Automatic Airway Deletion in Pulmonary Segmentation

A method of removing the airway from pulmonary segmentation image was proposed. This method firstly segments the image into several separate regions based on the optimum threshold and morphological operator,and then each region is labeled and noted with its mean grayscale. Therefore, most of the non-lung regions can be removed according to the tissue‘s Hounsfield units (HU) and the imaging modality. Fifially, the airway region is recognized and deleted automatically through using the priori information of its HU and size. This proposed method is tested using several clinical images, yielding satisfying results.     

中文文本信息过滤技术研究

随着互联网信息数量的急剧增加,文本信息过滤技术越来越受到重视。本文首先介绍了文本信息过滤技术的发展历史和研究现状,阐述了中文文本过滤的特点和要求。重点分析了中文文本过滤技术的关键技术和评价标准。     

汽油机瞬态排放信号测试与特征分析的新动向

针对内燃机瞬态排放与稳态排放之间的差异,认为分析内燃机瞬态排放信号要有特殊的手段;回顾了混沌时间序列分析 特征参数族及将其运用于内燃机振动信号分析的工作;同时回顾了国外同行们将由符号动力学理论,混沌时间序列分析和信息理论发展起来的符号时间序列分析技术运用于内燃机瞬态数据分析和辨识的研究工作,给出了国外汽油机瞬态排放测试技术的发展状况,提出了可以基于符号时间序列分析对汽油机瞬态排放信号进行分析,获得瞬态排放的特征和影响因素。     

荷载列作用下简支曲线梁的动力响应

用积分变换法求解了荷载列作用下简支曲线梁桥动力响应的解析解 .在讨论过程中将单轴、两轴和四轴三种荷载列模型用一标准荷载列模型来表示 ,使得荷载模型更具有普遍性 .在讨论过程中均采用标准函数 ,从而避免了公式推导过程中的不确定因素 .最后按本文所给出的计算方法编制了计算简支曲线梁在荷载列作用下的动力响应程序 ,得到了较好的结果     

集腋成裘，学林嘉音——从《莫友芝年谱长编》说开去

作为一代知名学者,莫友芝的学术活动具有重要的研究价值,《莫友芝年谱长编》甚多抉发。年谱之制,可以考见谱主生平交游,订其著述编年。此类述论,文献材料翔实,既可当谱主生平著述的动态历史,又能反映当时的世情物故,有阐述性研究不可替代的突出优点。《长编》正是如此,其引录巨富、涉猎广博、考证精良、条述清晰,堪称迄今有关莫友芝研究的最巨成果。     

基于GPS/GIS的列车实时监控系统设计

介绍列车位置实时监控系统.列车监控中心通过车载GPS回传的车辆定位信息实现对列车位置和列车运行状态进行监控,并将列车行驶的轨迹以动画的方式显示在电子地图上.当发出报警信号时及时派遣抢险车进行抢险.     

基于灰度变换的沥青混合料图像增强及分割实现

数字图像技术是提取和描述沥青混合料细观结构的有效途径,可以通过图像增强、图像分割实现集料和其他组分的分离。通过灰度变换方法调整图像的动态灰度范围,便于进行后续的图像分割处理。结合Matlab软件实现图像的灰度变换增强,同时采用代数运算、除噪滤波进行处理,实现了混合料图像的分割处理及边界识别。     

Methodology for global structural load effect analysis of the semi-submersible hull of floating wind turbines under still water,wind, and wave loads

In designing the support structures of floating wind turbines (FWTs), a key challenge is to determine the load effects (at the cross-sectional load and stress level). This is because FWTs are subjected to complex global, local, static, and dynamic loads in stochastic environmental conditions. Up to now, most of the studies of FWTs have focused on the dynamic motion characteristics of FWTs, while minimal research has touched upon the internal load effects of the support structure. However, a good understanding of the structural load effects is essential since it is the basis for achieving a good design. Motivated by the situation, this study deals with the global load effect analysis for FWT support structures. A semi-submersible hull of a 10-MW FWT is used in the case study. A novel analysis method is employed to obtain the time-domain internal load effects of the floater, which account for the static and dynamic global loads under the still water, wind, and wave loads and associated motions. The investigation of the internal stresses resulting from various global loads under operational and parked conditions and the dynamic behavior of the structural load effects in various environmental conditions are made. The dominating load components for structural responses of the semi-submersible floater and the significant dynamic characteristics under different wind and wave conditions are identified. The dynamic load effects of the floating support structure are investigated by considering the influence of the second-order wave loads, viscous drag loads induced global motions, and wind and wave misalignments. The main results are discussed, and the main findings are summarized. The insights gained provide a basis for improving the design and analysis of FWT support structures.     

气动载荷对半潜式海上风机运动响应的影响分析

以DeepCwind海上风机为研究对象,利用有限元软件ANSYS AQWA进行风机频域水动力数值仿真分析,得到水动力参数以及幅频响应曲线,将得到的水动力参数导入到FAST软件中,对风机气动-水动-锚泊系统的时域耦合运动分析。在此基础上,讨论了气动载荷对于半潜式风机运动响应的影响。结果表明,气动载荷对于半潜式风机运动响应的影响较大且不可忽略,横摇,横荡以及首摇运动随着气动载荷的增大而增大,垂荡运动随着气动载荷的增大而减小,风作用在叶片上所产生的气动阻尼削弱了垂荡运动,增强了横荡、横摇和首摇运动。     

A constraint programming model with time uncertainty for cooperative flight departures

The lack of a proper integration of strategic Air Traffic Management decision support tools with tactical Air Traffic Control interventions usually generates a negative impact on the Reference Business Trajectory adherence, and in consequence affects the potential of the Trajectory-Based Operations framework. In this paper, a new mechanism relaying on Reference Business Trajectories as a source of data to reduce the amount of Air Traffic Controller interventions at the tactical level while preserving Air Traffic Flow Management planned operations is presented. Artificial Intelligence can enable Constraint Programming as it is a powerful paradigm for solving complex, combinatorial search problems. The proposed methodology takes advantage of Constraint Programming and fosters adherence of Airspace User’s trajectory preferences by identifying tight interdependencies between trajectories and introducing a new mechanism to improve the aircraft separation at concurrence events considering time uncertainty. The underlying philosophy is to capitalize present degrees of freedom between layered Air Traffic Management planning tools, when sequencing departures at the airports by considering the benefits of small time stamp changes in the assigned Calculated Take-Off Time departures and to enhance Trajectory-Based Operations concepts.