独立需求生产批量优化问题的遗传算法实现

生产批量问题是企业生产和管理中一个常见的约束批量问题,在假定问题中各产品的需求独立,同时满足能力约束和生产平衡的条件下,建立基于独立需求的遗传算法模型,实现使生产费用、生产准备费用和库存费用综合指标最小的生产批量算法。并通过对实际问题的计算验证该模型和算法的有效性和可行性。     

基于声学测量的舰炮对空脱靶量算法研究

舰炮武器系统最基本、最重要的战术指标是射击精度,而通过舰炮对空射击脱靶量的测量能够评估对空射击精度及射击效力。在声学测量原理基础上,通过建立空间传感器阵进行多点测量,并利用弹丸激波参数与传播距离存在的关系,建立相应的数学模型,以完成舰炮武器系统对空射击脱靶量的测量。     

基于Morabito方法的滑行艇喷雾详细研究的计算机程序开发(英文)

Recently, Morabito(2010) has studied the water spray phenomena in planing hulls and presented new analytical equations. However, these equations have not been used for detailed parametric studies of water spray around planing hulls. In this paper, a straight forward analysis is conducted to apply these analytical equations for finding the spray geometry profile by developing a computer program based on presented computational process. The obtained results of the developed computer program are compared against existing data in the literature and favorable accuracy is achieved. Parametric studies have been conducted for different physical parameters. Positions of spray apex are computed and three dimensional profiles of spray are examined. It is concluded that spray height increases by an increase in the speed coefficient or the deadrise angle. Ultimately, a computational process is added to Savitsky's method and variations of spray apex are computed for different velocities. It is shown that vertical, lateral, and longitudinal positions of spray increase as the craft speed increases. On the other hand, two new angles are defined in top view and it is concluded that they have direct relation with the trim angle. However, they show inverse relation with the deadrise angle.     

Multi‐objective airport gate assignment problem in planning and operations

We consider the assignment of gates to arriving and departing flights at a large hub airport. This problem is highly complex even in planning stage when all flight arrivals and departures are assumed to be known precisely in advance. There are various considerations that are involved while assigning gates to incoming and outgoing flights (such a flight pair for the same aircraft is called a turn) at an airport. Different gates have restrictions, such as adjacency, last‐in first‐out gates and towing requirements, which are known from the structure and layout of the airport. Some of the cost components in the objective function of the basic assignment model include notional penalty for not being able to assign a gate to an aircraft, penalty for the cost of towing an aircraft with a long layover, and penalty for not assigning preferred gates to certain turns. One of the major contributions of this paper is to provide mathematical model for all these complex constraints that are observed at a real airport. Further, we study the problem in both planning and operations modes simultaneously, and such an attempt is, perhaps, unique and unprecedented. For planning mode, we sequentially introduce new additional objectives to our gate assignment problem that have not been studied in the literature so far—(i) maximization of passenger connection revenues, (ii) minimization of zone usage costs, and (iii) maximization of gate plan robustness—and include them to the model along with the relevant constraints. For operations mode, the main objectives studied in this paper are recovery of schedule by minimizing schedule variations and maintaining feasibility by minimal retiming in the event of major disruptions. Additionally, the operations mode models must have very, very short run times of the order of a few seconds. These models are then applied to a functional airline at one of its most congested hubs. Implementation is carried out using Optimization Programming Language, and computational results for actual data sets are reported. For the planning mode, analyst perception of weights for the different objectives in the multi‐objective model is used wherever actual dollar value of the objective coefficient is not available. The results are also reported for large, reasonable changes in objective function coefficients. For the operations mode, flight delays are simulated, and the performance of the model is studied. The final results indicate that it is possible to apply this model to even large real‐life problems instances to optimality within short run times with clever formulation of conventional continuous time assignment model. Copyright © 2013 John Wiley & Sons, Ltd.     

