基于BOM的STSS系统仿真设计与实现

以空间跟踪与监视系统（Space Tracking and Surveillance System,STSS）为仿真对象,基于高层体系结构（High Level Architecture,HLA）分布式仿真技术设计、开发STSS仿真系统。分析了STSS技术特点及仿真需求,按照基本对象模型（Base Object Model,BOM）开发标准构建系统的层次化联邦架构,提高了系统开发效率和模型的可重用性。通过对不同场景的多次仿真,初步验证了STSS的性能指标,说明该系统具有良好的适应性。

Abstract：

Based on HLA distributed simulation technology, design and implementation of STSS simulation system, the technical traits of STSS system and demands of simulation were analyzed. According to BOM development standard, a framework in hierarchy of STSS simulation system was constructed, which has effectively improved the efficiency of system realization and the capability of model reuse. By simulating the different scenarios repeatedly, the performance parameter of the STSS simulation system was tentatively verified, and applicability of the simulation system was proved.     

汽车轮缸压力传感器故障重构方法研究与仿真

针对汽车液压制动系统中轮缸压力传感器的故障重构问题,建立了汽车液压制动系统的轮缸压力非线性模型。在此基础上,给出了一种基于滑模观测器的轮缸压力传感器故障重构方法,并将滑模观测器的设计问题转化为LMI求解问题。最后对轮缸压力传感器断路故障进行了仿真研究,讨论了不同增益对故障估计的影响。

Abstract：

A fault reconstruction scheme based on the sliding mode observer was proposed for the fault reconstruction of the wheel cylinder pressure sensor in the vehicle hydraulic braking system, as well as a nonlinearity model of the wheel cylinder in the hydraulic braking system. Furthermore, the design of the sliding-mode observer was converted to the solving of the LMI. In conclusion, the wheel cylinder pressure sensor open circuit fault simulation experiment and the influence on fault estimation over the different gain were proposed.     

坦克炮控系统关联参数测试精度建模仿真分析

叙述了坦克武器系统的发展历程及其炮控系统定型试验项目,介绍了炮控系统性能参数测试系统的组成及工作原理,提出了坦克装甲车辆武器系统定型试验中,炮控系统关联参数测试时存在测试精度超差问题,通过建模仿真手段,建立了基于光纤陀螺的角位移测量误差模型,分析了影响测量精度的主要因素,给出了测量误差补偿方法,经试验验证,补偿方法合理可行。

Abstract：

Progress history and gun control system （GCS） approval test items of tank weapon systems were proposed. Composition and working principle of GCS performance parameter test system were introduced. The problem of GCS relevant parameters measuring accuracy running out of tolerance in tank armored vehicle weapon system approval test was put forward. Angle measuring error model based on FOG was modeled and the major influencing factors of measurement accuracy were analyzed by the means of modeling and simulation. Compensation process of measuring error, which was verified by experiment to be rational and feasible, was given out.     

基于Extend与HLA的装备保障仿真集成研究

分析了Extend应用于装备保障仿真的不足,在讨论基于HLA的装备保障仿真系统的基础上,提出了Extend与HLA/RTI的四种仿真集成方式,依据Extend模型是否需要与HLA/RTI进行时间同步分别给出了集成方法,设计了基于适配器的Extend与HLA集成框架,详细说明了适配器的组成功能及工作流程,最后利用一个装备保障仿真系统应用实例证明了仿真集成的思路是可行的和必要的。

Abstract：

Because of the shortages of Extend software applied to equipment support simulation,four integration types between Extend and HLA were proposed about the building of equipment support simulation system based on HLA.According to whether Extend simulation model was synchronous to HLA/RTI on the mechanism of advance simulation time,the methods were respectively put forward to support these types,and an integration architecture between Extend and HLA was designed based on a general adaptor.The components and functions of this adaptor,and its running mechanism were detailedly analyzed later.Finally,an application of a simulation system proves that the idea to integrate the two platforms is feasible.     

