Sliding mode friction observer based control for flexible spacecraft with reaction wheel-Reference-Cited by-同舟云学术

Sliding mode friction observer based control for flexible spacecraft with reaction wheel

Published:2017-05 Issue:8 Volume:11 Page:1274-1281
ISSN:1751-8652
Container-title:IET Control Theory & Applications
language:en
Short-container-title:IET Control Theory & Applications

Author:

Zhang Peixi¹,Qiao Jianzhong²³,Guo Lei²³,Li Wenshuo³

Affiliation:

1. School of Instrumentation Science and Opto‐Electronics Engineering, Beihang UniversityBeijing100191People's Republic of China

2. National Key Laboratory of Aircraft Control Technology, Beihang UniversityBeijing100191People'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

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.2016.0802

Reference46 articles.

1. Active vibration suppression in flexible spacecraft attitude tracking;Gennaro S.D.;J. Guid. Control Dyn.,1998

2. Vibration suppression of flexible spacecraft during attitude control

3. Nonsmooth attitude stabilization of a flexible spacecraft

4. Classical and robust H(infinity) control redesign for the Hubble Space Telescope

5. Modelling and testing of a soft suspension design for a reaction/momentum wheel assembly

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