The data contains the measurement data for the system identification, passive performance and the active vibration control of the rotor system. The used rotor test-rig has two active bearing which comprises two piezo actuators each, but only one bearing is activly used. Chirps have been applied to these actuators at two different rotor speeds for system identification of the gyroscopic rotor system. The rotor was controlled using IFF in combination with the LMS. Three control objectives have been defined: Minimization of the bearing forces; minimization of the bearing forces and the displacements; minimization of the beraing forces and the relative displacements which are porportional to the deformation of the rotor. Read the publication for more details