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Flight control design for small-scale helicopter using disturbance observer based backstepping

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posted on 15.07.2015, 10:46 by Hao Lu, Cunjia Liu, Lei Guo, Wen-Hua Chen
Flight control design for small-scale helicopter using disturbance observer based backstepping

Funding

This work was supported by the National Basic Research Program of China [2012CB720003] and the National Natural Science Foundation of China [61127007, 61121003, and 61320106010]. Hao Lu would like to thank the Chinese Scholarship Council for supporting his study in the United Kingdom.

History

School

  • Aeronautical, Automotive, Chemical and Materials Engineering

Department

  • Aeronautical and Automotive Engineering

Published in

Journal of Guidance, Control, and Dynamics (AIAA)

Citation

LU, H. ... et al, 2015. Flight control design for small-scale helicopter using disturbance observer based backstepping. Journal of Guidance, Control, and Dynamics (AIAA), 38(11), pp.2235-2240.

Publisher

© American Institute of Aeronautics and Astronautics (AIAA)

Version

AM (Accepted Manuscript)

Publisher statement

This work is made available according to the conditions of the Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International (CC BY-NC-ND 4.0) licence. Full details of this licence are available at: https://creativecommons.org/licenses/by-nc-nd/4.0/

Publication date

2015

Notes

This paper was accepted for publication in the Journal of Guidance, Control, and Dynamics (© AIAA) and the published version can be found at: http://dx.doi.org/10.2514/1.G001196

ISSN

0731-5090

eISSN

1533-3884

Language

en

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