Design of Eccentric Mass-Type Vibration-Damping Electric Actuator Control System for Non-Fixed-Wing Aircraft

Design of Eccentric Mass-Type Vibration-Damping Electric Actuator Control System for Non-Fixed-Wing Aircraft

The main spiral blade of non-fixed wing aircraft will produce periodic vibration force when rotating, which will not only reduce the service life of airborne equipment, but also greatly affect the working state of pilots. Due to the narrow damping band of passive damping device, it is difficult to m...

Full description

Bibliographic Details
Main Authors: Zhenyang Hao, Tao Wang, Xin Cao, Qiyao Zhang
Format: Article
Language:English
Published: IEEE 2020-01-01
Series:IEEE Access
Subjects:
Active vibration damping control
gear clearance
controller parameters
sensitivity <italic xmlns:ali="http://www.niso.org/schemas/ali/1.0/" xmlns:mml="http://www.w3.org/1998/Math/MathML" xmlns:xlink="http://www.w3.org/1999/xlink" xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance">H</italic>∞ control
robustness
Online Access:https://ieeexplore.ieee.org/document/9284434/

Internet

https://ieeexplore.ieee.org/document/9284434/

Similar Items