摘要
针对某航空弹药飞行特点,在采用传统的 PID 控制器设计方法的基础上,引入一种自适应控制系统方案。该方案采用合理的自适应律,对稳定回路的反馈控制参数进行在线调整,使系统的动态性能和稳态精度满足设计要求。数学仿真表明,在简化模型基础上设计的 PID+自适应控制器,可以应用于非线性复杂弹体的制导与控制系统中。
According to the flight characteristic of air ammunition and on the basis of designing classical PID controller, this paper puts forward a kind of adaptive control system scheme.This scheme adopting right adaptivc law.adjusts the feedback control parameters in stable control system loop on line,and make the system s dynamic performance and steady state precision meeting the requirements of design.The digital simulation is provided to indicate that the PID adaptive controller designed on the basis of simplif...
出处
《弹箭与制导学报》
CSCD
北大核心
2004年第S2期253-255,共3页
Journal of Projectiles,Rockets,Missiles and Guidance