Abstract
In this chapter, we aim to investigate the effect of piezoelectric actuator hysteresis on helicopter vibration control using trailing-edge flaps. The material and mechanical hysteresis in the piezoelectric actuator is modeled using the classical Preisach model. Experimental data from literature is used to estimate the Preisach distribution function.
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Ganguli, R., Thakkar, D., Viswamurthy, S.R. (2016). Piezoceramic Actuator Hysteresis. In: Smart Helicopter Rotors. Advances in Industrial Control. Springer, Cham. https://doi.org/10.1007/978-3-319-24768-7_7
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DOI: https://doi.org/10.1007/978-3-319-24768-7_7
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Online ISBN: 978-3-319-24768-7
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