Terminal Sliding Mode Control of Airship Pitch Channel simplified model
Guoqiang Liang, Yuliang Chen, Guangbin Wu
Available Online March 2016.
- https://doi.org/10.2991/icmmct-16.2016.387How to use a DOI?
- airship; pitch channel; adaptive; robustness; stability
- To make the response of airship system to be quicker, a kind of terminal sliding mode surface was constructed which can make the pitch angle trace the desired value in a finite time. Also a Lyapunov function was given to prove the sliding mode method is right and reasonable. But detailed simulation result shows that the response is very quick but it has chattering problem which is caused by the loss of integral item in the formation of control law. So a conclusion was got that terminal sliding mode surface should has enough damping ratio in the formation of control law or the system response will has oscillation.
- Open Access
- This is an open access article distributed under the CC BY-NC license.
Cite this article
TY - CONF AU - Guoqiang Liang AU - Yuliang Chen AU - Guangbin Wu PY - 2016/03 DA - 2016/03 TI - Terminal Sliding Mode Control of Airship Pitch Channel simplified model BT - 2016 4th International Conference on Machinery, Materials and Computing Technology PB - Atlantis Press SP - 1940 EP - 1945 SN - 2352-5401 UR - https://doi.org/10.2991/icmmct-16.2016.387 DO - https://doi.org/10.2991/icmmct-16.2016.387 ID - Liang2016/03 ER -