天津奥林匹克中心体育场消防安全疏散设计

介绍了天津奥林匹克中心体育场工程消防安全疏散设计存在若干与现行消防规范及相关技术标准不相符之处,但采用性能化设计的理念,对人员安全疏散设计进行分析评估,得出结论认为设计能满足人员安全疏散标准,即该工程的消防安全疏散设计是安全的。     

航母编队航渡过程中预警机阵位确定方法研究

提供了一种航母编队航渡过程中预警机的阵位确定方法。通过对航母编队防空区域划分与防空作战过程的分析,总结了航母编队航渡过程中预警机阵位确定的原则,建立了预警机阵位的数学模型,仿真计算了模型中各个参数对预警机前出距离的影响。这些模型可用于确定预警机的前出距离、方位和高度,满足航母编队作战使用的需要。     

航母编队反潜声纳舰阵位确定方法研究

针对航母编队航渡过程中拖曳式线列声纳舰的阵位确定问题,提出了一种分析方法。通过对航母编队反潜监视区划分与反潜作战过程的分析,总结了声纳舰阵位确定的原则,建立了确定航渡过程中拖曳式线列声纳舰阵位的数学模型,仿真计算了模型中各参数对声纳舰前出距离的影响。这些模型可用于确定拖曳式线列声纳舰的前出距离,满足航母编队作战使用的需要。     

毫米波被动隐身技术研究

在毫米波被动探测与制导的实际威胁下,为提高地面目标在未来战场的生存能力,进行了目标的毫米波被动隐身技术的研究。分析了毫米波被动隐身的必要性,在目标的毫米波辐射特性测试原理基础上,对毫米波被动探测距离进行了分析。指出毫米波被动隐身的主要措施为目标的形状和材料特性的控制,并从这2方面分析了控制的实际措施。     

On optimal system designs in reliability‐economics frameworks

Reliability Economics is a field that can be defined as the collection of all problems in which there is tension between the performance of systems of interest and their cost. Given such a problem, the aim is to resolve the tension through an optimization process that identifies the system which maximizes some appropriate criterion function (e.g. expected lifetime per unit cost). In this paper, we focus on coherent systems of n independent and identically distributed (iid) components and mixtures thereof, and characterize both a system's performance and cost as functions of the system's signature vector (Samaniego, IEEE Trans Reliabil (1985) 69–72). For a given family of criterion functions, a variety of optimality results are obtained for systems of arbitrary order n. Approximations are developed and justified when the underlying component distribution is unknown. Assuming the availability of an auxiliary sample of N component failure times, the asymptotic theory of L‐estimators is adapted for the purpose of establishing the consistency and asymptotic normality of the proposed estimators of the expected ordered failure times of the n components of the systems under study. These results lead to the identification of ε‐optimal systems relative to the chosen criterion function. © 2007 Wiley Periodicals, Inc. Naval Research Logistics, 2007     

Outbound supply chain network design with mode selection and lead time considerations

We present a large‐scale network design model for the outbound supply chain of an automotive company that considers transportation mode selection (road vs. rail) and explicitly models the relationship between lead times and the volume of flow through the nodes of the network. We formulate the problem as a nonlinear zero‐one integer program, reformulate it to obtain a linear integer model, and develop a Lagrangian heuristic for its solution that gives near‐optimal results in reasonable time. We also present scenario analyses that examine the behavior of the supply chain under different parameter settings and the performance of the solution procedures under different experimental conditions. © 2006 Wiley Periodicals, Inc. Naval Research Logistics, 2007     

飞翼布局飞行器研究现状分析

对飞翼布局飞行器的发展脉络进行了梳理,涵盖了从其早期的进化史到现阶段的研究进展,并对未来的发展方向进行了思考和展望。同时,论述了飞翼布局飞行器的几个主要控制难点,具体包括:宽速域非线性状态下的姿态控制问题、多效应耦合下的高精度自主起降控制问题、气动模型近似及强扰动状态下的鲁棒控制难题,以及因多舵面冗余而引起的控制分配问题。此外,还深入讨论了当前重点研究的飞翼布局飞行器的流动控制问题,并对接下来主动流动控制技术的研究动向进行了阐述。     

演化排列优化拉丁超立方设计方法

拉丁超立方设计是最常用的计算机试验设计方法之一,针对现有拉丁超立方设计方法采样一次性且难以兼顾设计的空间均匀性和计算效率的问题,提出了一种演化排列拉丁超立方试验设计方法。通过对小样本设计的演化、排列信息继承和扩充等操作,以较小的计算量实现了样本的扩充与优化。此外,所提方法可以兼顾现有样本和新增采样点之间的关系,实现样本的序列扩充,这在实际近似建模过程中十分方便。通过多组数值试验,验证了本文方法在空间均匀性和计算效率等方面的优越性。     

大型捆绑助推器总体/动力/轨道一体化设计与优化

在综合考虑固体火箭发动机设计、轨道设计和总体特性相互作用、相互影响的情况下,建立了捆绑助推器总体/动力/轨道一体化设计优化模型和系统分析模型,并应用遗传算法完成了某大型捆绑助推器6个设计参数的优选。结果表明:本文方法优化设计效果明显,优化所得助推器质量比原方案减轻了17.7%。