A Non-singular Terminal Sliding Mode Attitude Control for Space Robots
Author:
Publisher
Springer Nature Singapore
Link
https://link.springer.com/content/pdf/10.1007/978-981-19-6226-4_1
Reference9 articles.
1. Gui, H., Vukovich, G.: Dual-quaternion-based adaptive motion tracking of spacecraft with reduced control effort. Nonlinear Dyn. 83, 597–614 (2015). https://doi.org/10.1007/s11071-015-2350-4
2. Li, Y., Ye, D.: Robust PID controller for flexible satellite attitude control under angular velocity and control torque constraint. Asian J. Control 22(3), 1327–1344 (2020). https://doi.org/10.1002/asjc.1999
3. Li, K., Ji, H.: Inverse optimal adaptive backstepping control for spacecraft rendezvous on elliptical orbits. Int. J. Control 91(10), 2303–2313 (2018). https://doi.org/10.1080/00207179.2017.1340672
4. Luo, W., Chu, Y., Ling, K.: Inverse optimal adaptive control for attitude tracking of spacecraft. IEEE Trans. Autom. Control 50(11), 1639–1654 (2005). https://doi.org/10.1109/tac.2005.858694
5. Pukdeboon, C.: Optimal output feedback controllers for spacecraft attitude tracking. Asian J. Control 15(5), 1284–1294 (2013). https://doi.org/10.1002/asjc.615
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