基于FLAC3D桩-锚支护结构参数敏感性分析

该文以锦州石化公司新建柴油罐基坑工程为研究对象，利用大型有限差分软件FLAC3D对影响基坑开挖的桩锚支护结构敏感性参数进行了数值仿真分析，得出了桩锚支护敏感性参数对基坑变形的影响规律，并对重要参数进行了讨论，为今后类似工程提供了参考。     

中低纬度下惯导极区性能模拟测试方法

针对惯性导航系统极区性能试验难以实地开展的问题, 研究了一种模拟测试的方法, 并基于横向坐标系编排给出了以组合导航系统作为测量基准的惯导模拟测试方案。首先分析了模拟测试技术研究的必要性, 然后根据轨迹形变最小原则详细推导了基于横向坐标系编排的极区模拟测试转换公式, 之后针对测试中采用不同基准的情况, 提出了相应的惯性测量单元(inertial measurement unit, IMU)转换算法, 并提出以惯性导航系统/全球导航卫星系统(inertial navigation system/global navigation satellite system, INS/GNSS)为参照基准的一种具体测试方案, 最终完成了仿真实验, 验证了模拟测试理论的正确性。结果表明, 在基准误差不计的情形下，试验导航参数误差与惯导实地横向编排解算误差相当。初步验证了所提方法替代极区实地试验进行精度性能评估的可行性, 为后续极区模拟测试评估研究奠了定理论基础。     

基于改进四元数阻尼误差模型的SINS初始对准算法

针对传统捷联惯导系统(strapdown inertial navigation system, SINS)四元数非线性误差模型存在坐标系不一致的问题, 对姿态误差模型和速度误差模型进行改进, 将误差矢量统一投影至计算导航坐标系下。此外, 引入全球定位系统阻尼信息, 在阻尼SINS解算基础上, 结合四元数无迹估计器提出了一种改进四元数阻尼误差模型对准算法, 可应用于系泊状态下的SINS初始对准。仿真和车载试验结果表明, 在不同的大失准角下, 该改进算法相比传统四元数阻尼误差模型对准算法和欧拉角阻尼误差模型对准算法, 具有更好的对准精度、收敛速度以及稳定性。     

海堤非稳定渗流场渗透参数反演分析

针对受到快速涨落潮位作用的海堤进行非稳定渗流有限元分析,在此基础上结合实测渗压序列构建目标函数对海堤的渗透参数进行反演研究.反演中采用分层搜索技术,先由逐步扫描法确定出渗透参数一个合理的小区间,再用一阶梯度优化方法在该小区间上进行迭代优化以获得合适的渗透参数.以反演得到的渗透参数进行海堤非稳定渗流数值模拟,算例表明,计算及反演步骤合理可行,模拟计算得到的渗压结果与实测序列在数值和动态变化规律上都取得了理想的拟合效果.     

New rapid transfer alignment method for SINS of airborne weapon systems

Transfer alignment is an effective alignment method for the strapdown inertial navigation system （SINS） of airborne weapon systems. The traditional transfer alignment methods for large misalignment angles alignment use nonlinear transfer align- ment models and incorporate nonlinear filtering. A rapid transfer alignment method with linear models and linear filtering for ar- bitrary misalignment angles is presented. Through the attitude quaternion decomposition, the purpose of transfer alignment is converted to estimate a constant quaternion. Employing special manipulations on measurement equation, velocity and attitude linear measurement equations are derived. Then the linear trans- fer alignment model for arbitrary misalignment angles is built. An adaptive Kalman filter is developed to handle modeling errors of the measurement noise statistics. Simulation results show feasibili- ty and effectiveness of the proposed method, which provides an alternative rapid transfer alignment method for airborne weapons.     

具有漂移特征的退化可靠性评估方法研究

针对具有参数漂移特征的产品， 首先采用随机扩散理论描述其参数漂移规律， 并建立了参数漂移模型. 在此基础上， 提出了基于参数漂移特征的退化补充样本容量的确定方法， 建立了基于退化观测数据和补充样本数据的产品退化可靠性评估模型. 最后， 通过对某传感器电压数据进行处理， 说明了该方法得到的可靠性估计结果具有较好的精度和稳健性， 与工程实际相符.     

