Resonant motion, Micro/nano electromechanical system (M/NEMS), Modal combination, Design ofstructural vibration, Optimisation, Compliant links
," /> Resonant motion, Micro/nano electromechanical system (M/NEMS), Modal combination, Design ofstructural vibration, Optimisation, Compliant links
,"/> Resonant motion, Micro/nano electromechanical system (M/NEMS), Modal combination, Design ofstructural vibration, Optimisation, Compliant links,"/> Design and Optimisation of a Vibrating Wing Insect-Size Air Vehicle with Lumped Parameter Models and Compliant Links

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Journal of Bionic Engineering ›› 2025, Vol. 22 ›› Issue (5): 2396-2428.doi: 10.1007/s42235-025-00761-1

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Design and Optimisation of a Vibrating Wing Insect-Size Air Vehicle with Lumped Parameter Models and Compliant Links

Marguerite de La Bigne1; Mathieu Colin1; Éric Cattan2; Sofiane Ghenna2; Marie Zwingelstein2; Sébastien Grondel2; Olivier Thomas1 #br#   

  1. 1 Arts et Métiers Institute of Technology, LISPEN, HESAMUniversité, 59000 Lille, France
    2 Univ. Polytechnique Hauts-de-France, CNRS, Univ.Lille, UMR 8520-IEMN-Institut d’Electronique deMicroélectronique et de Nanotechnologie,59313 Valenciennes, France
  • Online:2025-10-15 Published:2025-11-19
  • Contact: Olivier Thomas1 E-mail:olivier.thomas@ensam.eu
  • About author:Marguerite de La Bigne1; Mathieu Colin1; éric Cattan2; Sofiane Ghenna2; Marie Zwingelstein2; Sébastien Grondel2; Olivier Thomas1

Abstract: This article presents the design of a microfabricated bio-inspired flapping-wing Nnano Aaerial Vvehicle (NAV), driven by an electromagnetic system. Our approach is based on artificial wings composed of rigid bodies connected by compliant links, which optimise aerodynamic forces though replicating the complex wing kinematics of insects. The originality of this article lies in a new design methodology based on a triple equivalence between a 3D model, a multibody model, and a mass/spring model (0D) which reduces the number of parameters in the problem. This approach facilitates NAV optimisation by using only the mass/spring model, thereby simplifying the design process while maintaining high accuracy. Two wing geometries are studied and optimised in this article to produce large-amplitude wing motions (approximately 40^\circ ), and enabling flapping and twisting motion in quadrature. The results are validated thanks to experimental measurements for the large amplitude and through finite element simulations for the combined motion, confirming the effectiveness of this strategy for a NAV weighing less than 40 mg with a wingspan of under 3 cm.

Key words: Resonant motion')">Resonant motion, Micro/nano electromechanical system (M/NEMS), Modal combination, Design ofstructural vibration, Optimisation, Compliant links