞鱼雷发射控制仿真方法和空中弹道仿真方法,突破了不同工况不同射程下发动机关机时间建模技术、保证大范围飞行一致性的火箭自适应控制器设计技术。应用表明,所形成的助飞鱼雷武器通道仿真模型能有效模拟助飞鱼雷从发射控制到弹道航行到命中目标的全过程以及作战效果,能够支撑助飞鱼雷发控算法研究以及作战使用研究。