导弹姿态控制发动机仿真模型研究  

Investigation of Simulating Models of Attitude Cotrol Motors for a Missile

作　　者：康长赓[1] 刘新民[1] 

机构地区：[1]北京理工大学机电控制工程系,北京100081

出　　处：《弹箭与制导学报》2001年第1期1-4,共4页Journal of Projectiles,Rockets,Missiles and Guidance

摘　　要：通过对某型导弹的姿态控制发动机模型及其在数字仿真中的实现进行研究。介绍了包括等效合力和旋转力的两种实用模型 ,给出模型的实现方法。数字仿真结果表明给出的旋转力模型较接近 ACM的实际工作过程 。A major motivation for this article is to investigate attitude control motor models of some kind of missile and achievement in digital simulations. Both of pragmatic models including equivalent combined forces model and rotating force model were presented, achieving methods of models in use were given. Results of digital simulation show that the model of rotating forces described in this paper more approach the practical work process of attitude control motors, and can be applied in simulating research with a controller on line.

关 键 词：导弹 模型 姿态控制发动机 仿真 旋转力 ACM 

分 类 号：TJ765.23[兵器科学与技术—武器系统与运用工程] TJ765.2