Terminal Sliding Mode Control of Airship Pitch Channel simplified model

DOI

10.2991/icmmct-16.2016.387How to use a DOI?

Keywords

airship; pitch channel; adaptive; robustness; stability

Abstract

To make the response of airship system to be quicker, a kind of terminal sliding mode surface was constructed which can make the pitch angle trace the desired value in a finite time. Also a Lyapunov function was given to prove the sliding mode method is right and reasonable. But detailed simulation result shows that the response is very quick but it has chattering problem which is caused by the loss of integral item in the formation of control law. So a conclusion was got that terminal sliding mode surface should has enough damping ratio in the formation of control law or the system response will has oscillation.

Copyright

© 2016, 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  - Guoqiang Liang
AU  - Yuliang Chen
AU  - Guangbin Wu
PY  - 2016/03
DA  - 2016/03
TI  - Terminal Sliding Mode Control of Airship Pitch Channel simplified model
BT  - Proceedings of the 2016 4th International Conference on Machinery, Materials and Computing Technology
PB  - Atlantis Press
SP  - 1940
EP  - 1945
SN  - 2352-5401
UR  - https://doi.org/10.2991/icmmct-16.2016.387
DO  - 10.2991/icmmct-16.2016.387
ID  - Liang2016/03
ER  -