From d646b313e4204b84e60fed717cafa68e2b942728 Mon Sep 17 00:00:00 2001
From: dave <dave@dtu.dk>
Date: Tue, 5 Apr 2016 18:43:39 +0200
Subject: [PATCH] first test for prepost.Simulations: generating input files,
including data
---
.../demo_dlc/ref/data/minimal_demo_file.txt | 1 +
.../data/demo_dlc/ref/demo_dlc_remote.zip | Bin 0 -> 9358 bytes
.../demo_dlc/ref/htc/DLCs/dlc01_demos.xlsx | Bin 0 -> 6554 bytes
.../ref/htc/_master/demo_dlc_master_A0001.htc | 850 ++++++++++++++++++
.../dlc01_demos/dlc01_steady_wsp10_noturb.htc | 850 ++++++++++++++++++
.../dlc01_demos/dlc01_steady_wsp8_noturb.htc | 850 ++++++++++++++++++
.../dlc01_demos/dlc01_steady_wsp9_noturb.htc | 850 ++++++++++++++++++
.../dlc01_demos/dlc01_steady_wsp10_noturb.p | 55 ++
.../dlc01_demos/dlc01_steady_wsp8_noturb.p | 55 ++
.../dlc01_demos/dlc01_steady_wsp9_noturb.p | 55 ++
.../tests/data/demo_dlc/ref/prepost/A0001.pkl | Bin 0 -> 4418 bytes
.../data/demo_dlc/ref/prepost/A0001_tags.txt | 178 ++++
.../source/data/minimal_demo_file.txt | 1 +
.../data/demo_dlc/source/demo_dlc_remote.zip | Bin 0 -> 9358 bytes
.../demo_dlc/source/htc/DLCs/dlc01_demos.xlsx | Bin 0 -> 6554 bytes
.../htc/_master/demo_dlc_master_A0001.htc | 850 ++++++++++++++++++
wetb/prepost/tests/test_Simulations.py | 55 ++
17 files changed, 4650 insertions(+)
create mode 100644 wetb/prepost/tests/data/demo_dlc/ref/data/minimal_demo_file.txt
create mode 100644 wetb/prepost/tests/data/demo_dlc/ref/demo_dlc_remote.zip
create mode 100755 wetb/prepost/tests/data/demo_dlc/ref/htc/DLCs/dlc01_demos.xlsx
create mode 100755 wetb/prepost/tests/data/demo_dlc/ref/htc/_master/demo_dlc_master_A0001.htc
create mode 100644 wetb/prepost/tests/data/demo_dlc/ref/htc/dlc01_demos/dlc01_steady_wsp10_noturb.htc
create mode 100644 wetb/prepost/tests/data/demo_dlc/ref/htc/dlc01_demos/dlc01_steady_wsp8_noturb.htc
create mode 100644 wetb/prepost/tests/data/demo_dlc/ref/htc/dlc01_demos/dlc01_steady_wsp9_noturb.htc
create mode 100644 wetb/prepost/tests/data/demo_dlc/ref/pbs_in/dlc01_demos/dlc01_steady_wsp10_noturb.p
create mode 100644 wetb/prepost/tests/data/demo_dlc/ref/pbs_in/dlc01_demos/dlc01_steady_wsp8_noturb.p
create mode 100644 wetb/prepost/tests/data/demo_dlc/ref/pbs_in/dlc01_demos/dlc01_steady_wsp9_noturb.p
create mode 100755 wetb/prepost/tests/data/demo_dlc/ref/prepost/A0001.pkl
create mode 100755 wetb/prepost/tests/data/demo_dlc/ref/prepost/A0001_tags.txt
create mode 100644 wetb/prepost/tests/data/demo_dlc/source/data/minimal_demo_file.txt
create mode 100644 wetb/prepost/tests/data/demo_dlc/source/demo_dlc_remote.zip
create mode 100755 wetb/prepost/tests/data/demo_dlc/source/htc/DLCs/dlc01_demos.xlsx
create mode 100755 wetb/prepost/tests/data/demo_dlc/source/htc/_master/demo_dlc_master_A0001.htc
create mode 100644 wetb/prepost/tests/test_Simulations.py
diff --git a/wetb/prepost/tests/data/demo_dlc/ref/data/minimal_demo_file.txt b/wetb/prepost/tests/data/demo_dlc/ref/data/minimal_demo_file.txt
new file mode 100644
index 00000000..8db26215
--- /dev/null
+++ b/wetb/prepost/tests/data/demo_dlc/ref/data/minimal_demo_file.txt
@@ -0,0 +1 @@
+just one demo line
diff --git a/wetb/prepost/tests/data/demo_dlc/ref/demo_dlc_remote.zip b/wetb/prepost/tests/data/demo_dlc/ref/demo_dlc_remote.zip
new file mode 100644
index 0000000000000000000000000000000000000000..60fe434ad3dc15cf5e1dd1977c630107c611ac55
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diff --git a/wetb/prepost/tests/data/demo_dlc/ref/htc/DLCs/dlc01_demos.xlsx b/wetb/prepost/tests/data/demo_dlc/ref/htc/DLCs/dlc01_demos.xlsx
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literal 0
HcmV?d00001
diff --git a/wetb/prepost/tests/data/demo_dlc/ref/htc/_master/demo_dlc_master_A0001.htc b/wetb/prepost/tests/data/demo_dlc/ref/htc/_master/demo_dlc_master_A0001.htc
new file mode 100755
index 00000000..6e956f80
--- /dev/null
+++ b/wetb/prepost/tests/data/demo_dlc/ref/htc/_master/demo_dlc_master_A0001.htc
@@ -0,0 +1,850 @@
+;this version was at some point based on: Avatar_10MW_RWT version 1, 06-08-14, Anyd
+begin simulation;
+ time_stop [time stop];
+ solvertype 1 ; (newmark)
+ on_no_convergence continue ;
+; convergence_limits 1E3 1.0 1E-7 ;
+ logfile ./logfiles/[Case folder]/[Case id.].log ;
+ begin newmark;
+ deltat 0.02;
+ end newmark;
+end simulation;
+;
+;----------------------------------------------------------------------------------------------------------------------------------------------------------------
+begin new_htc_structure;
+;--------------------------------------------------------------------------------------------------
+[staircase] beam_output_file_name ./res_eigen/[Case folder]/[Case id.]/[Case id.]_beam.dat;
+[staircase] body_output_file_name ./res_eigen/[Case folder]/[Case id.]/[Case id.]_body.dat;
+[staircase] struct_inertia_output_file_name ./res_eigen/[Case folder]/[Case id.]/[Case id.]_struct.dat;
+[staircase] body_eigenanalysis_file_name ./res_eigen/[Case folder]/[Case id.]/[Case id.]_body_eigen.dat;
+[staircase] structure_eigenanalysis_file_name ./res_eigen/[Case folder]/[Case id.]/[Case id.]_strc_eigen.dat;
+;---------------------------------------------------------------------------------------------------
+ begin main_body; tower 123.6m
+ name tower ;
+ type timoschenko ;
+ nbodies 3 ;
+ node_distribution c2_def ;
+ damping_posdef 0 0 0 4.7E-03 4.7E-03 4.3E-04 ; tuned by Anyd 12/8/14
+ begin timoschenko_input;
+ filename ./data/AVATAR_10MW_RWT_tower_st.dat;
+ set 1 1 ;
+ end timoschenko_input;
+ begin c2_def; Definition of centerline (main_body coordinates)
+ nsec 20;
+ sec 1 0 0 0.000 0 ; x,y,z,twist
+ sec 2 0 0 -12.293 0 ;
+ sec 3 0 0 -12.294 0 ;
+ sec 4 0 0 -24.585 0 ;
+ sec 5 0 0 -24.586 0 ;
+ sec 6 0 0 -36.878 0 ;
+ sec 7 0 0 -36.879 0 ;
+ sec 8 0 0 -49.171 0 ;
+ sec 9 0 0 -49.172 0 ;
+ sec 10 0 0 -61.463 0 ;
+ sec 11 0 0 -61.464 0 ;
+ sec 12 0 0 -73.756 0 ;
+ sec 13 0 0 -73.757 0 ;
+ sec 14 0 0 -86.049 0 ;
+ sec 15 0 0 -86.050 0 ;
+ sec 16 0 0 -98.341 0 ;
+ sec 17 0 0 -98.342 0 ;
+ sec 18 0 0 -110.634 0 ;
+ sec 19 0 0 -110.635 0 ;
+ sec 20 0 0 -123.600 0 ;
+ end c2_def ;
+ end main_body;
+;
+ begin main_body;
+ name towertop ;
+ type timoschenko ;
+ nbodies 1 ;
+ node_distribution c2_def ;
+ damping_posdef 7.50E-03 7.40E-03 7.00E-03 7.00E-03 7.00E-03 7.00E-03 ; "changed by Anyd
+ concentrated_mass 2.0 0.0 2.6870E+00 3.0061E-01 4.4604E+05 4.1060E+06 4.1060E+05 4.1060E+06 ; Nacel
+ begin timoschenko_input;
+ filename ./data/DTU_10MW_RWT_Towertop_st.dat ;
+ set 1 2 ;
+ end timoschenko_input;
+ begin c2_def; Definition of centerline (main_body coordinates)
+ nsec 2;
+ sec 1 0.0 0.0 0.0 0.0 ; x,y,z,twist
+ sec 2 0.0 0.0 -2.75 0.0 ;
+ end c2_def ;
+ end main_body;
