含参数λ微分方程类型的可积判据

提出几类含参数λ微分方程,借助变量替换法、线性化法、降阶法、交换变量位置法,论证其可积性,给出可积的判据及通解的表达式.扩大微分方程的可积范围,提供其求解的方法及通解公式.     

基于改进 HAF的线性调频雷达信号参数估计

针对多项式相位信号(PPS)中的线性调频(LFM)雷达信号参数估计,通过提出频谱方差极大值准则对PPS次优参数估计方法高阶模糊度函数(HAF)进行了改进,提出了适于单分量LFM参数估计的改进HAF。首先讨论了HAF对LFM参数的估计方法及其局限性,然后提出了分段频谱方差极大值法则下LFM调频斜率估计的方法,将其与HAF相结合提出了单分量LFM参数估计的改进HAF,克服了接收信号与实际信号起点不一致性对HAF带来的影响,降低了由于HAF局限性带来的调频斜率估计误差,改善了HAF的累积误差效应。MATLAB仿真验证了改进方法较HAF的优越性。     

南淝河水质S-P模型参数K1、K2的估值

对南淝河河流水质S-P模型中碳化BOD衰减系数K1和大气复氧系数K2分段进行了估值.根据实验测定数据,用最小二乘法、图解法和两点法等3种方法对K1进行了估值,应用公式估算法对K2进行了估值,并对估值的结果与南淝河的有机污染状况进行了对比和分析,从而为模型提供准确的参数值,也为南淝河的水污染控制和水质规划提供有益的借鉴.     

复杂背景下低信噪比点目标的实时检测算法及实现

为检测复杂背景中的低信噪比 (SNR)点目标 ,提出了一种局部自适应门限检测算法。该算法以低通滤波算法估计背景中的低频成分 ,及图像局部方差估计背景起伏 ,来计算出局部自适应的目标检测判决门限。该算法充分考虑了可实现性和实时性并采用现场可编程门阵列 (FPGA)设计实现该算法。理论分析和试验结果都表明 ,该算法可有效抑制云层、树木、地物等背景杂波、检测出复杂背景下的低信噪比点目标 ,具有恒虚警率和易于工程实现的优点。     

热轧圆钢外径的激光在线检测研讨

本文报导热轧圆钢激光在线检测外径的阶段性研究结果，给出仪器研制原理及光机结构设计同仪器精度关系的研讨．     

条纹动感投影片中条纹参数变化规律的实验研究

本文提出、论述和验证了条纹参数的变化规律,介绍了微机辅助验证的方法,找到了选择条纹参数的捷径和参数取值范围.     

双脉冲TEA CO_2激光器电路参数的选择

分析了电路参数及电路结构对双脉冲TEA CO_2激光器输出稳定性的影响,并提出合理选择电路参数与结构的原则。实验结果,证实了分析的正确性。     

一种基于数字水印的错误检测和定位技术

为了增强视频通信系统在有误码信道的适应能力 ,提出了一种基于数字水印技术的错误检测方法 ,使得解码器可以对误码块进行有效的补偿。其原理为编码器在量化后离散余弦变换 (DCT)系数中嵌入易碎的数字水印 ,解码器可以通过提取水印从而确认错误以及错误发生的首宏块位置。仿真结果证明 :在信道误码率为 5× 10 - 4时 ,与常用的基于语法的方法相比 ,本方法的错误检测率是其的 1.32～ 1.82倍 ,错误正确定位率是其的 2 .95～ 5 .32倍 ,而且 PSNR只有微弱降低 ,同时算法复杂度很低     

EBJ-120TP型掘进机的技术特点

介绍了EBJ-120TP型掘进机的主要技术参数、结构及其技术特点。     

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.