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.     

天基光学监视系统空间目标定轨精度仿真分析

天基光学监视系统具有获取空间态势信息的优势,是进行空间目标监视与跟踪的重要发展方向。主要研究基于天基光学监视平台的空间目标的可见区域分析和轨道确改进定算法,仿真实现了天基监视系统对空间目标的定轨功能,分析了天基光学监视平台对高、中、低轨三类典型空间目标的定轨精度。通过仿真实验可以得出,由高低轨监视平台组成的联合监视系统提高对空间目标的轨道确定精度,其中低轨空间目标定轨精度误差约20米,中高轨空间目标定轨精度300米左右。

Abstract：

Space-based optical surveillance system has advantages accepting state information of space-objects, and is an important tendency in the realization of surveillance and tracking for resident space objects. The orbit determination theory for space objects and its cover region by space-based optical surveillance system were analyzed. The function for space objects was simulated. The accuracy of three kinds of space objects based on space-based optics surveillance system was studied. Simulation experiment shows the surveillance system which constitutes of high/low orbit surveillance platforms can improve the accuracy of space objects, and therein the orbit determination precision for low-orbit space objects reaches 20m, while that for high-orbit space objects about 300m.     

基于LDPC频域编码MIMO-OFDM系统自适应调制算法研究

提出了一种基于发射功率、发送比特和误码率均受限时规则和非规则LDPC频域编码MIMO-OFDM系统自适应调制算法.仿真比较了规则、非规则LDPC编码及未编码自适应调制MIMO-OFDM系统性能,比较了LDPC-SISO-OFDM、LDPC-MIMO-OFDM系统子载波数变化对系统BER性能的影响,比较了收发天线数变化对LDPC-MIMO-OFDM系统BER性能的影响.仿真表明自适应调制MIMO-OFDM系统比非自适应调制系统性能有所提高,规则、非规则LDPC编码自适应调制MIMO-OFDM系统比未编码系统性能有很大提高,非规则LDPC编码自适应调制MIMO-OFDM系统比规则码自适应调制系统性能有提高,但在高信噪比时有错误平层.结果证明,适当设计非规则LDPC频域编码自适应调制算法,可以大大改善MIMO-OFDM系统性能.     

材料性能对汽车碰撞散落物运动特性的影响

为研究汽车碰撞散落物的材料性能对其运动特性的影响,进一步完善交通事故再现中汽车碰撞散落物的运动行为理论模型,建立汽车碰撞散落物的运动学仿真模型,通过仿真试验,模拟了在散落初始条件相同的情况下,汽车碰撞弹性、弹塑性、塑性散落体的运动,分析了在试验条件一定时,3种材料巨能的汽车碰撞散落体的运动特性的异同及其随散落速度、散落高度、散落角度的变化关系.模拟试验结果分析表明:存在散落角度的汽车碰撞散落体其非线性运动轨迹受材料性能影响较大.     

一种基于虚拟维修仿真的交互式电子技术手册生成方法

基于并行工程思想,提出了一种基于虚拟维修仿真分析过程的结果数据制作装备交互式电子技术手册(IETM)的方法。主要研究工作为:构建了一种基于主题的IETM内容数据模型(CDM),给出了典型装备IETM的组成结构;分析了典型虚拟维修仿真分析过程中的结果数据;提出了虚拟维修仿真系统和IETM创作系统的并行集成框架,设计了集成接口和相关模型,在产品生命管理平台下实现了二者的集成;在基于Jack软件环境的虚拟维修仿真系统中,以某型榴弹炮为例,进行虚拟维修样机建模、维修任务生成、虚拟维修仿真,最后通过以上结果数据生成了该榴弹炮的4级IETM系统。     

PDE-Based Medial Axis Extraction and Shape Manipulation of Arbitrary Meshes

Shape skeletonization （i.e., medial axis extraction） is powerful in many visual computing applications, such as pattern recognition, object segmentation, registration, and animation. In this paper, the authors expand the use of diffusion equations combined with distance field information to approximate medial axes of arbitrary 3D differential properties. It offers an alternative solids represented by polygonal meshes based on their but natural way for medial axis extraction for commonly used 3D polygonal models. By solving the PDE along time axis, this system can not only quickly extract diffusion-based medial axes of input meshes, but also allow users to visualize the extraction process at each time step. In addition, the proposed model provides users a set of manipulation toolkits to sculpt extracted medial axes, then use diffusion-based techniques to recover corresponding deformed shapes according to the original input datasets. This skeleton-based shape manipulation offers a fast and easy way for animation and deformation of complicated mesh objects.     

冲击噪声背景下宽频段信号三维参数的估计

提出了一种基于协变异矩阵的宽频段信号频率和二维到达角联合估计的算法。在冲击噪声环境下,该算法能精确地估计宽频段信号的三维参数,无需多维谱峰搜索和参数配对过程。另外,利用L型阵列的分维特点和ESPRIT算法进一步处理,成功地实现了具有频率兼并现象的宽频段信号的三维参数估计。计算机仿真结果验证了算法的有效性。     

基于VEGA PRIME的集束火箭仿真训练系统的研究

介绍了基于Vega Prime的集束火箭视景仿真训练系统的软硬件平台及开发该系统所用到的关键技术。在所用到的关键技术中,详细介绍了在MFC框架下开发基于Vega Prime的视景驱动程序的方法,并给出了相关程序代码;阐述了激光随动系统的工作原理及如何实现集束火箭单发和连发火箭弹的飞行,给出了碰撞检测方法和爆炸特效的制作方法,介绍了训练参数的设置方法以及模拟训练考评系统的工作原理。     

Vega Prime实时视景仿真中粒子系统的应用研究

介绍了利用粒子系统方法模拟动态自然景物的基本步骤。应用了VegaPrime实时视景仿真软件中的粒子系统,通过设置粒子系统的颜色、亮度、透明度、形状、纹理、大小、速度和位置,逼真的模拟了火焰和烟雾的特效。通过将火焰粒子系统在发射坐标系中的速度转换到场景坐标系中,实现了火焰随着发射装置的随动。     

ICU应急辅助决策系统的开发研究

分析了我国危重病医学的现状,阐明了研制ＩＣＵ（ｉｎｔｅｎｓｉｖｅ ｃａｒｅ ｕｎｉｔ）应急辅助决策系统的意义。结合ＩＣＵ的特点,说明了ＩＣＵ应急辅助决策系统的特点和实现方法,在此基础上,讨论了系统的主要功能模块,在知识库的设计国,用面向对象技术建立了一种多元知识库模型;而在推理机的设计中,从人类认知的角度出发,突出了应急的实时诊断,提出了一种由基于规则推理、证据推理和案例推理的集成推理机制,最后在