+;
+ begin main_body;
+ name shaft ;
+ type timoschenko ;
+ nbodies 1 ;
+ node_distribution c2_def ;
+; damping_posdef 8.00E-3 8.00E-03 8.00E-02 4.65E-04 4.65E-04 2.38E-02 ; "tuned by Anyd 22/2/13
+ damping_posdef 0.0 0.0 3.983E-03 4.65E-04 4.65E-04 3.983E-03 ; "tuned by Anyd 23/5/13 to 31.45 l
+ concentrated_mass 1.0 0.0 0.0 0.0 0.0 0.0 0.0 3.751E+06 ; generator equivalent slow shaft "re_tu
+ concentrated_mass 5.0 0.0 0.0 0.0 1.0552E+05 0.0 0.0 3.257E+05 ; hub mass and inertia; "re_tuned
+ begin timoschenko_input;
+ filename ./data/DTU_10MW_RWT_Shaft_st.dat ;
+ set 1 1 ;
+ end timoschenko_input;
+ begin c2_def; Definition of centerline (main_body coordinates)
+ nsec 5;
+ sec 1 0.0 0.0 0.0 0.0 ; Tower top x,y,z,twist
+ sec 2 0.0 0.0 1.5 0.0 ;
+ sec 3 0.0 0.0 3.0 0.0 ;
+ sec 4 0.0 0.0 4.4 0.0 ; Main bearing
+ sec 5 0.0 0.0 7.1 0.0 ; Rotor centre
+ end c2_def ;
+ end main_body;
+;
+ begin main_body;
+ name shaft_nonrotate ;
+ type timoschenko ;
+ nbodies 1 ;
+ node_distribution c2_def ;
+ damping_posdef 0.00E+00 0.00E+00 0.00E+00 1.0E-01 1.0E-01 1.0E-01 ;
+ begin timoschenko_input;
+ filename ./data/DTU_10MW_RWT_Shaft_st.dat ;
+ set 1 3; dummy light and stiff structure
+ end timoschenko_input;
+ begin c2_def;
+ nsec 2;
+ sec 1 0.0 0.0 0.0 0.0 ;
+ sec 2 0.0 0.0 0.1 0.0 ;
+ end c2_def;
+ end main_body;
+;
+ begin main_body;
+ name hub1 ;
+ type timoschenko ;
+ nbodies 1 ;
+ node_distribution c2_def ;
+ damping_posdef 2.00E-05 2.00E-05 2.00E-04 3.00E-06 3.00E-06 2.00E-05;
+ begin timoschenko_input;
+ filename ./data/DTU_10MW_RWT_Hub_st.dat ;
+ set 1 2 ;
+ end timoschenko_input;
+ begin c2_def; Definition of centerline (main_body coordinates)
+ nsec 2;
+ sec 1 0.0 0.0 0.0 0.0 ; x,y,z,twist
+ sec 2 0.0 0.0 2.8 0.0 ;
+ end c2_def ;
+ end main_body;
+;
+ begin main_body;
+ name hub2 ;
+ copy_main_body hub1;
+ end main_body;
+;
+ begin main_body;
+ name hub3 ;
+ copy_main_body hub1 ;
+ end main_body;
+;
+ begin main_body;
+ name blade1 ;
+ type timoschenko ;
+ nbodies 10 ;
+ node_distribution c2_def;
+; damping_posdef 0.0 0.0 0.0 2.5e-3 8.9e-4 3.2e-4 ; "Tuned by Anyd"
+; damping_posdef 0.0 0.0 0.0 1.5e-3 2.45e-3 3.2e-4 ; " 3% damping tuned by Anyd 20/02/12 unable to
+; damping_posdef 0.0 0.0 0.0 2.1e-3 1.9e-3 1.3e-4 ; " 3% damping tuned by Anyd 15/08/14 rev2
+ damping_posdef 0.0 0.0 0.0 1.68e-3 2.25e-3 1.0e-4 ; " 3% damping tuned by Anyd 16/12/14
+ begin timoschenko_input ;
+ filename ./data/AVATAR_10MW_RWT_Blade_st.dat ;
+ set 1 9 ;
+ end timoschenko_input;
+ begin c2_def;
+ nsec 27 ;
+ sec 1 -0.001 -0.001 0.000 -17.280 ;
+ sec 2 -0.005 -0.001 2.220 -17.280 ;
+ sec 3 -0.006 -0.000 4.440 -17.280 ;
+ sec 4 -0.086 0.022 6.660 -17.280 ;
+ sec 5 -0.231 0.069 11.039 -17.273 ;
+ sec 6 -0.447 0.121 15.418 -16.441 ;
+ sec 7 -0.690 0.161 19.797 -14.613 ;
+ sec 8 -0.812 0.162 24.176 -12.578 ;
+ sec 9 -0.891 0.158 28.555 -10.588 ;
+ sec 10 -0.865 0.124 32.934 -9.070 ;
+ sec 11 -0.833 0.112 37.313 -8.224 ;
+ sec 12 -0.797 0.102 41.692 -7.688 ;
+ sec 13 -0.760 0.093 46.071 -7.205 ;
+ sec 14 -0.721 0.083 50.450 -6.749 ;
+ sec 15 -0.683 0.075 54.829 -6.288 ;
+ sec 16 -0.644 0.066 59.208 -5.838 ;
+ sec 17 -0.606 0.058 63.587 -5.401 ;
+ sec 18 -0.567 0.050 67.966 -4.982 ;
+ sec 19 -0.529 0.044 72.345 -4.640 ;
+ sec 20 -0.492 0.037 76.724 -4.380 ;
+ sec 21 -0.456 0.032 81.103 -4.144 ;
+ sec 22 -0.422 0.026 85.482 -3.914 ;
+ sec 23 -0.392 0.021 89.861 -3.685 ;
+ sec 24 -0.346 0.014 94.240 -3.460 ;
+ sec 25 -0.307 0.010 96.190 -3.350 ;
+ sec 26 -0.249 0.005 98.130 -3.250 ;
+ sec 27 -0.089 0.006 100.080 -3.140 ;
+ end c2_def ;
+ end main_body;
+;
+ begin main_body;
+ name blade2 ;
+ copy_main_body blade1;
+ end main_body;
+;
+ begin main_body;
+ name blade3 ;
+ copy_main_body blade1 ;
+ end main_body;
+;-------------------------------------------------------------------------------------------------------------------------------
+;
+ begin orientation;
+ begin base;
+ body tower;
+ inipos 0.0 0.0 0.0 ; initial position of node 1
+ body_eulerang 0.0 0.0 0.0;
+ end base;
+;
+ begin relative;
+ body1 tower last;
+ body2 towertop 1;
+ body2_eulerang 0.0 0.0 0.0;
+ end relative;
+;
+ begin relative;
+ body1 towertop last;
+ body2 shaft 1;
+ body2_eulerang 90.0 0.0 0.0;
+ body2_eulerang 5.0 0.0 0.0; 5 deg tilt angle
+ body2_eulerang 0.0 0.0 [Rotor azimuth];
+[Free shaft rot] mbdy2_ini_rotvec_d1 0.0 0.0 -1.0 [init_wr] ; mbdy2_ini_rotvec_d1 0.0 0.0 -1.0 [init_wr];
+ end relative;
+;
+ begin relative; dummy non rotating hub coordinates
+ body1 towertop last;
+ body2 shaft_nonrotate 1;
+ body2_eulerang 90.0 0.0 0.0;
+ body2_eulerang 5.0 0.0 0.0; same 5 deg tilt angle as real shaft
+ end relative;
+;
+ begin relative;
+ body1 shaft last;
+ body2 hub1 1;
+ body2_eulerang -90.0 0.0 0.0;
+ body2_eulerang 0.0 180.0 0.0;
+ body2_eulerang 2.5 0.0 0.0; 2.5deg cone angle
+ end relative;
+;
+ begin relative;
+ body1 shaft last;
+ body2 hub2 1;
+ body2_eulerang -90.0 0.0 0.0;
+ body2_eulerang 0.0 60.0 0.0;
+ body2_eulerang 2.5 0.0 0.0; 2.5deg cone angle
+ end relative;
+;
+ begin relative;
+ body1 shaft last;
+ body2 hub3 1;
+ body2_eulerang -90.0 0.0 0.0;
+ body2_eulerang 0.0 -60.0 0.0;
+ body2_eulerang 2.5 0.0 0.0; 2.5deg cone angle
+ end relative;
+;
+ begin relative;
+ body1 hub1 last;
+ body2 blade1 1;
+ body2_eulerang 0.0 0.0 0;
+ end relative;
+;
+ begin relative;
+ body1 hub2 last;
+ body2 blade2 1;
+ body2_eulerang 0.0 0.0 0.0;
+ end relative;
+;
+ begin relative;
+ body1 hub3 last;
+ body2 blade3 1;
+ body2_eulerang 0.0 0.0 0.0;
+ end relative;
+;
+ end orientation;
+;-------------------------------------------------------------------------------------------------------------------------------
+begin constraint;
+;
+ begin fix0; fixed to ground in translation and rotation of node 1
+ body tower;
+ end fix0;
+;
+ begin fix1;
+ body1 tower last ;
+ body2 towertop 1;
+ end fix1;
+;
+[Free shaft rot] begin bearing1; free bearing
+[Free shaft rot] name shaft_rot;
+[Free shaft rot] body1 towertop last;
+[Free shaft rot] body2 shaft 1;
+[Free shaft rot] bearing_vector 2 0.0 0.0 -1.0; x=coo (0=global.1=body1.2=body2) vector in body2 coordinates where the free rotation is present
+[Free shaft rot] end bearing1;
+;
+[Rotor locked] begin bearing3; free bearing
+[Rotor locked] name shaft_rot;
+[Rotor locked] body1 towertop last;
+[Rotor locked] body2 shaft 1;
+[Rotor locked] bearing_vector 2 0.0 0.0 -1.0; x=coo (0=global.1=body1.2=body2) vector in body2 coordinates where the free rotation is present
+[Rotor locked] omegas 0.0 ;
+[Rotor locked] end bearing3;
+;
+ begin fix1;
+ body1 tower last ;
+ body2 shaft_nonrotate 1;
+ end fix1;
+;
+ begin fix1;
+ body1 shaft last ;
+ body2 hub1 1;
+ end fix1;
