This work was supported by the National Natural Science Foundation of China under
Grants 61503012 and 61673034, and the Fundamental Research Funds for the Central Universities under Grants YWF-18-BJ-Y-81 and YWF-17-BJ-Y-86.
History
School
Aeronautical, Automotive, Chemical and Materials Engineering
Department
Aeronautical and Automotive Engineering
Published in
Aerospace Science and Technology
Volume
81
Pages
348 - 361
Citation
LI, Z. ... et al., 2018. Nonlinear robust control of tail-sitter aircrafts in flight mode transitions. Aerospace Science and Technology, 81, pp. 348-361.
This paper was accepted for publication in the journal Aerospace Science and Technology and the definitive published version is available at https://doi.org/10.1016/j.ast.2018.08.021.