Commit d1d4a073 authored by Søren Andersen's avatar Søren Andersen
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SJAN: Update with new control settings from Fanzhong

parent 36690732
Pipeline #19008 failed with stage
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......@@ -7,26 +7,26 @@ settings_dict = {1: 10000.0, # Rated power [kW]
5: 0.0 , # Minimum pitch angle, theta_min [deg], !NOTE THIS WAS CHANGED to 0.0 FOR THE PYTHON TEST
# if |theta_min|>90, then a table of <wsp,theta_min> is read #
# from a file named 'wptable.n', where n=int(theta_min)
6: 82.0, # Maximum pitch angle [deg]
6: 20.0, # Maximum pitch angle [deg]
7: 10.0, # Maximum pitch velocity operation [deg/s]
8: 0.4, # Frequency of generator speed filter [Hz]
9: 0.7, # Damping ratio of speed filter [-]
10: 1.80, # Frequency of free-free DT torsion mode [Hz], if zero no notch filter used
# Partial load control parameters
11: 13013100.0, # Optimal Cp tracking K factor [Nm/(rad/s)^2], #
11: 0.849245e7, # Optimal Cp tracking K factor [Nm/(rad/s)^2], #
# Qg=K*Omega^2, K=eta*0.5*rho*A*Cp_opt*R^3/lambda_opt^3
12: 0.683456e8, # Proportional gain of torque controller [Nm/(rad/s)]
13: 0.153367e8, # Integral gain of torque controller [Nm/rad]
12: 0.708251e8, # Proportional gain of torque controller [Nm/(rad/s)]
13: 0.158931e8, # Integral gain of torque controller [Nm/rad]
14: 0.0, # Differential gain of torque controller [Nm/(rad/s^2)]
# Full load control parameters
15: 1 , # Generator control switch [1=constant power, 0=constant torque]
16: 1.06713, # Proportional gain of pitch controller [rad/(rad/s)]
17: 0.242445, # Integral gain of pitch controller [rad/rad]
15: 0 , # Generator control switch [1=constant power, 0=constant torque]
16: 1.20206, # Proportional gain of pitch controller [rad/(rad/s)]
17: 0.234833, # Integral gain of pitch controller [rad/rad]
18: 0.0, # Differential gain of pitch controller [rad/(rad/s^2)]
19: 0.4e-8, # Proportional power error gain [rad/W]
20: 0.4e-8, # Integral power error gain [rad/(Ws)]
21: 11.4, # Coefficient of linear term in aerodynamic gain scheduling, KK1 [deg]
22: 402.9, # Coefficient of quadratic term in aerodynamic gain scheduling, KK2 [deg^2] &
21: 11.22739, # Coefficient of linear term in aerodynamic gain scheduling, KK1 [deg]
22: 464.10617, # Coefficient of quadratic term in aerodynamic gain scheduling, KK2 [deg^2] &
# (if zero, KK1 = pitch angle at double gain)
23: 1.3, # Relative speed for double nonlinear gain [-]
# Cut-in simulation parameters
......
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