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991.
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。  相似文献   
992.
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  相似文献   
993.
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  相似文献   
994.
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.  相似文献   
995.
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.  相似文献   
996.
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.  相似文献   
997.
998.
本文用恒电量微扰法研究了Ce3+对铝合金在0.1mol·L-1NaCl介质中的缓蚀机理及抗孔蚀性。结果表明:铝合金孔蚀诱导过程及其表面形成林转化膜过程具有相同的电化学模式,电化学腐蚀速度控制步骤取决于钝化膜(转化膜)/溶液界面过程。Ce3+对铝合金孔蚀的诱导期和发展期均有抑制作用,形成铈转化膜后,铝基表面阻抗大大提高,耐孔蚀性增强。  相似文献   
999.
情报、监视、侦察(ISR)建模是战役级作战仿真建模的重点和难点,在仿真中不仅要求ISR模型能够准确地反映战场空间实体之间的感知交互,同时还要有较高的运行速度。为了解决此问题,以随机性理论为基础进行情报监视侦察的建模仿真,以区域侦察飞行器图像情报的建模全流程为例,阐述其主要环节的建模方法,并通过仿真实验验证了该套建模方法的适用性和有效性。与传统的确定性ISR建模方法相比,该方法在保证仿真精度的同时提高了运行效率,为战役级作战仿真中C4ISR建模与仿真提供了参考方法。  相似文献   
1000.
基于可拓方法的C3I作战方案生成与评价   总被引:3,自引:0,他引:3  
作战指挥决策支持系统是指挥自动化系统的重要组成部分,作战方案生成与评价是作战指挥决策支持系统的基本功能.根据作战指挥决策支持系统特点将可拓方法应用于作战方案生成与评价,并分析了其优势所在.结合空战案例运用发散树方法进行作战方案集的开拓,并利用优度评价方法进行作战方案的评价,从而得到最佳作战方案.  相似文献   
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