一种新型UUV半实物仿真系统设计与实现

针对UUV导航与控制系统高精度仿真的需要,设计了一种支持捷联惯导、多普勒测速仪、深度传感器和GPS接收机接入的半实物仿真系统,解决了GPS卫星导航信号仿真、多普勒测速仪水声回波模拟和UUV深浅水航行深度模拟问题,进行了导航与控制系统的半实物仿真试验,分别测试了GPS导航仿真子系统、多普勒测速仿真子系统和深度模拟子系统。试验结果表明,该仿真系统满足了仿真实时性和计算精度的要求,对于UUV研制具有重要的应用价值。

Abstract：

To satisfy the requirement of high accuracy simulation of complicated navigation and control system of unmanned underwater vehicle, a new plan of simulation system was proposed, which afforded the interface environment for SINS, Doppler velocity instrument, depth sensor and GPS receiver. The GPS satellite navigation signal simulation, the acoustic echo of Doppler velocity instrument and the sailing depth simulation were solved. The simulation experimentation combining hardware was processed, and the GPS simulation subsystem, the Doppler velocity simulation subsystem and the sailing depth simulation subsystem were all tested. The results show that the simulation system meets the real-time and accuracy requirements, and the system has important application value for UUV development.     

基于多粒度模型的导弹MDO方法研究

根据MDO环境的建模/仿真需求,针对某导弹多学科设计优化问题,分析了多粒度模型建模/仿真的必要性,以气动学科为例探讨了导弹MDO环境中多粒度模型的建模/仿真方法,研究了有限元分析软件FLUENT及其前处理软件GAMBIT的集成方法,并利用响应面分析、工程估算、数值计算三种方法对某导弹的气动学科进行多粒度的建模与解算,将输出的主要气动参数与风洞试验数据进行了比较与分析。研究结果表明多粒度模型的建模/仿真对提高导弹MDO效率具有重要意义。

Abstract：

According to the requirement of modeling and simulation in MDO environment, with consideration of missile’s Multidisciplinary Design Optimization problem, the necessity of modeling and simulation on multi-granularity model was analyzed. Taking pneumatic domain as an example, method of modeling and simulation on multi-granularity in missile’s MDO environment was discussed. The integration methods of finite element software FLUENT and its pre-processing software GAMBIT were studied. Through abundant experiments, data results of computing multi-granularity model were given using three methods, namely Response Surface Analysis, engineering prediction method and numerical computation method. Finally, comparison of the data got from above and from wind tunnel test was analyzed. The study results show that modeling and simulation on multi-granularity model are significant to improve MDO efficiency.     

卫星导航系统精度试验分析的设计与实现

导航系统精度（NSP,Navigation System Precision）分析是卫星导航系统定位、测速和授时性能仿真分析与评估的重要组成部分,NSP的可用性和连续性是导航系统服务能力的重要标志之一。研究了NSP的相关概念,分析了NSP的可用性和连续性算法,在此基础上提出了面向卫星导航系统的NSP仿真模型框架,并基于此框架设计和实现了支持NSP分析的插件工具,最后针对格网分辨率为5°×5°的区域格网进行了NSP的仿真试验分析,验证了提出的仿真模型框架和设计的插件工具的正确性。

Abstract：

Navigation System Precision Analysis is a part of the simulation analysis and evaluation of the Navigation System＇s performance on positioning,velocity-measuring and time-telling,and the availability and continuity of NSP is an important symbol of service capability of the navigation system. The NSP concept was introduced firstly,and then algorithms of the availability and continuity of NSP were researched,based on these,model architecture of the NSP was proposed and the NSP simulation analysis system was designed and implemented,finally,the simulated experiment of the grid with 10 resolution was implemented and the system architecture and the plug-in facility were testified.     

基于处理器在回路的卫星编队仿真验证系统

为了验证星载计算机的软/硬件性能,建立了以两个星载计算机为核心的卫星编队仿真验证系统。介绍了该系统的软、硬件构成,重点解决了动力学仿真机与星载计算机CAN总线双向数据传输、动力学仿真机以及星载计算机的进程同步、星载计算机的无线通信以及实时驱动STK场景动画显示等问题。在成功实现系统的基础上,进行了双星编队自主维持控制仿真。仿真结果校验了系统设计的合理性以及软硬件接口的正确性。

Abstract：

To verify the software and hardware performance of the on-board computer, a demonstration simulation system for formation flying satellites was established based on two on-board computers. The software and hardware architecture of the simulation system were introduced, and the key problems of the data communication between the dynamic simulation computers and the on-board computers via CAN bus, the synchronization of the dynamic simulation computers and the on-board computers, the wireless communication of the on-board computers, and the real-time visualization animation by driving STK were solved. Based on the developed processor-in-the-loop simulation system, the autonomous formation keeping control for dual satellites was performed. The simulation results demonstrate the validity of the simulation system and the correctness of the software and hardware interfaces.     