+;
+ begin fix1;
+ body1 shaft last ;
+ body2 hub2 1;
+ end fix1;
+;
+ begin fix1;
+ body1 shaft last ;
+ body2 hub3 1;
+ end fix1;
+;
+ begin bearing2;
+ name pitch1;
+ body1 hub1 last;
+ body2 blade1 1;
+ bearing_vector 2 0.0 0.0 -1.0;
+ end bearing2;
+;
+ begin bearing2;
+ name pitch2;
+ body1 hub2 last;
+ body2 blade2 1;
+ bearing_vector 2 0.0 0.0 -1.0;
+ end bearing2;
+;
+ begin bearing2;
+ name pitch3;
+ body1 hub3 last;
+ body2 blade3 1;
+ bearing_vector 2 0.0 0.0 -1.0;
+ end bearing2;
+end constraint;
+;
+end new_htc_structure;
+;----------------------------------------------------------------------------------------------------------------------------------------------------------------
+begin wind ;
+ density 1.225 ;
+ wsp [Windspeed] ;
+ tint [TI] ;
+ horizontal_input 1 ;
+ windfield_rotations [wdir] 8.0 0.0 ; yaw, tilt (positive=upflow=wind coming from below), rotation
+ center_pos0 0.0 0.0 -127 ; hub heigth
+ shear_format 3 [shear_exp] ;
+ turb_format [tu_model] ; 0=none, 1=mann,2=flex
+ tower_shadow_method 3 ; 0=none, 1=potential flow, 2=jet
+ scale_time_start [t0] ;
+ wind_ramp_factor 0.0 [t0] [wsp factor] 1.0 ;
+ [gust] iec_gust [gust_type] [G_A] [G_phi0] [G_t0] [G_T] ;
+;
+[staircase] wind_ramp_abs 400.0 401.0 0.0 1.0 ; wsp. after the step: 5.0
+[staircase] wind_ramp_abs 501.0 502.0 0.0 1.0 ; wsp. after the step: 6.0
+[staircase] wind_ramp_abs 602.0 603.0 0.0 1.0 ; wsp. after the step: 7.0
+[staircase] wind_ramp_abs 703.0 704.0 0.0 1.0 ; wsp. after the step: 8.0
+[staircase] wind_ramp_abs 804.0 805.0 0.0 1.0 ; wsp. after the step: 9.0
+[staircase] wind_ramp_abs 905.0 906.0 0.0 1.0 ; wsp. after the step: 10.0
+[staircase] wind_ramp_abs 1006.0 1007.0 0.0 1.0 ; wsp. after the step: 11.0
+[staircase] wind_ramp_abs 1107.0 1108.0 0.0 1.0 ; wsp. after the step: 12.0
+[staircase] wind_ramp_abs 1208.0 1209.0 0.0 1.0 ; wsp. after the step: 13.0
+[staircase] wind_ramp_abs 1309.0 1310.0 0.0 1.0 ; wsp. after the step: 14.0
+[staircase] wind_ramp_abs 1410.0 1411.0 0.0 1.0 ; wsp. after the step: 15.0
+[staircase] wind_ramp_abs 1511.0 1512.0 0.0 1.0 ; wsp. after the step: 16.0
+[staircase] wind_ramp_abs 1612.0 1613.0 0.0 1.0 ; wsp. after the step: 17.0
+[staircase] wind_ramp_abs 1713.0 1714.0 0.0 1.0 ; wsp. after the step: 18.0
+[staircase] wind_ramp_abs 1814.0 1815.0 0.0 1.0 ; wsp. after the step: 19.0
+[staircase] wind_ramp_abs 1915.0 1916.0 0.0 1.0 ; wsp. after the step: 20.0
+[staircase] wind_ramp_abs 2016.0 2017.0 0.0 1.0 ; wsp. after the step: 21.0
+[staircase] wind_ramp_abs 2117.0 2118.0 0.0 1.0 ; wsp. after the step: 22.0
+[staircase] wind_ramp_abs 2218.0 2219.0 0.0 1.0 ; wsp. after the step: 23.0
+[staircase] wind_ramp_abs 2319.0 2320.0 0.0 1.0 ; wsp. after the step: 24.0
+[staircase] wind_ramp_abs 2420.0 2421.0 0.0 1.0 ; wsp. after the step: 25.0
+ ;
+[windramp] wind_ramp_abs 400.0 2200.0 0.0 21.0 ; wsp. after the step: 25.0
+[windramp] wind_ramp_abs 2400.0 4200.0 0.0 -21.0 ; wsp. after the step: 25.0
+ ;
+ begin mann ;
+ create_turb_parameters 29.4 1.0 3.9 [tu_seed] 1.0 ; L, alfaeps, gamma, seed, highfrq compensation
+ filename_u ./[turb_dir][Turb base name]u.bin ;
+ filename_v ./[turb_dir][Turb base name]v.bin ;
+ filename_w ./[turb_dir][Turb base name]w.bin ;
+ box_dim_u 8192 [turb_dx] ;
+ box_dim_v 32 7.5;
+ box_dim_w 32 7.5;
+ std_scaling 1.0 0.7 0.5 ;
+ end mann ;
+;
+ begin tower_shadow_potential_2;
+ tower_mbdy_link tower;
+ nsec 2;
+ radius 0.0 4.15 ;
+ radius 123.6 2.75 ; (radius)
+ end tower_shadow_potential_2;
+end wind;
+;
+begin aerodrag ;
+ begin aerodrag_element ;
+ mbdy_name tower;
+ aerodrag_sections uniform 10 ;
+ nsec 2 ;
+ sec 0.0 0.6 8.3 ; tower bottom
+ sec 123.6 0.6 5.5 ; tower top (diameter)
+ end aerodrag_element;
+;
+ begin aerodrag_element ; Nacelle drag side
+ mbdy_name shaft;
+ aerodrag_sections uniform 2 ;
+ nsec 2 ;
+ sec 0.0 0.8 10.0 ;
+ sec 7.01 0.8 10.0 ;
+ end aerodrag_element;
+end aerodrag;
+;
+begin aero ;
+ nblades 3;
+ hub_vec shaft -3 ; rotor rotation vector (normally shaft composant directed from pressure to sustion side)
+ link 1 mbdy_c2_def blade1;
+ link 2 mbdy_c2_def blade2;
+ link 3 mbdy_c2_def blade3;
+ ae_filename ./data/AVATAR_10MW_RWT_ae.dat ;
+ pc_filename ./data/AVATAR_10MW_RWT_pc_hama_v1.dat ;
+ induction_method [Induction] ; 0=none, 1=normal
+ aerocalc_method 1 ; 0=ingen aerodynamic, 1=med aerodynamic
+ aero_distribution ae_file 1 ;
+ ae_sets 1 1 1;
+ tiploss_method 1 ; 0=none, 1=prandtl
+ dynstall_method [Dyn stall] ; 0=none, 1=stig øye method,2=mhh method
+;
+; ; --- Flaps --- ;
+ ; begin dynstall_ateflap ;
+ ; Ais 0.165 0.335 0.0 ;
+ ; Bis 0.0455 0.30 0.30 ;
+ ; flap 59.5925 85.5023 ./data/Flap_dturwt1_Thk24.ds ; Flap Sec: 1
+ ; end dynstall_ateflap;
+end aero ;
+;-------------------------------------------------------------------------------------------------
+begin dll;
+;
+ begin type2_dll;
+ name risoe_controller ;
+ filename ./control/risoe_controller.dll ;
+ dll_subroutine_init init_regulation ;
+ dll_subroutine_update update_regulation ;
+ arraysizes_init 52 1 ;
+ arraysizes_update 12 100 ;
+ begin init ;
+ ; Overall parameters
+ constant 1 10000.0 ; Rated power [kW]
+ constant 2 0.628 ; Minimum rotor speed [rad/s]
+ constant 3 1.005 ; Rated rotor speed [rad/s]
+ constant 4 15.6E+06 ; Maximum allowable generator torque [Nm]
+ 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 'wpdata.n', where n=int(theta_min)
+ 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 9 0.7 ; Damping ratio of speed filter [-]
+ constant 10 1.64 ; Frequency of free-free DT torsion mode [Hz], if zero no notch filter used
+ ; Partial load control parameters
+ constant 11 0.9648030e+07 ; 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 1.047610E+08 ; Proportional gain of torque controller [Nm/(rad/s)]
+ constant 13 0.153367E+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, 2=constant torque]
+ constant 16 0.762489 ; Proportional gain of pitch controller [rad/(rad/s)]
+ constant 17 0.224086 ; Integral gain of pitch controller [rad/rad]
+ constant 18 0.0 ; Differential gain of pitch controller [rad/(rad/s^2)]
+ constant 19 0.4e-9 ; Proportional power error gain [rad/W]
+ constant 20 0.4e-9 ; Integral power error gain [rad/(Ws)]
+ constant 21 10.6824 ; Coefficient of linear term in aerodynamic gain scheduling, KK1 [deg]
+ constant 22 601.25499 ; 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
+ constant 24 [Cut-in time] ; Cut-in time [s]
+ constant 25 1.0 ; Time delay for soft start of torque [1/1P]
+; Cut-out simulation parameters
+ constant 26 [Cut-out time] ; Cut-out time [s]
+ constant 27 5.0 ; Time constant for linear torque cut-out [s]
+ constant 28 [Stop type] ; Stop type [1=normal, 2=emergency]
