Adaptive predefined-time control for liquid-filled flexible spacecraft attitude stabilization during orbit maneuver-Reference-Cited by-同舟云学术

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Adaptive predefined-time control for liquid-filled flexible spacecraft attitude stabilization during orbit maneuver

Published:2023-03 Issue:6 Volume:71 Page:2733-2744
ISSN:0273-1177
Container-title:Advances in Space Research
language:en
Short-container-title:Advances in Space Research

Author:

Sun Yue,Lyu Yueyong,Guo Yanning,Gong Youmin,Zhu He

Funder

National Natural Science Foundation of China

National Key Research and Development Program of China

Publisher

Elsevier BV

Subject

Space and Planetary Science,Aerospace Engineering,General Earth and Planetary Sciences,Atmospheric Science,Geophysics,Astronomy and Astrophysics

Reference42 articles.

1. Model predictive sliding control for finite-time three-axis spacecraft attitude tracking;Bayat;IEEE Trans. Industr. Electron.,2018

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

3. Adaptive fuzzy mixed H2/H∞ attitude control of spacecraft;Chen;IEEE Trans. Aerosp. Electron. Syst.,2000

4. Robust spacecraft attitude tracking control with integral terminal sliding mode surface considering input saturation;Chen;Trans. Inst. Measur. Control,2019

5. Fixed-time attitude stabilization for a rigid spacecraft;Du;ISA Trans.,2020

Cited by 6 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Neural network observer-based predefined-time attitude control for morphing hypersonic vehicles;Aerospace Science and Technology;2024-09

2. Prescribed modal vibration control and disturbance load analysis of rigid-flexible satellites;Advances in Space Research;2024-08

3. Predefined-time sliding mode attitude control for liquid-filled spacecraft with large amplitude sloshing;European Journal of Control;2024-05

4. Neural Network Observer-Based Predefined-Time Attitude Control for Morphing Hypersonic Vehicles;2024

5. Cascade nonlinear observer design for large amplitude of slosh variables in spacecraft maneuver with liquid propellant tank;Acta Astronautica;2023-12

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