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NASA NTRS · 19920056634

Electromechanical simulation and testing of actively controlled rotordynamic systems with piezoelectric actuators

Abstract

Theoretical developments for the simulation of an actively controlled rotorbearing system with piezoelectric type actuators are summarized. Two simulation models were derived; the first assumes that the actuators and other electrical components in the feedback system operate at all frequencies without phase lag or rolloff, while the second model includes the nonideal behavior of these components which are modeled with linear electric circuits. The two models predict identical unbalance response at low frequencies, and the nonideal model also predicts instability-onset feedback gains. The agreement between the measured and predicted results for unbalance response and instability onset gain is very good. The predicted instability-onset feedback gain for active damping was found to be very sensitive to the tare (uncontrolled) damping in the unstable mode.

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BibTeXRIS

Lin, Reng R., Palazzolo, A. B., Kascak, A. F., Montague, G. T.. 1991-01-01. Electromechanical simulation and testing of actively controlled rotordynamic systems with piezoelectric actuators. https://ntrs.nasa.gov/citations/19920056634

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