摘要
采用一种独特的 PI 控制律,它可以显著改善,飞行器的飞行控制性能。该控制律的参数确定建立在飞行器的采样阶跃响应矩阵的基础上。仿真结果表明,此方法应用于飞行器的自适应控制系统,其控制效果是令人满意的。
This paper puts forward a kind of PI control law that might improve the flight control performances of aerocrafts remarkably.The determinate of this PI control law′s parameters is based on the sampling step response matrix of aerocrafts.Finally the control effect of this project is demonstrated by simulation,and the effect is satisfied.
出处
《弹箭与制导学报》
CSCD
北大核心
2003年第S2期101-102,共2页
Journal of Projectiles,Rockets,Missiles and Guidance
基金
国防科技预研基金(编号:51404030201JB2201)
