High Order Sliding Mode Control for the Aircraft Antiskid Braking System
Authors
Longfei Fu, Guanglai Tian, Yuren Li, Bo Liang, Hongling Wang
Corresponding Author
Longfei Fu
Available Online November 2015.
- DOI
- 10.2991/itms-15.2015.349How to use a DOI?
- Keywords
- high order sliding mode; slip ratio; anti-skid braking system; aircraft
- Abstract
A high order sliding mode control (HOSMC) algorithm is proposed to control the nonlinear system with parameter uncertainty in this paper, with the purpose of the chattering avoidance. According to the aircraft antiskid braking system(ABS) model, a HOSMC algorithm is presented and a bipolar sigmoid function is developed. The stability and convergence of proposed algorithm is analyzed with Lyapunov theory in finite time. The results indicate that the HOSMC algorithm has a better performance and chattering avoidance than the conditional ones. Additionally the maximum friction coefficient is acquired in a short time, and the optimal slip ratio is achieved under the runway simulation.
- Copyright
- © 2015, 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 - Longfei Fu AU - Guanglai Tian AU - Yuren Li AU - Bo Liang AU - Hongling Wang PY - 2015/11 DA - 2015/11 TI - High Order Sliding Mode Control for the Aircraft Antiskid Braking System BT - Proceedings of the 2015 International Conference on Industrial Technology and Management Science PB - Atlantis Press SP - 1429 EP - 1432 SN - 2352-538X UR - https://doi.org/10.2991/itms-15.2015.349 DO - 10.2991/itms-15.2015.349 ID - Fu2015/11 ER -