基于HLA的卫星轨道机动仿真研究

针对STK(Satellite Tool Kit)在联合作战仿真中实时互操作能力的不足,提出了一种灵活的基于HLA(High Level Architecture)的卫星轨道机动仿真系统设计方法。建立了圆轨道之间平面内霍曼转移、平面外单脉冲和双脉冲轨道转移三种轨道机动模型,设计了多视图可视化表现子系统和仿真对象模型(Simulation Object Model,SOM)。与STK的仿真结果对比表明了该方法的可行性和模型的有效性。     

多Agent虚拟测试仿真建模方法研究

结合光电经纬仪虚拟测试的需求,提出了一种分布式多Agent虚拟测试平台结构,确立了多Agent间交互协作测试的任务目标.讨论了虚拟测试中基于Agent的仿真建模策略,设计了可重构虚拟目标Agent及其仿真流程和基于消息的监控Agent,以此构建了多Agent仿真体系完成经纬仪虚拟测试的整体协作模型.开发了基于Agent的经纬仪虚拟测试平台,通过仿真测试应用,验证了仿真建模方法及其平台的有效性,满足了现阶段经纬仪的相关性能测试.     

一种基于Geometry Image的鲁棒三维水印

近年来三维水印作为保护三维模型版权的一类方法被提出并发展起来.通常使用的不规则三角网格的表示形式限制了信号处理方法在三维模型上的应用,阻碍了三维水印的发展.作者充分利用Geometry Image这种新的三维模型表示方法的特性,将三维模型转换为二维彩色图像,然后在其DCT变换域下嵌入水印.水印的提取过程通过将嵌入水印的模型与原始模型配准后进行顶点映射获得相应的二维图像,继而在DCT变换域下提取水印.实验结果证明所提三维水印算法能够有效抗击仿射变换、加噪、平滑、重采样、剪裁等多种攻击手段,是一种鲁棒的非盲三维水印算法.     

迟滞非线性系统自适应鲁棒控制

介绍用超磁致伸缩材料与压曲放大机构组合设计的微位移驱动器,并设计了控制系统.建立了超磁致伸缩执行器基于输入电压-输出位移的机电系统传递函数模型.对微位移驱动器的迟滞特性用微分方程建立了模型.在此基础上构造迟滞模型与传递函数相结合的系统模型.由滑模控制理论,对所建模型提出了可以调节信号跟踪精度的自适应鲁棒控制方法,用Lyapunov稳定性理论进行了系统稳定性证明.通过系统模型仿真与simulink中的半实物仿真实现了该控制率,并验证了模型的准确性和补偿控制的有效性.     

基于改进型随机Petri网的维修保障方案评估方法

一体化联合作战对诸军兵种装备系统及其维修保障体系提出了更高的要求,急需对装备维修保障体系运行规律进行建模与仿真分析,提高装备完好率和任务成功率.分析了Molloy形式的随机Petri网及其扩展模型在装备使用与维修过程建模与仿真分析中的不足,据此提出了全局时间的实现方法,改变了抑制孤的功能,选择了适当的变迁规则,提出了基于改进型随机Petri网的装备维修保障过程建模方法,开发了基于MATLAB的分析软件,针对某型导弹装备使用维修过程进行建模与分析,实现了保障方案的评估与优化.     

任务型CGF组织本体建模

针对作战模拟对人类行为表示的准确性要求,建立真实反映战场行为的组织模型是非常重要的。根据需求分析和已有研究的不足,提出了基于本体论的组织建模方法,阐述了该组织本体的构建原则,并从组织静态结构和动态行为两个方面定义了相关概念及概念间的关系。在此基础上采用一阶谓词逻辑描述了该组织本体的形式化过程。实验结果表明,该方法能够准确地建立起用于实体的组织模型,使得实体行为可以反映实际战场行为,且能够保证组织本体的通用性。     

新一代交通仿真技术综述

简要回顾了国内外交通仿真技术的发展历程,总结了新世纪以来新一代交通仿真技术的主要特点。然后,比较分析了当前主流交通仿真模型的特性,并对交通仿真应用程序接口、硬件在环和软件在环交通仿真、在线交通仿真等面向智能交通系统应用的高级仿真技术进行了深入解析。最后,根据我国交通仿真研究和应用的现状,在符合我国交通特性的基础仿真模型研究、交通仿真系统的开发模式、在线仿真技术的开发方法等方面提出了改进建议。

Abstract：

The historical course of traffic simulation in China and abroad was briefly reviewed firstly,and some major features of the new generation traffic simulation technology since 21st century were summarized then. Afterwards,the simulation model characteristics of some prevailing traffic simulation models were comparably analyzed,and several advanced traffic simulation techniques for ITS applications were expatiated,including traffic simulation API,hardware-in-the-loop traffic simulation,software-in-the-loop traffic simulation,online traffic simulation. Finally,based on the state-of-the-practice of traffic simulation in China,some suggestions were given on fundamental simulation modeling fitting for Chinese traffic characteristics,development modes of traffic simulation system,development methodologies of online traffic simulation,etc.     

