Non-fragile negative imaginary output feedback control for attitude stabilization of flexible spacecraft-Reference-Cited by-同舟云学术

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Non-fragile negative imaginary output feedback control for attitude stabilization of flexible spacecraft

Published:2023-07 Issue: Volume:208 Page:296-310
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Yang Ziyu,Liu Chuang^ORCID,Yue Xiaokui,Guo Ming

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference40 articles.

1. Modeling and observer-based vibration control of a flexible spacecraft with external disturbances;Liu;IEEE Trans. Ind. Electron.,2018

2. Agile attitude maneuver with active vibration-suppression for flexible spacecraft;Zhang;J. Franklin Inst.,2022

3. Robust fixed-time attitude stabilization control of flexible spacecraft with actuator uncertainty;Cao;Nonlinear Dyn.,2020

4. Coupled orbit-attitude dynamics and trajectory tracking control for spacecraft electromagnetic docking;Shi;Appl. Mathmat. Model.,2022

5. Rotation-matrix-based attitude tracking for multiple flexible spacecraft with actuator faults;Chen;J. Guid. Control Dyn.,2019

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1. Vibration model analysis and all-modal control of a rigid–flexible satellite in large-range planar motion;Journal of Vibration and Control;2024-06-20

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