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An optimization for alleviating pilot workload during tilt rotor aircraft conversion and reconversion maneuvers

Xin Yu Orcid Logo, Renliang Chen, Luofeng Wang Orcid Logo, Xufei Yan Orcid Logo, Ye Yuan Orcid Logo

Aerospace Science and Technology, Volume: 129, Start page: 107854

Swansea University Author: Ye Yuan Orcid Logo

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Published in: Aerospace Science and Technology
ISSN: 1270-9638
Published: Elsevier BV 2022
Online Access: Check full text

URI: https://cronfa.swan.ac.uk/Record/cronfa61022
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Keywords: Tilt rotor aircraft; Conversion maneuver; Reconversion maneuver; Pilot workload; Control allocation; Conversion path
College: Faculty of Science and Engineering
Funders: This study was supported by the National Natural Science Foundation of China (No. 11672128) and thanks for A Project Funded by the Priority Academic Program Development of Jiangsu Higher Education Institutions.
Start Page: 107854