Paper
28 April 2011 Self-actuating and self-diagnosing plastically deforming piezo-composite flapping wing MAV
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Abstract
In this work, we propose a constitutive model to describe the behavior of Piezoelectric Fiber Reinforced Composite (PFRC) material consisting of elasto-plastic matrix reinforced by strong elastic piezoelectric fibers. Computational efficiency is achieved using analytical solutions for elastic stifness matrix derived from Variational Asymptotic Methods (VAM). This is extended to provide Structural Health Monitoring (SHM) based on plasticity induced degradation of flapping frequency of PFRC. Overall this work provides an effective mathematical tool that can be used for structural self-health monitoring of plasticity induced flapping degradation of PFRC flapping wing MAVs. The developed tool can be re-calibrated to also provide SHM for other forms of failures like fatigue, matrix cracking etc.
© (2011) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Ajay B. Harish, Dineshkumar Harursampath, and D. Roy Mahapatra "Self-actuating and self-diagnosing plastically deforming piezo-composite flapping wing MAV", Proc. SPIE 7978, Behavior and Mechanics of Multifunctional Materials and Composites 2011, 797813 (28 April 2011); https://doi.org/10.1117/12.880218
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KEYWORDS
Composites

Micro unmanned aerial vehicles

3D modeling

Actuators

Structural health monitoring

Fused deposition modeling

Kinematics

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