摘要
在全系数自适应控制方法基础上,利用低阶等效和规范化模型方法,对自寻的导弹制导系统设计了一种新的自校正控制器.数字仿真结果表明,这种控制器对自寻的导弹有很好的控制效果,而且控制器算法简单,具有较强的鲁棒性。
For the homing missile control system, based on the all - coefficient adaptive control method, presents a new self-tuning controller based on lower order equivalence and the normalized model method. Digital simulation results show that this controller is satisfactory for the homing missile and that it has simple algorithm and strong robustness.
出处
《北京理工大学学报》
EI
CAS
CSCD
1993年第1期64-68,共5页
Transactions of Beijing Institute of Technology
关键词
自适应控制
导弹制导
全系数法
adaptive control
guided missile guidance/low-order equivalence
normalized model
all-coefficient method
decentralized control
generalized minimum variance control