Abstract
The experimental work presented demonstrates the use of
identification, feedback, and feedforward methods to
control rotor vibrations. The experiments were performed
on a rotor test rig having a 3-kg rotor supported by
journal bearings; the first bending resonance of the
rotor shaft was about 50 Hz. Identification was carried
out with a method taking into account the disturbances
due to rotation. The method, using a reference signal
generated from speed measurement, was able to discard the
forced vibrations due to the mass imbalance. The active
control objective was to reduce the radial response at
the rotor midpoint by an electromagnetic actuator located
outside the bearing span of the rotor. The feedback
system was a proportional-derivative-type controller,
which increased the damping of the system. A feedforward
control system was constructed to work together with the
feedback controller. The control methods produced a
significant decrease in the midpoint responses of the
rotor at sub-critical speeds. For super-critical speeds,
the decrease in the responses was more modest due to the
restricted control authority. The stability of the
feedforward controller was studied in order to explore
the relationship between the system damping and the
required modeling accuracy required by the feedforward
control system.
Original language | English |
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Pages (from-to) | 7-14 |
Journal | International Journal of Acoustics and Vibration |
Volume | 12 |
Issue number | 1 |
DOIs | |
Publication status | Published - 2007 |
MoE publication type | A1 Journal article-refereed |