期刊文献+

基于Simulink和HLA的导弹制导控制系统仿真 被引量:2

Missile Guidance Control System Simulation Based on HLA and Simulink
下载PDF
导出
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。 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 for digital simulation test, but also can be extended to the hardware-in-the-loop simulation test of missile's stabilization control system. This method proposed in this paper has high engineering practice value.
出处 《弹箭与制导学报》 CSCD 北大核心 2010年第5期13-16,共4页 Journal of Projectiles,Rockets,Missiles and Guidance
基金 国防基础科研基金(A2420061104-06)资助
关键词 导弹稳定控制系统 导弹制导 HLA SIMULINK missile stabilization control system missile guidance HLA Simulink
  • 相关文献

参考文献4

二级参考文献6

共引文献28

同被引文献14

引证文献2

二级引证文献4

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部