Composite anti‐disturbance attitude and vibration control for flexible spacecraft-Reference-Cited by-同舟云学术

Composite anti‐disturbance attitude and vibration control for flexible spacecraft

Published:2017-09 Issue:14 Volume:11 Page:2383-2390
ISSN:1751-8652
Container-title:IET Control Theory & Applications
language:en
Short-container-title:IET Control Theory & Applications

Author:

Sun Haibin¹,Hou Linlin²,Zong Guangdeng¹,Guo Lei³

Affiliation:

1. School of Engineering, Qufu Normal UniversityRizhao276826People's Republic of China

2. School of Information Science and Engineering, Qufu Normal UniversityRizhao276826People's Republic of China

3. School of Automation Science and Electrical Engineering, Beihang UniversityBeijing100191People's Republic of China

Funder

National Natural Science Foundation of China

Taishan Scholar Project of Shandong Province

Natural Science Foundation of Shandong Province

Postdoctoral Science Foundation of Jiangsu Province

Publisher

Institution of Engineering and Technology (IET)

Subject

Electrical and Electronic Engineering,Control and Optimization,Computer Science Applications,Human-Computer Interaction,Control and Systems Engineering

Link

https://onlinelibrary.wiley.com/doi/pdf/10.1049/iet-cta.2016.1225

Reference49 articles.

1. Output stabilization of flexible spacecraft with active vibration suppression

2. Attitude control without angular velocity measurement: a passivity approach

3. Optimal large‐angle attitude control of rigid spacecraft by momentum transfer;Yang C.C.;IET Control Theory Appl.,2007

4. Robust and optimal attitude stabilization of spacecraft with external disturbances

5. Geometric Approach to Spacecraft Attitude Control Using Magnetic and Mechanical Actuation

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