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Design of Flight Control Law of Tilt-Rotor Aircraft Based on Incremental Nonlinear Dynamic Inversion

Crossref DOI link: https://doi.org/10.1007/978-981-15-8155-7_391

Published Online: 2021-10-30

Published Print: 2022

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

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