Integral Sliding mode Control of Height Loop of a Kind of Airship Vehicle
Yuqiang Jin, Huali Wu, Junwei Lei
Available Online March 2016.
- https://doi.org/10.2991/icmmct-16.2016.388How to use a DOI?
- airship; pitch channel; adaptive; sliding mode; stability
- 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.
- 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 -