Vibration Control of a Flexible Spacecraft System With Input Backlash

Vibration Control of a Flexible Spacecraft System With Input Backlash

In this paper, we deal with the vibration control problem of a flexible spacecraft system with unknown external disturbance and uncertain input backlash nonlinearity. The considered system is described by two partial differential equations and an ordinary differential equation as governing equations...

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Bibliographic Details
Main Authors: Zhiqiang Lin, Shimin Lin, Sen Wu, Ge Ma, Zhongwei Liang
Format: Article
Language:English
Published: IEEE 2019-01-01
Series:IEEE Access
Subjects:
Vibration control
adaptive control
flexible satellite
input backlash
Online Access:https://ieeexplore.ieee.org/document/8754765/

Internet

https://ieeexplore.ieee.org/document/8754765/

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