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炮射导弹反武装直升机可行性仿真研究
引用本文:王狂飙,张天桥.炮射导弹反武装直升机可行性仿真研究[J].北京理工大学学报(英文版),2001,10(1):75-80.
作者姓名:王狂飙  张天桥
作者单位:北京理工大学 机电工程学院,
基金项目:MinisterialLevelAdvancedResearchFoundation
摘    要:研究通过炮射反坦克导弹赋予坦克有限反武装直升机能力的可行性 .建立了一种炮射导弹与武装直升机对抗的仿真模型 ,并在各种情况下进行了系统仿真与导弹控制系统参数优化 .经参数优化的炮射导弹在给定的武装直升机各种航迹下 ,均可直接命中 ,脱靶量均小于 1m ,最大过载不超过可用过载 .仿真结果表明炮射导弹是坦克对抗武装直升机的一种可行的选择 .

关 键 词:炮射导弹  武装直升机  旋转导弹  驾束制导  仿真  控制系统
收稿时间:2000/2/23 0:00:00

Simulation Study on the Feasibility of Gun-Launched Missile Against Attack Helicopters
WANG Kuang biao and ZHANG Tian qiao.Simulation Study on the Feasibility of Gun-Launched Missile Against Attack Helicopters[J].Journal of Beijing Institute of Technology,2001,10(1):75-80.
Authors:WANG Kuang biao and ZHANG Tian qiao
Affiliation:School of Mechano Electronics Engineering, Beijing Institute of Technology, Beijing100081, China;School of Mechano Electronics Engineering, Beijing Institute of Technology, Beijing100081, China
Abstract:The feasibility of providing the tank a limited anti helicopter ability with gun launched missile is studied. A type of simulation model of gun launched missile against attack helicopters is established. The simulation and the parameter optimization of missile control system under various circumstances are done. The gun launched missile can directly hit the helicopters in the typical tracks, all the missdistances are less than 1?m and the maximum overload is less than available overload. Gun launched missile is a feasible choice for tanks against attack helicopters.
Keywords:gun  launched missile  attack helicopters  rolling missile  beam riding guidance  simulaion  control system
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