曲面薄壳有限元离散误差分析和修正方法研究

基于曲面薄壳几何/物理方程和有限元离散原理推导,揭示了壳单元离散方法特点、刚度矩阵误差产生机理和范数表示方法。以航空涡轮发动机测压探针为例,深入研究了利用协调平板壳单元、非协调平板壳单元、一次和二次实体退化壳单元等不同类型单元离散曲面薄壳时,应力计算误差影响因素及变化规律,综述了单元的适用条件。基于Boltzmann模型提出了应力计算结果修正通式,通过FORTRAN语言编程修正应力仿真结果和ANSYS二次开发语言APDL命令实现应力修正结果的读取和后处理,应力修正结果与理论解相对误差小于5%,满足曲面薄壳设计和稳定性分析应用要求。

Abstract：

Based on the geometric physical equations and deduction of discrete process of finite element for curved thin-walled structure,characteristics of shell elements for discretion and discrete error for element stiffness matrix were analyzed theoretically,and the norm expression of discrete error for element stiffness matrix was put forward.Then,as an illustration,a probe for detecting the pressure inside turboprops was meshed by curved thin-walled shell element,compatible flat shell element,incompatible flat shell element and 3D degenerated shell element,respectively,and the stress of the probe was numerically calculated by FEM.On the basis of solved results,the stress error was analyzed thoroughly,the influence factors on the error and the applying situations for different elements were determined.Finally,the general form of correctional function was put forward according to the Boltzmann model.The program developed with FORTRAN was used to correct the numerical results and the APDL commands inside ANSYS software were utilized to read and plot the correctional stress results.Through the correction,the discrete error can be reduced within 5% that satisfies the requirement of application for structural design and stability analysis.     

基于IMU/GPS的性能导航方法研究

利用直角坐标系与大地坐标系之间的关系,将状态方程直接采用经纬度描述,GPS测量数据与电子地图上的经纬度相匹配,建立了混合模型,给出了一种新的GPS与IMU融合估计方法,提高了重复定位精度,更方便地实现组合导航系统功能。采用GPS和IMU装置进行了地面车辆试验和实际飞行试验,说明了模型和方法的适用性。

Abstract：

A mixed model was established and a new fusion estimation method for GPS and IMU was proposed through the relationship between the Cartesian coordinate system and the ground coordinate system,and the state equation described by the latitude and longitude directly,and the GPS measurement data and electronic map matched to the latitude and longitude.The provided method has improved the repeatability positioning accuracy and more easily integrated navigation system functions.The ground and actual flight were tested to illustrate the applicability of the model and method with GPS and IMU device.     

基于岭回归径向基神经网络的MIMU误差建模

对MEMS（Micro Electro Mechanical systems微电子机械系统）IMU（Inertial Measurement Unit惯性测量单元）的随机漂移和误差进行建模和补偿是提高捷联惯导系统性能的主要方法之一。为了避免径向基（RBF）神经网络输出之间可能存在的复共线性,更加准确有效的对MIMU的输出误差建模,提出将岭回归径向基神经网络用于MIMU的误差建模中。通过与时间序列建模方法的仿真比较表明,在对MIMU误差补偿上所建立的岭回归RBF网络与四阶AR模型方法精度相当,比一阶AR模型精度高,而且无需对数据平稳性处理。

Abstract：

It is one of the main methods to improve the performance of Strap-down Inertial Navigation System for compensating the random drift and bias of MEMS （Micro Electro Mechanical systems） IMU （Inertial Measurement Unit）. In order to eliminate latent multicollinearity of radial basis function neuron network output layer and model the drift and bias of MIMU accurately,the radial basis function neuron network based on ridge regression method was proposed which was applied in modeling and compensating MIMU errors. The simulation shows,compared to the AR model,the precision of compensation of MIMU error using radial basis function neuron network based on ridge regression method is equal to the fourth order AR model,better than first order AR model,and no data stabilization processing.     

