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

Integral Sliding mode Control of Height Loop of a Kind of Airship Vehicle

Authors
Yuqiang Jin, Huali Wu, Junwei Lei
Corresponding Author
Yuqiang Jin
Available Online March 2016.
DOI
https://doi.org/10.2991/icmmct-16.2016.388How to use a DOI?
Keywords
airship; pitch channel; adaptive; sliding mode; stability
Abstract
A kind of integral sliding mode surface method is firstly used in the height loop of airship system based on the assumption that the pitch angle control loop is stable. The expected pitch angle signal is caused by the sliding mode surface which is produced by height error .Compared with traditional PID height loop control strategy, this integral sliding mode method has a very quick output response and simulation result shows that the proposed method is also very accurate in the task of tracking of desired height.
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This is an open access article distributed under the CC BY-NC license.

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Volume Title
Proceedings of the 2016 4th International Conference on Machinery, Materials and Computing Technology
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-16.2016.388How 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  - Yuqiang Jin
AU  - Huali Wu
AU  - Junwei Lei
PY  - 2016/03
DA  - 2016/03
TI  - Integral Sliding mode Control of Height Loop of a Kind of Airship Vehicle
BT  - Proceedings of the 2016 4th International Conference on Machinery, Materials and Computing Technology
PB  - Atlantis Press
SP  - 1946
EP  - 1951
SN  - 2352-5401
UR  - https://doi.org/10.2991/icmmct-16.2016.388
DO  - https://doi.org/10.2991/icmmct-16.2016.388
ID  - Jin2016/03
ER  -