+ constant 29 1.0 ; Time delay for pitch stop after shut-down signal [s]
+ constant 30 [Pitvel 1] ; Maximum pitch velocity during initial period of stop [deg/s]
+ constant 31 3.0 ; Time period of initial pitch stop phase [s] (maintains pitch speed specified in constant 30)
+ constant 32 [Pitvel 2] ; Maximum pitch velocity during final phase of stop [deg/s]
+; Expert parameters (keep default values unless otherwise given)
+ constant 33 2.0 ; Lower angle above lowest minimum pitch angle for switch [deg]
+ constant 34 2.0 ; Upper angle above lowest minimum pitch angle for switch [deg], if equal then hard switch
+ constant 35 95.0 ; Ratio between filtered speed and reference speed for fully open torque limits [%]
+ constant 36 2.0 ; Time constant of 1st order filter on wind speed used for minimum pitch [1/1P]
+ constant 37 1.0 ; Time constant of 1st order filter on pitch angle used for gain scheduling [1/1P]
+; Drivetrain damper
+ constant 38 0.0 ; Proportional gain of active DT damper [Nm/(rad/s)], requires frequency in input 10
+; Over speed
+ constant 39 25.0 ; Overspeed percentage before initiating turbine controller alarm (shut-down) [%]
+; Additional non-linear pitch control term (not used when all zero)
+ constant 40 0.0 ; Err0 [rad/s]
+ constant 41 0.0 ; ErrDot0 [rad/s^2]
+ constant 42 0.0 ; PitNonLin1 [rad/s]
+; Storm control command
+ constant 43 28.0 ; Wind speed 'Vstorm' above which derating of rotor speed is used [m/s]
+ constant 44 28.0 ; Cut-out wind speed (only used for derating of rotor speed in storm) [m/s]
+; Safety system parameters
+ constant 45 25.0 ; Overspeed percentage before initiating safety system alarm (shut-down) [%]
+ constant 46 1.5 ; Max low-pass filtered tower top acceleration level [m/s^2] - max in DLC 1.3=1.1 m/s^2
+; Turbine parameter
+ constant 47 205.8 ; Nominal rotor diameter [m]
+; Parameters for rotor inertia reduction in variable speed region
+ constant 48 0.0 ; Proportional gain on rotor acceleration in variable speed region [Nm/(rad/s^2)] (not used when zero)
+; Parameters for alternative partial load controller with PI regulated TSR tracking
+ constant 49 0.0 ; Optimal tip speed ratio [-] (only used when K=constant 11 = 0 otherwise Qg=K*Omega^2 is used)
+; Parameters for adding aerodynamic drivetrain damping on gain scheduling
+ constant 50 0.0 ; Proportional gain of aerodynamic DT damping [Nm/(rad/s)]
+ constant 51 0.0 ; Coefficient of linear term in aerodynamic DT damping scheduling, KK1 [deg]
+ constant 52 0.0 ; Coefficient of quadratic term in aerodynamic DT damping scheduling, KK2 [deg^2]
+ end init ;
+;
+ begin output ;
+ general time ; [s]
+ constraint bearing1 shaft_rot 1 only 2 ; Drivetrain speed [rad/s]
+ constraint bearing2 pitch1 1 only 1; [rad]
+ constraint bearing2 pitch2 1 only 1; [rad]
+ constraint bearing2 pitch3 1 only 1; [rad]
+ wind free_wind 1 0.0 0.0 -127 ; Global coordinates at hub height
+ dll inpvec 2 2 ; Elec. power from generator servo .dll
+ dll inpvec 2 8 ; Grid state flag from generator servo .dll
+ mbdy state acc tower 10 1.0 global only 1 ; Tower top x-acceleration [m/s^2]
+ mbdy state acc tower 10 1.0 global only 2 ; Tower top y-acceleration [m/s^2]
+ end output;
+ end type2_dll;
+;
+ begin type2_dll;
+ name generator_servo ;
+ filename ./control/generator_servo.dll ;
+ dll_subroutine_init init_generator_servo ;
+ dll_subroutine_update update_generator_servo ;
+ arraysizes_init 7 1 ;
+ arraysizes_update 4 8 ;
+ begin init ;
+ constant 1 20.0 ; Frequency of 2nd order servo model of generator-converter system [Hz]
+ constant 2 0.9 ; Damping ratio 2nd order servo model of generator-converter system [-]
+ constant 3 15.6E+06 ; Maximum allowable LSS torque (pull-out torque) [Nm]
+ constant 4 0.94 ; Generator efficiency [-]
+ constant 5 1.0 ; Gearratio [-]
+ constant 6 0.0 ; Time for half value in softstart of torque [s]
+ constant 7 [Grid loss time] ; Time for grid loss [s]
+ end init ;
+;
+ begin output;
+ general time ; Time [s]
+ dll inpvec 1 1 ; Electrical torque reference [Nm]
+ constraint bearing1 shaft_rot 1 only 2; Generator LSS speed [rad/s]
+ mbdy momentvec shaft 1 1 shaft only 3 ; Shaft moment [kNm] (Qshaft)
+ end output;
+;
+ begin actions;
+ mbdy moment_int shaft 1 -3 shaft towertop 2 ; Generator LSS torque [Nm]
+ end actions;
+ end type2_dll;
+;
+ begin type2_dll;
+ name mech_brake ;
+ filename ./control/mech_brake.dll ;
+ dll_subroutine_init init_mech_brake ;
+ dll_subroutine_update update_mech_brake ;
+ arraysizes_init 7 1 ;
+ arraysizes_update 4 6 ;
+ begin init ;
+ constant 1 5225.35 ; Fully deployed maximum brake torque [Nm] (0.6*max torque)
+ constant 2 100.0 ; Parameter alpha used in Q = tanh(omega*alpha), typically 1e2/Omega_nom
+ constant 3 0.5 ; Delay time for before brake starts to deploy [s]
+ constant 4 0.74 ; Time for brake to become fully deployed [s]
+ end init ;
+;
+ begin output;
+ general time ; Time [s]
+ constraint bearing1 shaft_rot 1 only 2 ; Generator LSS speed [rad/s]
+ dll inpvec 1 25 ; Command to deploy mechanical disc brake [0,1]
+ end output;
+;
+ begin actions;
+ mbdy moment_int shaft 1 -3 shaft towertop 2 ; Generator LSS torque [Nm]
+ end actions;
+ end type2_dll;
+;
+ begin type2_dll;
+ name servo_with_limits ;
+ filename ./control/servo_with_limits.dll ;
+ dll_subroutine_init init_servo_with_limits ;
+ dll_subroutine_update update_servo_with_limits ;
+ arraysizes_init 10 1 ;
+ arraysizes_update 5 9 ;
+ begin init ;
+ constant 1 3 ; Number of blades [-]
+ constant 2 1.0 ; Frequency of 2nd order servo model of pitch system [Hz]
+ constant 3 0.7 ; Damping ratio 2nd order servo model of pitch system [-]
+ constant 4 10.0 ; Max. pitch speed [deg/s]
+ constant 5 15.0 ; Max. pitch acceleration [deg/s^2]
+ constant 6 -5.0 ; Min. pitch angle [deg]
+ constant 7 90.0 ; Max. pitch angle [deg]
+ constant 8 [Time pitch runaway] ; Time for pitch runaway [s]
+ constant 9 [Time stuck DLC22b] ; Time for stuck blade 1 [s]
+ constant 10 [Pitch 1 DLC22b] ; Angle of stuck blade 1 [deg]
+ end init ;
+ begin output;
+ general time ; Time [s]
+ dll inpvec 1 2 ; Pitch1 demand angle [rad]
+ dll inpvec 1 3 ; Pitch2 demand angle [rad]
+ dll inpvec 1 4 ; Pitch3 demand angle [rad]
+ dll inpvec 1 26 ; Flag for emergency pitch stop [0=off/1=on]
+ end output;
+;
+ begin actions;
+ constraint bearing2 angle pitch1 ; Angle pitch1 bearing [rad]
+ constraint bearing2 angle pitch2 ; Angle pitch2 bearing [rad]
+ constraint bearing2 angle pitch3 ; Angle pitch3 bearing [rad]
+ end actions;
+ end type2_dll;
+;
+; --- DLL for tower-blade tip distance -- ;
+ begin type2_dll;
+ name disttowtip ;
+ filename ./control/towclearsens.dll ;
