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.     

小波多尺度分解及其在SAR图象目标检测中的应用

合成孔径雷达图象的目标检测是最重要的任务之一.目前用于目标检测的现有方法速度较慢、准确率较低、精度较差.作者提出小波分解的方法用于目标检测.同尺度目标检测采用二维离散二进小波分解方法,提高检测速度.不同尺度的目标检测采用多尺度二维离散小波分解方法,提高检测准确率.图象匹配采用灰度归一化的灰度相关匹配方法,提高匹配精度.实验证明,采用该法进行目标检测能获得较好的效果.     

基于数学形态学多级平均的图像边缘检测

提出了一种基于多级平均的数学形态学图像边缘检测方法，分析了图像边缘提取的特点．与其它形态学边缘检测方法进行了比较知，该方法在保持良好边缘的同时，提高了抗噪能力．     

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。     

GOSCA－CFAR检测器在干扰边缘中的性能分析

本文研究ＧＯＳＣＡ—ＣＦＡＲ检测器￣［１，２］干扰边缘中的性能。文中推导出了它的干扰边缘环境中虚警概率的解析表达式，分析了它抗边缘干扰的性能，并且与ＯＳ、ＣＡ、ＧＯ和ＳＯ等检测器进行了比较。结果表明，ＧＯＳＣＡ的抗干扰边缘性能比ＣＡ和Ｋ＿（ｏｓ）＝（ｋ＋ｌ）＿（ＧＯＳＣＡ）和ＯＳ相近，比抗边缘干扰性能较好的ＧＯ要差。     

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。