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JRM Vol.36 No.5 pp. 1156-1166
doi: 10.20965/jrm.2024.p1156
(2024)

Paper:

Senswing: A Force Sensing Wing for Intelligent Flapping-Wing Aerial Vehicles—Wing Design and Comprehensive Evaluation of Force Sensing Capabilities

Hidaka Sato ORCID Icon, Muhammad Labiyb Afakh ORCID Icon, and Naoyuki Takesue ORCID Icon

Department of Mechanical Systems Engineering, Graduate School of Systems Design, Tokyo Metropolitan University
6-6 Asahigaoka, Hino, Tokyo 191-0065, Japan

Received:
April 22, 2024
Accepted:
August 4, 2024
Published:
October 20, 2024
Keywords:
flapping-wing aerial vehicles, force sensing, strain gauge
Abstract

This paper proposes a force-sensing wing, Senswing, to enhance the intelligence of flapping-wing aerial vehicles (FWAVs). Force perception is a crucial capability for robots to interact safely and effectively in unknown environments. However, FWAVs perform flapping motions with significant acceleration and deceleration, which can cause the flexure element inside force sensors to deteriorate due to repeated loading or even fail due to impulsive forces. To address this, we constructed a force measurement system by attaching 16 strain gauges directly to the wing root while maintaining high rigidity. We confirmed that the external force measurement capability closely matched the values obtained by a six-axis force sensor, with almost no error. Additionally, when measuring aerodynamic forces during wing flapping, the sensor could detect differences in wind speed even during flapping. With this sensor, FWAVs can achieve in-flight measurement of thrust and lift through a force-sensing system.

Structure of the Senswing

Structure of the Senswing

Cite this article as:
H. Sato, M. Afakh, and N. Takesue, “Senswing: A Force Sensing Wing for Intelligent Flapping-Wing Aerial Vehicles—Wing Design and Comprehensive Evaluation of Force Sensing Capabilities,” J. Robot. Mechatron., Vol.36 No.5, pp. 1156-1166, 2024.
Data files:
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