Dynamic Flight Stability of a Hovering Flapping-Rotary-Wing Vehicle

The aerodynamic performance and mechanisms of the compound layout of flapping-rotary-wing (FRW) vehicles have been studied extensively in the literature, but open-loop stability has rarely been involved. To bridge this gap, a hovering stability analysis of a 30 g FRW prototype has been conducted. Av...

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Veröffentlicht in:	AIAA journal 2023-12, Vol.61 (12), p.5584-5597
Hauptverfasser:	Jianghao, Wu, Xinyi, Wu, Peng, Tang, Yanlai, Zhang, Chao, Zhou
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerodynamic stability Center of gravity College professors Coupling Dynamic stability Efficiency Eigenvalues Eigenvectors Engineering Equilibrium Flapping wings Gravity Helicopters Hovering flight Hovering stability Inertia Mathematical models Pitch (inclination) Reynolds number Rolling motion Rotation Stability analysis Stability derivatives Vehicles Velocity
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