A Simple Fuzzy Backstepping Control Method for Saucer-shaped Aircraft
Authors
HuaLi Wu, LingLing Wang, LiLi Yang, Junwei Lei
Corresponding Author
HuaLi Wu
Available Online April 2017.
- DOI
- 10.2991/icmmct-17.2017.158How to use a DOI?
- Keywords
- Fuzzy control, Backstepping Control; Saucer-shaped Aircraft, Stability, Lyapunov function
- Abstract
A simplified linear model is studied for the complex nonlinear model for a class of saucer-shaped aircraft in this paper. Then a feedback control law is designed to achieve the tracking of given attitude angle. What is more, a kind of gain adjusting law by fuzzy changes with errors is designed in order to achieve better matching of backstepping gains. Finally, detailed analysis results of the simulation show the effectiveness of the proposed fuzzy control law.
- Copyright
- © 2017, 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 - HuaLi Wu AU - LingLing Wang AU - LiLi Yang AU - Junwei Lei PY - 2017/04 DA - 2017/04 TI - A Simple Fuzzy Backstepping Control Method for Saucer-shaped Aircraft BT - Proceedings of the 2017 5th International Conference on Machinery, Materials and Computing Technology (ICMMCT 2017) PB - Atlantis Press SP - 784 EP - 788 SN - 2352-5401 UR - https://doi.org/10.2991/icmmct-17.2017.158 DO - 10.2991/icmmct-17.2017.158 ID - Wu2017/04 ER -