Adaptive robust control of unmanned helicopter angular rate

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/).

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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  -