核裂变过程动态模拟计算的动力学系数

本文利用(c,h,a)三参数旋转体模型计算了形变核的相对表面能、相对库仑能及相对转动能。这些相对能量与具体核无关,具有普适性,可以用于核裂变动态过程的模拟计算。利用这些结果,计算了一些核的形变位能随三参数变化的情况,给出了裂变位垒高度,与实验结果符合较好。对~(236)U的形变位能曲面作了较详细的分析,得出一些有益的结论。用Werner—Wheeler方法计算了形变核的惯性质量和粘滞张量随三参数变化情况,对断点线方程作了深入讨论,为核裂变动态过程的计算机模拟准备了必要的系数。     

基于控制通道融合的瞄准线组合稳定技术

提出一种光电二级稳定粗、精控制通道融合新方案,并与现有粗、精控制通道相互独立二级稳定方案相比较。仿真结果表明,粗、精控制融合方案无论在成本、体积、性能和精度上,都优于现有二级稳定方案。新方案的可行性已通过原理样机得到验证。     

瞄准具多因素误差分析模型

本文利用坐标轴旋转公式建立了瞄准具多因素误差分析模型。为机械式、半独立式瞄准具的不解体检测提供了理论基础.     

CAD/CAM 中的两种曲线保凸拟合

文中描述了一种保凸参数拟合方法。对于任意给定一个平面开(闭)的凸多边形、可用二次(三次)Bezier曲线段构造了一条C~1二次(C~2三次)的保凸插值样条曲线,并且简略讨论了该方法在CAD/CAM中的应用,如凸轮轮廓曲线的拟合,外形的几何设计等。我们在IBM-PC机上编制了通用的交互式作图软件,只要输入相应的坐标和控制参数,即可快速绘制出C~1二次(C~2三次)的保凸插值样条曲线。     

均匀试验设计在无人机关键参数设计中的应用

针对所采用CFD软件FLUENT对无人机的气动特性数值模拟,消耗大量时间这一问题,进行了试验设计,来减少试验次数。首先对各种常见的试验设计方法的优点局限性及试验次数进行了全面而详细的分析与总结,然后选取了均匀试验设计的方法来安排试验,实践了均匀试验设计在无人机关键参数设计中应用的案例,并通过曲线拟合建立了相应的模型,对均匀试验设计的可行性进行了验证。     

基于高精度景象匹配的SAR平台定位方法研究

为了提高SAR平台定位精度，本文提出了一种基于景象匹配的SAR平台定位的方法。该方法利用成像中间时刻SAR平台与SAR图像中心线上物点共线的特性，先在图像中心线上均匀选取若干点作为匹配点，并与光学基准图进行高精度景象匹配获取它们的物点坐标；然后根据这些物点坐标估计出图像中心线在当地水平面投影的直线方程；最后利用直线信息和斜距高度信息计算SAR平台在水平面上的投影点位置，进而计算得到成像中间时刻SAR平台的空间位置。为了进一步提高匹配精度，分别提出了对正侧视和斜视SAR图像匹配区域进行几何粗校正的方法。本文还分析了不同误差因素对平台定位精度的影响，并给出了精度估计公式。仿真和实际图像实验结果表明，本文方法正确可行，具有较高的定位精度，具备工程实用价值。     

Modeling and analysis of multiobjective lot splitting for N‐product M‐machine flowshop lines

Lot splitting is a new approach for improving productivity by dividing production lots into sublots. This approach enables accelerating production flow, reducing lead‐time and increasing the utilization of organization resources. Most of the lot splitting models in the literature have addressed a single objective problem, usually the makespan or flowtime objectives. Simultaneous minimization of these two objectives has rarely been addressed in the literature despite of its high relevancy to most industrial environments. This work aims at solving a multiobjective lot splitting problem for multiple products in a flowshop environment. Tight mixed‐integer linear programming (MILP) formulations for minimizing the makespan and flowtime are presented. Then, the MinMax solution, which takes both objectives into consideration, is defined and suggested as an alternative objective. By solving the MILP model, it was found that minimizing one objective results in an average loss of about 15% in the other objective. The MinMax solution, on the other hand, results in an average loss of 4.6% from the furthest objective and 2.5% from the closest objective. © 2010 Wiley Periodicals, Inc. Naval Research Logistics, 2010     

利用声光衍射测量甘草折射率的研究

本文是利用声光衍射测量甘草稀溶液折射率尝试。提出了胶体溶液大分子的球状散射模型，得出了测量使用的一个简化公式，并对甘草溶液的折射率给出了一个实验结论。     

瞄准线稳定精度的影响因素仿真

瞄准线稳定精度是直升机载稳瞄系统的关键技术指标之一,它影响着系统的其他关键性指标如照射精度、跟踪精度、作用距离等。因此提高瞄准线稳定精度是设计和研制机载稳瞄系统至关重要的一项任务。论文分析和研究了影响瞄准线稳定精度的因素,并采用Simulink建立数学模型,对瞄准线稳定精度的影响因素进行仿真分析,得到各因素对稳定精度的影响趋势,为机载稳瞄系统的设计工作提供了理论基础。     

The impact of demand uncertainty on product line design under endogenous substitution

The existing product line design literature devotes little attention to the effect of demand uncertainty. Due to demand uncertainty, the supply‐demand mismatch is inevitable which leads to different degrees of lost sales depending on the configuration of product lines. In this article, we adopt a stylized two‐segment setup with uncertain market sizes and illustrate the interplay between two effects: risk pooling that mitigates the impact of demand uncertainty and market segmentation that facilitates consumer differentiation. Compared to downward substitution, inducing bidirectional substitution through product line decisions including quality levels and prices can yield greater risk pooling effects. However, we show that the additional benefit from the risk pooling effect cannot compensate for the reduced market segmentation effect. We demonstrate that the presence of demand uncertainty can reduce the benefit of market segmentation and therefore the length of product lines in terms of the difference between products. We also propose three heuristics that separate product line and production decisions; each of these heuristics corresponds to one particular form of demand substitution. Our numerical studies indicate that the best of the three heuristics yields performance that is close to optimality. © 2015 Wiley Periodicals, Inc. Naval Research Logistics 62: 143–157, 2015