Modeling And Robust Sliding Mode Control Of A Kind Airship Aircraft
Authors
Guangbin Wu, Guoqiang Liang, Junwei Lei, Huali Wu
Corresponding Author
Guangbin Wu
Available Online August 2015.
- DOI
- 10.2991/icmeis-15.2015.36How to use a DOI?
- Keywords
- airship; pitch channel; adaptive; robustness; modeling
- Abstract
The airship modeling is the basic of the airship control problem, a class of simplified nonlinear model of pitching channel is studied in this paper. On the base of all above mentioned, the speed control is separated from the attitude control, and the speed is controlled by a simple constant control scheme. This paper has proposed a control scheme that is similar to robust sliding mode control scheme in the condition that the information of the unknown portion of the assumed airship model satisfy the norm-bounded condition and the boundary is known. Finally this control scheme is proved to be effective by detailed 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 - Guangbin Wu AU - Guoqiang Liang AU - Junwei Lei AU - Huali Wu PY - 2015/08 DA - 2015/08 TI - Modeling And Robust Sliding Mode Control Of A Kind Airship Aircraft BT - Proceedings of the 3rd International Conference on Mechanical Engineering and Intelligent Systems (ICMEIS 2015) PB - Atlantis Press SP - 185 EP - 190 SN - 2352-5401 UR - https://doi.org/10.2991/icmeis-15.2015.36 DO - 10.2991/icmeis-15.2015.36 ID - Wu2015/08 ER -