Demonstration of Stable Vertical Takeoff of an Insect-Mimicking Flapping-Wing System
Flapping
Takeoff
Insect flight
DOI:
10.5302/j.icros.2012.18.2.076
Publication Date:
2012-04-26T07:18:57Z
AUTHORS (6)
ABSTRACT
This paper demonstrates how to implement inherent pitching stability in an insect-mimicking flapping-wing system for vertical takeoff. Design and fabrication of the is briefly described focusing on recent modification. Force produced by systems estimated using UBET (Unsteady Blade Element Theory) developed previous work. The estimation shows that wing twist placed modified can improve thrust production about 10 %. compared with measured thrust, which proves provides fairly good estimations systems. takeoff test be implemented aligning aerodynamic force center gravity.
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