钢球侵彻不同靶标的相似性分析

为研究相同弹丸侵彻不同靶标所造成损伤之间的相似性,以钢球侵彻明胶造成的瞬时空腔的最大直径为研究对象,基于相似理论推导出瞬时空腔最大直径的相似准则方程,利用钢球侵彻明胶的实验数据求解出准则方程的系数和指数,最后通过钢球侵彻猪后腿实验验证了所得到的准则方程可用于不同靶标之间的相似性分析,并具有准确性和合理性。     

带有可信度因子的直觉模糊近似推理方法

针对基于相似度的直觉模糊近似推理问题,提出一种基于加权相似度量的直觉模糊推理方法。首先定义一种新的直觉模糊相似度度量公式,加入权重参数解决各维特征分配不均匀的问题,弥补了现有直觉模糊相似度量的缺陷。然后构建基于直觉模糊产生式规则的直觉模糊近似推理模型,加入可信度因子解决了随机性引起的信息不确定问题,同时给出模型的推理算法和计算步骤。最后通过实例验证了该方法的实用性和有效性,其在意图识别、目标识别等信息融合领域有良好的应用前景。     

基于相似原理的点特征松弛匹配算法

利用感兴趣点检测算子提取点特征,构建三角形并利用其相似度来定义点特征的匹配度,提出了一种新的具有比例与旋转不变特性的点特征松弛匹配算法.实验表明,所提出的匹配算法有很快的运算速度和很高的匹配正确率.     

一种改进AHP方法及其在C3I系统效能分析中的应用

针对Satty教授提出的传统AHP方法在实际应用中存在的缺陷,给出了标度改进的合理性原则,并基于该原则提出了标度改进的方法、改进权值的计算原理及计算方法。运用改进AHP方法,对防空C3I系统的效能度量进行了定量分析和计算。结果表明该方法易于理解和计算,适用于系统分析和系统评价。     

Equivalent accelerated life testing plans for log‐location‐scale distributions

Accelerated life testing (ALT) is widely used to determine the failure time distribution of a product and the associated life‐stress relationship in order to predict the product's reliability under normal operating conditions. Many types of stress loadings such as constant‐stress, step‐stress and cyclic‐stress can be utilized when conducting ALT. Extensive research has been conducted on the analysis of ALT data obtained under a specified stress loading. However, the equivalency of ALT experiments involving different stress loadings has not been investigated. In this article, a log‐location‐scale distribution under Type I censoring is considered in planning ALT. An idea is provided for the equivalency of various ALT plans involving different stress loadings. Based on this idea, general equivalent ALT plans and some special types of equivalent ALT plans are explored. For demonstration, a constant‐stress ALT and a ramp‐stress ALT for miniature lamps are presented and their equivalency is investigated. © 2010 Wiley Periodicals, Inc. Naval Research Logistics, 2010     

A novel modeling approach for express package carrier planning

Express package carrier networks have large numbers of heavily‐interconnected and tightly‐constrained resources, making the planning process difficult. A decision made in one area of the network can impact virtually any other area as well. Mathematical programming therefore seems like a logical approach to solving such problems, taking into account all of these interactions. The tight time windows and nonlinear cost functions of these systems, however, often make traditional approaches such as multicommodity flow formulations intractable. This is due to both the large number of constraints and the weakness of the linear programming (LP) relaxations arising in these formulations. To overcome these obstacles, we propose a model in which variables represent combinations of loads and their corresponding routings, rather than assigning individual loads to individual arcs in the network. In doing so, we incorporate much of the problem complexity implicitly within the variable definition, rather than explicitly within the constraints. This approach enables us to linearize the cost structure, strengthen the LP relaxation of the formulation, and drastically reduce the number of constraints. In addition, it greatly facilitates the inclusion of other stages of the (typically decomposed) planning process. We show how the use of templates, in place of traditional delayed column generation, allows us to identify promising candidate variables, ensuring high‐quality solutions in reasonable run times while also enabling the inclusion of additional operational considerations that would be difficult if not impossible to capture in a traditional approach. Computational results are presented using data from a major international package carrier. © 2008 Wiley Periodicals, Inc. Naval Research Logistics, 2008     

面向能力需求的武器装备组合规划模型与算法

针对武器装备组合规划中存在的选择难、规划难问题,在给定能力需求的条件下,从分析装备的组合变更对整体体系的影响出发,考虑了总的经费预算、年度费用分配、装备规划周期等约束,以能力差距和发展风险最小为准则,构建了双目标优化模型,并设计了基于差分进化和非支配排序的遗传算法的求解算法,获得模型的Pareto解。通过逼近理想解排序法方法从所求Pareto解中求得令决策者满意的折中解。通过一个具体示例验证了模型和算法的有效性,能够为武器装备组合规划提供辅助决策。     

某型运载火箭1/5动力学缩比模型设计

缩比模型试验是获取大型运载火箭动特性的一种有效途径,其中一项重要内容是动力学缩比模型设计。本文以某型运载火箭为原型对象,首先根据其结构组成分别推导各部件的相似关系;然后,利用横向刚度和质量相似系数保持一致性,联立形成了运载火箭横向动特性相似关系;同时,考虑实际加工制造条件,分析了横向刚度和质量相似系数的约束;最后,根据上述相似关系和相似系数约束设计了1/5缩比模型,并对该缩比模型的动特性相似进行了有限元数值计算验证。验证结果表明,设计所得1/5缩比模型在动特性方面与原型具有较高的相似性,相关方法能够有效应用于运载火箭的动力学缩比模型设计。     

大规模串行分布式检测的性能

串行分布式（Ｎ＝２,３,４）检测的最优协调门限组难以求取,因而只能就由少量传感器组成的小规模串行网,通过数值计算来考察检测性能。本文在一定条件下,给出了求取串行分布式检测性能的解析方法,进而可得到大规模串行分布式检测的性能,使我们能考察和了解检测性能在积累数增加时的变化趋势。     

点邻域尺度差异描述的点云配准算法

针对传统特征描述符计算复杂度高、配准精度低的问题,提出一种基于不同尺度点邻域特征信息差异的点云配准算法。在特征描述符方面,对关键点选取不同尺度的邻域空间,计算各尺度空间之间的特征值归一化向量差异和法向量夹角,建立点邻域尺度差异描述符,特征描述符计算简单且节省时间。在关键点选取方面,根据曲面形状指数设计了一种寻找关键点的方法,提取的点具有很好的代表性。在对应关系寻找方面,提出一种基于欧式距离的对应点二重筛选方法,找出对应点对集,设计了基于全局距离的全局最优点云变换矩阵求取方法。实验结果表明,点邻域尺度差异描述的点云配准算法具有良好的配准精度和稳健的噪声鲁棒性。