Smart flapping wings with a PVDF sensor to modify aerodynamic performance of a micro UAV

被引：0

作者：

Yang, Lung-Jieh ^{[1
]}

Hsu, Cheng-Kuei ^{[1
]}

Feng, Chao-Kang ^{[2
]}

Shih, H. -M. ^{[1
]}

Feng, C. -H. ^{[1
]}

Gao, M. -W. ^{[1
]}

机构：

[1] Tamkang Univ, Dept Mech & Electromech Engn, Tamsui, Taiwan

[2] Tamkang Univ, Dept Aerosp Engn, Tamsui, Taiwan

来源：

TRANSDUCERS '07 & EUROSENSORS XXI, DIGEST OF TECHNICAL PAPERS, VOLS 1 AND 2 | 2007年

关键词：

micro UAV; polyvinylidenefluoride; flapping wing;

D O I：

暂无

中图分类号：

TM [电工技术]; TN [电子技术、通信技术];

学科分类号：

0808 ; 0809 ;

摘要：

This paper describes a new configuration of flapping wings to study the aerodynamic behavior of a micro UAV (unmanned aerial vehicle.) The flapping wings are composed of a pure parylene right wing and a PVDF-parylene composite left wing on purpose. The PVDF (polyvinylidene fluoride) sensor could only export the lift signals from the left wing. In comparison to the total lift signal picked by the load cell from the wind-tunnel facility, we can figure out and separate the lift contributions donated by left wing and right wing, respectively. Therefore, we found a new design methodology to adjust the aerodynamic performance of micro UAVs by changing the phase lag between the two flapping wings through fine tuning the mechanism linkages.

引用

页数：2

共 6 条

[1]

CLOUPEAU M, 1979, J EXP BIOL, V80, P1

[2]

Dickinson MH, 1996, J EXP BIOL, V199, P2085

[3] Unsteady aerodynamics and flow control for flapping wing flyers [J].