Design, simulation and experimental verification of an active inductance for a low frequency tuned mass damper in an aircraft fuselage active vibration cancellation system

Citation:

Tsioustas C, Loupis M. Design, simulation and experimental verification of an active inductance for a low frequency tuned mass damper in an aircraft fuselage active vibration cancellation system. In: IEEE; 2018. pp. 1 - 5.

Date Presented:

2018