基于离散正则模型的时变信道盲辨识算法

以CDMA时变信道离散正则模型为基础,提出了基于改进的矩阵外积分解的时变信道盲辨识算法。算法对传统的矩阵外积分解算法进行修正,使其适应离散正则模型两级盲辨识,并引入了精确的时延阶数估计,克服了现有算法需要预先知道信道时延实际阶数的局限,使其在仅知道信道阶数上界的条件下完成盲辨识。仿真结果表明了该算法的有效性。     

基于加权映射模型的主干网流量特性分析

网络测量表明,IP主干网上流量在次秒级的时间尺度下呈现出非平稳的泊松特性,而不是近10年大量研究的自相似现象。从分析因特网的结构出发,提出了一种加权映射模型来解释这种特性。该模型通过引入混沌变化因子和流量特征间的关系,对接入网中的具有自相似特性的流量进行了变换得到具有趋泊松性的流量。最后,通过在NS2上的仿真实验证实了该模型的合理性。     

基于循环累积量的星形QAM载波盲估计

针对通信对抗和正交幅度调制(QAM)信号解调的实际应用,提出一种利用特定高阶循环累积量估计星形QAM载波的方法。由于高阶循环累积量能有效抑制平稳噪声和非平稳高斯噪声,通过理论分析可证明在上述噪声背景下,星形8、16 QAM信号的特定四阶循环累积量仅在载波位置处存在,因此可以通过检测此循环频率实现载波的估计。该算法可推广到更高阶星形QAM信号。仿真实验验证了该算法的有效性。     

Adaptive SPC monitoring scheme for DOE-based APC

Automatic process control （APC） based on design of experiment （DOE） is a cost-efficient approach for variation reduction. The process changes both in mean and variance owing to online parameter adjustment make it hard to apply traditional SPC charts in such DOE-based APC applied process. An adaptive SPC scheme is developed, which can better track the process transitions and achieve the possible SPC run cost reduction when the process is stable. The control law of SPC parameters is designed by fully utilizing the estimation properties of the process model instead of traditionally using the data collected from the production line. An example is provided to illustrate the proposed adaptive SPC design approach.     

基于X射线脉冲星的高轨卫星自主初轨确定

介绍了X射线脉冲星轨道确定原理,在分析脉冲星相位模型的基础上,推导了X射线脉冲星轨道确定算法,讨论了时间估计法在解模糊度问题中的应用,针对高轨卫星提出了利用其大致高度信息辅助解模糊度的方法。对地球静止轨道卫星初轨确定进行了仿真,结果表明选用周期较大的脉冲星并采用时间估计与高度信息辅助的方法可以有效解决模糊度问题,并达到几十公里级的初轨确定精度。     

提升类小波变换加速的模基参数估计算法

将提升类小波变换(lifting wavelet-like transform, LWLT)应用于矩量法（method of moment, MOM）快速求解电场积分方程（electric field integral equation, EFIE）,对生成的稀疏化线性系统采用模基参数估计（model based parameter estimation, MBPE）算法求解,可获得小波域的宽带解,结合小波逆变换,最终实现目标电磁散射特性的宽频分析。通过不同三维散射体的计算分析,验证了算法的正确性。与传统模基参数估计算法相比,所提算法在计算时间和内存耗费上均有很大改善。     

飞机结冰包线保护对开环飞行性能影响与仿真

在所有的飞机失事事故中,由于飞机结冰造成的灾难是很重要的因素之一。为了解决飞机结冰后造成的飞机失速迎角减小以及飞行包线萎缩等安全隐患,通过引入结冰参数等,采用一种简化的飞机结冰模型的方法来仿真。仿真计算各种输入或者扰动下,结冰飞机纵向各项性能响应。通过在线计算结冰失速迎角,建立开环状态下飞机包线保护系统,实时反馈失速迎角告警信息以提醒飞行员操作,从而保证飞机飞行的安全。仿真计算表明,该方法行之有效,而且概念清晰,计算简便,可以在实验条件不足的情况下,为仿真研究提供一种良好的方法。

Abstract：

In-flight icing is one of the most important factors for all of the aircraft accident.A brief method was utilized to simulate the aeroplane iced in order to solve the problem which was caused by ice,such as low stall of angle of attack and flight envelope atrophy.All the longitudinal dynamic of aircraft could be got in different input.Ice aircraft envelope protection could provide the pilot with enough time to avoid icing related accidents by calculating the stall limits of angle of attack online.The result of simulation can show that the system is working effectively,furthermore its method is simple and concept is obvious.It provides a good way for simulation research,especially in the condition of experiment lacking.     

基于主模型CAD/CAE集成的卷绕锭轴结构参数优化

高速卷绕头是化纤长丝纺丝机的重要单元机,国内之前研究相对较少。采用虚拟产品开发技术进行高速卷绕头新产品开发的技术创新,提高卷绕头产品开发效率。与同类研究类似,在高速卷绕头产品的虚拟开发过程中,集成CAD/CAE系统存在若干技术瓶颈。基于CAD/CAE系统集成方法的对比分析,建立了主模型CAD/CAE集成框架,并在该框架下进行了高速卷绕头锭轴结构参数优化设计,其优化设计的动力性能分析结果验证了基于主模型CAD/CAE集成框架进行高速卷绕锭轴部件虚拟开发的有效性。

Abstract：

Researches based on the high speed winder, which is a key unit machine for filaments treatment, are relatively rare in China. The techniques of virtual product development （VPD） were applied to improve the new product development of the high speed winder, which would raise the product development efficiency of the high speed winder. Similarly to the research of this kind, in the procedure of developing the virtual product for the high speed winder, there were several key technical problems in the CAD/CAE integrated system. The contrast analysis of the CAD/CAE integrated methods was given; furthermore, the CAD/CAE integrated framework based on master model was built, in which the structural parameters of the high-speed winder chuck was optimized for design. The dynamic characteristics analysis for the optimization design was done; consequently, the result indicates that in the CAD/CAE integrated framework based on master model, the structural parameter optimization of high-speed winder chuck is available.     

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.     

地球静止卫星位置自主确定方法与仿真研究

给出了利用星敏感器测量信息自主确定地球静止卫星位置的方法,利用不同精度的星敏感器测量数据和不同控制精度的卫星姿态测量数据,可以直接计算卫星位置.同时又对测量数据应用卡尔曼滤波进行卫星位置计算仿真,比较两种处理结果的精度.仿真结果表明,提出的方法可以实时自主获取静止卫星的轨道位置,满足静止卫星定点的不同精度需求.