/PiezoelectricActuator_for_FWMAV

For the piezoelectric-driven Flapping Wing Micro Aerial vehicle (FWMAV), the optimal design and theoretical calculation of the curved double-cantilever piezoelectric actuator and the torsional piezoelectric actuator were carried out.

Primary LanguageMATLABGNU General Public License v3.0GPL-3.0

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