Publishers version - DTU Orbit
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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