火箭弹简易控制系统分析  

Study and Analysis of the Simple Control System of a Rocket

作　　者：孟秀云[1] 刘藻珍[1] 邹静涛[1] 

机构地区：[1]北京理工大学,北京100081

出　　处：《弹箭与制导学报》2001年第4期60-62,79,共4页Journal of Projectiles,Rockets,Missiles and Guidance

摘　　要：简单概述了目前火箭弹武器所采用的简易控制系统的特点 ,分析了火箭弹简易控制系统总体方案的设计思想及设计依据。对姿态控制系统方案、系统特点以及姿态控制系统敏感元件及执行机构的选择依据进行了详细分析 。The features of the simple control system adopted by some rocket weapon system are simply summarized. First the design idea and basis of system concept of a simple control rocket is analyzed. Then the system plan, the features of attitude control system, the select principle of measurement element and actuating mechanism are detailed analyzed. Finally the design principle of the range correction system is simply analyzed.

关 键 词：火箭弹 姿态控制系统 距离修正系统 敏感分件 执行机构 

分 类 号：TJ415[兵器科学与技术—火炮、自动武器与弹药工程]