Robust Finite Time Control for Stabilization of Rigid Spacecraft
- 10.2991/ecae-17.2018.27How to use a DOI?
- state-space-like; attitude stabilizer; finite-time convergence; disturbance observer
This paper investigates finite-time attitude stabilization of a rigid spacecraft in presence of external disturbance and model uncertainties. Based on Modified Rodriguez parameters (MRPs), attitude kinematics and dynamics are converted into state-space-like form, and then robust finite-time controller is designed for attitude stabilization of a rigid spacecraft. Furthermore, smooth second order sliding mode and disturbance observer, by virtue of geometric homogeneity, are employed to construct finite time attitude stabilizer, which eliminates the chattering phenomenon and the requirement of the upper bounds of the total uncertainties. Simulation results are provided to demonstrate the effectiveness of the proposed attitude controllers.
- © 2018, the Authors. Published by Atlantis Press.
- Open Access
- This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).
Cite this article
TY - CONF AU - Yaohua Tang AU - Yuanli Cai AU - Jiwei Gao AU - Huaizhong Hu AU - Weimin Guo PY - 2017/12 DA - 2017/12 TI - Robust Finite Time Control for Stabilization of Rigid Spacecraft BT - Proceedings of the 2017 2nd International Conference on Electrical, Control and Automation Engineering (ECAE 2017) PB - Atlantis Press SP - 123 EP - 127 SN - 2352-5401 UR - https://doi.org/10.2991/ecae-17.2018.27 DO - 10.2991/ecae-17.2018.27 ID - Tang2017/12 ER -