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Piezoceramic Actuator Hysteresis

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Part of the book series: Advances in Industrial Control ((AIC))

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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References

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Correspondence to Ranjan Ganguli .

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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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  • Publisher Name: Springer, Cham

  • Print ISBN: 978-3-319-24766-3

  • Online ISBN: 978-3-319-24768-7

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