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Damping of Wind Turbine Tower Oscillations through Rotor Speed ...

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transition to Laplace domain simple algebraic<br />

manipulations yield transfer functions that are<br />

needed for controller design. Those transfer<br />

functions are:<br />

and<br />

( )<br />

G s<br />

β<br />

w<br />

( )<br />

G s<br />

Δω<br />

=<br />

Δβ<br />

w<br />

( s)<br />

( s)<br />

( s)<br />

( )<br />

Δω<br />

=<br />

Δv<br />

s<br />

(14)<br />

. (15)<br />

These transfer functions are <strong>of</strong> the third order.<br />

A good insight in system properties <strong>of</strong> the<br />

wind turbine can be gained if we examine<br />

frequency characteristics <strong>of</strong> transfer function<br />

(14) shown in fig. 3.<br />

Figure 3: Frequency characteristics <strong>of</strong> G β .<br />

It can be observed that frequency<br />

characteristics <strong>of</strong> transfer function (14) at<br />

tower modal frequency exhibits magnitude and<br />

phase drop. Similar phenomena are present in<br />

frequency characteristics <strong>of</strong> (15) as well. This<br />

fact makes the pitch controller design very<br />

difficult. Physical explanation for observed<br />

effects becomes clear from the following<br />

analysis. Change in wind speed causes change<br />

in rotor speed what requires controller action<br />

and pitching <strong>of</strong> the blades in order to regulate<br />

the rotor speed to its rated value. Pitching the<br />

rotor blades, besides the aerodynamic torque,<br />

alters the thrust force significantly. Thrust<br />

force, according to (13), causes change in wind<br />

turbine tower top speed and thus the wind<br />

speed seen by the rotor is changed. This alters<br />

the aerodynamic conversion and in this way a<br />

feedback is formed. For this reason wind<br />

turbine can easily be driven into oscillatory<br />

behavior if the pitch controller is not designed<br />

properly.<br />

To prevent the pitch controller from driving the<br />

wind turbine into oscillatory behavior it must be<br />

assured that system frequency bandwidth is<br />

below the first tower modal frequency.<br />

Moreover, sufficiently small magnitude is<br />

required at the first modal frequency. As it can<br />

be seen from fig. 3. the first modal frequency <strong>of</strong><br />

the turbine in scope is 3 rad/s so a bandwidth <strong>of</strong><br />

1 rad/s was chosen. PID controller was designed<br />

to assure phase margin <strong>of</strong> around 60 o what gives<br />

satisfactory behavior <strong>of</strong> the system.<br />

To fully explore the system behavior with<br />

chosen controller simulation tool GH Bladed<br />

was used. GH Bladed is pr<strong>of</strong>essional simulation<br />

package designed for wind turbine simulations<br />

and load calculations [5]. It relies upon very<br />

complex mathematical model based on<br />

combined blade element and momentum theory<br />

[1]. Structural properties <strong>of</strong> the wind turbine are<br />

modeled in detail and inertial and gravitational<br />

loads are taken into account along with<br />

aerodynamic ones. Extensive testing showed<br />

that simulation results obtained in Bladed are in<br />

accordance with measurements taken on actual<br />

wind turbines what was recognized by major<br />

standardization and certification institutions<br />

(e.g. Germanischer Llyod).<br />

To model the structural properties <strong>of</strong> explored<br />

turbine many modes are used [5]. <strong>Tower</strong><br />

nodding is modeled with two modes as well as<br />

tower naying (tower side-side motion). <strong>Rotor</strong><br />

blades' motion in flapwise direction is modeled<br />

with 6 modal frequencies while blades' motion<br />

in edgewise direction (displacement <strong>of</strong> the rotor<br />

blades in the plane <strong>of</strong> rotation) is modeled with<br />

5 modal frequencies. <strong>Wind</strong> shear and tower<br />

shadow are included in the model as well. PID<br />

controller designed based on linearised model<br />

(14) and (15) was implemented in C and<br />

included as external discrete time controller. In<br />

that way we could use Bladed for controller<br />

testing.<br />

In the following figures behavior <strong>of</strong> the system<br />

when PID controller is used for rotor speed<br />

control is shown for one representative<br />

operating point ( v w = 15 m/s). <strong>Wind</strong> that was<br />

used for simulation observed positive and<br />

negative stepwise change shown in fig. 4.<br />

Responses <strong>of</strong> rotor speed, pitch angle and tower<br />

top displacement are shown in figs. 5. 6. and 7.<br />

respectively. From these figures it can be seen<br />

that rotor speed is well regulated and quickly<br />

compensated for the influences <strong>of</strong> wind speed<br />

changes. The pitch control actions are moderate<br />

without any oscillations. Similar results were<br />

obtained for all operating points <strong>through</strong>out<br />

wind turbine operating range.

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