摘要
针对最小相位高超音速飞行器非线性系统的调节器方程无法求出解析解的情况,提出利用三层神经网络来近似输出反馈控制器中的前馈函数的方法,得到基于神经网络的输出反馈控制器可以解决高超音速飞行器系统的跟踪控制问题的结论.
In view of the fact that the regulator equation of non-minimum phase hypersonic vehicle nonlinear system cannot be solved analytically,a method of using a three-layer neural network to approximate the feedforward function in the output feedback controller is proposed,and it is obtained that the output feedback controller based on the neural network can solve the tracking control problem of hypersonic vehicle systems.
作者
游茜
陈晓锋
苏友峰
YOU Xi;CHEN Xiaofeng;SU Youfeng(College of Mathematics and Computer Science,Fuzhou University,Fuzhou,Fujian 350108,China)
出处
《福州大学学报(自然科学版)》
CAS
北大核心
2021年第2期143-148,共6页
Journal of Fuzhou University(Natural Science Edition)
基金
国家自然科学基金面上资助项目(61773122)。
关键词
高超音速飞行器
跟踪控制
神经网络
输出反馈
hypersonic vehicle
tracking control
neural network
output feedback control