应急辅助定位及精度评估方法研究

在可视导航卫星数少于四颗、无法进行传统导航解算的恶劣环境下,导航接收机可利用外部高程气压计提供的高程或者内部守时模块的钟差等信息进行应急辅助定位。在该应急辅助定位工作模式的误差分析中,传统导航定位误差传递模型无法适用。针对此问题,本文在研究三星结合高程、三星结合钟差、双星结合高程钟差等几种应急辅助定位原理的基础上,给出了新的应急辅助定位误差传递的分析模型,利用仿真算例验证了该模型的正确性。通过对定位精度的分析,说明根据卫星分布特点可以按照本文方法量化得到伪距测量与辅助信息的精度的最优数量级关系,可以用最小代价实现定位精度的提升。该结论可指导接收机外部辅助器件的选择。     

基于功能角色模型的反馈系统故障模式影响分析

从系统功能设计过程出发,在分析反馈系统工作原理及其功能角色模型构造特点的基础上,认为反馈信号在输入端可等效为正、负、零三种误差信号。以此为基础,提出了反馈系统基于该理论的故障传播分析方法和技术。最后以飞机发动机燃料计量系统为例,阐述该方法在反馈系统中应用的可行性。经案例分析表明,该方法可以比较有效地解决一类带反馈环的故障分析问题,大大提高了功能角色模型的应用范围。     

FLAMES仿真系统中目标毁伤仿真的实现

为了构建FLAMES中的目标毁伤仿真系统,在对FLAMES仿真系统体系结构分析的基础上,通过研究FLAMES中目标毁伤仿真的相关模型、函数及计算方法,归纳出目标毁伤仿真的实现流程。最后以飞机轰炸停机坪目标的毁伤计算为例,具体实现了FLAMES中的目标毁伤仿真。     

Automated integration of real-time and non-real-time defense systems

Various application domains require the integration of distributed real-time or near-real-time systems with non-real-time systems.Smart cities,smart homes,ambient intelligent systems,or network-centric defense systems are among these application domains.Data Distribution Service(DDS)is a communi-cation mechanism based on Data-Centric Publish-Subscribe(DCPS)model.It is used for distributed systems with real-time operational constraints.Java Message Service(JMS)is a messaging standard for enterprise systems using Service Oriented Architecture(SOA)for non-real-time operations.JMS allows Java programs to exchange messages in a loosely coupled fashion.JMS also supports sending and receiving messages using a messaging queue and a publish-subscribe interface.In this article,we pro-pose an architecture enabling the automated integration of distributed real-time and non-real-time systems.We test our proposed architecture using a distributed Command,Control,Communications,Computers,and Intelligence(C4I)system.The system has DDS-based real-time Combat Management System components deployed to naval warships,and SOA-based non-real-time Command and Control components used at headquarters.The proposed solution enables the exchange of data between these two systems efficiently.We compare the proposed solution with a similar study.Our solution is superior in terms of automation support,ease of implementation,scalability,and performance.     

基于系统动力学的导弹体系作战效能仿真研究

简要介绍了系统动力学的概念;分析了导弹作战体系的构成以及各子系统对体系的贡献效能;针对导弹体系对抗作战效能仿真,运用系统动力学方法,建立了导弹体系对抗的系统动力学模型;并对在不同对策条件下的仿真结果进行了分析,为导弹体系结构优化、体系能力的提高提供了依据。     

基于数值SEA算法的反潜C3I系统效能分析

在分析了反潜C3I效能指标的基础上,采用数值SEA逼近算法求解反潜C3I使命轨迹和系统效能度量,建立了反潜C3I的SEA效能分析模型,并给出了系统效能指标灵敏度与关联度分析模型.     

无人炮塔系统关键技术组合分析

无人炮塔系统是未来火力系统发展的方向,在坦克和装甲车辆炮塔部分被命中概率高的现实情况下,无人炮塔对乘员来说相对安全。文章初步分析了无人炮塔系统的关键技术——遥控火炮技术和自动输弹技术实现的可能性和途径,并且针对在相同底盘上配置更大威力火炮的要求,探讨了膨胀波技术在无人炮塔上的应用。     

仿真系统可信度分析

系统仿真可信度研究是合理利用系统仿真结果的前提。分析了系统仿真可信度的研究现状,提出了利用层次分析法进行可信度评估的思路,阐述了仿真试验结果与飞行试验结果进行静态一致性检验和动态一致性检验的方法。讨论了静态一致性检验的置信度,给出了置信度与弃真概率和采伪概率的关系,为提高和考核系统仿真精度奠定了基础。     

基于数据分发服务的无人机任务载荷综合仿真平台研究

现代无人机在军用、民用等领域都有着越来越广泛的应用,而载荷是无人机完成特定重要任务的必要设备,对载荷设备的选型和验证是非常重要的一个环节.针对无人机载荷选型以及载荷试验过程复杂、试验周期长、试验成本高的问题,设计了一种基于数据分发服务通信技术的无人机任务载荷综合仿真平台.该平台以载荷仿真为主体,同时结合任务仿真、通信仿...     

Modeling and simulation of muzzle flow field of railgun with metal vapor and arc

During the electromagnetic railgun launching process, there will be a complex flow field with high temperature in the muzzle area because of the high-speed friction, transition and secondary arc-ignition. This paper models the muzzle area of railgun when the projectile is far away from the muzzle, and the dynamic simulation of the flow field with secondary arc in the muzzle area is carried out based on the magneto hydrodynamic equations. Meanwhile, a multi-component plasma transport model is used to analyze the muzzle arc plasma flow process of the mixed gas of Al vapor and the air. Furthermore, the pressure boundary conditions are fitted by the dynamic mesh simulation results. The current and voltage of the muzzle are obtained through the emission experiment of the railgun experimental prototype. We load the current data into the simulation model and the voltage of experiments and simulations are compared, which proves the accuracy of the simulation. Then the plasma temperature and the composition of Al vapor in the muzzle flow process are analyzed in-depth.