Finite-Time Attitude Tracking Control of Rigid Spacecraft With Multiple Constraints-Reference-Cited by-同舟云学术

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Finite-Time Attitude Tracking Control of Rigid Spacecraft With Multiple Constraints

Published:2024-06 Issue:3 Volume:60 Page:3688-3697
ISSN:0018-9251
Container-title:IEEE Transactions on Aerospace and Electronic Systems
language:
Short-container-title:IEEE Trans. Aerosp. Electron. Syst.

Author:

Yang Xue-Rong¹^ORCID,Lin Xiuxiu²^ORCID,Yang Yajun³^ORCID,Zou An-Min²^ORCID

Affiliation:

1. School of Aeronautics and Astronautics, Sun Yat-sen University, Shenzhen, China

2. College of Engineering and the Key Laboratory of Intelligent Manufacturing Technology, Ministry of Education, Shantou University, Shantou, China

3. China Aerospace Science and Industry Corporation, Guizhou Aerospace Fenghua Precision Equipment Company Ltd., Guiyang, China

Funder

Basic and Applied Basic Research Foundation of Guangdong Province

Publisher

Institute of Electrical and Electronics Engineers (IEEE)

Link

http://xplorestaging.ieee.org/ielx7/7/10552647/10413596.pdf?arnumber=10413596

Reference32 articles.

1. Adaptive tracking control using synthesized velocity from attitude measurements

2. Unit Quaternion-Based Output Feedback for the Attitude Tracking Problem

3. Fixed-time attitude tracking control for rigid spacecraft

4. Attitude tracking control of spacecraft with preset‐time preset‐bounded convergence

5. A Predefined-Time Extended-State Observer-Based Approach for Velocity-Free Attitude Control of Spacecraft

Cited by 1 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. Distributed finite‐time attitude coordination control of spacecraft formations with multiple constraints;International Journal of Robust and Nonlinear Control;2024-06-11

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