翼伞系统纵向动力学建模研究

动力翼伞是一种具有广泛应用价值的独特飞行器,其低速飞行和较大的载荷重量的特点可以使得它成为航空拍摄或军事侦察监视等应用的平台。通过建立简单适用的纵向动力学模型,可以对其速度、姿态等方面的稳定性进行相应的分析。通过推力来控制飞行器的爬升、下降或平飞,起到调整高度的作用。仿真结果表明通过合理的设计载荷与翼伞的质量比、连接绳的长度、翼伞质心与压心的相对位置等影响参数,可以得到较为理想的效果。

Abstract：

Powered parafoils represent a very unique class of aircraft which has broad applied value. Their slow flight and large payload characteristics make them a practical platform for applications such as aerial screen and military surveillance. The stability of speed and attitude was analyzed by designing a simple and applied longitudinal dynamic model. The climbing, descending or flying straight-and-level of the aircraft were controlled by thrust, which had an effect to adjust the altitude. The simulation results show an ideal purpose can be gained by designing the parameters such as the mass ratio of the payload and parafoil, the length of the link, and the relative position between the center of mass and center of pressure rationally.     

大雨对飞机降落影响效应仿真研究与定量分析

为全面、定量分析大雨对飞机降落阶段的严重影响,选取波音737-300作为典型代表,首先对于降落阶段大雨造成的飞机性能损失进行了量级评估。然后重点针对降雨所导致的粗糙表面因素,利用CFD仿真方法和改进的湍流壁面函数,对于不同降雨强度下的波音737-300中段翼型气动性能进行了仿真模拟,给出了升阻力系数、失速攻角等定量结果,并与实验结果进行了对比。结果表明：大雨所导致的粗糙机翼表面将引起严重的气动性能损失。在降落阶段,对于波音737-300中段翼型而言,短时500毫米/小时降雨条件下,最大升力系数减少约28%,阻力系数平均增加达98.1%,失速攻角减小约5度。

Abstract：

Heavy rain might influence aerodynamic performance of an aircraft seriously, especially when it is landing. It requires an intensive investigation and quantitative analysis. Choosing Boeing 737-300 as the representative of aircraft, magnitude calculation for the penalty associated with severe rainfall was firstly made. Then the roughness factor was studied in detail using evolutional turbulence boundary function and CFD simulation tools. The aerodynamic character of Boeing 737-300 midspan airfoil was simulated under different rainfall environment. The quantitative results of lift-drag coefficients and stall angle were proposed and compared with experiment data. The results indicate that, the roughness surface caused by rainfall is most likely to cause significant aerodynamic penalties. For Boeing 737-300 midspan airfoil, when it is landing under severe rainfall of 500mm/hour over 30s periods, it could lead to the loss of maximum lift coefficient by about 28%, the decrease of stall angle by 5 and the increase of drag coefficient by 98.1%.     

红外探测器成像仿真

红外探测器是红外成像技术的核心,直接影响着红外成像系统的性能。在分析目标成像尺寸的基础上,详细分析光学弥散、探测器噪声、成像阵列盲元等的形成机理,并进行建模和仿真,最后将这些模型依次叠加。采用此方法得到的仿真图像充分考虑了探测器各种效应的影响,提高了仿真图像的真实性与逼真度,可为红外成像系统的研制及目标检测识别算法提供测试场景与依据。

Abstract：

Infrared detector, which can directly influence the performance of infrared imaging system, plays a key role in infrared imaging technology. The scale of the target image, the causation of optics dispersion, noise of the detector and blind pixels in the imaging arrays were detailed analyzed. More actual infrared images would be simulated by adding the effects mentioned above to the theoretical image model, because the ill effects were calculated. The simulated images could be used to test infrared imaging system or the algorithm of target detecting and recognition.