Robust attitude control of a flexible satellite assembled with a partially expanded coilable mast-Reference-Cited by-同舟云学术

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Robust attitude control of a flexible satellite assembled with a partially expanded coilable mast

Published:2024-05 Issue: Volume:148 Page:109093
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Fan Liming^ORCID,Xing Yanjun,He Zongbo,Zhang Qiang,Chen Zeming

Publisher

Elsevier BV

Reference36 articles.

1. Spacecraft reorientation control in presence of attitude constraint considering input saturation and stochastic disturbance;Cheng;Acta Astronaut.,2018

2. Saturated attitude control for rigid body under input delay and pointing constraints;Xu;Aerosp. Sci. Technol.,2022

3. Design of a controller for a rigid-flexible satellite using the H-infinity method considering the parametric uncertainty;Souza;Mech. Syst. Signal Process.,2019

4. Intelligent neural integral sliding-mode controller for a space robotic manipulator mounted on a free-floating satellite;Delgado;Adv. Space Res.,2023

5. A deep learning based data-driven thruster fault diagnosis approach for satellite attitude control system;Xiao;IEEE Trans. Ind. Electron.,2021

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