TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
Online ISSN : 2189-4205
Print ISSN : 0549-3811
ISSN-L : 0549-3811
Difficulty of Controlling a Flapping-wing Aircraft Compared to a Rotary-wing Aircraft
Kengo KIMURAShigeru SUNADA
Author information
JOURNAL OPEN ACCESS

2023 Volume 66 Issue 4 Pages 130-140

Details
Abstract

The inherent stability of two-dimensional motion when hovering using beating wings that have a passive feathering motion is compared with that of rotary wings that have a passive flapping motion. The passive flapping motion of the rotary wings is determined by the bending elasticity, which is expressed by a spring at the wing root. The feathering motion of the beating wings is determined by the torsional elasticity, which is expressed by a damper and a spring at the wing root. The values of the damper and spring were determined by minimizing the necessary power in the present analysis. Unlike rotary wings with passive flapping motion, beating wings with passive feathering motion do not have pitch/roll damping. A flying robot with beating wings requires quicker flight control than one with rotary wings. The results indicate that a flying robot mimicking a living creature is more difficult to control than one with rotary wings.

Content from these authors
© 2023 The authors. JSASS has the license to publish of this article.

This is an open access article distributed under the Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International (CC BY-NC-ND 4.0), which permits non-commercially distribute and reproduce an unmodified in any medium, provided the original work is properly cited.
https://creativecommons.org/licenses/by-nc-nd/4.0/
Previous article Next article
feedback
Top