集团军反空袭战役空中威胁评估

运用定量和定性分析相结合的方法,对集团军反空袭战役空中威胁问题进行了分析,提出了评估的方法和步骤,建立了评估模型,并结合实例对评估方法、步骤、模型进行了分析验证。实例计算表明,利用该方法所实现的判断结果预见性好、可靠性强,对未来集团军反空袭作战有一定的现实意义。     

DMMP气溶胶的分析方法研究

实验研究了DMMP气溶胶的色质分析方法,确定了其色谱分离条件和质谱分析条件。并采用炭管法、碳氢总量分析方法进行了对比分析,获得了很好的一致性结果．解决了滤毒罐防沙林的DMMP模拟剂检验方法。     

武器装备体系能力多视图模型研究

针对武器装备体系能力概念抽象、关系复杂特点导致建模困难、重用性差、语义不一致等诸多问题,提出了一种基于本体的能力多视图模型构建方法,建立了6个能力视图的元模型.该方法首先明确能力领域问题,确定武器装备体系能力领域核心本体及构建原则,然后采用形式化方法描述本体,建立核心本体的关系模型,最后面向能力视图内容建立元模型,通过...     

雷达抗干扰性能多层次灰色评估模型研究

通过分析现代战争中雷达抗干扰的具体措施,建立了雷达抗干扰性能评估指标体系.采用多层次灰色评估方法对指标体系进行评估,并针对方法中线性白化函数在转折点处不能反应实际的问题,用了一种符合现实评估规律的Logistic函数代替传统的线性函数,从而使白化曲线更能符合实际.最后将改进后的评估模型应用于实例,结果表明改进后的方法可行,具有较高的科学性.     

航空自导深弹和磁探仪攻潜模型与仿真

针对反潜巡逻机使用磁探仪和自导深弹的攻潜效能研究,提出了一种基于蒙特卡洛法的计算模型。在建立攻潜坐标系的基础上,给出了连投深弹射击深度的定义;结合磁探仪定位原理,提出了基于峰值追踪的定位目标和连投攻击的方法,仿真结果表明该方法能够提高命中概率;给出了目标分布和连投深弹的散布模型,依据攻潜过程和命中判定条件,进行了攻潜效能的计算;仿真分析了影响攻潜效能的主要因素,并研究了投弹间隔的确定方法。     

作战实体概念模型结构研究

本文将动态的作战实体视为智能实体,运用系统六元抽象方法对作战实体概念模型构成要素进行分析,明确了要素之间的相互关系,并从作战实体内部的状态、结构、行为出发,提出了一种以知识系统为中心的作战实体的概念模型结构。     

遵义会议前后周恩来的军事实践

人民的好总理周恩来,已经离开我们整整30周年了。他的一生都献给了中国人民的革命事业。遵义会议前后一段时期,周恩来身处党和红军的重要领导岗位,其军事实践直接与党和红军的前途命运密切相关。在红军渡过湘江、局势仍然十分险恶的关键时刻,他客观分析形势,迅速从红军遭受的重大挫折中汲取教训,果敢支持、采纳毛泽东等人的正确意见,铸造了符合中国革命战争实际的科学战争观念和杰出战略素养;在遵义会议上,他主动承担军事领导上的责任,坚决推举毛泽东出来领导和指挥红军,为实现党和红军历史上的重大转折立下了不朽功勋;在率师转战中,他协助毛泽东运筹帷幄,巧渡金沙江,飞夺泸定桥,练就精湛指挥艺术和顽强战斗作风;他始终以确保对敌作战的胜利为最高原则,眼光远大,意志坚定,坚持北上,同张国焘进行了针锋相对的斗争,捍卫了党和红军的统一。     

考虑专家偏好的基于概率犹豫模糊熵的多属性决策方法

针对现有概率犹豫模糊多属性决策研究中,专家权重和属性权重的确定存在主观随意性的问题,提出了一种考虑专家偏好的基于概率犹豫模糊熵和前景理论的决策方法.基于贴近度度量,考虑专家的偏好性,以追求整体一致性为原则确定专家权重;基于概率犹豫模糊熵,考虑专家的决策差异,度量评估信息的犹豫性和模糊性,确定属性权重;采用前景理论对方案评估信息进行集结,根据价值函数和权重函数得到方案的前景价值,并以此进行方案排序.通过算例对比分析,验证了所提方法的科学性和合理性.     

Thermal and combustion behavior of Al-MnO2 nanothermite with poly(vinylidene fluoride -co- hexafluoropropylene) energetic binder

Fluoropolymers get increasing attention in energetic materials application due to the high fluorine content. To explore the effect of poly(vinylidene fluoride-co-hexafluoropropylene) (P(VDF-HFP)) on Al/MnO2 nanothermite, the samples with different contents are prepared and characterized by SEM, TG-DSC, XRD, and their ignition and combustion behavior are tested and recorded. The results show that P(VDF-HFP) as an energetic binder can combine the nanothermite components together, even exist in the gaps. The integrity of energetic materials has been improved. Thermal analysis shows that the addition of P(VDF-HFP) greatly changes the thermal reaction processes, and the exothermic peaks appear early, but the utilization of fuel and oxidizer is not efficient from the XRD results. Furthermore, the appropriate addition of P(VDF-HFP) can directly reduce the ignition energy threshold and increase the combustion time, which is necessary for the potential ignition charge application. The possible reasons for above phenomena are discussed and analyzed. This research provides a reference for improvement of thermite-based ignition charge formulation.     

Effect of projectile parameters on opening behavior of PELE penetrating RC target

When a penetrator with enhanced lateral effect (PELE) impacts on a reinforced concrete (RC) target, the target is damaged with a large opening. An understanding of how PELE projectile parameters affect the opening dimension, is essential for effective design of the PELE projectile. In this study, under the condition that the impact velocity and target parameters (strength and thickness) were fixed values, the important influence factors of the PELE (jacket wall thickness B, jacket material strength Y1, filling material strength Y2 and angle of monolithic jacketθ) were determined by a dimensional analysis. Tests and simulations of the PELE penetrating the RC target were conducted to analyze the influence of these factors on opening diameter ((D), an equivalent diameter under relative kinetic energy). Based on the test and simulation results, it is found that the influence of these factors B, Y1 andθon the deformation mode of the jacket shows a similar trend:as values of the three factors decrease, the jacket deforms from small bending deformation to large one, and then to curling deformation. This causes the opening diameter to first increase with the decrease of these three factors, and then decreases. It is well known that the bending resistance of the jacket is related to these factors B, Y1 andθ. Therefore, a plastic limit bending moment (M0) of the jacket was quoted to characterize the influence of these factors on the bending deformation of the jacket and the opening diameter of the target. The influence factor Y2 causes (D) to first increase with the increase of Y2, and then decreases. A formula was developed to predict the opening diameter, whose influence parameters were considered in a dimensionless way. It has been shown that the dimensionless opening diameter (D)/d1 is dependent on two dimensionless parameters Q = (d31fc/M0) and G = (fc/Y2), where d1 and fc are the outer diameter of the projectile and the compressive strength of the target, respectively.