船速复合误差调节器半实物仿真及稳定性分析

船舶航速的稳定性主要取决于主机负荷调节系统的响应特性,为抑制负荷扰动,提高船舶航速的控制精度,提出了基于Lyapunov方法的船速复合误差调节器,并进行了稳定性分析,实现了船速自适应控制。在实验室条件下,建立了船速复合误差调节器半实物仿真系统。仿真结果表明,在系统模型不确定性的情况下,船速复合误差调节器能提高系统抗干扰能力和船舶航速的稳定性。     

三维射击精度的Winterbottom逼近

为避免导弹武器三维射击精度降维评估带来的信息损失问题,在三维射击精度一阶逼近法研究的基础上,引进SEP对分布参数的二阶偏导数,依据Winterbottom展开给出了SEP的置信上界和置信区间表达式。详细推导了具体计算公式,提出Box-Cox变换参数λ的选取原则,列出了优化λ的计算方程,并以示例说明Winterbottom逼近对中小样本的具体运用和实际效果,结果表明该方法具有良好的使用前景。首次将渐进正态性理论和逼近理论引入三维精度评估领域,解决了球概率误差分布未知问题。     

基于非线性预测滤波的卫星姿态确定

为了提高卫星姿态确定系统的精度和可靠性,采用由姿态动力学与运动学方程构成的非线性卫星姿态运动模型,结合陀螺和矢量观测信息来确定卫星姿态。针对转动惯量变化等引起的模型不准确问题,研究基于预测滤波实现姿态估计的关键技术。仿真结果表明,在恰当选取加权阵的前提下,该方法可实时估计模型误差,当用低通滤波去除高频噪声的模型误差进行补偿后,大大削弱了模型不准确对姿态估计精度的影响,其估计效果明显优于传统的扩展卡尔曼滤波,由此验证了预测滤波在卫星姿态确定中的有效性和精确性。     

舰载导弹系统联调试验精度分析仪设计研究

针对舰载导弹系统精度检测分析自动化问题和缺乏检测全系统总体精度指标的问题,根据大闭环思想和导弹武器系统特点设计了导弹武器系统联调精度分析仪的结构,建立了联调战术态势运动学和误差分析模型。为保证实装系统安全性要求,对实装数据的采集采用外挂方式和软硬件结合方式,并建立实装系统数据采集和分析的数学模型。确定射击精度和捕捉概率来作为系统总体精度指标,并论述了总体精度指标的检验原理和方法。设计的精度分析仪无论对实装的日常检测还是舰艇大修后的整体精度指标测试,都有经济和军事意义。     

我国通货膨胀的混合回归和时间序列模型

回归模型的残差项反映了对被解释变量有影响但未列入解释变量的因素所产生的噪音 ,这部分噪音可由时间序列模型进行拟合 .本文对通货膨胀建立了一个混合回归和时间序列模型 ,并将该模型的预测结果与单纯用回归模型的预测结果进行了比较.     

FINITE ELEMENT METHOD AND ANALYSIS FOR CHEMICAL-FLOODING SIMULATION

1.IntroductionThisarticlediscussestheenhanced0ilrecoverynumericalsimulationofthechemicalflood-ing(suchassurfactats,alcohol,polymers)c0mposed0f3-dimensional,multicomponent,muLtiphaseandincompressiblemixedfluids.Aftertheoilfieldiswaterfi0oded,thereisstillalargeamountofcrudeoilleftintheoildeposit.Thisamountofoil,boundedbycapillarypressure,cannotflow;or)asaresultofthedisadvantageousrateofflowbetweenthedisplacinganddisplacedphases,thevolumethattheinjectionfiowaffectsistoosmalltodrivethecrudeoil.By…     

飞机空面精确打击武器火控系统精度仿真分析

空对面精确打击武器火控系统是现代作战飞机对付地面(或海面)目标的一种重要武器系统,在现代战争中有着无可替代的作用,其武器系统精度是关键技术指标。在分析精度分析评价指标体系的基础上,分析了影响飞机空面精确导弹武器火控系统的误差因素,确定了从飞机火控系统和导弹制导系统两个方面来分析武器火控系统精度误差链的分析方法。针对防区外空地电视遥控制导导弹火控系统进行精度分析与评估,利用蒙特卡罗法对防区外空地导弹火控系统进行了全武器精度分析仿真。其结果对评价空对面精确打击武器火控系统精度具有很好的工程应用价值。