Numerical Research on The Stability of Launching Devices During Firing

被引：0
|
作者：
Pamfil ?OMOIAG [1 ]
Cristian-Emil MOLDOVEANU [1 ]
机构：
[1] Department of Weapon Systems Engineering and Mechatronics,Military Technical Academy
来源：
Defence Technology | 2013年 / 04期
关键词：
Launching device; Unguided rocket; Oscillations; Vehicle chassis; Tilting platform; Mathematical model;
D O I：
暂无
中图分类号：
TJ768 [发射设施];
学科分类号：
082501 ; 082601 ; 082602 ;
摘要：
An important problem in studying the sloped rocket launch is to determine the oscillations and their effects on the initial conditions of the rocket path.This phenomenon influences the stability of the launching device and the firing precision.It is assumed that the launching device and the moving rocket form a complex oscillating system that join together into a sum of rigid bodies bound by elastic elements(the vehicle chassis,the tilting platform and the rockets in the containers).The calculations of the launching device oscillations during the launch by numerical methods are presented.
引用
收藏
页码：242 / 248
页数：7
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