基于公式法的某型水陆坦克海上火力打击效能

针对某型水陆坦克火力威力和火控系统特点,运用定性与定量分析相结合的方式,研究水陆坦克的火力打击效能。运用公式法,从分析某型水陆坦克海上射击误差入手,结合海上作战环境,研究其命中概率,并结合环境特点,分析条件毁伤概率,确定其对M60A3坦克和工事目标的火力打击的能力,得出了水陆坦克的开火距离、弹种选择等相关结果。研究结论对于分析火力打击效能提供了较为合理的方法,对于指导某型水陆坦克海上火力运用提供了借鉴作用。     

面元法的红外制导图像边缘检测

红外图像通常存在着噪声大、目标和背景之间具有较小的灰度差、边缘较模糊的特点,使现有的方法不能有效地提取红外图像的边缘。而图像的表面积特征能较好地针对红外图像的这些特征提取出边缘,因此利用图像的表面积特征提出了一种实用的面元边缘检测法。在对图像灰度值变化情况进行分析的基础上,使用了一种十字面积计算公式以满足边缘检测的需要。通过噪声误差对面元法和梯度法计算结果的影响分别进行分析,发现面元法比梯度法的噪声抑制能力至少高两倍,而且在边缘处的噪声抑制能力更高。将面元法几种常用模板算子法的红外图像边缘检测结果进行实际对比后发现,所提出的面元法对红外图像的目标边缘检测能取得良好的结果。     

System reliability based on diffusion models for fatigue crack growth

Diffusion processes are commonly used to describe the dynamics of complex systems arising in a wide range of application fields. In this paper we propose, on the basis of diffusion processes, two models concerned with the stochastic behavior of fatigue cracks in a system. They are then used to get the distribution of the failure time, the first time the crack size of at least one of the cracks exceeds a given value. Several properties of our proposed models are presented, and the unknown parameters are estimated by the method of maximum likelihood. From these an estimate of failure time distribution is obtained. In this part, contrary to common practice, we do not assume availability of failure data. © 2004 Wiley Periodicals, Inc. Naval Research Logistics, 2005     

Double window acceptance sampling

We introduce the concept of a sequential double window procedure and compare the resulting acceptance test with both a fixed sample size method as well as with the Wald sequential probability ratio test. © 2003 Wiley Periodicals, Inc. Naval Research Logistics, 2004     

Preparation and characterization of HMX/EVA/hBNNSs micro-composites with improved thermal stability and reduced sensitivity

Hexagonal boron nitride nanosheets(HBNNSs)have huge potential in the field of coating materials owing to their remarkable chemical stability,mechanical strength and thermal conductivity.Thin-layer hBNNSs were obtained by a liquid-phase exfoliation of h-BN powders and incorporated into EVA coatings for improving the safety performance of 1,3,5,7-tetranitro-1,3,5,7-tetrazocane(HMX).HBNNSs and ethylene-vinyl acetate copolymer(EVA)were introduced to HMX by a solvent-slurry process.For com-parison,the HMX/EVA and HMX/EVA/graphene(HMX/EVA/G)composites were also prepared by a similar process.The morphology,crystal form,surface element distribution,thermal decomposition property and impact sensitivity of HMX/EVA/hBNNSs composites were contrastively investigated.Results showed that as prepared HMX/EVA/hBNNSs composites were well coated with hBNNSs and EVA,and exhibited better thermal stability and lower impact sensitivity than that of HMX/EVA and HMX/EVA/G composites,suggesting superior performance of desensitization of hBNNSs in explosives.     

An efficient SPH methodology for modelling mechanical characteristics of particulate composites

Particulate composites are one of the widely used materials in producing numerous state-of-the-art components in biomedical, automobile, aerospace including defence technology. Variety of modelling techniques have been adopted in the past to model mechanical behaviour of particulate composites. Due to their favourable properties, particle-based methods provide a convenient platform to model failure or fracture of these composites. Smooth particle hydrodynamics (SPH) is one of such methods which demonstrate excellent potential for modelling failure or fracture of particulate composites in a Lagrangian setting. One of the major challenges in using SPH method for modelling composite materials depends on accurate and efficient way to treat interface and boundary conditions. In this paper, a master-slave method based multi-freedom constraints is proposed to impose essential boundary conditions and interfacial displacement constraints in modelling mechanical behaviour of composite materials using SPH method. The proposed methodology enforces the above constraints more accurately and requires only smaller condition number for system stiffness matrix than the procedures based on typical penalty function approach. A minimum cut-off value-based error criteria is employed to improve the compu-tational efficiency of the proposed methodology. In addition, the proposed method is further enhanced by adopting a modified numerical interpolation scheme along the boundary to increase the accuracy and computational efficiency. The numerical examples demonstrate that the proposed master-slave approach yields better accuracy in enforcing displacement constraints and requires approximately the same computational time as that of penalty method.     

Survivability assessment of spacecraft impacted by orbit debris

To help optimize the spacecraft design and reduce the risk of spacecraft mission failure, a new approach to assess the survivability of spacecraft in orbit is presented here, including the following three steps:1) Sensitivity Analysis of spacecraft. A new sensitivity analysis method, a ray method based on virtual outer wall, is presented here. Using rays to simulate the debris cloud can effectively address the component shadowing issues. 2) Component Vulnerability analysis of spacecraft. A function"Component functional reduction degree — Component physical damage degree"is provided here to clearly describe the component functional reduction. 3) System-level Survivability Assessment of spacecraft. A new method based on expert knowledge reasoning, instead of traditional artificial failure tree method, is presented here to greatly improve the efficiency and accuracy of calculation.     

Adaptive phasefield modelling of crack propagation in orthotropic functionally graded materials

In this work, we extend the recently proposed adaptive phase field method to model fracture in orthotropic functionally graded materials (FGMs). A recovery type error indicator combined with quadtree decomposition is employed for adaptive mesh refinement. The proposed approach is capable of capturing the fracture process with a localized mesh refinement that provides notable gains in computational efficiency. The implementation is validated against experimental data and other nu-merical experiments on orthotropic materials with different material orientations. The results reveal an increase in the stiffness and the maximum force with increasing material orientation angle. The study is then extended to the analysis of orthotropic FGMs. It is observed that, if the gradation in fracture properties is neglected, the material gradient plays a secondary role, with the fracture behaviour being dominated by the orthotropy of the material. However, when the toughness increases along the crack propagation path, a substantial gain in fracture resistance is observed.     

高炮射弹飞行时间拟合

用插值拟合和最小二乘逼近拟合方法对高炮射弹飞行时间拟合问题进行了研究。通过对插值拟合公式原理及误差规律的分析,提出确定可用区间的"去值检验"方法,说明了插值拟合公式的应用范围。通过对最小二乘拟合公式实际计算结果的分析,得出了"拟合公式阶数取3为最佳"的结论。对其他口径高炮的射弹飞行时间拟合也基本适用。     

部队作战效能综合评估法

高技术条件下局部战争的显著特点是参战单位多、对抗关系复杂、战争不确定因素增加,如何在此情况下客观评估部队的作战效能是作战研究领域一个重点和难点。通过综合运用定性分析法、网络分析法、战斗效能指数法、作战模拟及系统动力学等多种方法和理论,建立了一种可对部队作战效能进行评估的综合评估法。并以高技术条件下岛上进攻作战中装甲团的作战效能评估为例,详细介绍了该方法的实施过程,认为该综合评估法是行之有效的。