陆军战术作战仿真想定生成方法

针对作战仿真中想定数据的生成需求,在分析仿真想定内容的基础上,规范了仿真想定的生成流程,给出了指挥规则的抽取和量化方式,提出了面向实体的仿真想定结构化表示方法和基于XML的仿真想定存储结构,分析了利用G IS和3D技术实现作战计划和行动协同规划的方法途径,探讨了仿真想定数据的校核内容和重用机制,为实现仿真想定生成工具提供了一种有效的思路。     

远程迷惑式干扰效果评估模型

在分析远程迷惑式干扰机理的基础上,研究迷惑式干扰的各种影响因素,分别引入了箔条云相似因子、时间有效性因子、编队模拟逼真度因子、雷达识别影响因子和战术选择影响因子等多个效果评估指标,提出了多箔条云数目的整合模型,然后求导出在远程迷惑式干扰务件下搜索雷达对真实目标的捕捉概率计算模型,最后验证了模型的合理性.     

Study of high-speed-impact-induced conoidal fracture of Ti alloy layer in composite armor plate composed of Ti-and Al-alloy layers

In order to understand the mechanism of conoidal fracture damage caused by a high-speed fragment-simulating projectile in titanium alloy layer of a composite armor plate composed of titanium- and aluminum-alloy layers, the ballistic interaction process was successfully simulated based on the Tuler-Butcher and GISSMO coupling failure model. The simulated conoidal fracture morphology was in good agreement with the three-dimensional industrial-computed-tomography image. Further, three main damage zones (zones I, II, and III) were identified besides the crater area, which are located respectively near the crater area, at the back of the target plate, and directly below the crater area. Under the high-speed-impact conditions, in zone II, cracks began to form at the end of the period of crack formation in zone I, but crack formation in zone III started before the end of crack formation in zone II. Further, the damage mechanism differed for different stress states. The microcracks in zone I were formed both by void connection and shear deformation. In the formation of zone I, the stress triaxiality ranged from-2.0 to-1.0, and the shear failure mechanism played a dominant role. The microcracks in zone II showed the combined features of shear deformation and void connection, and during the for-mation process, the stress triaxiality was between 0 and 0.5 with a mixed failure mode. Further, the microcracks in zone III showed obvious characteristics of void connection caused by local melting. During the zone III formation, the triaxiality was 1.0-1.9, and the ductile fracture mechanism was dominant, which also reflects the phenomenon of spallation.     

Damage mechanics and energy absorption capabilities of naturalfiber reinforced elastomeric based bio composite for sacrificial structural applications

The present study deals with the experimental, finite element (FE) and analytical assessment of low ballistic impact response of proposedflexible'green' composite make use of naturally available jute and rubber as the constituents of the composite with stacking sequences namely jute/rubber/jute (JRJ), jute/rubber/rubber/jute (JRRJ) and jute/rubber/jute/rubber/jute (JRJRJ). Ballistic impact tests were carried out by firing a conical projectile using a gas gun apparatus at lower range of ballistic impact regime. The ballistic impact response of the proposed flexible composites are assesses based on energy absorption and damage mechanism. Results revealed that inclusion of natural rubber aids in better energy ab-sorption and mitigating the failure of the proposed composite. Among the three different stacking se-quences of flexible composites considered, JRJRJ provides better ballistic performance compared to its counterparts. The damage study reveals that the main mechanism of failure involved in flexible com-posites is matrix tearing as opposed to matrix cracking in stiff composites indicating that the proposedflexible composites are free from catastrophic failure. Results obtained from experimental, FE and analytical approach pertaining to energy absorption and damage mechanism agree well with each other. The proposed flexible composites due to their exhibited energy absorption capabilities and damage mechanism are best suited as claddings for structural application subjected to impact with an aim of protecting the main structural component from being failed catastrophically.     

Investigate the effects of magnetic fields on the penetration ability of a shaped charge jet at different standoffs

The influence of a magnetic field on the stability of a shaped charge jet is experimentally investigated at standoffs of 490, 650 and 800 mm. The experimental results without and with the magnetic field are compared in terms of the shaped charge jet form, stability and penetration ability. A theoretical model based on one-dimension fluid dynamics is then developed to assess the depth of penetration of the shaped charge at those three standoffs and magnetic conditions. The results show that the penetration capability can be enhanced in more than 70% by the magnetic field. The theoretical calculations are compared with the experimental results with reasonably good correlation. In addition, the parameters introduced in the theory are discussed together with the experiments at three standoffs studied.     

对一体化联合作战的思考

对一体化联合作战的概念及基本特征作了介绍,探讨了研究一体化联合作战的迫切性,对我军一体化联合作战的的现状及如何加速提高我军一体化联合作战的能力作了详细的论述。     

基于SEA的舰载C3I系统防空作战效能评估模型

现代海战中,空中目标对舰艇的威胁越来越大,舰艇的防空作战能力已成为衡量其综合作战能力的主要指标。而C3I系统作为舰艇的指挥中枢,其性能直接决定着舰艇防空作战的成败。根据现代海战中空中目标的武器作战使用方式,并针对SEA方法的要求,提出了评估C3I系统在防空作战时系统效能的三个主要性能量度(MOP),通过分析C3I系统在防空作战时的特点,建立了评估C3I系统防空作战效能的SEA方法模型。并利用该模型比较了不同的C3I系统的作战效能,对结果进行了简要分析,证明了SEA方法模型对舰载防空C3I系统进行效能评估的可行性。     

网络中心作战体系效能评估方法初探

网络中心作战体系是信息化战争要求下的一个具体作战体系,其效能评估是网络中心战研究领域的重要问题,是解决网络中心作战体系建设中方案论证、性能效能指标、经济因素等诸多问题的有效方法。首先提出了网络中心作战体系效能评估的基本概念;然后阐述了网络中心作战体系效能评估方法问题,分析介绍了几种较为成熟的评估方法的特点、适用性和不足;最后提出一种基于探索性建模与分析方法的网络中心作战体系效能评估框架,作为研究网络中心作战体系效能评估的参考评估框架。     

基于可拓工程方法的舰空导弹作战通道性能分析

分析了舰空导弹作战通道性能的影响因素,应用可拓工程方法建立了舰空导弹作战通道性能多指标参数的物元可拓评估模型,以定量的结果对舰空导弹作战通道性能进行了评估分级,并与层次分析法的结果进行了比较,结论基本一致。为舰空导弹作战通道性能评估问题寻求出一种新方法,其评估结果可为决策提供定量依据。     

某供弹机构现存问题动力学分析及参数优化探讨

介绍了环形杠杆供弹机构的工作原理及其在实际使用中常见的问题,建立了机构的动力学模型,对模型进行动态求解,模拟了机构的工作过程。借助求解结果,针对问题产生的原因进行了动力学分析,在理论上找到了问题产生的根源。在此基础上建立了机构的最优化数学模型,给出了优化方案,最后对优化方案和现有结构进行了比较。