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SOA的分布并行SMP2仿真体系结构研究

为了提高SMP2模型在分布式环境下的互操作与可组合性,提出了基于模型驱动架构的分布并行SMP2仿真体系结构。针对分布式环境模型组合的特点,提出了基于代理的SMP2仿真模型分布式组合方法。针对在分布式环境下进行模型调度的两个问题,提出了基于时间管理器和消息管理器的仿真模型分布式并行调度方法。设计实现了原型系统,包括基于空消息的异步仿真协议时间管理器、基于WebService的消息管理器、仿真控制管理器和仿真应用客户端。最后并以导航系统DOP分析仿真为例,验证了方法的可行性,并讨论了下一步研究方向。

Abstract：

To enhance the interoperability and composability of the Simulation Model Portability Standard 2 （SMP2） in distributed environment, a simulation architecture based on Service-Oreinted Architecture （SOA） was promoted. To satisfy the composition and schedule requirment under destributed environment, a proxy-based model composition method and a model schedule method based on time manager and message manager were studied. A prototype system was designed and implemented, including CMB-based time manager, web-service-based message manager, simulation control manager and simulation client. Finally, an application of Navigation System DOP analysis simulation demonstrates the validity and feasibility of the method.     

基于博弈论组网多机动目标协同跟踪技术研究

在卫星多目标跟踪的背景下,针对传感器网络的协同问题,首次建立了完整的基于移动动态联盟的多目标协同跟踪模型,并针对协同过程中的移动动态联盟形成问题,提出了基于博弈论的联盟形成算法。该协同模型在跟踪多目标时利用移动动态联盟来交换并协调节点间的信息,使节点的行为一致,具有分布式和自组织的特点。仿真实验验证了该协同模型应用在传感器网络多目标跟踪中的有效性。

Abstract：

As to the collaborative technique in sensor network,an integrated multi-target collaborative tracking model was constructed based on mobile dynamic coalition under the background of multi-satellite tracking.Then as to the mobile dynamic coalition formation,a coalition formation method was proposed based on game theory.Using mobile dynamic coalition,this collaborative model exchanged and coordinated the information of nodes to accord their action.So it is distributive and self-organizing.Simulation results validate the effectiveness of collaborative model in sensor network tracking multi-target.     

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.     

复杂电磁环境生灭模型及特征生成

复杂电磁环境主要由各类辐射源辐射的电磁信号交互作用而产生。应用随机理论,建立了辐射源的生灭过程模型,采用蒙特卡洛方法动态仿真辐射源状态;建立了给定目标点的有效辐射源筛选、功率密度计算和辐射脉冲流密度计算模型;给出了仿真流程。满足电磁环境仿真的适应性、动态性和实时性需求。

Abstract：

Complex electromagnetic environment comes from many different radiations and their interaction. A birth-death model of radiant points was built on the stochastic theory, and then the states of radiant points were dynamically simulated by Monte Carlo. Some characters creating models were built, including model of filtering valid radiant points, model of power density computing and model of pulse steam density computing. Finally, a simulation process was proposed. All of those have met electromagnetic environment simulation requirement in adaptability, dynamic and real-time.     

Primary safe criterion of earth-brushing flight for flying vehicle over digital surface model

In modern terrain-following guidance it is an important index for flight vehicle to cruise about safely and normally. On the basis of a constructing method of digital surface model (DSM), the definition, classification and scale analysis of an isolated obstacle threatening flight safety of terrain-following guidance are made. When the interval of vertical-and cross-sections on DSM is 12. 5 m, the proportion of isolated obstacles to the data amount of DSM model to be loaded is optimal. The main factors influencing the lowest flying height in terrain-following guidance are analyzed, and a primary safe criterion of the lowest flying height over DSM model is proposed. According to their test errors, the lowest flying height over 1:10 000 DSM model can reach 40. 5 m~45. 0 m in terrain-following guidance. It is shown from the simulation results of a typical urban district that the proposed models and methods are reasonable and feasible.     

