各向异性板料成形极限面的研究

成形极限曲线(FLD)是表示板料成形性能的重要指标。由于板料各向异性的存在,导致了使用1条FLD来表示板料整个面内的成形极限存在很大误差。通过试验分析了板料面内的各向异性对板料应力和应变成形极限曲线的影响,研究了利用三维空间的成形极限曲面代替二维坐标下的FLD来表示材料整个面内的成形极限的方法,经过分析认为板料成形极限面可以为板料成形有限元仿真提供更准确的成形极限判据。     

膨胀剂对混凝土变形性能的影响

膨胀剂在我国被广泛地应用于补偿大体积混凝土收缩。不同品种的膨胀剂对混凝土的补偿收缩效果有所不同。氧化钙类和硫铝酸钙类(AF t)可补偿混凝土的早期收缩,但分别在28和60 d后仍会出现后期收缩现象。水泥品种、养护条件对膨胀剂的膨胀效果有不同的影响。掺氧化镁类膨胀剂的混凝土没有出现后期收缩现象,比较适合水工大体积混凝土。在做好基础混凝土温度控制的同时,选择适宜品种的膨胀剂,可有效地控制混凝土的变形,减少收缩开裂,提高混凝土的结构耐久性能和建筑物的质量。     

基于机体振动的直升机桨毂阻尼故障诊断

研究了仅用机体振动信号诊断旋翼减摆器阻尼失效、轴向铰卡涩和水平铰卡涩3种桨毂阻尼故障的可行性。在旋翼试验台上分别设置上述3种阻尼故障,测取机体振动响应,利用快速傅立叶变换分析其频谱特征。分析表明,3种阻尼故障引起的机体振动谱图互不相同。采用概率神经网络实现了3种阻尼故障的正确分类。研究表明,仅用机体振动响应实现旋翼阻尼故障诊断是可行的。     

模拟三维重力波传播过程的并行数值模式

从三维大气运动的基本控制方程出发, 基于MPI消息传递接口和区域分解的思想, 建立了模拟三维可压缩大气中重力波传播过程的并行数值模式. 在对垂直方向进行区域分解的基础上, 针对跳点网格的特点, 以垂直速度主格点线为子区域的下边界, 状态变量主格点线为子区域的上边界进行区域分解. 利用MPI消息传递接口来传递计算各子区域中变量时所要用到的相邻子区域上相应变量, 从而顺利地完成对整个计算域的并行计算. 根据线性重力波理论, 通过模拟小振幅重力波的传播过程对所建模式进行了验证. 结果表明, 模式可以很好地模拟小振幅重力波在三维空间中的传播过程, 模拟的重力波振幅随着传播高度的增加以指数形式增长, 对能量传播路径以及有效扰动位能和扰动动能的模拟结果均与理论预测的结果吻合很好. 另外, 随着进程个数的增加, 完成相同的计算量所用的计算时间也显著减少. 这表明本文建立的并行数值模式不但能够很好的模拟重力波的传播过程, 而且能够有效地节约计算时间.     

用液相电导法研究氧化镁的水化活性

为了了解MgO在大体积混凝土中的补偿效果,采用液相电导法研究了MgO的水化活性, 结果表明:氧化镁水化活性与煅烧温度、粒径大小和养护温度有关.煅烧温度升高,MgO的晶格畸变逐渐变小,电导率下降,活性减少;颗粒尺寸减少,MgO与水接触面积增大,电导率增长,反应活性加快;养护温度升高,电导率增加,反应活性大幅度增加.     

粒子激发X射线谱仪的热设计和热仿真计算

粒子激发X射线谱仪(APXS)安装在月面巡视器外部,利用巡视器的机动性和机械臂的灵活性,可以对月面有研究价值的月岩及月壤进行有针对性的探测.由于裸露在巡视器外部,月球复杂外热流会对APXS产生较大影响.鉴于此,需对APXS进行合理的热设计,以保证APXS的探测器和电子学器件工作在允许的温度范围内.提出了APXS的热设计方案,据此对APXS进行热仿真计算,计算结果得到了相应热平衡试验的较好验证.     

基于AMS-01实验估算羊八井处原初宇宙线的流强和能谱

利用Alpha Magnetic Spectrometer(AMS)实验对近地空间不同地磁纬度处不同能量原初宇宙线微分能谱的观测,通过积分近似计算和拟合方法,研究得出西藏羊八井地磁纬度处原初宇宙线质子动能在0.44～4.31GeV,4.31～12.38GeV,12.38～199.06GeV区间内的积分流强与拟合能谱函数以及原初宇宙线氦核在刚度区间6.92～14.45GV,14.45～229.9GV的积分流强与拟合能谱函数,为近一步进行羊八井处本底宇宙线流强估算奠定了基础.     

激光绝对测距中相位信号的数字处理方法综述

随着工业4. 0时代的来临,精密测量的技术发展变得越来越重要。绝对距离测量作为精密测量的一个重要组成部分,其测量精度离不开对信号相位信息的分析,而相位信息一般可以通过数字处理方法来获得。本文介绍了激光绝对距离测量中涉及到的相位信号数字处理方法的相关原理及应用。     

Chang'E-1 Lunar Mission:An Overview and Primary Science Results

Chang'E-1 is the first lunar mission in China, which was successfully launched on Oct. 24th, 2007. It was guided to crash on the Moon on March 1, 2009, at 52.36ºE, 1.50ºS, in the north of Mare Fecunditatis. The total mission lasted 495 days, exceeding the designed life-span about four months. 1.37 Terabytes raw data was received from Chang'E-1. It was then processed into 4 Terabytes science data at different levels. A series of science results have been achieved by analyzing and applicating these data, especially "global image of the Moon of China's first lunar exploration mission'. Four scientific goals of Chang'E-1 have been achieved. It provides abundant materials for the research of lunar sciences and cosmochemistry. Meanwhile these results will serve for China's future lunar missions.     

A variational Bayesian-based robust adaptive filtering for precise point positioning using undifferenced and uncombined observations

In the application of precise point positioning (PPP), especially in the dynamic mode, the classical Kalman filter (KF) usually produces a large number of estimation errors or diverges when there are gross errors in the observation data or unexpected turbulences occur in target motion state or both of them. For such problem, a variational Bayesian (VB)-based robust adaptive Kalman filtering (VB-RAKF) is proposed in this paper. This filter introduces a classification robust equivalent weight function to resist observation gross error and the inverse Wishart prior to model inaccurate process noise covariance matrix (PNCM). To improve the instantaneous accuracy of state estimation, the VB approach is used to obtain better estimations of inaccurate PNCM. Several sets of observation data collected by IGS reference stations and vehicles are employed to check the robustness and positioning accuracy of the VB-RAKF model. The results show that the VB-RAKF algorithm is more robust than the KF, and can effectively resist the gross error in observation data and control state disturbance. In the IGS reference station tests, when compared to the KF, the static positioning accuracies of the VB-RAKF in the north, east and up directions are improved by 13%, 8% and 22%, respectively, and the simulated dynamic positioning accuracies of the VB-RAKF in the north, east and up directions are improved by 19%, 9% and 21%, respectively. The in-vehicle dynamic test verifies that the VB-RAKF outperforms the KF, and shows that the VB-RAKF has better performance than the KF when dealing with observation data which has obvious gross errors, and similar performance as the KF when gross errors are small.