首页 | 本学科首页   官方微博 | 高级检索  
     检索      

基于Simulink的子导弹全弹道仿真
引用本文:杨艳明,唐胜景.基于Simulink的子导弹全弹道仿真[J].系统仿真学报,2006,18(6):1442-1444,1449.
作者姓名:杨艳明  唐胜景
作者单位:北京理工大学,机电工程学院,北京,100081
摘    要:在MATLAB/Simulink环境下,针对子导弹武器系统,应用全弹道建模方法开发了包括运动学与动力学模块、制导与控制系统模块,弹目相对运动模块等组成的仿真系统数学模型,进行了全弹道数字仿真。仿真实验表明,该仿真系统较好的模拟了子导弹的飞行弹道,为子导弹武器系统的开发研制提供了必要的仿真工具。

关 键 词:系统模型  弹道仿真  子导弹
文章编号:1004-731X(2006)06-1442-03
收稿时间:2005-04-07
修稿时间:2005-04-072006-01-13

Trajectory Simulation of Submunitions Based on Simulink
YANG Yan-ming,TANG Sheng-jing.Trajectory Simulation of Submunitions Based on Simulink[J].Journal of System Simulation,2006,18(6):1442-1444,1449.
Authors:YANG Yan-ming  TANG Sheng-jing
Institution:School of Mechatronic Engineering, Beijing Institute of Technology, Beijing 100081, China
Abstract:According to a submuniton weapon system, a simulation system mathematical model was developed in Matlab/ Simulink environment based on the whole trajectory modeling method, including kinematic and dynamic model, guidance system model, control system model, missile-target relative movement model and so on. And the simulation of the whole trajectory was made. Simulations show that the flight trajectory of the submunition can be simulated preferably by means of this system, and the necessary simulating tool in the development of the submunition system can be delivered.
Keywords:Simulink
本文献已被 CNKI 维普 万方数据 等数据库收录!
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号