Fully-Actuated System Approach Based Optimal Attitude Tracking Control of Rigid Spacecraft with Actuator Saturation
Author:
Publisher
Springer Science and Business Media LLC
Subject
Information Systems,Computer Science (miscellaneous)
Link
https://link.springer.com/content/pdf/10.1007/s11424-022-1515-8.pdf
Reference34 articles.
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4. Xia Y, Zhu Z, Fu M, et al., Attitude tracking of rigid spacecraft with bounded disturbances, IEEE Transactions on Industrial Electronics, 2011, 58(2): 647–659.
5. Dong R Q, Wu A G, and Zhang Y, Anti-unwinding sliding mode attitude maneuver control for rigid spacecraft, IEEE Transactions on Automatic Control, 2021, arXiv: 2004.07001.
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