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Magnitude Squared<br />

10 8<br />

10 7<br />

10 6<br />

10 5<br />

10 4<br />

|H |<br />

y0 ,u<br />

hh<br />

2<br />

|H |<br />

yv ,Δ<br />

v<br />

2<br />

|H |<br />

yh ,Δ<br />

h<br />

2<br />

Wind to Blade Root Bending Moment<br />

10 −2<br />

10 −1<br />

Frequency (Hz)<br />

Figure 146: Transfer functions from hub height wind speed uhh to the collective component<br />

of flapwise blade root bending moment y0 as well as the transfer functions from vertical<br />

shear ∆v and horizontal shear ∆h to the vertical component yv and horizontal component<br />

yh of blade root bending moment. The transfer functions correspond to the NREL 5-MW<br />

turbine model at above-rated wind speed 13 m/s including feedback control of blade pitch<br />

and generator torque.<br />

torque feedback control (Jonkman et al., 2009) using rotor speed measurements.<br />

Alidarmeasurementscenarioisproposedthatusesthreerotatingmeasurementstoestimate<br />

the three rotating blade effective wind speeds û1, û2, and û3, using Eq. (236). The collective<br />

and shear components of the wind are then estimated from the three lidar measurements<br />

using<br />

⎡<br />

⎡ ⎤<br />

ûhh ⎢<br />

⎣ ˆ∆v ⎦ = ⎢<br />

⎣<br />

ˆ∆h<br />

1<br />

3<br />

1<br />

3<br />

4<br />

3U cos(ψ) 4<br />

3U cosψ + 2π<br />

3<br />

− 4 4<br />

3U sin(ψ) −3U sinψ + 2π<br />

3<br />

<br />

1<br />

3<br />

4<br />

3U cosψ + 4π<br />

3<br />

<br />

4 −3U sinψ + 4π<br />

3<br />

<br />

<br />

10 0<br />

⎤<br />

⎡<br />

⎥<br />

⎥⎣<br />

⎦<br />

û1<br />

û2<br />

û3<br />

⎤<br />

⎦. (240)<br />

A measurement scenario based on the lidar scenario in Fig. 133 is investigated for the purpose<br />

of minimizing the variance of the three blade root bending moment components using lidarbased<br />

estimates of the collective and shear wind speed terms and ideal feedforward control<br />

(Eq. (216)). Since the three lidars rotate at the rotor speed to provide measurements of blade<br />

effective wind speed, the only design variables are the scan radius r and preview distance d.<br />

10.6.1 Optimizing the Measurement Scenario<br />

The design problem is formulated to minimize the variance of the blade root bending moment<br />

felt by the three blades. The measurement geometry is to be chosen to minimize the sum of<br />

the variances of the three bending moment components:<br />

(r ∗ ,d ∗ ) = argmin<br />

r,d<br />

<br />

Var(y0)+ 1 1<br />

Var(yv)+<br />

2 2 Var(yh)<br />

<br />

. (241)<br />

As a blade rotates through the wind field, it experiences the vertical and horizontal components<br />

of bending moment scaled by the cosine and sine of the azimuth angle ψ, respectively.<br />

Since variance is equivalent to the mean square value over time and thus azimuth angle, and<br />

the mean square value of a sinusoid is 1<br />

2<br />

, the factor of 1<br />

2<br />

appears in front of the vertical<br />

and horizontal terms in Eq. (241). Using Eq. (219) from Section 10.2.1 for calculating variance<br />

based on measurement coherence with feedforward control and optimal prefiltering, the<br />

<strong>DTU</strong> Wind Energy-E-Report-0029(EN) 209

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