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.     

徐变对钢管混凝土偏心受压构件挠度的影响分析

在分析钢管混凝土偏心受压构件的徐变分析的基础上,进一步考虑徐变对偏心受压构件挠度的影响进行了分析,构造了一个计算在徐变过程中,钢管混凝土偏心受压构件挠度的计算公式.应用这个方法计算受徐变影响的构件挠度,得出了一些有价值的结论.     

火力发电厂高温过热器爆管分析

针对广州发电厂3号锅炉高温过热器发生爆管的情况，通过化学成分分析、力学性能试验和金相检验，认定原管子材质符合设计要求。在金相检验中，发现爆管处存在大量蠕变孔洞及裂纹，从而判定此次爆管是在高温和外弧切向最大拉应力作用下引起的蠕变脆性断裂造成的。     

黄土滑坡形变分析预报方法研究

基于黄土滑坡的变形特征和演化规律，利用滑体总形变量与滑坡演变过程形变量之间的逼近关系，建立了一种简单，实用的滑坡预报数学模型，其效果良好，为黄土滑坡时间预报由定性分析向定量评价提供了途径。     

弹性梁大挠度问题的纵横弯曲法

将纵横弯曲的梁柱在原基准坐标系中的大变形问题转换到某一局部坐标系中，近似以小变形问题处理，建立起一组“三弯矩方程”组，使问题求解。通过算例，验证了本方法的正确性。     

关于用奇异函数求解阶梯形梁变形的两个问题

对于n段阶梯形梁,X_o=0,X_1,X_2,……,X_(n-1)为第一、第二、……、第n段梁左截面的坐标,J_1,J_2,.....,J_n为相应段梁的惯性矩。根据,先将梁惯性矩的倒数用阶梯函数表示:其中此时,梁的挠曲线微分方程为其中E为材料的弹性模量;M(X)为梁的弯矩,由奇异函数法求出。依据奇异函数的积分规则,由(3)式可分别得到梁的转角方程和挠度方程:     

连铸坯鼓肚变形的粘弹性分析

本文以发生柱型弯曲的粘弹性簿板为模型,应用Maxwell定律,分析并计算了连铸板坯的鼓肚变形及应力。     

简支阶梯轴弯曲变形的傅里叶级数近似计算

利用广义函数和傅里叶正弦级数来求解简支阶梯轴的挠曲线四阶近似微分方程，推得简支阶梯轴的挠曲线近似方程，进而可以近似计算出其任一截面处的弯曲变形。     

LW-13/22型压缩机三级活塞的三维有限元分析

通过对实际工况下LW-13／22型压缩机三级活塞的受力分析,建立了有限元分析模型,对整个载荷循环过程进行应力和变形分析,并由此得到了LW-13/22型压缩机三级活塞在实际工况时的应力分布特点及变形规律,求得了活塞最大应力位置和最大应力时的主轴转角。     

ANSYS在钢筋混凝土梁有限元中的应用

文章结合钢筋混凝土材料的特殊性,利用大型有限元计算软件ANSYS计算受弯构件梁的变形及其正截面应力应变。最后将有限元计算的结果(裂缝开展深度、钢筋应力、混凝土应力)与精确解比较,分析误差存在的原因及改进的方法和措施。