机械制造与自动化Issue(6)：126-128,3.
多管火箭炮不同方向角发射动力学仿真分析
Simulation Analysis of Launch Dynamics for Multiple Rocket Launcher in Different Direction Angles
摘要
Abstract
The direction angle of multiple rocket launcher is changed along with the direction of vehicle body at the attack on fixed target. In order to improve firing intensity, the launching performance of the rocket launcher in different direction angles is studied. The dynamics model of multiple rocket launcher is built in Adams and the launching process in direction angle 0°,20°,40°and 60°is simulated respectively. The intermediate deviation of rocket initial disturbance is calculated, using the data from dynamic simulation. Contrastive analysis of simula-tion and calculation results in different direction angles show that both the directors’ vibration and the intermediate deviation of the rocket initial disturbance are reduced with the increase of the direction angle, and the firing intensity is improved.关键词
多管火箭炮/方向角/发射/动力学/仿真Key words
multiple rocket launcher/direction angle/launching/dynamcs/simulation分类
军事科技引用本文复制引用
陶声祥,凌帅..多管火箭炮不同方向角发射动力学仿真分析[J].机械制造与自动化,2014,(6):126-128,3.
