某型反坦克导弹控制系统仿真实验研究  

Control System Simulation of an Anti-tank Missile

作　　者：郭希维[1] 赵慎[1,2] 何鹏[1] 

机构地区：[1]军械工程学院导弹工程系,石家庄050003 [2]国防科学技术大学机电工程与自动化学院,长沙410073

出　　处：《战术导弹技术》2015年第3期101-105,110,共6页Tactical Missile Technology

摘　　要：针对某型反坦克导弹高海拔条件下的飞行稳定性问题,采用攻角曲线仿真与频域特性分析相结合的方法,研究控制系统性能。根据导弹控制系统的组成,建立其仿真模型,并对积分方法、仿真时间、步长、初值等问题进行探讨,实现飞行过程中的攻角、高度变化规律仿真。结果表明,在高海拔条件下,导弹攻角呈发散趋势,控制系统表现出不稳定。通过分析控制系统参数,不稳定由空气密度下降引起,为适应高原改进设计提供依据。Aimed at the flight stability problem of an anti-tank missile at high altitudes,the performance of the control system is researched adopting a method combing simulation on the incidence angle curve and the frequency domain analysis. The model of the control system is established according to its composing,and the associate problems as integral method,simulation interval,simulation scale,and initial value are analyzed,to simulate the variation law of the incidence angle and gravity height center in flight.The result indicates that incidence angle tends to divergence,and the control system shows instability at high altitudes. The decreasing of air density leads to instability by investigating the control system parameters,which offers some improvement principles of the control system for high altitudes adaptation.

关 键 词：反坦克导弹 控制系统 频域特性分析 稳定性 

分 类 号：TJ765.233[兵器科学与技术—武器系统与运用工程]