Nonlinear modeling and designing transition flight control scenarios for a dual thrust hybrid UAV
Crossref DOI link: https://doi.org/10.1007/s41315-024-00354-x
Published Online: 2024-06-27
Published Print: 2024-09
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Mohammadi, Navid
Tayefi, Morteza
Zhu, Man
Text and Data Mining valid from 2024-06-27
Version of Record valid from 2024-06-27
Article History
Received: 9 April 2024
Accepted: 7 June 2024
First Online: 27 June 2024
Declarations
:
: The authors declare no competing interests.