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Figure 149: Collective flap response to collective wind: dashed line indicates open loop (no<br />

feedback control); each level of preview is indicated by the progression from blue to red.<br />

The notch near 0.7 Hz corresponds to the rejection of 1P loading that is provided by the<br />

augmented dynamics.<br />

in wind speed. This goal is evident in the frequency responses provided in Fig. 149.<br />

10.7.2 Controller Performance Simulations<br />

As shown in Fig. 148, TurbSim is used to generate wind speeds at the turbine that are<br />

consistent with the von Karman spectral model. Then the technique presented in Laks et al.<br />

(2013) is used to induce evolved wind speeds located at 60 evenly spaced azimuths that are at<br />

a measurement radius of r = 15 m (= 75% blade span). The evolution distance d = iTs×U<br />

is chosen based upon i samples at the control system sample rate of 20 Hz (= 1/Ts) and the<br />

nominal wind speed of U = 18 m/s.<br />

The controller is simulated using feedback only, and also with increments of i samples of<br />

preview<br />

Kff = Kw0 ··· Kwi 0 ··· 0 , (243)<br />

up to i = 10 samples. For previews 0 ≤ i ≤ 10, the controller uses gains up through Kwi,<br />

and for i > 10, the controller uses preview gains through Kw10. In the latter case, this is<br />

equivalent to taking measurements further than 1/2 s (at 18 m/s average wind speed) ahead<br />

of the turbine, and then waiting until those wind speeds are within 1/2 s of reaching the<br />

turbine before storing them in the feedforward MEMORY.<br />

ThecontrollerissimulatedusingthesamebaseTurbSimwindfieldfirstusingfeedbackonly,<br />

and then multiple times using feedback plus preview feedforward. For the preview simulations,<br />

evolved wind speed measurements are pre-computed for the base wind field at distances<br />

that correspond to preview times in the range [0.05,10] s (or preview distances in the range<br />

[0.9,180]m). The computationdonefor each distance produces60 time-varying measurement<br />

waveforms arranged spatially in a ring in front of the turbine as depicted in Fig. 133. As<br />

indicated in Fig. 148, the present rotor position θR(k) and speed ΩR(k) are used to predict<br />

1/2 s worth of blade rotation, and then the evolved wind speeds at the 60 azimuth locations<br />

are interpolated to the predicted blade positions. This gives the controller a preview of wind<br />

speeds that the blades will encounter over a 1/2 s horizon.<br />

There are three sets of measurements generated corresponding to (i) an ideal preview<br />

case without evolution, (ii) a set that includes the evolution model, and (iii) a set that<br />

uses evolution and lidar distortion as discussed in Section 10.5. The turbine and controller<br />

simulation is repeated for each set of pre-computed wind measurements and the RMS blade<br />

load and preview measurement error (relative to the wind at the blades) are computed. The<br />

<strong>DTU</strong> Wind Energy-E-Report-0029(EN) 213

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