The detection of structural deformation errors in attitude determination

In the determination of the attitude parameters from a multi-antenna GPS array, one of the major assumptions is that the body frame is rigid at all times. If this assumption is not true then the derived attitude parameters will be in error. It is well known that in airborne platforms the wings often experience some displacement during flight, especially during periods of initializing maneouvres, such as taking off, landing,and banking. Often it is at these points in time that it is most critical to have the most precise attitude parameters.There are a number of techniques available for the detection of modeling errors.The CUSUM algorithm has successfully been implemented in the past to detect small persistent changes. In this paper the authors investigate different methods of generating the residuals, to be tested by the CUSUM algorithm, in an effort to determine which technique is best suited for the detection of structural deformation of an airborne platform. The methods investigated include monitoring the mean of the residuals generated from the difference between the known body frame coordinates, and those calculated from the derived attitude parameters. The generated residuals are then passed to a CUSUM algorithm to detect any small persistent changes. An alternative method involves transforming the generated residuals into the frequency domain through the use of the Fast Fourier Transform. The CUSUM algorithm is then used to detect any frequency changes. The final technique investigated involves transforming the generated residuals using the Haar wavelet. The wavelet coefficients are then monitored by the CUSUM algorithm in order to detect any significant change to the rigidity of the body frame.Detecting structural deformation, and quantifying the degree of deformation, during flight will ensure that these effects can be removed from the system, thus ensuring the most precise and reliable attitude parameter solutions. This paper, through a series ofsimulations, will assess the effectiveness of the above mentioned techniques for detecting structural deformation effects on a GPS multi-antenna array. These principles are then tested with experimental data.     

基于RTDX技术的多用户检测实验平台设计

介绍了一种基于RTDX技术的多用户检测试验平台设计方法,同时阐述了如何利用RTDX技术实现多用户检测试验平台设计的具体方法。     

综合孔径微波辐射探测系统仿真平台设计

由于综合孔径微波辐射探测系统在理论分析和大型阵列物理系统构建方面都十分复杂,因而仿真成为十分重要的研究手段。从系统建模、“搭积木”设计、模型/算法库设计、多级仿真设计以及体系架构等方面论述了综合孔径微波辐射探测系统仿真平台的设计,仿真内容涵盖被探测目标、环境、天线阵列、接收机通道和信号处理等。实验结果表明,该平台能正确模拟对远距空中目标的微波辐射探测,可用于综合孔径微波辐射探测理论及系统设计的研究。     

基于不同摄像机配置的空间点检测模型及精度研究

针对空间点检测问题给出了一种简便而精确的空间点检测方法并建立了实验环境下的数学模型,提出了视差为零时,所测得的空间点深度最接近真实值的假设,并得到如下结论：给定空间点,深度不变,基线越短,光轴的夹角越小；深度改变时,基线一定,则深度越长,夹角越小。推导出在不同基线、不同深度下摄像机光轴之间理想夹角的数学模型并通过实验进行了验证。该方法对实际双目检测系统的摄像机配置有一定的指导作用。     

“解方程器”软件包(EQNS-SOLVER)

作者提出了对于任意多项式方程组的一种带有普遍性的求解方法。多项式方程组可能没有解,或者有无穷多个解,或者有有限个解,解是实数也可以是复数。在有限个解的情况下,所创建的方法能够求出所有的解。作者完成了一个软料包,称为《解方程器》,曾在微型计算机上用FORTRAN语言完成计算过程。本文是《解方程器》软料包的说明,内容包括基本原理、方法、程序结构、应用举例以及使用的步骤。     

蓄电池监控模块的可扩充性设计

为使蓄电池监控模块在不断扩充的电源监控系统中能可靠、稳定地运行 ,从硬件和软件两个方面进行了蓄电池监控模块的可扩充性设计 ,其中采用多种网络接口并存的硬件结构和对接收数据的特殊软件处理方法 ,该模块能成功地应用于多个通信局 (站 )的电源监控系统     

G-X5CrNi13.4不锈钢水斗现场检测方法

针对国内水头最高的水电站——西藏羊卓雍湖抽水蓄能电站4^#机水斗断裂事故，开展了在役机组水斗检测方法的研究，对照各种检测方法的差异，找出了最为有效的检测手段。     

基于层次注意力机制的垃圾用户检测模型

目前基于网络的垃圾用户检测方法只考虑了简单社会关系,缺乏对更多复杂社会语义关系的利用,难以达到最优性能.针对这一挑战,提出一种基于层次注意力机制的垃圾用户检测模型(HAM-SD).模型首先使用异质信息网络对社交媒体进行建模,挖掘丰富的语义与结构信息,接着利用节点级注意力层聚合元路径邻居增强节点表示,同时利用自适应层级聚合模块选择不同层级特征提升表征能力,然后通过语义级注意力层融合不同元路径下的节点表示,最后带入分类检测模块实现垃圾用户检测.在公开数据集上的实验结果表明该模型能够有效检测垃圾用户,并在不平衡数据分布时保持较强的稳定性.     

车用电控汽油机实时爆震检测方案的研究

研究一种可以满足准确性,实时性要求的车用电控汽油机爆震检测方案,方法 测量缸盖的振动信号,确定爆震检测频率,运用概率和数理统计的方法。对缸盖振动信号进行分析,找出规律性,在非爆震,严重爆震,爆震时,爆震检测区间内信号峰值都服从对数正态分布。     

超声心动图象内外膜的自动检测与测量

为定量计算一些重要的心脏功能数据,提高心脏病的诊断水平,研究了超声心动图象内外膜的自动检测与测量技术．首先对超声心动图象进行滤波以消除图象中的噪声,并运用模糊数学理论进行模糊边缘增强,提取超声心动图象的内外膜边缘信息;接着对超声心动图象作二值化处理和椭圆曲线拟合,初步得到心脏的内外膜边缘;再采用相应的三次样条插值和平滑技术,得到光滑、连续的心脏内外膜边缘．在此基础上,再对心脏进行节段划分,并计算有关的心脏功能数据．经实验证实,用此方法可快速得到较准确的结果．