摘要
本文研究的内容属于多变量自适应控制技术范畴。从内部耦合结构出发,应用模型匹配方法和自适应技术,实现了线性时变强耦合对象的解耦控制,并证明了系统的稳定性和输出一致收敛性。具体设计了某型导弹的控制系统,进行了数字仿真和混合仿真。
The content of this paper belongs to multivariable adaptive control technique. The coupled structure is considered, we apply model-maching method and adaptive control technique to design the linear time-varing and strong coupled plant. The stability of adaptive systems and their output convergence are proved. Through digtal and hybrid stimulations the results demenstrate the control system design of a missile is practical.
出处
《宇航学报》
EI
CAS
CSCD
北大核心
1989年第4期79-86,共8页
Journal of Astronautics