
Mogens Blanke
Address: Kgs. Lyngby, Capital Region, Denmark
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Papers by Mogens Blanke
damping, which poses challenges for safe operation in presence of disturbances. Enhanced damping can be achieved
through active lubrication techniques using feedback control laws. Such control design requires models with low
complexity, able to describe the dominant dynamics from actuator input to sensor output over the relevant range of
operation. The mathematical models based on first principles are not easy to obtain, and in many cases, they cannot
be directly used for control design due to their complexity and parameter uncertainties. As an alternative, this paper
presents an experimental technique for ”in situ” identification of low complexity models of the entire rotor-bearingactuator
system. Using grey-box identification techniques, the approach is shown to be easily applied to industrial
rotating machinery with gas bearings and to allow for subsequent control design. The paper shows how piezoelectric
actuators in a gas bearing are eciently used to perturb the gas film for identification over relevant ranges of rotational
speed and gas injection pressure. Parameter-varying linear models are found to capture the dominant dynamics of the
system over the range of operation. Based on the identified models, decentralised proportional control is designed and
is shown to obtain the required damping in theory as well as in a laboratory test rig.
Parameter uncertainty in the network originates from the grid
and the number of wind turbines connected. Power converter
based turbines inject harmonic currents, which are attenuated
by passive filters. A robust high order active filter controller is
proposed to complement the passive filtering. The H1 design
of the control loop enables desired tracking with integral effect
while bounding the induced change. The design was tested in
an aggregated model of the London Array offshore wind power
plant and compared with traditional PI controller designs. Robust stability and performance and a reduction of control effort by 25% are obtained over the full envelope of operation.
damping, which poses challenges for safe operation in presence of disturbances. Enhanced damping can be achieved
through active lubrication techniques using feedback control laws. Such control design requires models with low
complexity, able to describe the dominant dynamics from actuator input to sensor output over the relevant range of
operation. The mathematical models based on first principles are not easy to obtain, and in many cases, they cannot
be directly used for control design due to their complexity and parameter uncertainties. As an alternative, this paper
presents an experimental technique for ”in situ” identification of low complexity models of the entire rotor-bearingactuator
system. Using grey-box identification techniques, the approach is shown to be easily applied to industrial
rotating machinery with gas bearings and to allow for subsequent control design. The paper shows how piezoelectric
actuators in a gas bearing are eciently used to perturb the gas film for identification over relevant ranges of rotational
speed and gas injection pressure. Parameter-varying linear models are found to capture the dominant dynamics of the
system over the range of operation. Based on the identified models, decentralised proportional control is designed and
is shown to obtain the required damping in theory as well as in a laboratory test rig.
Parameter uncertainty in the network originates from the grid
and the number of wind turbines connected. Power converter
based turbines inject harmonic currents, which are attenuated
by passive filters. A robust high order active filter controller is
proposed to complement the passive filtering. The H1 design
of the control loop enables desired tracking with integral effect
while bounding the induced change. The design was tested in
an aggregated model of the London Array offshore wind power
plant and compared with traditional PI controller designs. Robust stability and performance and a reduction of control effort by 25% are obtained over the full envelope of operation.