@inproceedings{33b6ea902bd44a3cac965edc3244e4ec,
title = "Adaptive sliding mode based controller design for spacecraft attitude stabilization",
abstract = "An adaptive sliding mode controller that take the advantage of adaptive control method and sliding mode control method is designed for rigid spacecraft with external bounded disturbances. By using adaptive control law, the external disturbances can be estimated which can thus improve the robustness of the control system. System vibration is eliminated by substituting the signal function with hyperbolic tangent function. The designed controller is applied in spacecraft attitude stabilization system, and we analysis the asymptotic stability of the close loop system by employing Lyapunov stability theory. The simulation results show that this method has a good robustness to external disturbances. High precision attitude stabilization control is achieved.",
keywords = "Adaptive, Attitude Stabilization, Sliding mode, Spacecraft, Vibration",
author = "Long Li and Jianwen Hou and Xiaoping Shi and Jing Yang and Xianting Bi and Hailong Liu",
note = "Publisher Copyright: {\textcopyright} 2015 IEEE.; 27th Chinese Control and Decision Conference, CCDC 2015 ; Conference date: 23-05-2015 Through 25-05-2015",
year = "2015",
month = jul,
day = "17",
doi = "10.1109/CCDC.2015.7161855",
language = "英语",
series = "Proceedings of the 2015 27th Chinese Control and Decision Conference, CCDC 2015",
publisher = "Institute of Electrical and Electronics Engineers Inc.",
pages = "620--623",
booktitle = "Proceedings of the 2015 27th Chinese Control and Decision Conference, CCDC 2015",
address = "美国",
}