地地战术导弹制导控制系统仿真  

Simulation of Control and Guidance System of Surface-to-surface Tactical Missile

作　　者：肖宝亮[1] 赵成旺[1] 霍隽秀[1] 

机构地区：[1]炮兵指挥学院,河北廊坊065000

出　　处：《战术导弹技术》2009年第6期80-84,共5页Tactical Missile Technology

摘　　要：建立了包括外弹道、内弹道和控制系统在内的导弹制导控制系统数学模型,用数值积分法将数学模型转化为计算机程序,仿真了导弹飞行过程中的制导与控制.仿真曲线、数据与地面试验和靶场飞行试验结果的对比分析,验证了仿真模型的正确有效性.Modeling of the control system for the missile including outer ballistic trajectory and inner ballistic trajectory is proposed,the model is converted into program with integral,and the navigation and control of flight phase is simulated.Compared with ground experiment and flight experiment results,the simulation result demonstrates the effectiveness of the model.

关 键 词：战术导弹 制导控制 仿真 模型 

分 类 号：TJ765.4[兵器科学与技术—武器系统与运用工程]