Flight control design for small-scale helicopter using disturbance observer based backstepping
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.
- Aeronautical, Automotive, Chemical and Materials Engineering
- Aeronautical and Automotive Engineering
Published inJournal of Guidance, Control, and Dynamics (AIAA)
CitationLU, 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)
VersionAM (Accepted Manuscript)
Publisher statementThis 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/
NotesThis 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