基于颜色矢量角的彩色图像检索算法研究

通过分析利用颜色直方图进行图像检索时存在的问题,提出了一种基于图像边缘空间分布特征的图像检索算法。即利用颜色矢量角对亮度不敏感,对色度和饱和度敏感的特性来提取图像的边缘信息。在图像的边缘空间,提取图像边缘点的颜色矢量角直方图,以此来描述图像的内容。该算法充分利用了图像的颜色信息、边缘信息及形状信息,实验表明该算法具有较好的光照不变性、尺度不变性、平移不变性和旋转不变性。     

多振子声子晶体的低频特性研究

本文设计了一种由硅橡胶包覆层包裹4个钨振子的新型声子晶体结构,通过有限元法计算该结构的色散曲线、振动模态和传输损失谱。结果表明,该结构的带隙范围为18.85~225.28 Hz,与传输损失谱频率衰减范围相吻合,能够有效抑制20~200 Hz的弹性波在声子晶体中传播。通过分析色散曲线上点的振动模态,说明带隙产生的原因。本文讨论了声子晶体板的缺口角度和振子之间的纵向和横向间距对带隙的影响,结果表明:当缺口角度减小时,带隙下边界几乎保持不变,带隙上边界升高从而增加了带隙的宽度;振子之间横向或纵向间距增大时,带隙下边界和上边界均上升,带隙变宽,进而优化了声子晶体模型的带隙。同时声子晶体板的缺口设计能够节省材料,从而减轻结构的质量。     

动态雷达目标仿真中目标姿态角的计算

为了对动态雷达目标建立合适的数学模型,逼真地复现目标的运动特性和回波特性,从而实现动目标仿真,提出了利用野外真实试验中实际测得的目标RCS数据建立动目标仿真模型,实现动态雷达目标仿真的一种新方法.文章首先探讨了采用该方法对动态雷达目标RCS仿真的具体步骤,然后对实现仿真的一项关键技术--运动目标姿态角的求解进行了公式推导,并列举了应用实例,为进行良好的动态雷达目标仿真提出了一个新思路.要实现仿真还需要做许多工作,如对动态目标RCS起伏规律进行分析,计算统计参数,应用常见RCS起伏模型对目标动态RCS统计分布进行拟合等.     

叶片扩压器进口安装角对离心压缩机性能影响的数值与实验研究

对不同扩压器进口安装角下离心压缩机的性能进行了实验研究,并详细计算分析了相应的流场分布。分析表明, 不同的进口安装角对压缩机的流动有较大的影响,压缩机的性能曲线也有不同程度的左右偏移;进口处较大的正冲角和负冲角均会在扩压器叶片表面出现大尺度的分离涡团;在给定的流量工况下,应存在一个最佳的进口安装角,使得扩压器效率最高;设计工况下,最高效率所对应的冲角并非为零。     

基于特征圆单目视觉的飞机舵面角位移标定技术

提出了一种基于特征圆单目视觉的非接触式飞机舵面角位移标定技术。用一台数码摄像机对固定在飞机舵面上的特征圆进行拍照,经数字图像处理后确定五个特征点的坐标,利用针孔成像和射影变换原理建立物像空间坐标解算模型,计算出特征圆的法线相对方向和圆心的相对位置,舵面角位移由该圆的法线方向确定。仿真结果表明,该方法具有标定过程简单、实时、快速和准确的特点,标定精度可达到0.1°。该技术也可用于航天器上实时测量交会对接时的相对位姿参数。     

利用菌紫质薄膜进行角度复用和偏振复用全息存储实验研究

全息光存储以其高密度、大容量、高速并行数据存取而成为光存储领域的一个重要研究方向。生物光致变色材料———菌紫质是一种新型可擦重写全息记录介质。实验证明了使用菌紫质薄膜进行角度复用和偏振复用全息存储的可行性。利用菌紫质的光致变色特性,采用90°角度复用全息存储光路,在BR-D96N薄膜样品同一位置上实现了6幅全息图存储,并分别读出了无串扰的再现像。利用菌紫质薄膜的光致各向异性进行了偏振复用全息存储,在BR-D96N薄膜样品的同一位置上存储了两幅正交偏振光记录的图像,用原参考光再现和偏振片选择,可分别读出这两幅图像。     

一种新型对称分束偏光棱镜的设计

为了提高偏光棱镜出射光束的对称性,在Wallaston棱镜的基础上,对出射光端面倾斜适当的角度,在结构角一定的情况下,即可以保证分束角相对入射光方向的对称性。以589.3nm钠黄光为例,给出了出射光端面倾角,棱镜结构角和分束角之间的关系式,并分析了分束角随出射光端面倾角的变化趋势,同时提出了两种相关设计方案。测试结果表明,两出射光束的对称性相当好,理论值与实验值几乎完全吻合,表明该棱镜确是一种较理想的对称分束偏光器件。     

Wide viewing optically clear adhesives using PMMA/TiO2 core-shell micro/nanoparticles

Abstract

Optically clear adhesives (OCAs) are widely used in optoelectronic displays because of their high outdoor visibility. Here, we develop new transparent adhesive films with wide-viewing-angle characteristics using poly(methyl methacrylate) (PMMA)/TiO₂ core–shell micro/nanoparticles. TiO₂ nanoparticles are embedded in the shell of PMMA microparticles, forming an organic–inorganic hybrid structure. To examine the optical transmittance of the films in the visible wavelength region, ultraviolet-visible spectroscopy is performed and light diffusion is evaluated. The TiO₂ nanoparticles in the shell of the PMMA microparticles exhibit improved light scattering, and the new functional OCAs are expected to provide wide-viewing-angle characteristics for future flexible displays.     

Aeroelastic analysis of swept pre-twisted wings

In this paper, aeroelastic modeling of aircraft wings with variations in sweep angle, taper ratio, and variable pre-twist angle along the span is considered. The wing structure is modeled as a classical beam with torsion and bending flexibility. The governing equations are derived based on Hamilton’s principle. Moreover, Peters’ finite state aerodynamic model which is modified to take into account the effects of the wing finite-span, the wing sweep angle, and the wing pre-twist angle, is used to simulate the aerodynamic loads on the wing. The coupled partially differential equations are discretized to a set of ordinary differential equations using Galerkin’s approach. By solving these equations the aeroelastic instability conditions are derived. The results are compared with some experimental and analytical results of previous published papers and good agreement is attained. Effects of the wing sweep angle, taper ratio, bending to torsional rigidity, and pre-twist angle on the flutter boundary in several cases are studied. Results show that these geometrical and physical parameters have considerable effects on the wing flutter boundary.     

Wettability and surface energy of parylene F deposited on PDMS

For the first time, the wettability and surface energy of parylene F were investigated. The results showed that parylene F had a hydrophobic surface with an eigen water contact angle of 104.7 ± 0.6°. We found that 3.5 μl probe liquid was an optimal value for the contact angle measurement of parylene F. Moreover, we found that the Lifshitz–van der Waals/acid–base approach was unsuitable for determining the surface energy of parylene F, whereas the Owens–Wendt–Kaelble approach and the limitless liquid–solid interface wetting system were compatible. The surface energy of parylene F was estimated to be 27.06 mJ/m² (Owens–Wendt–Kaelble) and 40.41 mJ/m² (Limitless liquid-solid interface wetting system). Furthermore, this investigation also provided a reference for the applications of empirical and physics-based semi-empirical approaches for the estimation of surface energy.