+ dll_subroutine_init initialize ;
+ dll_subroutine_update update ;
+ arraysizes_init 1 1 ;
+ arraysizes_update 12 4 ;
+ begin init ;
+ constant 1 3.87 ; Tower radius close to downward blade tip [m]
+ end init ;
+ begin output;
+ mbdy state pos tower 5 0.00 global ; [1,2,3]. Tower position: 24.58 m
+ mbdy state pos blade1 26 1.0 global ; [4,5,6]
+ mbdy state pos blade2 26 1.0 global ; [7,8,9]
+ mbdy state pos blade3 26 1.0 global ; [10,11,12]
+ end output;
+ end type2_dll;
+end dll;
+;
+;----------------------------------------------------------------------------------------------------------------------------------------------------------------
+;
+begin output;
+ filename ./res/[Case folder]/[Case id.] ;
+ time [t0] [time stop] ;
+ data_format [out_format];
+ buffer 1 ;
+;
+ general time;
+ constraint bearing1 shaft_rot 2; angle and angle velocity
+ constraint bearing2 pitch1 5; angle and angle velocity
+ constraint bearing2 pitch2 5; angle and angle velocity
+ constraint bearing2 pitch3 5; angle and angle velocity
+ aero omega ;
+ aero torque;
+ aero power;
+ aero thrust;
+ wind free_wind 1 0.0 0.0 -127; local wind at fixed position: coo (1=global,2=non-rotation rotor coo.), pos x, pos y, pos z
+ ; non rotating coordinates shaft tip: equivalent to stationary hub in BLADED
+ mbdy momentvec shaft 3 2 shaft_nonrotate # non rotating shaft tip ;
+ mbdy forcevec shaft 3 2 shaft_nonrotate # non rotating shaft tip ;
+ ; Moments:
+ mbdy momentvec tower 1 1 tower # tower base ;
+ mbdy momentvec tower 19 2 tower # tower yaw bearing ;
+ mbdy momentvec shaft 4 1 shaft # main bearing ;
+ mbdy momentvec blade1 3 2 blade1 # blade 1 root ;
+ mbdy momentvec blade2 3 2 blade2 # blade 2 root ;
+ mbdy momentvec blade3 3 2 blade3 # blade 3 root ;
+ ; blade 2,3 root section loads
+ mbdy momentvec blade2 3 2 local # blade 2 section root;
+ mbdy momentvec blade3 3 2 local # blade 3 section root;
+ ; blade 1 sectional loads in local coordinates
+ mbdy momentvec blade1 2 2 local # blade 1 section;
+ mbdy momentvec blade1 3 2 local # blade 1 section root;
+ mbdy momentvec blade1 4 2 local # blade 1 section;
+ mbdy momentvec blade1 5 2 local # blade 1 section;
+ mbdy momentvec blade1 6 2 local # blade 1 section;
+ mbdy momentvec blade1 7 2 local # blade 1 section;
+ mbdy momentvec blade1 8 2 local # blade 1 section;
+ mbdy momentvec blade1 9 2 local # blade 1 section;
+ mbdy momentvec blade1 10 2 local # blade 1 section;
+ mbdy momentvec blade1 11 2 local # blade 1 section;
+ mbdy momentvec blade1 12 2 local # blade 1 section;
+ mbdy momentvec blade1 13 2 local # blade 1 section;
+ mbdy momentvec blade1 14 2 local # blade 1 section;
+ mbdy momentvec blade1 15 2 local # blade 1 section;
+ mbdy momentvec blade1 16 2 local # blade 1 section;
+ mbdy momentvec blade1 17 2 local # blade 1 section;
+ mbdy momentvec blade1 18 2 local # blade 1 section;
+ mbdy momentvec blade1 19 2 local # blade 1 section;
+ mbdy momentvec blade1 20 2 local # blade 1 section;
+ mbdy momentvec blade1 21 2 local # blade 1 section;
+ mbdy momentvec blade1 22 2 local # blade 1 section;
+ mbdy momentvec blade1 23 2 local # blade 1 section;
+ mbdy momentvec blade1 24 2 local # blade 1 section;
+ mbdy momentvec blade1 25 2 local # blade 1 section;
+ mbdy momentvec blade1 26 2 local # blade 1 section;
+ ; blade root out and in of plane forces
+ mbdy momentvec blade1 3 2 hub1 # blade 1 root ;
+ mbdy momentvec blade2 3 2 hub2 # blade 2 root ;
+ mbdy momentvec blade3 3 2 hub3 # blade 3 root ;
+; mbdy momentvec blade1 14 1 local # blade 1 50% local e coo ;
+; mbdy momentvec blade2 14 1 local # blade 2 50% local e coo ;
+; mbdy momentvec blade3 14 1 local # blade 3 50% local e coo ;
+ ; Displacements and accellerations
+ mbdy state pos tower 19 1.0 global only 1 # Tower top FA displ;
+ mbdy state pos tower 19 1.0 global only 2 # Tower top SS displ;
+ mbdy state acc tower 19 1.0 global only 1 # Tower top FA acc;
+ mbdy state acc tower 19 1.0 global only 2 # Tower top SS acc;
+;
+ mbdy state pos blade1 26 1.0 global # gl blade 1 tip pos ;
+ mbdy state pos blade2 26 1.0 global # gl blade 2 tip pos ;
+ mbdy state pos blade3 26 1.0 global # gl blade 3 tip pos ;
+ mbdy state pos blade1 26 1.0 blade1 # blade 1 tip pos ;
+ mbdy state pos blade2 26 1.0 blade2 # blade 2 tip pos ;
+ mbdy state pos blade3 26 1.0 blade3 # blade 3 tip pos ;
+;
+ mbdy state pos tower 5 0.00 global ; [1,2,3]. Tower position: 24.58 m
+;
+ ; elastic twist (torsional deformation) along the blade
+ aero tors_ang 1 45.56;
+ aero tors_ang 1 59.19;
+ aero tors_ang 1 70.87;
+ aero tors_ang 1 80.61;
+ aero tors_ang 1 84.50;
+ aero tors_ang 1 88.40;
+ aero tors_ang 1 92.29;
+ aero tors_ang 1 96.19;
+ aero tors_ang 1 98.13;
+ aero tors_ang 1 100.08; tip
+;
+; - Monitor Aerodynamics - ;
+ aero windspeed 3 1 1 72.5;
+ aero alfa 1 72.5;
+ aero alfa 2 72.5;
+ aero alfa 3 72.5;
+ aero cl 1 72.5;
+ aero cl 2 72.5;
+ aero cl 3 72.5;
+ aero cd 1 72.5;
+ aero cd 2 72.5;
+ aero cd 3 72.5;
+; - Main Controller -
+; Output to controller
+ ; dll outvec 1 1 # time;
+ ; dll outvec 1 2 # slow speed shaft rad/s;
+ ; dll outvec 1 3 # pitch angle 1;
+ ; dll outvec 1 4 # pitch angle 2;
+ ; dll outvec 1 5 # pitch angle 3;
+ ; dll outvec 1 6 # WSP_x_global;
+ ; dll outvec 1 7 # WSP_y_global;
+ ; dll outvec 1 8 # WSP_z_global;
+ ; dll outvec 1 9 # Elec. pwr ;
+ ; dll outvec 1 10 # Grid flag ;
+; Input from controller
+ dll inpvec 1 1 # Generator torque reference [Nm] ;
+ dll inpvec 1 2 # Pitch angle reference of blade 1 [rad] ;
+ dll inpvec 1 3 # Pitch angle reference of blade 2 [rad] ;
+ dll inpvec 1 4 # Pitch angle reference of blade 3 [rad] ;
+ ; dll inpvec 1 5 # Power reference [W] ;
+ ; dll inpvec 1 6 # Filtered wind speed [m/s] ;
+ ; dll inpvec 1 7 # Filtered rotor speed [rad/s];
+ ; dll inpvec 1 8 # Filtered rotor speed error for torque [rad/s];
+ ; dll inpvec 1 9 # Bandpass filtered rotor speed [rad/s];
+ ; dll inpvec 1 10 # Proportional term of torque contr. [Nm] ;
+ ; dll inpvec 1 11 # Integral term of torque controller [Nm] ;
+ ; dll inpvec 1 12 # Minimum limit of torque [Nm] ;
+ ; dll inpvec 1 13 # Maximum limit of torque [Nm] ;
+ dll inpvec 1 14 # Torque limit switch based on pitch [-] ;
+ ; dll inpvec 1 15 # Filtered rotor speed error for pitch [rad/s];
+ ; dll inpvec 1 16 # Power error for pitch [W] ;
+ ; dll inpvec 1 17 # Proportional term of pitch controller [rad] ;
+ ; dll inpvec 1 18 # Integral term of pitch controller [rad] ;
+ ; dll inpvec 1 19 # Minimum limit of pitch [rad] ;
+ ; dll inpvec 1 20 # Maximum limit of pitch [rad] ;
+ dll inpvec 1 21 # Torque reference from DT dammper [Nm] ;
+ dll inpvec 1 22 # Status signal [-] ;
+ ; dll inpvec 1 23 # Total added pitch rate [rad/s] ;
