平面弹性连杆机构的KED分析

本文放弃了文献中引用的运动学假设和瞬时结构假定,考虑了刚体运动和弹性变形运动之间的耦合项,分析了梁的横向位移对轴向应变的影响。利用虚位移原理和达明贝尔原理,建立了构件和系统的运动微分方程式。以四杆较接机构为例,进行了KED分析。从所得结果可以看出,本文更好地反映出弹性对机构动态误差的影响。     

数学规划模型的建模语言（FQL）

对数学规划模型的结构作了深入分析。从纵向揭示了数学规划模型自然、清晰的层次结构；横向又把复合模型分解成若干基本模型，而基本模型又可由决策用户十分熟悉的二维形式加以描述。在此基础上，给出了建模语言（ＦＱＬ）的语法和语义。它除了具有建模能力外，消除了代数形式的索引；更重要的是具有数据库查询和模型操作能力。     

Minkowski时空中的四维力

Ｍｉｎｋｏｗｓｋｉ时空中的四维力刘泽文（物理系）关键词：相对论／类时；类空；类光；四维力分类号：Ｏ４１２在Ｍｉｎｋｏｗｓｋｉ时空中，诸如四维电流密度Ｊ￣μ、粒子的四维加速度ω￣μ＝ｄＵ￣μ／ｄτ以及四维波矢Ｋ￣μ等向量，其类时、类空以及类光性质一般是...     

Poisson单和—类广义Poisson单的刻划

讨论了Ｐｏｉｓｓｏｎ单和一类广义Ｐｏｉｓｓｏｎ单的基本刻划问题。     

铝合金变形抗力的实验研究

采用恒应变速率凸轮式形变压缩试验机试验了四种铝合金材料的变形抗力 ,分析了应变率和应变速率对变形抗力的影响 ,结果表明随应变的增加 ,变形抗力以近似幂函数关系增加 ,在此基础上建立了简单、适用的变形抗力计算模型     

基于B/S模式的年度考核管理系统的设计与实现

本文阐述了新疆师范大学年度考核管理系统的功能、设计与实现。     

基于Pro/E 的机翼型风机叶片的建模及平面展开

基于先进的3D设计软件Pro/Engineer，模拟离心式风机叶片的成形理论及构形特点，将风机叶片的建模、运算、绘图、下料全部由计算机完成，直接输出精确的下料图纸，大大简化了设计过程，并且提高了设计精度。     

加强民间组织能力建设的有效途径

伴随着中国社会改革进程,民间组织发展迅速,并在经济建设和社会进步中发挥着越来越广泛的积极作用。但民间组织的整体素质和自律水平有待进一步提高,如何加强民间组织的能力建设,作者提出了中国民间组织能力建设的五方面的有效途径,供社会各界关心民间组织发展的人士共同探讨。     

B/S三层体系结构模式

随着WEB技术的迅速发展和应用,如何利用WEB技术,建立集主机-终端方式和C/S方式优点为一体的新的应用模式是计算模式研究的一个新课题.论及了Internet/Intranet环境下,B/S三层体系结构模式的构成、工作原理,从多方面对比分析了B/S与C/S模式的优劣,认为B/S模式是当今应用软件的首选体系结构.     

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.