线性驱动下一级相变的重正化群理论

把重正化群理论应用于一受外场驱动而发生一级相变的系统中，结果表明，与有序化过程一样，该系统也由零温不动点所决定，并得到磁化强度及结构函数的新的动力学标度关系．由此可获得滞后回约面积与变场速率的标度关系．     

一种减小反射式0－π调相器尺寸的新方法

在微波频率低端，按常规方法研制的调相器尺寸是大的，该文采用金属化孔和改变调整元件，结果证明，在不降低性能指标的情况下，可以减小调相器的尺寸。     

差分方程非振动的充要条件

本文运用拉普拉斯变换证明了一类常系数线性差分方程有最终无界正解当且仅当相应的齐线性差分方程的特征方程有正解。     

HoBa2Cu3Ox的超导电性

通过交流磁化率和X-ray衍射分析，对用固态反应法制备的HoBa2Cu3Ox超导体的超导电性进行了研究．实验结果表明：随淬火温度的升高．由正交相(123相)向介于正交和四方相之间的过渡相变化；超导转变温度Tc(0)(零场下)从90K降到38．5K；交流磁化率虚部峰值温Tp(H)随附加直流磁场的增加而降低，Tp与Hdc之间的关系偏离[1一Tp(H)／丁(0)]∞H^2/3规律．     

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     

氮－烃类二元低温混合工质的工作机理分析

用ＰＲ方程计算氮－烃类二元混合物的自由焓，提出判别氨－烃类二元混合物互溶性的方法，并计算了该类混合工质的汽液平衡、液液平衡和汽液液平衡特性，为寻求新的混合工质对提供了一种有效的理论预测方法。     

层流液柱吸收法测定气体在液相中的扩散系数

采用射流吸收的简捷方法，通过测定由Ｓｈｏｕｔｈｗｅｌｌ型孔板所产生的截面速度均匀的层流喷射液柱所吸收的气体量，由渗透理论所导出的模型，可计算出一定温度、压力下的微溶气体在液相中的分子扩散系数Ｄ。在温度为３０～４５℃的范围，测试结果与文献值吻合良好．     

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.     

GLOBAL ASYMPTOTIC STABILITY IN N-SPECIES COOPERATIVE SYSTEM WITH TIME DELAYS

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