+ dll inpvec 1 24 # Filtered Mean pitch for gain sch [rad] ;
+ dll inpvec 1 25 # Flag for mechnical brake [0=off/1=on] ;
+ dll inpvec 1 26 # Flag for emergency pitch stop [0=off/1=on] ;
+ dll inpvec 1 27 # LP filtered acceleration level [m/s^2] ;
+; ; Output to generator model
+ ; dll outvec 2 1 # time ;
+ ; dll outvec 2 2 # Electrical torque reference [Nm] ;
+ ; dll outvec 2 3 # omega LSS ;
+; Input from generator model
+ dll inpvec 2 1 # Mgen LSS [Nm];
+ dll inpvec 2 2 # Pelec W ;
+ dll inpvec 2 3 # Mframe ;
+ dll inpvec 2 4 # Mgen HSS ;
+ dll inpvec 2 5 # Generator Pmech kW ;
+ dll inpvec 2 6 # Filtered Gen speed ;
+ dll inpvec 2 7 # Resulting Eff ;
+ dll inpvec 2 8 # Grid flag ;
+; Output to mechanical brake
+ dll inpvec 3 1 # Brake torque [Nm] ;
+; ; Input from mechanical brake
+ ; dll outvec 3 1 # Time [s] ;
+ ; dll outvec 3 2 # Generator LSS speed [rad/s] ;
+ ; dll outvec 3 3 # Deploy brake ;
+; ; Output to pitch servo
+ ; dll outvec 4 1 # time;
+ ; dll outvec 4 2 # pitchref 1;
+ ; dll outvec 4 3 # pitchref 2;
+ ; dll outvec 4 4 # pitchref 3;
+ ; dll outvec 4 5 # Emerg. stop;
+; Input from pitch servo
+ dll inpvec 4 1 # pitch 1;
+ dll inpvec 4 2 # pitch 2;
+ dll inpvec 4 3 # pitch 3;
+; Check tower clearence
+ dll inpvec 5 1 # Bltip tow min d [m];
+; general constant 1.0 ; constant 1.0 - to mesure activity of flap in terms of displacement
+; - Check on flap control:
+ ; ; - From flap controller: -
+ ; dll type2_dll cyclic_flap_controller inpvec 1 # Ref flap signal bl 1 [deg] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 2 # Ref flap signal bl 2 [deg] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 3 # Ref flap signal bl 3 [deg] ;
+ ; ; - Mbc values
+ ; dll type2_dll cyclic_flap_controller inpvec 4 # momvec mbc cos [kNm] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 5 # momvec mbc sin [kNm] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 6 # momvec mbc filt cos [kNm] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 7 # momvec mbc filt sin [kNm] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 8 # flap mbc cos [deg] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 9 # flap mbc sin [deg] ;
+ ; ; - Check Gains - ;
+ ; dll type2_dll cyclic_flap_controller inpvec 10 # lead angle [deg] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 11 # scaling on rat pow [-] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 12 # actual kp [deg/kNm] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 13 # actual ki [deg/kNms] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 14 # actual kd [deg s/kNm] ;
+ ; ; - Actual deflections -
+ ; [dis_setbeta] aero beta 1 1 ;
+ ; [dis_setbeta] aero beta 2 1 ;
+ ; [dis_setbeta] aero beta 3 1 ;
+ ; ; - Mbc values
+ ; dll type2_dll cyclic_flap_controller inpvec 4 # momvec mbc cos [kNm] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 5 # momvec mbc sin [kNm] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 6 # momvec mbc filt cos [kNm] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 7 # momvec mbc filt sin [kNm] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 8 # flap mbc cos [deg] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 9 # flap mbc sin [deg] ;
+end output;
+;
+exit;
diff --git a/wetb/prepost/tests/data/demo_dlc/ref/htc/dlc01_demos/dlc01_steady_wsp10_noturb.htc b/wetb/prepost/tests/data/demo_dlc/ref/htc/dlc01_demos/dlc01_steady_wsp10_noturb.htc
new file mode 100644
index 00000000..c54c20d0
--- /dev/null
+++ b/wetb/prepost/tests/data/demo_dlc/ref/htc/dlc01_demos/dlc01_steady_wsp10_noturb.htc
@@ -0,0 +1,850 @@
+;this version was at some point based on: Avatar_10MW_RWT version 1, 06-08-14, Anyd
+begin simulation;
+ time_stop 40;
+ solvertype 1 ; (newmark)
+ on_no_convergence continue ;
+; convergence_limits 1E3 1.0 1E-7 ;
+ logfile ./logfiles/dlc01_demos/dlc01_steady_wsp10_noturb.log ;
+ begin newmark;
+ deltat 0.02;
+ end newmark;
+end simulation;
+;
+;----------------------------------------------------------------------------------------------------------------------------------------------------------------
+begin new_htc_structure;
+;--------------------------------------------------------------------------------------------------
+; beam_output_file_name ./res_eigen/dlc01_demos/dlc01_steady_wsp10_noturb/dlc01_steady_wsp10_noturb_beam.dat;
+; body_output_file_name ./res_eigen/dlc01_demos/dlc01_steady_wsp10_noturb/dlc01_steady_wsp10_noturb_body.dat;
+; struct_inertia_output_file_name ./res_eigen/dlc01_demos/dlc01_steady_wsp10_noturb/dlc01_steady_wsp10_noturb_struct.dat;
+; body_eigenanalysis_file_name ./res_eigen/dlc01_demos/dlc01_steady_wsp10_noturb/dlc01_steady_wsp10_noturb_body_eigen.dat;
+; structure_eigenanalysis_file_name ./res_eigen/dlc01_demos/dlc01_steady_wsp10_noturb/dlc01_steady_wsp10_noturb_strc_eigen.dat;
+;---------------------------------------------------------------------------------------------------
+ begin main_body; tower 123.6m
+ name tower ;
+ type timoschenko ;
+ nbodies 3 ;
+ node_distribution c2_def ;
+ damping_posdef 0 0 0 4.7E-03 4.7E-03 4.3E-04 ; tuned by Anyd 12/8/14
+ begin timoschenko_input;
+ filename ./data/AVATAR_10MW_RWT_tower_st.dat;
+ set 1 1 ;
+ end timoschenko_input;
+ begin c2_def; Definition of centerline (main_body coordinates)
+ nsec 20;
+ sec 1 0 0 0.000 0 ; x,y,z,twist
+ sec 2 0 0 -12.293 0 ;
+ sec 3 0 0 -12.294 0 ;
+ sec 4 0 0 -24.585 0 ;
+ sec 5 0 0 -24.586 0 ;
+ sec 6 0 0 -36.878 0 ;
+ sec 7 0 0 -36.879 0 ;
+ sec 8 0 0 -49.171 0 ;
+ sec 9 0 0 -49.172 0 ;
+ sec 10 0 0 -61.463 0 ;
+ sec 11 0 0 -61.464 0 ;
+ sec 12 0 0 -73.756 0 ;
+ sec 13 0 0 -73.757 0 ;
+ sec 14 0 0 -86.049 0 ;
+ sec 15 0 0 -86.050 0 ;
+ sec 16 0 0 -98.341 0 ;
+ sec 17 0 0 -98.342 0 ;
+ sec 18 0 0 -110.634 0 ;
+ sec 19 0 0 -110.635 0 ;
+ sec 20 0 0 -123.600 0 ;
+ end c2_def ;
+ end main_body;
+;
+ begin main_body;
+ name towertop ;
+ type timoschenko ;
+ nbodies 1 ;
+ node_distribution c2_def ;
+ damping_posdef 7.50E-03 7.40E-03 7.00E-03 7.00E-03 7.00E-03 7.00E-03 ; "changed by Anyd
+ concentrated_mass 2.0 0.0 2.6870E+00 3.0061E-01 4.4604E+05 4.1060E+06 4.1060E+05 4.1060E+06 ; Nacel
+ begin timoschenko_input;
+ filename ./data/DTU_10MW_RWT_Towertop_st.dat ;
+ set 1 2 ;
+ end timoschenko_input;
+ begin c2_def; Definition of centerline (main_body coordinates)
+ nsec 2;
+ sec 1 0.0 0.0 0.0 0.0 ; x,y,z,twist
+ sec 2 0.0 0.0 -2.75 0.0 ;
+ end c2_def ;
+ end main_body;
+;
+ begin main_body;
+ name shaft ;
+ type timoschenko ;
+ nbodies 1 ;
+ node_distribution c2_def ;
+; damping_posdef 8.00E-3 8.00E-03 8.00E-02 4.65E-04 4.65E-04 2.38E-02 ; "tuned by Anyd 22/2/13
+ damping_posdef 0.0 0.0 3.983E-03 4.65E-04 4.65E-04 3.983E-03 ; "tuned by Anyd 23/5/13 to 31.45 l
