A High-Order Load Model and the Control Algorithm for an Aerospace Electro-Hydraulic Actuator

It is difficult to describe precisely, and thus control satisfactorily, the dynamics of an electro-hydraulic actuator to drive a high thrust liquid launcher engine, whose structural resonant frequency is usually low due to its heavy inertia and complicated mass distribution, let alone one to drive a...

Full description

Bibliographic Details
Main Authors: Shoujun Zhao, Keqin Chen, Xiaosha Zhang, Yingxin Zhao, Guanghui Jing, Chuanwei Yin, Xue Xiao
Format: Article
Language:English
Published: MDPI AG 2021-03-01
Series:Actuators
Subjects:
Online Access:https://www.mdpi.com/2076-0825/10/3/53