三维粒子测速系统中遗传匹配法的设计

提出了基于遗传算法的三维粒子图像匹配方法及实际中的优化设计。该方法以视差为编码、结合SSD(sum of square difference)与SAD(sum of absolute difference)法对结果进行评估,并通过单点、多点的双交叉、变异与序列的混沌化处理达到对分析空间的搜索;最后,局部处理结合全局唯一性迭代检测进一步增加了匹配结果的可信度。利用优化前后所提算法对空间粒子图进行了对比及误差分析。结果表明:所提算法适用于粒子测速系统的立体匹配,能够给出较准确的视差信息。     

Exploration of TCM Masters Knowledge Mining

Traditional Chinese medicine （TCM） has a rich knowledge about human health and disease by its special way evolved along a very long history. As modern medicine is achieving much progress, arguments and disputes toward TCM never end. To avoid losing precious knowledge of living TCM masters, endeavors have been engaged to systematic collection of those knowledge of TCM masters, such as their growth experiences, effective practical cases toward diseases and typical therapeutic principles and methods. Knowledge mining methods have been expected to explore some useful or hidden patterns to unveil some mysteries of the TCM system. In the paper, some computerized methods are applied toward those collected materials about some living TCM masters in China mainland to show a different way of exposing essential ideas of those TCM masters by correspondence visualization which aims to help people understand TCM holistic views toward disease and body, and facilitate tacit knowledge transfer and sense-making of the essence of TCM. The work is one kind of qualitative meta-synthesis of TCM masters＇ knowledge.     

用系统科学理论指导循环经济，推动鄂尔多斯市又好又快发展

用系统论指导循环经济,推动鄂尔多斯市又快又好发展的重要性及其思路。     

协同仿真技术在行星框架动态优化中的应用研究

行星框架作为行星传动机构的重要零部件,在设计时依然采用传统静强度设计理论,不能充分反映动载荷工况下的动态特征,导致工作过程中发生裂纹、突然断裂的现象,严重影响了行星传动机构的可靠性,给维修和保障带来很大的困难。因此对行星框架进行动态优化设计具有十分重要的意义。以行星轮数目为设计变量,采用基于接口的协同仿真技术作为求解工具,对某任务剖面下的行星框架进行动态结构优化,完善了行星传动设计方法,为设计部门提供有关寿命预测的参考数据。     

具有不同到达时间的差异工件批调度问题的蚁群聚类算法

研究具有不同到达时间的差异工件在单机环境下的批调度问题.通过引入工件单元的概念并对分批约束进行松弛,提出了该问题的一个新的下界,证明了该下界的有效性.将蚁群算法和聚类算法相结合,提出了一种基于多阶段聚类的蚁群聚类算法ACC(Ant colony clustering).算法首先利用K-均值聚类将工件分簇,在簇内部通过蚁群算法搜索分批,最后提出一个全局优化算法对局部分批结果进行合成和优化.克服了蚁群算法随着工件规模增大求解时间过长的问题,适合于求解大规模算例.实验结果表明:与现有的启发式规则LPTBFF(Longest processing time batchfirst fit)和HGA(Hybrid Genetic algorithm)算法相比,该算法求解效果更好.     

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.     

四轮转向直接横摆力矩鲁棒集成控制仿真研究

将四轮转向与直接横摆力矩相结合,考虑模型摄动优化权函数抑制外扰,基于模型跟踪设计μ综合鲁棒集成控制器.采用J-turn操纵方式高速下验证控制器的鲁棒性,比较前轮转向直接横摆力矩,四轮转向与四轮转向直接横摆力矩三种车辆控制系统的操纵性能,仿真表明设计的四轮转向直接横摆力矩集成μ综合控制器更能有效地提高车辆闭环系统的鲁棒性,抵制外部扰动的鲁棒稳定性,且避免了H∞控制器的保守性.     

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.