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Magnitude (abs)<br />

blade pitch<br />

gen speed<br />

10 5<br />

10 0<br />

10 −5<br />

10 −10<br />

10 0<br />

10 −10<br />

10 −4<br />

feedback only<br />

typical measurement<br />

perfect measurement<br />

10 −3<br />

Bode Diagram<br />

10 −2<br />

Frequency (Hz)<br />

Figure 151: Frequency responses of closed-loop transfer functions, with wind spectrum included,<br />

showing generator speed error and blade pitch actuation with H2 optimal combined<br />

feedforward/feedback control for the NREL 5-MW turbine at a 13 m/s wind speed operating<br />

point with 9 seconds of available preview time.<br />

lidar is removing high frequency content from the measurement, the remaining low frequency<br />

errors due to evolution do not become significant until at least 7 s (126 m) of preview, when<br />

even the low frequencies of turbulence have significantly evolved. Additional details regarding<br />

this control study can be found in Laks et al. (2013).<br />

10.8 Control Example 2: H2 Optimal Control with Model<br />

of Measurement Coherence<br />

In this section, an H2 optimal controller design is described where a model of wind measurement<br />

coherence is included in the design process. This combined feedforward/feedback<br />

controller is designed to minimize a weighted sum of RMS generator speed error and RMS<br />

blade pitch (deviation from the operating point) using the NREL 5-MW model, assuming the<br />

Kaimal wind spectrum, class B turbulence (medium turbulence) and the normal turbulence<br />

model (NTM) (Jonkman, 2009).<br />

Figure 151 shows the resulting closed-loop generator speed and pitch actuation responses<br />

for three different cases: feedback only, typical measurements (measurement coherence is<br />

modeled as the magnitude squared of a single-pole low-pass filter with bandwidth of 0.2 Hz),<br />

and perfect measurements. We see that with lidar measurements, generator speed error is<br />

improved at both lowand highfrequencies, and pitch actuationis reduced at highfrequencies.<br />

Figure 152 shows the magnitudes of the optimal controllers. As the lidar measurement<br />

improves, the feedforward controller action increases at low frequencies, and the feedback<br />

controller action decreases at low frequencies, freeing it to act more at mid frequencies if<br />

necessary. The decrease in low-frequency feedback action is helpful because feedback control<br />

performance is fundamentally limited by the Bode sensitivity integral (Franklin et al., 2006),<br />

which essentially says that a decrease in sensitivity to disturbance at one frequency must be<br />

balanced by an increase in sensitivity to disturbance at another frequency. When feedforward<br />

takes over at low frequencies, feedback can increase sensitivity to low-frequency disturbance,<br />

and therefore can decrease sensitivity to mid-frequency disturbance. Thus low-frequency wind<br />

measurements can lead to reductions in mid-frequency loads. This increase in mid-frequency<br />

feedbackactionoccursfortypicallidarmeasurements,butforperfectmeasurements,feedback<br />

is unnecessary because the feedforward controller takes over at all frequencies, assuming<br />

<strong>DTU</strong> Wind Energy-E-Report-0029(EN) 215<br />

10 −1<br />

10 0

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