High Order Sliding Mode Control for the Aircraft Antiskid Braking System

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/).

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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  -