The Dynamics of Two-State Public Opinion Propagation On Signed Networks

The formation of public opinion on the network is a hot issue in the field of complex network research, and some classical dynamic models are used to solve this problem. The signed network is a particular form of the complex network, which can adequately describe the amicable and hostile relationships in complex real-world systems. However, the methods for studying the dynamic process of public opinion propagation on signed networks still require to be further discussed. In this paper, the authors pay attention to the influence of negative edges in order to design a two-state public opinion propagation mechanism suitable for signed networks. The authors first set the interaction rules between nodes and the transition rules of node states and then apply the model to synthetic and real-world signed networks. The simulation results show that there is a critical value of the negative edge ratio.When the negative edge ratio exceeds this critical value, the evolutionary result of public opinion will change from a consistent state to a split state. This conclusion is also consistent with the distribution result of opinions within communities in the signed network. Besides, the research on the network structural balance shows that the model makes the network evolve in a more balanced direction.     

Flight control for a flexible air-breathing hypersonic vehicle based on quasi-continuous high-order sliding mode

The focus of this paper is on control design and simulation for the longitudinal model of a flexible air-breathing hypersonic vehicle(FAHV).The model of interest includes flexibility effects and intricate couplings between the engine dynamics and flight dynamics.To overcome the analytical intractability of this model,a nominal control-oriented model is constructed for the purpose of feedback control design in the first place.Secondly,the multi-input multi-output(MIMO) quasi-continuous high-order sliding mode(HOSM) controller is proposed to track step changes in velocity and altitude,which is based on full state feedback.The simulation results are presented to verify the effectiveness of the proposed control strategy.     

战斗机编队协同作战效能评估研究

在分析了编队协同作战特点的基础上,利用层次分析方法建立了编队协同作战效能评估指标体系。重点研究了信息优势、决策能力、协同能力和攻击能力对编队协同作战效能影响,并建立了这四个指标的评估模型。接下来,利用成对比较矩阵计算出了准则层中各因素的权重系数。最后对分别红蓝编队协同空战的作战模式进行了作战效能仿真分析。

Abstract：

Based on the analysis of formation cooperative combat＇s characteristic,the effectiveness evaluation frame of formation cooperative combat was established by AHP. The factor that can influence the effectiveness of formation cooperative combat was emphatically studied. At the same time,the model of information predominance,decision-making capability,cooperative capability and attacking capability was established. Then,the weight of each factor was figured out by compare matrix. At last,the combat effectiveness evaluation of formation cooperative combat about red and blue was carried out.     

空中加受油仿真中尾流扰动的建模与仿真

对现代军机空中加受油仿真中的加油机尾流仿真进行了研究,论述了加油机尾流的组成流场、形成原因和对受油机的扰动作用。根据飞行试验数据资料和缜密的理论推导,将加油机尾流对受油机的扰动作用分为纵向和横向两个通道,并分别建立了空中加受油仿真的尾流扰动仿真模型,并给出了在实际工程应用中的调试方法。建立的加油机尾流扰动仿真模型在某型飞机飞行仿真系统应用中收到了很好的效果。     

基于ARENA的场站飞行保障过程建模与仿真

运用离散事件仿真(DES)方法建立了航空兵场站飞行保障过程的数学模型,包括单个保障类型Ack模型、和整个飞行保障过程的层次结构模型PRi,以及飞行保障过程仿真策略模型PS。并在所建的数学模型的框架下利用离散事件仿真软件ARENA对航空兵场站网络化飞行保障过程进行了仿真。仿真结果表明:网络化条件下的主动保障方式的保障时间可以比传统的被动保障方式的保障时间缩短4.3分钟,提高保障效率10.5%。     

飞行仿真模型库及虚拟样机建模环境的研究

飞行仿真模型库是飞行实时仿真系统研究的基础，仿真建模环境是为了让用户快速，方便地建立仿真所需的模型，并向外系统提供接口，从而使建模者和软件编制人员分开，本文论述了在飞行仿真模型库及虚拟样机建模环境方面的研究，介绍一个自行开发的具有良好的继承性和可扩充性的飞行仿真建模的软件开发环境，在飞行仿真模型库和建模环境的基础上，探讨了虚拟样机技术在飞机优化设计中的应用。     

