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

DOI

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.

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  - 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  - 10.2991/icmmct-16.2016.388
ID  - Jin2016/03
ER  -