期刊文献+

基于HLA的火箭自导深弹仿真系统研究 被引量:2

Study on HLA Simulation System of Rocket Homing Depth Charge
下载PDF
导出
摘要 为了研究火箭自导深弹的作战效能以及作战使用方法,通过分析德国"海矛"火箭自导深弹的攻潜过程,根据公开报道的参数和一般性的假设,建立了水面舰艇使用火箭自导深弹攻潜的数学模型,实现了基于HLA框架的模块化火箭自导深弹全数字仿真系统。该仿真系统以Visual C++6.0作为软件开发架构,应用联邦开发技术构建HLA联邦成员间的信息交互,采用Malab/Simulink作为计算引擎来解算探测效果、攻潜弹道以及潜艇与深弹的运动态势,利用Open GL和3D Studio MAX实现了火箭自导深弹攻潜过程的三维实景可视化显示,并对仿真态势与结果进行存盘与复盘。仿真结果显示,所建立的仿真系统能够满足研究火箭自导深弹作战效能的需求,可为该装备的作战使用、总体技术研究提供支撑。 To study on the operational effectiveness and operational use method of the rocket homing depth charge such as “Seapike”, a modularized HLA all-digital simulation system was established through going into analyzing every phase of the weapon's anti-sub procedure. The simulation system took Visual C++6.0 as software development framework, adopted federal development technology to realize information exchange between federal members, used Matlab/Simulink to calculate ballistic parameters, used OpenGL and 3D Studio MAX to realize 3D scene visualization. The simulation results in the case of representative condition show that the simulation system can meet the requirement of calculating the weapon's operational effectiveness and lay a solid foundation to study the new anti-sub weapon's operational use method and overall technology.
机构地区 海军装备研究院
出处 《系统仿真学报》 CAS CSCD 北大核心 2014年第12期2874-2881,共8页 Journal of System Simulation
基金 国家自然科学基金项目资助(60902071)
关键词 火箭自导深弹 HLA 仿真系统 模块化 可视化 rocket homing depth charge HLA simulation system modularized visualization
  • 相关文献

参考文献6

二级参考文献24

  • 1High level architecture run-time infrastructure programner' s guide[DB/OL]. DMSO, 1999
  • 2Federation development and execution process(FEDEP) model, Version1.4[DB/OL]. http://www. dmso. mil
  • 3High level architecture interface specification, Version1.3[DB/OL].http://www. dmso. mil
  • 4龚光红.DIS环境下的计算机生成兵力研究[D].北京:北京航空航天大学自动化科学与电气工程学院,1999Gong Guanghong. Computer generated forces research in DIS environment[D]. Beijing: School of Automation Science and Electrical Engineering, Beijing Univemity of Aeronautics and Astronautics,1997( in Chinese)
  • 5张青斌.载人飞船降落伞回收系统动力学研究[D].长沙:国防科学技术大学,2003.
  • 6Cockrell D J,Haidar N I A.Influence of the canopy-payload coupling on the dynamic stability in pitch of a parachute system[J].AIAA93-1248.
  • 7Fallon I.Parachute dynamics and stability analysis of the queen match recovery systems[J].AIAA91-0879.
  • 8Botton W R.Trajectory simulation of parachute system[J].AIAA74-0470.
  • 9Tory C.Computer model of a fully deployed parachute[J].J Aircraft,1977,14(7):675-679.
  • 10White F M,Wolf D F.A theory of three dimensional parachute dynamic stability[J].Aircraft,1968,5(1):86-92.

共引文献63

同被引文献11

引证文献2

二级引证文献2

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