基于Creator的飞行视景三维模型数据库优化技术

根据飞行视景仿真中三维建模的特点和要求,利用Creator强大的可视化建模功能和模型数据库优化技术,从调整模型数据库层级结构、减少模型复杂度和减小模型文件尺寸等几个方面着手,创建飞行视景仿真中所必需的飞机/导弹、座舱仪表和地形等典型对象的三维模型,在模型的复杂度和逼真度之间进行平衡,通过某飞行模拟训练系统软件开发中三维模型优化前后运行性能参数的对比,表明了优化建模的必要性和该建模技术在普通PC平台上支持飞行视景实时仿真的可行性.     

高超音速飞机模型的仿真研究

为了掌握高超音速飞机复杂的动态特性,提出了一种研究高超音速飞机模型的新方法.该方法采用MATLAB插值函数和S函数分别估算和建立高超音速飞机的气动参数及其六自由度的微分方程组,并在不同高度和速度下计算飞行的平衡点,然后通过比较平衡条件与约束条件,近似得到了整个飞行过程的飞行包线.仿真研究表明,该方法适合用在高超音速飞机模型上,仿真结果与期望要求相符合.     

用于飞行实时仿真的微下击暴流建模研究

分析了微下击暴流的特征和用于飞行实时仿真中的建模需求。基于流体力学的涡环原理构建三维微下击暴流的参数化模型,并对涡环法建模进行了深入改进。基于流体力学方法解决了涡环法模型的中心轴处和涡核内的奇异问题。针对真实微下击暴流风场的特点,设计了倾斜涡环模型和多涡环模型,从而高逼真度地模拟复杂的微下击暴流风场。简要讨论了该模型在飞行实时仿真中的应用方法。该建模方法灵活性高,可重配置,不仅可用于变化风场中的飞行实时仿真,还可用于对实际风场测量数据进行辨识建模和再现研究。     

基于PC的武装直升机编队飞行训练仿真系统

现有武装直升机飞行模拟训练设备价格昂贵、功能单一,因而其应用受到限制。为此,系统地研究了基于PC机和虚拟现实技术的武装直升机飞行仿真互联系统的关键技术,开发了基于PC机的武装直升机编队飞行训练仿真系统,为武装直升机编队飞行模拟训练及反坦克战术训练提供了一种经济实用的仿真训练手段。     

飞行模拟器综合导航系统建模与仿真

模拟器导航系统主要为飞行员提供模拟飞行中的位置及其航行参数并安全导引飞机沿既定航线飞行。结合航空仿真技术发展和全任务飞行模拟器样机的任务需求,在MATLAB/SIMULINK平台上构建了捷联惯导及基于区域导航法的无线电导航仿真模型。采用VAPS6.3制作出主飞行仪表,作为导航系统仿真的终端显示。利用RT-LAB平台构建分布式飞行仿真系统,实现导航外部特性的半实物仿真。经系统调试证明了该方法的有效性。     

分布式飞行仿真系统中的参数分布技术

详细研究了基于共享内存机制的分布式飞行仿真系统中仿真模块发布或定购参数时应该遵循的参数声明原则，并分析了仿真系统的参数发布区、参数定购区以及自定购区的构成与特点，最后给 各参数区的生成算法和一个简单易懂的例子。结合这些技术方法，并采用共享内存机制可以实现飞行仿真系统模块参数在节点间透明共享，从而可以实现分布式飞行仿真应用。     

全系统网络延迟分析方法

针对飞行仿真系统实时性要求高的特点,构建了以以太网、实时反射内存网及现场总线技术等多种技术为主的飞行仿真系统分布式网络结构。分析了影响系统延迟的因素及其改进的方法,提出并建立了以太网、实时反射内存网及现场总线技术的延迟计算的数学模型,并提出了一种综合估算全系统时间延迟的方法。这些方法在相关的产品研发中得以运用并取得很好的实时性效果。