Commit 42183484 authored by Jenni Rinker's avatar Jenni Rinker

retuning for 7.5 and report poles

parent f35b5dda
Pipeline #16271 passed with stage
in 4 minutes and 43 seconds
......@@ -361,26 +361,26 @@ begin dll; dlls used in model
constant 5 100.0 ; Minimum pitch angle, theta_min [deg],
; if |theta_min|>90, then a table of <wsp,theta_min> is read ;
; from a file named 'wptable.n', where n=int(theta_min)
constant 6 82.0 ; Maximum pitch angle [deg]
constant 6 90.0 ; Maximum pitch angle [deg]
constant 7 10.0 ; Maximum pitch velocity operation [deg/s]
constant 8 0.4 ; Frequency of generator speed filter [Hz]
constant 8 0.2 ; Frequency of generator speed filter [Hz]
constant 9 0.7 ; Damping ratio of speed filter [-]
constant 10 1.80 ; Frequency of free-free DT torsion mode [Hz], if zero no notch filter used
constant 10 1.85 ; Frequency of free-free DT torsion mode [Hz], if zero no notch filter used
; Partial load control parameters
constant 11 0.925933e7 ; Optimal Cp tracking K factor [Nm/(rad/s)^2], ;
constant 11 0.118011E+08 ; 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
constant 12 0.683456e8 ; Proportional gain of torque controller [Nm/(rad/s)]
constant 13 0.153367e8 ; Integral gain of torque controller [Nm/rad]
constant 12 0.708420E+08 ; Proportional gain of torque controller [Nm/(rad/s)]
constant 13 0.158969E+08 ; Integral gain of torque controller [Nm/rad]
constant 14 0.0 ; Differential gain of torque controller [Nm/(rad/s^2)]
; Full load control parameters
constant 15 1 ; Generator control switch [1=constant power, 0=constant torque]
constant 16 1.06713 ; Proportional gain of pitch controller [rad/(rad/s)]
constant 17 0.242445 ; Integral gain of pitch controller [rad/rad]
constant 16 0.373061E+03 ; Proportional gain of pitch controller [rad/(rad/s)]
constant 17 0.323595E+00 ; Integral gain of pitch controller [rad/rad]
constant 18 0.0 ; Differential gain of pitch controller [rad/(rad/s^2)]
constant 19 0.4e-8 ; Proportional power error gain [rad/W]
constant 20 0.4e-8 ; Integral power error gain [rad/(Ws)]
constant 21 11.4 ; Coefficient of linear term in aerodynamic gain scheduling, KK1 [deg]
constant 22 402.9 ; Coefficient of quadratic term in aerodynamic gain scheduling, KK2 [deg^2] &
constant 21 12.69412 ; Coefficient of linear term in aerodynamic gain scheduling, KK1 [deg]
constant 22 440.78045 ; Coefficient of quadratic term in aerodynamic gain scheduling, KK2 [deg^2] &
; (if zero, KK1 = pitch angle at double gain)
constant 23 1.3 ; Relative speed for double nonlinear gain [-]
; Cut-in simulation parameters
......
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