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Simulation of Helicopter Dynamic Landing Based on Path Planning and Dynamic Inverse Control

This paper proposes a dynamic landing simulation method for helicopters, considering the effects of ship wake, atmospheric turbulence, and ship motion, as well as the ground effect between the rotor and the deck, on the control quantities and attitude during the dynamic landing process of helicopter...

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Detalhes bibliográficos
Principais autores: YANG Shuhan, CHEN Renliang, YE Yi
Formato: Artigo
Idioma:Chinês
Publicado em: Editorial Office of Journal of Nanjing University of Aeronautics and Astronautics 2026-04-01
coleção:Nanjing Hangkong Hangtian Daxue Xuebao
Assuntos:
Acesso em linha:https://jnuaa.nuaa.edu.cn/njhkht/article/abstract/202602005
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