支板喷射超声速燃烧流场三维大涡模拟

利用火焰面模型和混合LES/RANS方法对某支板构型超燃冲压发动机进行模拟,讨论了化学反应对湍流流场的影响,并比较了3D和2D模拟的差别.结果表明,不考虑化学反应时剪切层中的大尺度结构控制着整个混合过程,且剪切层具有明显的三维特性;2D模拟能捕捉到涡的配对与合并现象,而3D模拟中涡的拉伸、扭曲及破碎特性更加显著;考虑化...     

一种控制学科在设计回路的多学科设计优化方法

提出了一种直接针对设计参数不确定性描述的鲁棒控制器设计方法,并将该方法的研究和多学科设计优化方法的研究结合起来,实现了控制学科在设计回路的多学科设计优化。以某无尾布局微型飞行器为例开展了气动、控制学科的并行设计优化研究,说明了该方法的可行性。     

An adaptive forecasting algorithm and inventory policy for products with short life cycles

Products with short life cycles are becoming increasingly common in many industries, such as the personal computer (PC) and mobile phone industries. Traditional forecasting methods and inventory policies can be inappropriate for forecasting demand and managing inventory for a product with a short life cycle because they usually do not take into account the characteristics of the product life cycle. This can result in inaccurate forecasts, high inventory cost, and low service levels. Besides, many forecasting methods require a significant demand history, which is available only after the product has been sold for some time. In this paper, we present an adaptive forecasting algorithm with two characteristics. First, it uses structural knowledge on the product life cycle to model the demand. Second, it combines knowledge on the demand that is available prior to the launch of the product with actual demand data that become available after the introduction of the product to generate and update demand forecasts. Based on the forecasting algorithm, we develop an optimal inventory policy. Since the optimal inventory policy is computationally expensive, we propose three heuristics and show in a numerical study that one of the heuristics generates near‐optimal solutions. The evaluation of our approach is based on demand data from a leading PC manufacturer in the United States, where the forecasting algorithm has been implemented. © 2004 Wiley Periodicals, Inc. Naval Research Logistics, 2004.     

共面编队飞行卫星星座的控制

共面编队飞行的卫星星座的相对运动轨迹是一个椭圆,但卫星由于受摄动力的影响,其椭圆队形会发生变化。提出了一个简单而又节约燃料的队形保持控制方案,即在Hill轨道坐标系中,通过测量x轴和z轴,利用小推力喷气发动机进行控制,消除椭圆中心的相位漂移和各卫星轨道的不共面。     

攻防对抗仿真中高炮火力单元射击指挥模型

在分析高炮火力单元射击指挥过程的基础上,着重对高炮火力单元射击指挥仿真中的目标搜索模型与杀伤效果评估模型进行了深入探讨和构建。在实现高炮杀伤效果评估方面,运用蒙特卡罗方法构建了符合实际、满足仿真粒度要求的高炮着发射与空炸射击毁伤概率计算模型。实际应用表明:模型满足仿真可信度和实时性要求,对开展地面防空作战仿真具有一定的借鉴意义。     

A spatial rank‐based multivariate EWMA control chart

Nonparametric control charts are useful in statistical process control when there is a lack of or limited knowledge about the underlying process distribution, especially when the process measurement is multivariate. This article develops a new multivariate self‐starting methodology for monitoring location parameters. It is based on adapting the multivariate spatial rank to on‐line sequential monitoring. The weighted version of the rank‐based test is used to formulate the charting statistic by incorporating the exponentially weighted moving average control scheme. It is robust to non‐normally distributed data, easy to construct, fast to compute and also very efficient in detecting multivariate process shifts, especially small or moderate shifts which occur when the process distribution is heavy‐tailed or skewed. As it avoids the need for a lengthy data‐gathering step before charting and it does not require knowledge of the underlying distribution, the proposed control chart is particularly useful in start‐up or short‐run situations. A real‐data example from white wine production processes shows that it performs quite well. © 2012 Wiley Periodicals, Inc. Naval Research Logistics 59: 91–110, 2012     

一种基于混合模拟的计算组合电路中软错误率的方法与工具

随着工艺尺寸的不断缩小,组合电路引起的SER(Soft Error Rates)越来越严重.针对使用HSPICE计算组合电路软错误率速度较慢以及使用传统的组合电路软错误率分析工具在对待重汇聚时计算精度不高的问题,本文提出了一种混合模拟的方法,并基于该方法实现了组合电路软错误率分析工具.该混合模拟方法使用HSPICE模拟发生重汇聚的逻辑门;使用快速的脉冲传播算法模拟其他逻辑门.模拟结果表明,该方法可以在速度和精度上达到很好的折中.通过与国际上常用的组合电路软错误率分析工具进行比较发现,在重汇聚发生较多的电路中,该混合模拟方法更能真实地反应组合逻辑中的软错误率.     

基于X射线脉冲星的导航半实物仿真系统

为验证X射线脉冲星导航的关键技术,本文描述了基于X射线脉冲星导航的半实物仿真系统组成和工作原理,并搭建了基于X射线脉冲星导航的半实物仿真系统。系统由信号模拟单元、信号接收单元和导航估计单元组成,此系统可有效模拟X射线脉冲星导航的星源强度、周期及脉冲轮廓,记录X射线脉冲星单光子到达时间,恢复X射线脉冲星脉冲轮廓,计算X射线脉冲到达时间及导航估计解算。所设计的半实物仿真系统为X射线脉冲星导航算法测试提供了有效手段,对X射线脉冲星自主导航研究的可行性验证、动态性能测试以及工程应用具有一定的参考价值。     

Screening and selection procedures with control variates and correlation induction techniques

We consider the problem of identifying the simulated system with the best expected performance measure when the number of alternatives is finite and small (often < 500). Recently, more research efforts in the simulation community have been directed to develop ranking and selection (R&S) procedures capable of exploiting variance reduction techniques (especially the control variates). In this article, we propose new R&S procedures that can jointly use control variates and correlation induction techniques (including antithetic variates and Latin hypercube sampling). Empirical results and a realistic illustration show that the proposed procedures outperform the conventional procedures using sample means or control variates alone. © 2012 Wiley Periodicals, Inc. Naval Research Logistics, 2012     

起重机吊重摆角的产生机理与动态仿真研究

针对吊重二自由度摆角非线性动力学模型,研究了起重机吊重摆角的产生机理和摆角的影响因素。起重机小车和大车同时做加（减）速的复合运动时,产生吊重二自由度摆角,摆角的大小受起升绳长度和小车运行加（减）速度大小的影响。动态仿真表明：小车运行加（减）速度对摆角的影响比绳长度显著;小车起动和制动时,吊重做受迫摆动;当小车加（减）速度增大l倍时,吊重摆角约增大0．12rad,摆速约增大0．164rad／s;当绳长度增加2m时,摆角和摆速无明显变化,吊重自由摆动的周期约增加1．3s。