Proceedings of the 2016 4th International Conference on Machinery, Materials and Computing Technology

Terminal Sliding Mode Control of Airship Pitch Channel simplified model

Authors
Guoqiang Liang, Yuliang Chen, Guangbin Wu
Corresponding Author
Guoqiang Liang
Available Online March 2016.
DOI
https://doi.org/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.
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Proceedings
2016 4th International Conference on Machinery, Materials and Computing Technology
Part of series
Advances in Engineering Research
Publication Date
March 2016
ISBN
978-94-6252-165-0
ISSN
2352-5401
DOI
https://doi.org/10.2991/icmmct-16.2016.387How to use a DOI?
Open Access
This is an open access article distributed under the CC BY-NC license.

Cite this article

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  - 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  - https://doi.org/10.2991/icmmct-16.2016.387
ID  - Liang2016/03
ER  -