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Adaptive Tracking Control for the Conversion Mode of Tilt-Rotor Aircraft with Switched Fuzzy Modeling

Crossref DOI link: https://doi.org/10.1007/s40815-023-01661-4

Published Online: 2024-02-17

Published Print: 2024-06

Update policy: https://doi.org/10.1007/springer_crossmark_policy

Authors

Li, Wen https://orcid.org/0000-0001-7707-1761
Shi, Shuang

Chen, Mou

Wu, Qingxian
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Text and Data Mining valid from 2024-02-17

Version of Record valid from 2024-02-17
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Article History

Received: 2 August 2023

Revised: 19 October 2023

Accepted: 27 November 2023

First Online: 17 February 2024