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基于Simulink和HLA的导弹制导控制系统仿真
引用本文:陈涛,张文翰,郭立民,张国耀. 基于Simulink和HLA的导弹制导控制系统仿真[J]. 弹箭与制导学报, 2010, 30(5)
作者姓名:陈涛  张文翰  郭立民  张国耀
作者单位:哈尔滨工程大学信息与通信工程学院,哈尔滨,150001
基金项目:国防基础科研基金(A2420061104-06)资助
摘    要:为解决基于Simulink的导弹稳定控制系统仿真实时性与交互性问题,文中充分融合Simulink和C++语言的优点,利用Simulink和C++混合编程技术完成导弹制导控制仿真系统模型的建立;并依据HLA标准将仿真系统改造成一个可与外界交互的联邦成员,最终实现了基于HLA的可视化的数字仿真试验平台。该系统既可用于全数字仿真,也可经扩展后,进行导弹稳定控制系统的半实物仿真试验,有很好的工程实用价值。

关 键 词:导弹稳定控制系统  导弹制导  HLA  Simulink  

Missile Guidance Control System Simulation Based on HLA and Simulink
CHEN Tao,ZHANG Wenhan,GUO Limin,ZHANG Guoyao. Missile Guidance Control System Simulation Based on HLA and Simulink[J]. Journal of Projectiles Rockets Missiles and Guidance, 2010, 30(5)
Authors:CHEN Tao  ZHANG Wenhan  GUO Limin  ZHANG Guoyao
Affiliation:CHEN Tao,ZHANG Wenhan,GUO Limin,ZHANG Guoyao (College of Information , Communication Engineering,Harbin Engineering University,Harbin 150001,China)
Abstract:In order to resolve issues including lack of real-time and interaction of missile stabilization control system based on Simulink tools,the simulation system was completed by use of Simulink and C++mixed programming technique which can combine the merits of these two language tools.The control model was transformed into a member of the federation which can interact with the other members based on HLA,so the high-level visual simulation testing system was realized based on HLA.Not only is this system suitable...
Keywords:missile stabilization control system  missile guidance  HLA  Simulink  
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