+ concentrated_mass 1.0 0.0 0.0 0.0 0.0 0.0 0.0 3.751E+06 ; generator equivalent slow shaft "re_tu
+ concentrated_mass 5.0 0.0 0.0 0.0 1.0552E+05 0.0 0.0 3.257E+05 ; hub mass and inertia; "re_tuned
+ begin timoschenko_input;
+ filename ./data/DTU_10MW_RWT_Shaft_st.dat ;
+ set 1 1 ;
+ end timoschenko_input;
+ begin c2_def; Definition of centerline (main_body coordinates)
+ nsec 5;
+ sec 1 0.0 0.0 0.0 0.0 ; Tower top x,y,z,twist
+ sec 2 0.0 0.0 1.5 0.0 ;
+ sec 3 0.0 0.0 3.0 0.0 ;
+ sec 4 0.0 0.0 4.4 0.0 ; Main bearing
+ sec 5 0.0 0.0 7.1 0.0 ; Rotor centre
+ end c2_def ;
+ end main_body;
+;
+ begin main_body;
+ name shaft_nonrotate ;
+ type timoschenko ;
+ nbodies 1 ;
+ node_distribution c2_def ;
+ damping_posdef 0.00E+00 0.00E+00 0.00E+00 1.0E-01 1.0E-01 1.0E-01 ;
+ begin timoschenko_input;
+ filename ./data/DTU_10MW_RWT_Shaft_st.dat ;
+ set 1 3; dummy light and stiff structure
+ end timoschenko_input;
+ begin c2_def;
+ nsec 2;
+ sec 1 0.0 0.0 0.0 0.0 ;
+ sec 2 0.0 0.0 0.1 0.0 ;
+ end c2_def;
+ end main_body;
+;
+ begin main_body;
+ name hub1 ;
+ type timoschenko ;
+ nbodies 1 ;
+ node_distribution c2_def ;
+ damping_posdef 2.00E-05 2.00E-05 2.00E-04 3.00E-06 3.00E-06 2.00E-05;
+ begin timoschenko_input;
+ filename ./data/DTU_10MW_RWT_Hub_st.dat ;
+ set 1 2 ;
+ end timoschenko_input;
+ begin c2_def; Definition of centerline (main_body coordinates)
+ nsec 2;
+ sec 1 0.0 0.0 0.0 0.0 ; x,y,z,twist
+ sec 2 0.0 0.0 2.8 0.0 ;
+ end c2_def ;
+ end main_body;
+;
+ begin main_body;
+ name hub2 ;
+ copy_main_body hub1;
+ end main_body;
+;
+ begin main_body;
+ name hub3 ;
+ copy_main_body hub1 ;
+ end main_body;
+;
+ begin main_body;
+ name blade1 ;
+ type timoschenko ;
+ nbodies 10 ;
+ node_distribution c2_def;
+; damping_posdef 0.0 0.0 0.0 2.5e-3 8.9e-4 3.2e-4 ; "Tuned by Anyd"
+; damping_posdef 0.0 0.0 0.0 1.5e-3 2.45e-3 3.2e-4 ; " 3% damping tuned by Anyd 20/02/12 unable to
+; damping_posdef 0.0 0.0 0.0 2.1e-3 1.9e-3 1.3e-4 ; " 3% damping tuned by Anyd 15/08/14 rev2
+ damping_posdef 0.0 0.0 0.0 1.68e-3 2.25e-3 1.0e-4 ; " 3% damping tuned by Anyd 16/12/14
+ begin timoschenko_input ;
+ filename ./data/AVATAR_10MW_RWT_Blade_st.dat ;
+ set 1 9 ;
+ end timoschenko_input;
+ begin c2_def;
+ nsec 27 ;
+ sec 1 -0.001 -0.001 0.000 -17.280 ;
+ sec 2 -0.005 -0.001 2.220 -17.280 ;
+ sec 3 -0.006 -0.000 4.440 -17.280 ;
+ sec 4 -0.086 0.022 6.660 -17.280 ;
+ sec 5 -0.231 0.069 11.039 -17.273 ;
+ sec 6 -0.447 0.121 15.418 -16.441 ;
+ sec 7 -0.690 0.161 19.797 -14.613 ;
+ sec 8 -0.812 0.162 24.176 -12.578 ;
+ sec 9 -0.891 0.158 28.555 -10.588 ;
+ sec 10 -0.865 0.124 32.934 -9.070 ;
+ sec 11 -0.833 0.112 37.313 -8.224 ;
+ sec 12 -0.797 0.102 41.692 -7.688 ;
+ sec 13 -0.760 0.093 46.071 -7.205 ;
+ sec 14 -0.721 0.083 50.450 -6.749 ;
+ sec 15 -0.683 0.075 54.829 -6.288 ;
+ sec 16 -0.644 0.066 59.208 -5.838 ;
+ sec 17 -0.606 0.058 63.587 -5.401 ;
+ sec 18 -0.567 0.050 67.966 -4.982 ;
+ sec 19 -0.529 0.044 72.345 -4.640 ;
+ sec 20 -0.492 0.037 76.724 -4.380 ;
+ sec 21 -0.456 0.032 81.103 -4.144 ;
+ sec 22 -0.422 0.026 85.482 -3.914 ;
+ sec 23 -0.392 0.021 89.861 -3.685 ;
+ sec 24 -0.346 0.014 94.240 -3.460 ;
+ sec 25 -0.307 0.010 96.190 -3.350 ;
+ sec 26 -0.249 0.005 98.130 -3.250 ;
+ sec 27 -0.089 0.006 100.080 -3.140 ;
+ end c2_def ;
+ end main_body;
+;
+ begin main_body;
+ name blade2 ;
+ copy_main_body blade1;
+ end main_body;
+;
+ begin main_body;
+ name blade3 ;
+ copy_main_body blade1 ;
+ end main_body;
+;-------------------------------------------------------------------------------------------------------------------------------
+;
+ begin orientation;
+ begin base;
+ body tower;
+ inipos 0.0 0.0 0.0 ; initial position of node 1
+ body_eulerang 0.0 0.0 0.0;
+ end base;
+;
+ begin relative;
+ body1 tower last;
+ body2 towertop 1;
+ body2_eulerang 0.0 0.0 0.0;
+ end relative;
+;
+ begin relative;
+ body1 towertop last;
+ body2 shaft 1;
+ body2_eulerang 90.0 0.0 0.0;
+ body2_eulerang 5.0 0.0 0.0; 5 deg tilt angle
+ body2_eulerang 0.0 0.0 0;
+ mbdy2_ini_rotvec_d1 0.0 0.0 -1.0 0.5 ; mbdy2_ini_rotvec_d1 0.0 0.0 -1.0 0.5;
+ end relative;
+;
+ begin relative; dummy non rotating hub coordinates
+ body1 towertop last;
+ body2 shaft_nonrotate 1;
+ body2_eulerang 90.0 0.0 0.0;
+ body2_eulerang 5.0 0.0 0.0; same 5 deg tilt angle as real shaft
+ end relative;
+;
+ begin relative;
+ body1 shaft last;
+ body2 hub1 1;
+ body2_eulerang -90.0 0.0 0.0;
+ body2_eulerang 0.0 180.0 0.0;
+ body2_eulerang 2.5 0.0 0.0; 2.5deg cone angle
+ end relative;
+;
+ begin relative;
+ body1 shaft last;
+ body2 hub2 1;
+ body2_eulerang -90.0 0.0 0.0;
+ body2_eulerang 0.0 60.0 0.0;
+ body2_eulerang 2.5 0.0 0.0; 2.5deg cone angle
+ end relative;
+;
+ begin relative;
+ body1 shaft last;
+ body2 hub3 1;
+ body2_eulerang -90.0 0.0 0.0;
+ body2_eulerang 0.0 -60.0 0.0;
+ body2_eulerang 2.5 0.0 0.0; 2.5deg cone angle
+ end relative;
+;
+ begin relative;
+ body1 hub1 last;
+ body2 blade1 1;
+ body2_eulerang 0.0 0.0 0;
+ end relative;
+;
+ begin relative;
+ body1 hub2 last;
+ body2 blade2 1;
+ body2_eulerang 0.0 0.0 0.0;
+ end relative;
+;
+ begin relative;
+ body1 hub3 last;
+ body2 blade3 1;
+ body2_eulerang 0.0 0.0 0.0;
+ end relative;
+;
+ end orientation;
+;-------------------------------------------------------------------------------------------------------------------------------
+begin constraint;
+;
+ begin fix0; fixed to ground in translation and rotation of node 1
+ body tower;
+ end fix0;
+;
+ begin fix1;
+ body1 tower last ;
+ body2 towertop 1;
+ end fix1;
+;
+ begin bearing1; free bearing
+ name shaft_rot;
+ body1 towertop last;
+ body2 shaft 1;
+ bearing_vector 2 0.0 0.0 -1.0; x=coo (0=global.1=body1.2=body2) vector in body2 coordinates where the free rotation is present
+ end bearing1;
+;
+; begin bearing3; free bearing
+; name shaft_rot;
+; body1 towertop last;
+; body2 shaft 1;
+; bearing_vector 2 0.0 0.0 -1.0; x=coo (0=global.1=body1.2=body2) vector in body2 coordinates where the free rotation is present
+; omegas 0.0 ;
+; end bearing3;
+;
+ begin fix1;
+ body1 tower last ;
+ body2 shaft_nonrotate 1;
+ end fix1;
+;
+ begin fix1;
+ body1 shaft last ;
+ body2 hub1 1;
+ end fix1;
+;
+ begin fix1;
+ body1 shaft last ;
+ body2 hub2 1;
+ end fix1;
+;
+ begin fix1;
+ body1 shaft last ;
+ body2 hub3 1;
+ end fix1;
+;
+ begin bearing2;
+ name pitch1;
+ body1 hub1 last;
+ body2 blade1 1;
+ bearing_vector 2 0.0 0.0 -1.0;
+ end bearing2;
+;
+ begin bearing2;
+ name pitch2;
+ body1 hub2 last;
+ body2 blade2 1;
+ bearing_vector 2 0.0 0.0 -1.0;
+ end bearing2;
+;
+ begin bearing2;
+ name pitch3;
+ body1 hub3 last;
+ body2 blade3 1;
+ bearing_vector 2 0.0 0.0 -1.0;
+ end bearing2;
