Composite Control of Attitude Tracking and Vibration Suppression of a Rigid–Flexible Coupled System-Reference-Cited by-同舟云学术

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Composite Control of Attitude Tracking and Vibration Suppression of a Rigid–Flexible Coupled System

Published:2021-07 Issue:4 Volume:34 Page:
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Jin Qibao¹^ORCID,Yuan Jianping²,Li Yinghua³

Affiliation:

1. Associate Professor, School of Mechanical and Power Engineering, Guangdong Ocean Univ., Zhanjiang 524088, China (corresponding author). ORCID: .

2. Professor, School of Ocean Engineering, Guangdong Ocean Univ., Zhanjiang 524088, China.

3. Associate Professor, School of mathematics and computer science, Guangdong Ocean Univ., Zhanjiang 524088, China.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0001256

Reference11 articles.

1. A hybrid control scheme for attitude and vibration suppression of a flexible spacecraft using energy-based actuators switching mechanism

2. Passive Attitude Control of Flexible Spacecraft from Quaternion Measurements

3. Dynamics of flexible multibody systems with variable-speed control moment gyroscopes

4. Vibration suppression of flexible spacecraft during attitude maneuver using CMGs

5. Precision Spacecraft Pointing Using Single-Gimbal Control Moment Gyroscopes with Disturbance

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