Adaptive robust control of unmanned helicopter angular rate
Authors
Xingwen Zhang, Ming Chen, PeiZhi Liu, Jinhua Wang, Yi Qian, Xianxiang Chen
Corresponding Author
Xingwen Zhang
Available Online November 2015.
- DOI
- 10.2991/icmmita-15.2015.287How to use a DOI?
- Keywords
- extended state observer; unmanned helicopter; sliding-mode control; uncertain system.
- Abstract
Put forward a compound control strategy, which is designed with extended state observer and sliding mode variable structure control. The angular rate control of unmanned helicopter is validated through a Hardware-in-the-loop simulation, the simulation results show that the proposed control strategy can not only make the angular rate control of helicopter stable under the flight condition of turbulent, but also can ensure the angular rate accurate tracking according to different helicopter model without changing model parameters. The results indicate that the controller has strong robustness and adaptive ability.
- 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 - Xingwen Zhang AU - Ming Chen AU - PeiZhi Liu AU - Jinhua Wang AU - Yi Qian AU - Xianxiang Chen PY - 2015/11 DA - 2015/11 TI - Adaptive robust control of unmanned helicopter angular rate BT - Proceedings of the 2015 3rd International Conference on Machinery, Materials and Information Technology Applications PB - Atlantis Press SP - 1553 EP - 1557 SN - 2352-538X UR - https://doi.org/10.2991/icmmita-15.2015.287 DO - 10.2991/icmmita-15.2015.287 ID - Zhang2015/11 ER -