Attitude control of flapping wing aircraft based on energy optimization and ESO

Aiming at the problem of insufficient endurance performance of flapping wing aircraft, a stable attitude control algorithm based on energy optimization and ESO (extended state observer) is designed, which effectively reduces the energy consumption in cruise phase. Firstly, the longitudinal dynamic m...

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Detalles Bibliográficos

Autores principales:	Luo Li, Hongwei Wang, Long Cui
Formato:	Artigo
Lenguaje:	Inglês
Publicado:	KeAi Communications Co., Ltd. 2021-06-01
Colección:	Biomimetic Intelligence and Robotics
Materias:	Flapping wing Energy optimal control ESO (Extended State Observer)
Acceso en línea:	http://www.sciencedirect.com/science/article/pii/S266737972100005X
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