基于虚拟集成技术的ESP硬件在环仿真

针对汽车电子稳定性控制系统的开发,提出了集成ADAMS/Car的整车虚拟样机、MATLAB/Simulink的虚拟控制器和LabVIEW的测控平台的汽车电子稳定性控制的硬件在环仿真方法（VCHIL）,阐述了该方法的实现原理,讨论了基于虚拟集成技术的硬件在环仿真系统的组成及其相互关系,并以此为向导,研制了汽车电子稳定程序（ESP）的硬件在环仿真实验平台,并进行了实验验证。

Abstract：

Aiming at the development of ESP system,hardware-in-loop simulation method based on virtual cross technology （VCHIL）,which combined virtual modal by ADAMS/CAR,virtual controller by MATLAB/Simulink and LabVIEW platform,was addressed.The realization principle of the method was introduced.The structure and relation between parts of hardware-in-loop simulation system based on virtual cross technology were discussed,and according to these,the hardware-in-loop simulation testing platform was developed.Test on this platform was performed and the results were analyzed and compared.     

舰载相控阵雷达仿真系统研究与实现

对于舰载相控阵雷达这类复杂系统的仿真,软件系统的设计起着至关重要的作用。为了更有效的进行舰载相控阵雷达的仿真研究,在模块化的基础上,引入了分层设计的思想,建立了分层模块化、易于扩展的仿真软件体系结构,给出了总仿真流程,并着重分析研究了其核心模块的功能、原理和实现流程,构建了仿真软件系统。仿真结果充分验证了模型和方法的可行性和有效性。

Abstract：

The design of software system is very important to the simulation of complex system such as shipborne phased array radar. To make the research of shipborne phased array radar simulation more efficiency, the idea of layered design was imported based on modularization, a hierarchy modularized and easy expansible simulation software architecture was established, and the whole simulation flow was suggested, the function and the theory and the realization flow of the core model was mainly researched, and the simulation software system was developed. The result of the simulation has validated the model and the method.     

液体推进剂导弹全动力系统稳态故障仿真(一)

为了对液体推进剂导弹动力系统进行稳态故障分析、仿真、检测、诊断以及研制箭载监控系统，必须建立其全系统稳态故障模型。通过对动力系统稳态工作过程，特别是自生增压系统的动力学分析、故障特性分析、故障因素的作用机理的分析、故障因素的引入方法研究等，依据某导弹动力系统的实际结构，完整地建立了该导弹动力系统的全系统稳态故障模型方程。与单纯的发动机系统模型相比，该模型能够模拟飞行状态的稳态故障，能更全面更好地分析动力系统的稳态故障特性。     

液体推进剂导弹全动力系统动态故障仿真(二)

为了分析其故障特性和获取各种动态故障模式，采用性能优良的Runge-Kutta-Fehlberg(R-K-F)方法求解动态故障模型方程，仿真液体推进剂导弹(液体导弹)动力系统全系统动态故障。对已发生过或可能出现的故障形式，进行了过渡过程动态故障模拟计算和特性分析，获得了动力系统全系统动态故障模式库。计算结果表明，所建模型正确合理，数值模拟计算方法满足要求。该研究开辟了导弹动力系统动态过程故障分析、检测和诊断方法的新途径。     

分布式仿真系统容错机制研究

就分布式仿真中的容错问题进行了初步的研究和分析。首先针对分布式仿真系统的特点，提出了系统分层模型，就每层中错误类型进行了分析和描述。然后构建了基于HLA的分布式仿真容错系统DSFT(Distributed Simulation Fault-tolerancesy stem)，该系统主要由三部分组成：仿真资源状态监控模块、数据保存模块及错误恢复模块，文章就该系统的相应模块跟RTI的关系进行了分析。最后，就利用网格技术来简化容错系统实现的可行性进行了初步研究。     