铁磁性金属Co的合成及形貌控制

通过简单的水热法成功合成了不同维度、不同形貌的金属Co单质,如六角片状、柱状、杨桃状等结构。前驱体混合溶液中乙二胺的剂量可以调节反应体系pH值的反应速度。-NH2可以选择性的吸附在不同的晶面上以改变其晶面的生长速率,合成出不同维度的单质Co磁性纳米材料。在溶液中加入了不同量的十二烷基磺酸钠表面活性剂,改变不同晶面的表面能,在一定程度上改变晶体的生长方式,最终合成出了不同形貌的单质Co颗粒。通过对不同形貌的颗粒进行磁学参数的检测,可知室温下二维片状Co的饱和磁化强度远小于柱状,而矫顽力有较大的提高,同时,表面粗糙的样品具有较大饱和磁化强度和较小矫顽力。     

Self-alignment of full skewed RSINS：observability analysis and full-observable Kalman filter

Traditional orthogonal strapdown inertial navigation sys-tem （SINS） cannot achieve satisfactory self-alignment accuracy in the stationary base： taking more than 5 minutes and al the iner-tial sensors biases cannot get ful observability except the up-axis accelerometer. However, the ful skewed redundant SINS （RSINS） can not only enhance the reliability of the system, but also improve the accuracy of the system, such as the initial alignment. Firstly, the observability of the system state includes attitude errors and al the inertial sensors biases are analyzed with the global perspective method： any three gyroscopes and three accelerometers can be assembled into an independent subordinate SINS （sub-SINS）;the system state can be uniquely confirmed by the coupling connec-tions of al the sub-SINSs;the attitude errors and random constant biases of al the inertial sensors are observable. However, the ran-dom noises of the inertial sensors are not taken into account in the above analyzing process. Secondly, the ful-observable Kalman filter which can be applied to the actual RSINS containing random noises is established; the system state includes the position, ve-locity, attitude errors of al the sub-SINSs and the random constant biases of the redundant inertial sensors. At last, the initial self-alignment process of a typical four-redundancy ful skewed RSINS is simulated： the horizontal attitudes （pitch, rol ） errors and yaw error can be exactly evaluated within 80 s and 100 s respectively, while the random constant biases of gyroscopes and accelero-meters can be precisely evaluated within 120 s. For the ful skewed RSINS, the self-alignment accuracy is greatly improved, mean-while the self-alignment time is widely shortened.     

Long Memory of Financial Time Series and Hidden Markov Models with Time‐Varying Parameters

Hidden Markov models are often used to model daily returns and to infer the hidden state of financial markets. Previous studies have found that the estimated models change over time, but the implications of the time‐varying behavior have not been thoroughly examined. This paper presents an adaptive estimation approach that allows for the parameters of the estimated models to be time varying. It is shown that a two‐state Gaussian hidden Markov model with time‐varying parameters is able to reproduce the long memory of squared daily returns that was previously believed to be the most difficult fact to reproduce with a hidden Markov model. Capturing the time‐varying behavior of the parameters also leads to improved one‐step density forecasts. Finally, it is shown that the forecasting performance of the estimated models can be further improved using local smoothing to forecast the parameter variations. Copyright © 2016 John Wiley & Sons, Ltd.     

Mapinfo数据的坐标转换方法研究

本文根据三种方式深入探讨了带属性的MapInfo数据的坐标转换方法：一种通过VC和MapX编程调入“.tab”文件,实现WINDOWS窗口界面化的输入和显示方式,通过输入七参数或四参数,快速实现了坐标系之间的一系列转换;一种通过AutoCAD Map 3D软-导入和导出“.tab”文件,利用平移、旋转、缩放命令实现四参数转换;一种在.prj文件中定义坐标系,通过改变投影来进行转换.这三种方式最终都以WGS-84坐标转换为BJ54坐标为例子进行了验证,取得良好结果.