摘要
本文基于现代控制理论对飞机横航向控制律设计进行研究,运用具有工程意义的线性二次型最优控制方法、特征结构配置方法和动态逆方法,通过状态反馈,得到飞机横航向反馈控制律,并对其进行仿真与验证。
On the basis of modern control theory,this paper studies the design of the aircraft's control law in lateral heading by means of linear quadratic optimal control method with engineering significance,eigenstructure assignment and dynamic inversion approach.The aircraft's control law in lateral heading is obtained via status feedback for simulation and verification.
作者
刘诗超
翁雪花
邹俊俊
冷国旗
Liu Shichao;Weng Xuehua;Zou Junjun;Leng Guoqi(Military Representative Office of Naval Equipment Department in Nanchang,Nanchang,Jiangxi,330024;AVIC Hongdu,Nanchang,Jiangxi,330024)
出处
《教练机》
2021年第2期22-26,共5页
Trainer
关键词
现代控制理论
最优控制
特征结构配置
动态逆
横航向控制律
SIMULINK仿真
Modern control theory
Optimal control
eigenstructure assignment
Dynamic inversion
Control law in lateral heading
Simulink simulation