集成模糊推理与定量仿真的故障预测系统研究

为解决传统故障诊断方法在装备维修保障方面的不足，将虚拟样机作为一种新的定量推理机制引入到故障仿真和预测领域，提出了基于虚拟样机的装备故障仿真预测模型。以某型自行火炮为研究对象，在ADAMS环境下建立了火炮虚拟样机。仿真预测过程根据用户输入的初始参量由虚拟样机获取初始状态，由基于动态模糊综合评判的预测方法生成候选故障集，虚拟样机结合知识库确认实际发生的故障并找出相应的故障原因和故障部件。虚拟样机的仿真结果和相关的预测实例验证了模型的有效性，表明基于上述模型的故障仿真预测系统可以获得较高的预测精度，能够满足装备预知维修保障的需求。     

无刷直流电动机系统故障检测方法的仿真研究

首先建立了无刷直流电动机系统正常运行时的系统模型。在此模型的基础上,针对系统中功率开关管开路、绕组开路和绕组匝间短路三种故障分别建立了故障运行时的系统模型。通过对系统正常运行和上述各种故障运行的仿真研究,确定了能够识别故障的特征波形。根据仿真结果提出了基于模型监控的故障在线检测方法,即通过正常运行时系统模型的输出值与系统实际输出值之间的偏差来检测系统的故障。     

基于虚拟样机的装备故障灵敏度分析及参数阈值获取

作为常规主战陆基武器的火炮，目前在战争中仍然起着不可替代的作用。首先分析了火炮后坐动力学过程和典型故障因素，概括了表征火炮工作性能的三个指标和工作准则。基于ADAMS建立了用于仿真火炮故障的虚拟样机模型，仿真结果与试验数据对比说明了虚拟样机建立的准确性。利用相对灵敏度分析获得各典型故障因素对火炮工作性能指标的影响程度，解决了具有不同量纲的故障因素影响性能指标的比较难题。根据火炮极限射击条件，利用虚拟样机仿真获得了典型故障参数的变化阈值，为火炮预防性维修和精确化保障奠定了基础。最后，展望了下一步工作重点和虚拟样机技术在武器装备仿真领域的应用前景。     

基于SVM的超高压直流输电系统故障诊断模型研究

针对非线性、高度可控的超高压直流输电（HVDC）系统,提出将支持向量机（SVM）用于系统的故障诊断研究中。首先利用电磁暂态仿真软件EMTDC/PSCAD建立系统模型,对常见故障进行仿真研究。为有效提取故障特征,对直流电压波形进行S变换。变换后的特征量作为SVM的输入,建立系统故障诊断模型,并比较了不同参数下的SVM模型性能。仿真结果表明SVM用于HVDC系统故障诊断是合理、有效的。     

基于系统参数估计时间序列的小波分析故障诊断方法

提出了一种失效性故障诊断的新方法.这种方法将基于解析模型的故障诊断技术和基于信号分析的故障诊断技术结合起来,对系统参数的递推最小二乘估计时间序列进行小波分析,得到故障特征值,兼有两种故障诊断技术的优点.本文还讨论了对于模型参数估计时间序列小波分析的基函数及尺度选取方法问题,仿真结果表明该方法的有效性和准确性非常明显,具有一定的实用价值.     

基于模型的飞控系统安全性分析研究

针对飞控系统安全性分析问题, 提出一种基于系统拓展模型(extended system model, ESM)的安全性分析方法。首先, 运用Simulink建立系统名义模型。然后, 对名义模型进行故障注入, 得到系统扩展模型, 观察故障情况下的系统响应并对系统进行安全性分析。最后, 选取操纵舵面系统(副翼/方向舵)为例。结果表明，系统故障拓展模型使得模型保持完整性和一致性, 能够模拟系统故障多状态模式, 保证了安全性分析结果的准确性和完整性。     

三相SPWM逆变电源故障检测与诊断的仿真研究

该文建立了三相SPWM逆变电源的非线性的MATLAB仿真模型,通过仿真试验获得逆变电源发生开关器件断路时的数据矩阵,构造系统神经网络的学习样本,并以此训练神经网络,确定了用于三相SPWM逆变电源故障诊断的神经网络结构和参数。仿真验证试验结果表明所设计的基于人工神经网络的电力电子逆变电路的故障诊断系统是可行的。