石浦港下湾门航道工程潮流数值模拟研究

依据最新的水文实测资料,对石浦港的潮汐潮流特征进行了分析;并建立了基于不规则三角形网格的二维潮流数学模型,根据实测资料对模型进行了验证。在验证的基础上,对下湾门5万t级航道工程(开挖及炸礁通航)实施前后的流场进行了数值模拟计算,根据计算结果对工程前后的潮流特征及其变化进行了分析。研究结果表明:(1)工程海区潮汐属于正规半日潮类型,潮流性质属正规半日潮流型,潮流运动呈往复流形式;(2)岸线走向与涨落潮流走向基本一致;(3)航道总体挖深较小,流速变化很小,并未改变大范围海域潮流运动整体特征;开挖段航道流速呈减小的趋势,深槽水域流速呈增加趋势;(4)炸礁使得口门处航道轴线水域的流场趋于平顺,流向与航道走向基本一致,对周边流场基本没有影响;(5)方案实施后,对潮位变化无影响;下湾门口门处潮量增加,而其他口门潮量降低;(6)航道转弯位置、进港口门以及外海航道处横流较强,其他区段横流较弱。     

电磁斥力机构数学建模

建立了电磁斥力机构的数学模型,在此基础上,对一组参数的电磁斥力机构分别进行了编程计算与软件仿真,仿真结果与编程计算结果非常接近,验证了数学模型的准确性.     

刘老涧船闸通航水流条件改善措施

刘老涧船闸是位于京杭运河苏北段上的复线船闸。为解决船闸在二、三线同时泄水时,一线船闸下闸首反向水头过高而使人字门启闭机机构损坏的问题,建立了平面二维水流数学模型对船闸上、下游水流条件进行计算,并按照《船闸总体设计规范》相关要求,判别改善方案通航水流条件的优劣,提出符合实际要求的工程措施。针对天然河道边界复杂等特点,采用非结构三角形网格,利用有限体积法对水流控制方程进行了离散计算。     

长江南京以下12.5 m深水航道二期工程口岸直河段选槽数学模型

采用平面二维潮流泥沙数学模型的技术手段,配合长江南京以下12.5 m深水航道二期工程口岸直河段选槽专题 研究,选取典型的水沙计算条件,进行了选槽方案实施前后潮流泥沙运动的对比计算分析及设计航槽内疏浚位置回淤量计 算,为鳗鱼沙河段选槽方案的确定提供科学依据。数学模型计算表明：方案1具有护滩和增加航道浅区段水流动力的效果, 对周边水域影响较小,同时考虑航道的可维护性、与交通组织适应性、与沿岸港口的适应性几个方面,推荐方案1（左右汊 单向航道）作为口岸直鳗鱼沙河段12.5 m深水航道选槽方案,但建议该方案左槽中段航线位置稍向左岸调整,以适应深槽 变化趋势。     

车辆荷载特性影响下的碰撞时间分布规律

受车辆荷载特性影响的碰撞时间(Time-To-Collision, TTC),被认为是车辆避撞系统中跟驰过程风险评估的有效指标.本文以车辆类型、超重和超速指标量化表征车辆荷载特性,分解前后车辆不同荷载特性组合的12类跟驰场景.基于动态称重技术获取融合荷载特性的交通流数据,分析车辆荷载特性对自由流交通状态下12类跟驰场景TTC分布的影响,利用KS 检验对比TTC分布的显著性.结果表明：TTC累计频率分布服从指数模型,在5%置信度水平上,跟驰前后车的车辆类型对TTC分布无显著影响;前后车均为超重轻车显著增加了潜在冲突风险,超重增加了轻车跟驰重车,轻车跟驰轻车场景的潜在冲突风险;前后车不超速跟驰场景下,轻车跟驰重车的风险比例高于轻车跟驰轻车.     

无齿减速器研究与试制

介绍了圆柱凸轮机构的一种特殊应用形式,特殊在于多圈螺旋的圆柱凸轮,使多个滚子同时处于啮合状态,提高系统的刚度和承载能力。该传动件虽为超静定机构,但通过控制间隙（精度）和构件的弹性变形来实现连续传动。在传动设计合理的前提下将该机构应用于减速器行业,设计出无齿减速器。通过在工厂加工试制样品并实验表明：类比于同类减速器,无齿减速器具有传动平稳,承载能力强,传动精度大,大传动比,制作工艺简单等特点。