@inproceedings{7ad507253b2e4e7c9dc0c03d92f79e93,
title = "Attitude tracking of rigid spacecraft with bounded input",
abstract = "Attitude control is essential for spacecraft to accomplish various tasks, and the attitude tracking is one of the most important attitude control tasks. In this paper the attitude tracking of a rigid spacecraft with bounded input is examined. At the same time, the unknown external disturbances are finite, but their boundaries are unknown. In order to make sure the attitude tracking errors converge to zero, the nonlinear system model and problem formulation are obtained using quaternion method. Meanwhile a novel adaptive-robust-sliding mode control algorithm is designed, which can be applied in spacecraft systems with large parametric uncertainty or even with unknown inertial matrix. At last simulation results can illustrate the effectiveness of the control law.",
keywords = "Adaptive-robust-sliding mode control, Attitude tracking, Bounded input, Component, Unknown external disturbances",
author = "Xibin Wang and Shuli Guo and Lina Han",
note = "Publisher Copyright: {\textcopyright} 2017 IEEE.; 4th International Conference on Information Science and Control Engineering, ICISCE 2017 ; Conference date: 21-07-2017 Through 23-07-2017",
year = "2017",
month = nov,
day = "14",
doi = "10.1109/ICISCE.2017.297",
language = "English",
series = "Proceedings - 2017 4th International Conference on Information Science and Control Engineering, ICISCE 2017",
publisher = "Institute of Electrical and Electronics Engineers Inc.",
pages = "1425--1430",
editor = "Ying Dai and Shaozi Li and Yun Cheng",
booktitle = "Proceedings - 2017 4th International Conference on Information Science and Control Engineering, ICISCE 2017",
address = "United States",
}