Development of cost effective personnel armour through structural hybridization

The objective of the present study is to develop cost effective thermoplastic hybrid laminate using Dyneema® HB50 and Tensylon®HSBD 30A through structural hybridization method. Laminates having 20 mm thickness were fabricated and subjected to 7.62 × 39 mm mild steel core projectile with an impact velocity of 730 ± 10 ms⁻¹. Parameters such as energy absorption, back face deformation and rate of back face deformation were measured as a function of hybridization ratio. It was observed that hybrid laminate with 50:50 ratio (w/w) of Tensylon® and Dyneema® with Tensylon® as front face showed 200% more energy absorption when compared to 100% Tensylon® laminate and showed equal energy absorption as that of expensive 100% Dyneema® laminate. Moreover, hybrid laminate with TD50:50 ratio showed 40% lower in terms of final back face deformation than Dyneema® laminate. Rate of back face deformation was also found to be slow for hybrid laminate as compared to Dyneema® laminate. Dynamic mechanical analysis showed that, Tensylon® laminate has got higher stiffness and lower damping factor than Dyneema® and hybrid laminates. The interface between Tensylon® and Dyneema® layers was found to be separating during the penetration process due to the poor interfacial bonding. Failure behaviour of laminates for different hybridization ratios were studied by sectioning the impacted laminates. It was observed that, the Tensylon® laminate has undergone shear cutting of fibers as major failure mode whereas the hybrid laminate showed shear cutting followed by tensile stretching, fiber pull out and delamination. These inputs are highly useful for body armour applications to design cost effective armour with enhanced performance.     

Analysis of the stress wave and rarefaction wave produced by hypervelocity impact of sphere onto thin plate

Shock wave is emitted into the plate and sphere when a sphere hypervelocity impacts onto a thin plate. The fragmentation and phase change of the material caused by the propagation and unloading of shock wave could result in the formation of debris cloud eventually. Propagation models are deduced based on one-dimensional shock wave theory and the geometry of sphere, which uses elliptic equations (corresponding to ellipsoid equations in physical space) to describe the propagation of shock wave and the rarefaction wave. The “Effective thickness” is defined as the critical plate thickness that ensures the rarefaction wave overtake the shock wave at the back of the sphere. The “Effective thickness” is directly related to the form of the debris cloud. The relation of the “Effective thickness” and the “Optimum thickness” is also discussed. The impacts of Al spheres onto Al plates are simulated within SPH to verify the propagation models and associated theories. The results show that the wave fronts predicted by the propagation models are closer to the simulation result at higher impact velocity. The curvatures of the wave fronts decrease with the increase of impact velocities. The predicted “Effective thickness” is consistent with the simulation results. The analysis about the shock wave propagation and unloading in this paper can provide a new sight and inspiration for the quantitative study of hypervelocity impact and space debris protection.     

Halo轨道编队构型重构最优控制研究

变长度的测量基线与空间构型的多样性是航天器以编队方式执行深空探测任务的优势之一,该优势的发挥与航天器编队构型重构能力密切相关.针对Halo轨道编队构型重构问题开展研究,分析了Halo轨道编队的构型特性,推导了Halo轨道编队构型重构最优控制的Hamilton方程,基于第一类生成函数构造了最优控制Hamilton方程的迭...     

多目标跟踪的神经网络实现方法

多目标跟踪在军事和民用方面得到广泛的应用。自适应网络模型 ART对已学习过的对象具有稳定的快速识别能力 ,同时又能适应未学习的新对象 ,ART模型的这种优势可直接应用于雷达的多目标跟踪。经过仿真验证 ,利用 ART模型解决多目标跟踪数据关联问题的方法较为有效。     

新型舰炮武器情报指挥系统模拟试验方法

在简要介绍模拟试验系统及搜索雷达模拟器功能和工作原理的基础上,针对某型近程反导舰炮武器情报指挥系统,提出了包括模拟试验流程、仿真数学模型及评估方法的一套模拟试验方法,弥补了单一外场试验考核不充分的不足,达到了全面科学评价被试系统的目的。该模拟方法是外场试验的补充和完善,开拓了靶场试验的新思路。     

军事设施建设项目环境影响评价有关问题分析及建议

根据《中国人民解放军环境保护条例》,军事设施建设项目应进行环境影响评价。由于军事项目建设内容高度机密、国防需要迫切、建设时间紧迫等,再加上一些从事军事设施项目建设的管理人员对环境影响评价的理解还存在某些偏差,使许多军事设施建设项目未进行环境影响评价,影响了我军的环境保护工作。简要介绍了军事设施的范围及军事设施建设项目的环境影响评价概况,结合军事设施建设项目环境影响评价中出现的一些问题,提出了进行军事设施建设项目环境影响评价工作的几点建议。     

弹道导弹落点预报的雷达系统仿真

根据弹道理论建立了雷达探测弹道导弹的仿真模型 ,并对仿真的雷达探测跟踪弹道数据给出了处理方法 ,预报了导弹落点范围 ,并与理论落点进行了比较 ,给出落点精度。仿真结果表明 :雷达对导弹的探测数据经过一定数据处理 ,可得到预定的落点精度 ,说明该种仿真方法是可行的     

基于恒虚警的多卫星信号快速盲检测算法?

在分析实际盲卫星通信信号的基础上,提出了一种对不重叠多卫星信号数量、中心频率进行实时估计的快速盲检测算法。算法基于恒虚警率准确地估计了噪声的统计特性进而设置了信噪分离的门限,并根据卫星通信信号的实际带宽特性实现了盲信号的检测。仿真结果表明,算法能够在较低的信噪比下实现对多卫星信号的快速准确盲检测,且与其他算法相比,该算法准确率高、通用性强,更能满足实际工程的需要。     

基于多目标权重分析的舰载反潜武器优先级选择

针对舰载反潜武器优先级选择问题,利用多目标权重分析法,通过构建影响因素的层次结构,建立多目标权重分析模型,确定指标矩阵和相对优越度矩阵,对反潜武器优先级选择方案进行评定,并进行了实例分析,得到的反潜武器选择方案综合体现了反潜武器作战能力和指挥员作战决策意图。     

调频斜率极性捷变SAR欠采样转发干扰

针对传统欺骗干扰难以对调频斜率极性捷变SAR形成有效干扰的问题,研究了对调频斜率极性捷变SAR进行欠采样转发干扰的方法。通过建立调频斜率极性捷变SAR有限时长欠采样转发干扰信号模型,分析欠采样转发干扰对调频斜率极性捷变SAR的干扰效果。给出假目标数目、位置以及幅度的理论计算公式,在此基础上讨论欠采样周期对干扰效果的影响。利用数字仿真验证了理论分析的正确性。