空空导弹控制系统的HLA仿真研究
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摘要
空空导弹研制涉及到空气动力学、材料、结构、导航制导与控制等多个仿真平台和专业领域,高层体系结构HLA(high level architecture)是新一代的分布式协同仿真结构,其分布式的结构使其能够充分利用局域网的计算机资源,使得各专业各领域的仿真都能够通过该平台进行交互。HLA技术实现了模型的重用和扩展,本文采用HLA技术实现空空导弹控制系统的HLA协同仿真,为导弹仿真系统整体设计与优化提供理论依据和技术支持。
     首先针对多学科、跨平台的HLA/RTI分布式仿真方法进行研究,研究该平台运行支撑环境中的联盟管理、声明管理、对象管理等机理。以组件的重用和可扩展为目标,分析构建分布式设计的优化协调技术与方法。然后以空空导弹、飞机为仿真对象,分析了导弹攻击空中目标仿真系统的功能,建立了空空导弹的HLA分布式仿真系统结构。
     分析研究了已有Simulink模型和HLA集成的方案,在空空导弹控制系统各功能模块需求和能力分析的基础上,为实现已有控制系统模型的重用和扩展,利用代码扩展法实现了控制系统的HLA转换;适配器方法的运用则实现了各联盟成员之间的数据交互。重点阐述了在VC++开发环境下,将Matlab/Simulink开发的空空导弹控制系统代码进行扩展的过程,以及通过MATLAB引擎实现控制器盟员和受控对象盟员的设计。通过HLA仿真验证系统的研究,使基于Matlab/Simulink开发的控制系统算法应用于分布式协同仿真中,与具有HLA接口的仿真模型进行交互。
Air-to-air missile involves in aerodynamics、materials、structure、guidance and control and many other simulation platforms and areas of expertise. High-level architecture HLA is a new generation co-simulation of distributed architecture and its distributed structure enable them to take full advantage of the LAN computer resources. Allowing simulation of various professional fields are able to interact through the platform. HLA technology implemented the component reusability and model expandability. Using HLA technology, the HLA co-simulation of air-to-air missile control system was achieved. And it provides a theoretical basis and technical support for missile simulation system design and optimization.
     First, the paper studied HLA distributed simulation ways of the multi-disciplinary and cross-platform. Federation management、declaration management and object management mechanism were studied in the Run-time Infrastructure . With the target of the component reusability and expandability, the optimization of the coordination of technology and methods of building distributed design were analyzed. Then air-to-air missiles、plane were main simulation objects and the functions of missile attacking air target simulation system was analyzed. HLA distributed simulation system architecture of air-to-air missiles was established.
     Based on the analysis of air-to-air missile control system function modules' demand and ability, the paper analyzed and researched the integrated solutions of existing simulink models to HLA. In order to achieve the reuse of existing control system model and expansion, code extension method was used to achieve the control system HLA conversion. Adapter method was used to accomplish the data exchange among members. The paper described emphatically the process of code expansion of the Matlab / Simulink development of air to air missile control system in the VC + + development environment, and the design of controller federate and controlled object federate were achieved through the MATLAB engine. By studying the HLA simulation system, Matlab / Simulink control system algorithm was applied to the development of distributed collaborative simulation, and the interaction was achieved among simulation models with HLA interface to interact.
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