Adaptive Sliding Mode Control of Airship Pitch Channel Attitude Angle
Authors
Guoqiang Liang, Guangbin Wu, Lingling Wang, Junwei Lei
Corresponding Author
Guoqiang Liang
Available Online August 2015.
- DOI
- 10.2991/icmeis-15.2015.33How to use a DOI?
- Keywords
- airship; pitch channel; adaptive; robustness; stability
- Abstract
On the basic of nonlinear model of pitching channel of airship, assuming the condition that the information of the unknown portion of the assumed airship model satisfy the norm-bounded condition and the boundary is known. A adaptation method has been used to solve the unknown information problem in this paper, and this paper has proposed a class of sliding mode control method in order to control attitude angle of pitching channel of airship. Finally, this control method is proved to be effective by numerical simulation.
- Copyright
- © 2015, 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/).
Cite this article
TY - CONF AU - Guoqiang Liang AU - Guangbin Wu AU - Lingling Wang AU - Junwei Lei PY - 2015/08 DA - 2015/08 TI - Adaptive Sliding Mode Control of Airship Pitch Channel Attitude Angle BT - Proceedings of the 3rd International Conference on Mechanical Engineering and Intelligent Systems (ICMEIS 2015) PB - Atlantis Press SP - 169 EP - 174 SN - 2352-5401 UR - https://doi.org/10.2991/icmeis-15.2015.33 DO - 10.2991/icmeis-15.2015.33 ID - Liang2015/08 ER -