Predictor-Based Control for a Flexible Satellite Subject to Output Time Delay
This article investigates a flexible satellite consisting of a central hub and two flexible solar panels. Different from previous control works, the output time delay is considered in vibration control for the satellite, whose model is more complex and strongly coupled. For dealing with output time...
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Published in | IEEE transactions on control systems technology Vol. 30; no. 4; pp. 1420 - 1432 |
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Main Authors | , , , |
Format | Journal Article |
Language | English |
Published |
New York
IEEE
01.07.2022
The Institute of Electrical and Electronics Engineers, Inc. (IEEE) |
Subjects | |
Online Access | Get full text |
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Summary: | This article investigates a flexible satellite consisting of a central hub and two flexible solar panels. Different from previous control works, the output time delay is considered in vibration control for the satellite, whose model is more complex and strongly coupled. For dealing with output time delay, a compensated strategy based on a Luenberger observer and a predictor is developed to obtain the estimation of the current state. Then, a predictor-based control law is proposed to eliminate the vibration of flexible solar panels. Finally, the stability of the closed-loop system is analyzed by Lyapunov's direct method, and simulation results are given to demonstrate the efficiency of the developed method. |
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Bibliography: | ObjectType-Article-1 SourceType-Scholarly Journals-1 ObjectType-Feature-2 content type line 14 |
ISSN: | 1063-6536 1558-0865 |
DOI: | 10.1109/TCST.2021.3109270 |