Dynamic surface control for satellite attitude of the chained three-body tethered system during deployment
Author:
Funder
Natural Science Basic Research Program of Shaanxi Province
Natural Science Foundation of Shaanxi Province
National Natural Science Foundation of China
Publisher
Elsevier BV
Reference32 articles.
1. Alsaade, F.W., Yao, Q., Al-zahrani, M.S., Alzahrani, A.S., Jahanshahi, H., 2023. Neural-based fixed-time attitude tracking control for space vehicle subject to constrained outputs. Advances in Space Research 71, 3588–3599. URL: https://www.sciencedirect.com/science/article/pii/S0273117722007141, doi: 10.1016/j.asr.2022.07.081. application of Artificial Intelligence in Tracking Control and Synchronization of Spacecraft.
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4. Artificial potential incorporated adaptive fixed-time sliding mode control for target capture;Cai;Adv. Space Res.,2023
5. Sliding-mode-based attitude tracking control of spacecraft under reaction wheel uncertainties;Chen;IEEE-CAA J. Automat. Sin.,2023
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