纺织结构复合材料强度性能的研究

考究了由两种不同纺织结构制备的碳繁华只物／环氧树脂复合的制备方法及强度性能，探讨了复合材料强度与织物结构参数－纤维取向之间的关系，导出了计算纺织结构复合强度公式，其估算值与实测值吻合。     

高效图像资源管理器的设计与实现

针对数据存储量大引起的访问广域网服务器速度慢、不能对访问的客户进行细粒度的权限控制问题,研究了B/S模式下基于.NET平台的图像资源管理器的设计和实现技术。系统综合采用权限管理模型、动态加载、文档对象模型（DOM）等技术以及非点击无刷新伸缩控制方法,实现了图像资源管理器的分权限控制、高速访问以及无刷新高效联动等操作。实验验证了方法的可行性。     

动态试验中支架对三角翼涡破碎影响研究

在南京航空航天大学低我洞中用前缘后掠角分别为６５°和７０°三角翼模型，采用不同厚度和不同位置安装的类似后横向支架进行过失速非定常破碎涡的测定实验，涡及破碎点位置由ＴｉＣｌ４烟流显示，并用相机记录。实验表明，在非定常过失速情况下，涡的破碎位置和非定常气动力一样具有迟滞环特性。     

Hierarchical object oriented classification using very high resolution imagery and LIDAR data over urban areas

Urban land cover information extraction is a hot topic within urban studies. Heterogeneous spectra of high resolution imagery—caused by the inner complexity of urban areas—make it difficult. In this paper a hierarchical object oriented classification method over an urban area is presented. Combining QuickBird imagery and light detection and ranging (LIDAR) data, nine kinds of land cover objects were extracted. The Spectral Shape Index (SSI) method is used to distinguish water and shadow from black body mask, with 100% classification accuracy for water and 95.56% for shadow. Vegetation was extracted by using a Normalized Difference Vegetation Index (NDVI) image at first, and then a more accurate classification result of shrub and grassland is obtained by integrating the height information from LIDAR data. The classification accuracy of shrub was improved from 85.25% to 92.09% and from 82.86% to 97.06% for grassland. More granularity of this classification can be obtained by using this method. High buildings and low buildings can, for example, be distinguished from the original building class. Road class can also be further classified into roads and crossroads. The comparison of the classification accuracy between this method and the traditional pixel-based method indicates that the total accuracy is improved from 69.12% to 89.40%.     

Multi-UAV coordination control by chaotic grey wolf optimization based distributed MPC with event-triggered strategy

The paper proposes a new swarm intelligence-based distributed Model Predictive Control (MPC) approach for coordination control of multiple Unmanned Aerial Vehicles (UAVs). First, a distributed MPC framework is designed and each member only shares the information with neighbors. The Chaotic Grey Wolf Optimization (CGWO) method is developed on the basis of chaotic initialization and chaotic search to solve the local Finite Horizon Optimal Control Problem (FHOCP). Then, the distributed cost function is designed and integrated into each FHOCP to achieve multi-UAV formation control and trajectory tracking with no-fly zone constraint. Further, an event-triggered strategy is proposed to reduce the computational burden for the distributed MPC approach, which considers the predicted state errors and the convergence of cost function. Simulation results show that the CGWO-based distributed MPC approach is more computationally efficient to achieve multi-UAV coordination control than traditional method.     

Virtual target guidance-based distributed model predictive control for formation control of multiple UAVs

The paper proposes a Virtual Target Guidance (VTG)-based distributed Model Predictive Control (MPC) scheme for formation control of multiple Unmanned Aerial Vehicles (UAVs). First, a framework of distributed MPC scheme is designed in which each UAV only shares the information with its neighbors, and the obtained local Finite-Horizon Optimal Control Problem (FHOCP) can be solved by swarm intelligent optimization algorithm. Then, a VTG approach is developed and integrated into the distributed MPC scheme to achieve trajectory tracking and obstacle avoidance. Further, an event-triggered mechanism is proposed to reduce the computational burden for UAV formation control, which takes into consideration the predictive state errors as well as the convergence of cost function. Numerical simulations show that the proposed VTG-based distributed MPC scheme is more computationally efficient to achieve formation control of multiple UAVs in comparison with the traditional distributed MPC method.     

