一种能考虑动升力影响的高速艇迎浪纵向运动的数学模型

根据高速艇在静水及波浪中运动的特点,提出了高速艇迎浪纵向运动的基本假设,建立了能考虑动升力影响的高速艇迎浪纵向运动基本方程,并提出了高速艇迎浪纵向运动预报的一种新方法(滑航法),编制了理论预报程序,进行了模型试验验证研究.结果表明,中高航速时,滑航法可用于高速艇迎浪纵向运动的预报.     

再入快速抵达轨迹优化设计方法

针对再入初始速度大、飞行时间约束苛刻的轨迹设计问题,提出一种基于遗传算法和攻角+倾侧角联合优化的再入快速抵达轨迹优化设计方法。该方法在再入初段利用较大攻角迅速减小弹道倾角和拉平弹道,在再入后段/滑翔段联合设计和优化攻角+倾侧角变化规律以显著降低终端飞行速度,同时满足终端高度、终端航向角、最大动压、最大热流等约束条件。该方法能够提升传统升力体飞行器再入快速到达能力并拓展其应用范围。仿真结果表明,在典型飞行器参数和较大初始再入速度条件下,全程飞行时间小于12 min,终端速度能够小于7Ma,横向机动距离超过800 km。     

电场作用下w／o型乳状液液滴的极化模型及计算

为了更好地研究电场破乳的动力学机理，以单水滴为研究对象，建立电场作用下油中椭球形水滴的极化模型，研究w／o型（油包水）乳化油进行电场破乳脱水过程中水滴的极化特性，分析水滴极化的影响因素，推导体系中各个基本要素的关系式。分别对电场作用下水滴在向日葵油、棕榈油和校准油中的极化强度进行模拟计算。结果表明，电场中油水界面张力及油的介电常数均对水滴的极化产生直接影响；基于椭球形水滴的极化模型得出水滴单位体积极化率相对于基于圆球形水滴极化模型的结果有明显改善，低压区和高压区的最大相对误差分别为22．5％和13．5％。利用椭球形水滴的极化模型分析水滴的极化特性对深入研究乳化油电场破乳动力学机理具有积极意义。     

便携式自寻的反坦克导弹攻顶弹道研究

便携式反坦克导弹在通过击顶方式打击目标时,要同时满足落角和精度的要求,以达到对目标的毁伤效能。首先推导带落角约束的最优比例导引律;然后设计携式反坦克导弹击顶弹道方案,导弹先出筒无控,以指数规律完成爬升,采用定攻角进行滑翔飞行,弹道末端运用推导的导引律来满足对落点和落角的约束。仿真结果表明,当反坦克导弹攻击不同距离的目标时,该弹道方案具有较强的有效性。     

Complexity and workload considerations in product mix decisions under the theory of constraints

The literature on the product mix decision (or master production scheduling) under the Theory of Constraints (TOC), which was developed in the past two decades, has addressed this problem as a static operational decision. Consequently, the developed solution techniques do not consider the system's dynamism and the associated challenges arising from the complexity of operations during the implementation of master production schedules. This paper aims to address this gap by developing a new heuristic approach for master production scheduling under the TOC philosophy that considers the main operational factors that influence actual throughput after implementation of the detailed schedule. We examine the validity of the proposed heuristic by comparison to Integer Linear Programming and two heuristics in a wide range of scenarios using simulation modelling. Statistical analyses indicate that the new algorithm leads to significantly enhanced performance during implementation for problems with setup times. The findings show that the bottleneck identification approach in current methods in the TOC literature is not effective and accurate for complex operations in real‐world job shop systems. This study contributes to the literature on master production scheduling and product mix decisions by enhancing the likelihood of achieving anticipated throughput during the implementation of the detailed schedule. © 2015 Wiley Periodicals, Inc. Naval Research Logistics 62: 357–369, 2015     

Synchronization in hub terminals with the circular arrangement problem

Hub terminals are important entities in modern distribution networks and exist for any transportation device, that is, cross docks and parcel distribution centers for trucks, container ports for ships, railway yards for trains, and hub airports for aircraft. In any of these hubs, the mid‐term planning task of synchronizing the transshipment of goods and passengers when servicing the transportation devices has to be solved, for which many different solution approaches specifically tailored to the respective application exist. We, however, take a unified view on synchronization in hubs and aim at a general building block. As a point of origin, a basic vertex ordering problem, the circular arrangement problem (CAP), is identified. We explain the relation between the CAP and hub processes, develop suited algorithms for solving the CAP, and extend the basic CAP by multiple additions, for example, arrival times, limited storage space, and multiple service points, make the problem adaptable to a wide range of hub terminals. © 2015 Wiley Periodicals, Inc. Naval Research Logistics 62: 454–469, 2015     

嵌入式在线航空摄影测量方法

为满足空间数据实时处理的需求,提高航空摄影测量系统在线处理能力,研究一种在线摄影测量的理论与方法,运用嵌入式架构设计一种在线摄影测量系统,使用可编程门阵列(FPGA)方法、高级精简指令集机器组合数字信号处理器(ARM+DSP)方法等嵌入式计算技术建立专门的硬件运行环境,移植并优化现有算法到嵌入式系统中,实现摄影测量数据的在线处理。机载航摄实验结果表明,该方法能够实现对摄影测量数据进行快速稳定的在线处理,验证了运用嵌入式架构的在线摄影测量的可行性,把摄影测量的处理效率提高到了一个更高的水平,同时也进一步拓宽了摄影测量技术的应用领域。     

临近空间高超声速目标拦截弹弹道规划

利用弹道规划设计了针对临近空间高超声速飞行器的拦截弹道。分析了临近空间高超声速目标拦截问题,将其定性为临近空间的远程高超声速拦截,并提出弹道规划需求;设计了一种两级助推的拦截弹,建立了考虑地球曲率和自转的拦截弹质点平面运动模型;根据弹道规划需求设计弹道约束,以末速最大、与终点距离误差最小和全程热量最小为指标建立拦截弹弹道规划问题;采用粒子群算法求解弹道,结果表明:符合约束的规划弹道是高抛再入形式,与比例导引弹道和准最佳弹道相比,拦截弹大部分时间飞行在大气层外,有效降低了气动热效应影响和对弹体材料的性能需求,且为末制导段提供良好的初始工作环境。     

训练电磁环境生成和逼真度评估方法

构建与战场电磁环境尽可能相似的训练电磁环境、评估所构建的训练电磁环境与战场电磁环境的相似程度,是基地训练电磁环境构建必须解决的突出问题。基于相似理论基本原理和相似度计算基本方法,结合基地训练电磁环境构建实践,采用精确值相似度计算生成训练电磁环境,采用区间值相似度计算评估训练电磁环境的逼真度。     

基于复杂网络理论的航材配送网络抗毁性分析

航材配送是航材保障工作的重要环节,科学地构建航材配送网络是提高航材保障效率的前提和基础。深入开展航材配送网络研究,对提高航材保障工作效益具有重要意义。针对航材配送网络节点繁多、线路交错的特点,分析了航材配送网络的复杂特性,构建了基于复杂网络理论的航材配送网络模型,设计了航材配送网络的拓扑特征参数,研究了航材配送网络的抗毁性。理论分析和实验结果表明,随机攻击时航材配送网络的抗毁性要大于选择性攻击,节点选择攻击时航材配送网络的抗毁性小于边选择攻击。