An adaptive sequential experiment design method for model validation

Efficient experiment design is of great significance for the validation of simulation model with high nonlinearity and large input space. Excessive validation experiment raises the cost while insufficient test increases the risks of accepting an invalid model. In this paper, an adaptive sequential experiment design method combining global exploration criterion and local exploitation criterion is proposed. The exploration criterion utilizes discrepancy metric to improve the space-filling property of the design points while the exploitation criterion employs the leave one out error to discover informative points. To avoid the clustering of samples in the local region, an adaptive weight updating approach is provided to maintain the balance between exploration and exploitation. Besides, the credibility distribution function characterizing the relationship between the input and result credibility is introduced to support the model validation experiment design. Finally, six benchmark problems and an engineering case are applied to examine the performance of the proposed method. The experiments indicate that the proposed method achieves satisfactory performance for function approximation in accuracy and convergence.     

复合材料MMB试件I-II混合型层间裂纹扩展分析

基于经典层合板理论及双线性黏聚区本构关系，建立了含一般分层裂纹层合板的理论模型，对I-Ⅱ混合型弯曲（MMB）断裂试件进行了裂纹扩展理论分析。提出了一种I-Ⅱ混合型断裂叠加模型，引入I型裂纹分量的刚体转动位移，同时考虑了裂纹长度超过试件半长后中部载荷分量对裂纹扩展的闭合效应，并根据黏聚区力学响应，分段获得了位移函数通解。结合叠加模型的边界条件与连续性条件，分析了MMB试件的裂纹扩展过程，求解获得了载荷-位移曲线。通过与梁模型预测以及试验结果进行对比，验证了本文模型对I-Ⅱ混合型裂纹扩展预测的有效性和准确性，并讨论了初始断裂模式混合比及闭合效应对裂纹扩展过程的影响。结果表明：初始Ⅱ型裂纹比重较大时，中部载荷的闭合效应更为明显，可能出现I型裂纹完全闭合的情况；裂纹扩展过程中，当裂纹长度小于试件半长时，断裂混合比基本保持常数；当裂纹扩展超过试件半长后，闭合效应明显，混合裂纹形式逐渐向单一型断裂模式退化。     

复合材料缠绕制品性能测试

本文对复合材料缠绕制品力学性能、耐燃烧性、吸水性、老化性能的测试进行了论述,这些试验方法、标准将为缠绕制品的可靠性的进一步研究奠定实验基础。     

飞机连接结构防护涂层老化损伤量化评估方法

飞机连接结构防护涂层体系的老化过程具有多属性、模糊性和动态性的特点,综合量化评估防护涂层体系老化损伤程度对保障飞机连接结构的功能和使用安全具有重要作用。本文分析了现阶段的涂层老化损伤评级方法,提出了用等级描述老化损伤程度的量化评估技术途径,建立了基于模糊综合评判的量化评估方法。在国标、ISO和ASTM标准给出的单项评级方法的基础上提出了适用于飞机连接结构防护涂层体系老化损伤的单项评级方法,确定了因素集和评价集。采用专家打分法统计得到了各因素的权重分配,确定了权重集。选用正态分布隶属函数来确定评价矩阵,给出了隶属函数参数的计算方法和结果,建立了评价矩阵的确定方法。进行了某型飞机机翼上下表面连接部位模拟试件的加速腐蚀试验,采用本文提出的量化评估方法对防护涂层体系的老化损伤进行了评估,确定了老化损伤等级,评估结果与试验结果相符,与腐蚀动力学规律一致,从而验证了本文提出的方法。