+end constraint;
+;
+end new_htc_structure;
+;----------------------------------------------------------------------------------------------------------------------------------------------------------------
+begin wind ;
+ density 1.225 ;
+ wsp 10 ;
+ tint 0.2096 ;
+ horizontal_input 1 ;
+ windfield_rotations 0 8.0 0.0 ; yaw, tilt (positive=upflow=wind coming from below), rotation
+ center_pos0 0.0 0.0 -127 ; hub heigth
+ shear_format 3 0 ;
+ turb_format 0 ; 0=none, 1=mann,2=flex
+ tower_shadow_method 3 ; 0=none, 1=potential flow, 2=jet
+ scale_time_start 20 ;
+ wind_ramp_factor 0.0 20 0.8 1.0 ;
+ ; iec_gust ;
+;
+; wind_ramp_abs 400.0 401.0 0.0 1.0 ; wsp. after the step: 5.0
+; wind_ramp_abs 501.0 502.0 0.0 1.0 ; wsp. after the step: 6.0
+; wind_ramp_abs 602.0 603.0 0.0 1.0 ; wsp. after the step: 7.0
+; wind_ramp_abs 703.0 704.0 0.0 1.0 ; wsp. after the step: 8.0
+; wind_ramp_abs 804.0 805.0 0.0 1.0 ; wsp. after the step: 9.0
+; wind_ramp_abs 905.0 906.0 0.0 1.0 ; wsp. after the step: 10.0
+; wind_ramp_abs 1006.0 1007.0 0.0 1.0 ; wsp. after the step: 11.0
+; wind_ramp_abs 1107.0 1108.0 0.0 1.0 ; wsp. after the step: 12.0
+; wind_ramp_abs 1208.0 1209.0 0.0 1.0 ; wsp. after the step: 13.0
+; wind_ramp_abs 1309.0 1310.0 0.0 1.0 ; wsp. after the step: 14.0
+; wind_ramp_abs 1410.0 1411.0 0.0 1.0 ; wsp. after the step: 15.0
+; wind_ramp_abs 1511.0 1512.0 0.0 1.0 ; wsp. after the step: 16.0
+; wind_ramp_abs 1612.0 1613.0 0.0 1.0 ; wsp. after the step: 17.0
+; wind_ramp_abs 1713.0 1714.0 0.0 1.0 ; wsp. after the step: 18.0
+; wind_ramp_abs 1814.0 1815.0 0.0 1.0 ; wsp. after the step: 19.0
+; wind_ramp_abs 1915.0 1916.0 0.0 1.0 ; wsp. after the step: 20.0
+; wind_ramp_abs 2016.0 2017.0 0.0 1.0 ; wsp. after the step: 21.0
+; wind_ramp_abs 2117.0 2118.0 0.0 1.0 ; wsp. after the step: 22.0
+; wind_ramp_abs 2218.0 2219.0 0.0 1.0 ; wsp. after the step: 23.0
+; wind_ramp_abs 2319.0 2320.0 0.0 1.0 ; wsp. after the step: 24.0
+; wind_ramp_abs 2420.0 2421.0 0.0 1.0 ; wsp. after the step: 25.0
+ ;
+; wind_ramp_abs 400.0 2200.0 0.0 21.0 ; wsp. after the step: 25.0
+; wind_ramp_abs 2400.0 4200.0 0.0 -21.0 ; wsp. after the step: 25.0
+ ;
+ begin mann ;
+ create_turb_parameters 29.4 1.0 3.9 0 1.0 ; L, alfaeps, gamma, seed, highfrq compensation
+ filename_u ./turb/noneu.bin ;
+ filename_v ./turb/nonev.bin ;
+ filename_w ./turb/nonew.bin ;
+ box_dim_u 8192 0.048828125 ;
+ box_dim_v 32 7.5;
+ box_dim_w 32 7.5;
+ std_scaling 1.0 0.7 0.5 ;
+ end mann ;
+;
+ begin tower_shadow_potential_2;
+ tower_mbdy_link tower;
+ nsec 2;
+ radius 0.0 4.15 ;
+ radius 123.6 2.75 ; (radius)
+ end tower_shadow_potential_2;
+end wind;
+;
+begin aerodrag ;
+ begin aerodrag_element ;
+ mbdy_name tower;
+ aerodrag_sections uniform 10 ;
+ nsec 2 ;
+ sec 0.0 0.6 8.3 ; tower bottom
+ sec 123.6 0.6 5.5 ; tower top (diameter)
+ end aerodrag_element;
+;
+ begin aerodrag_element ; Nacelle drag side
+ mbdy_name shaft;
+ aerodrag_sections uniform 2 ;
+ nsec 2 ;
+ sec 0.0 0.8 10.0 ;
+ sec 7.01 0.8 10.0 ;
+ end aerodrag_element;
+end aerodrag;
+;
+begin aero ;
+ nblades 3;
+ hub_vec shaft -3 ; rotor rotation vector (normally shaft composant directed from pressure to sustion side)
+ link 1 mbdy_c2_def blade1;
+ link 2 mbdy_c2_def blade2;
+ link 3 mbdy_c2_def blade3;
+ ae_filename ./data/AVATAR_10MW_RWT_ae.dat ;
+ pc_filename ./data/AVATAR_10MW_RWT_pc_hama_v1.dat ;
+ induction_method 1 ; 0=none, 1=normal
+ aerocalc_method 1 ; 0=ingen aerodynamic, 1=med aerodynamic
+ aero_distribution ae_file 1 ;
+ ae_sets 1 1 1;
+ tiploss_method 1 ; 0=none, 1=prandtl
+ dynstall_method 2 ; 0=none, 1=stig øye method,2=mhh method
+;
+; ; --- Flaps --- ;
+ ; begin dynstall_ateflap ;
+ ; Ais 0.165 0.335 0.0 ;
+ ; Bis 0.0455 0.30 0.30 ;
+ ; flap 59.5925 85.5023 ./data/Flap_dturwt1_Thk24.ds ; Flap Sec: 1
+ ; end dynstall_ateflap;
+end aero ;
+;-------------------------------------------------------------------------------------------------
+begin dll;
+;
+ begin type2_dll;
+ name risoe_controller ;
+ filename ./control/risoe_controller.dll ;
+ dll_subroutine_init init_regulation ;
+ dll_subroutine_update update_regulation ;
+ arraysizes_init 52 1 ;
+ arraysizes_update 12 100 ;
+ begin init ;
+ ; Overall parameters
+ constant 1 10000.0 ; Rated power [kW]
+ constant 2 0.628 ; Minimum rotor speed [rad/s]
+ constant 3 1.005 ; Rated rotor speed [rad/s]
+ constant 4 15.6E+06 ; Maximum allowable generator torque [Nm]
+ 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 'wpdata.n', where n=int(theta_min)
+ 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 9 0.7 ; Damping ratio of speed filter [-]
+ constant 10 1.64 ; Frequency of free-free DT torsion mode [Hz], if zero no notch filter used
+ ; Partial load control parameters
+ constant 11 0.9648030e+07 ; 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 1.047610E+08 ; Proportional gain of torque controller [Nm/(rad/s)]
+ constant 13 0.153367E+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, 2=constant torque]
+ constant 16 0.762489 ; Proportional gain of pitch controller [rad/(rad/s)]
+ constant 17 0.224086 ; Integral gain of pitch controller [rad/rad]
+ constant 18 0.0 ; Differential gain of pitch controller [rad/(rad/s^2)]
+ constant 19 0.4e-9 ; Proportional power error gain [rad/W]
+ constant 20 0.4e-9 ; Integral power error gain [rad/(Ws)]
+ constant 21 10.6824 ; Coefficient of linear term in aerodynamic gain scheduling, KK1 [deg]
+ constant 22 601.25499 ; 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
+ constant 24 -1 ; Cut-in time [s]
+ constant 25 1.0 ; Time delay for soft start of torque [1/1P]
+; Cut-out simulation parameters
+ constant 26 -1 ; Cut-out time [s]
+ constant 27 5.0 ; Time constant for linear torque cut-out [s]
+ constant 28 1 ; Stop type [1=normal, 2=emergency]
+ constant 29 1.0 ; Time delay for pitch stop after shut-down signal [s]
+ constant 30 3 ; Maximum pitch velocity during initial period of stop [deg/s]
+ constant 31 3.0 ; Time period of initial pitch stop phase [s] (maintains pitch speed specified in constant 30)
+ constant 32 4 ; Maximum pitch velocity during final phase of stop [deg/s]
+; Expert parameters (keep default values unless otherwise given)
+ constant 33 2.0 ; Lower angle above lowest minimum pitch angle for switch [deg]
+ constant 34 2.0 ; Upper angle above lowest minimum pitch angle for switch [deg], if equal then hard switch
+ constant 35 95.0 ; Ratio between filtered speed and reference speed for fully open torque limits [%]
+ constant 36 2.0 ; Time constant of 1st order filter on wind speed used for minimum pitch [1/1P]
+ constant 37 1.0 ; Time constant of 1st order filter on pitch angle used for gain scheduling [1/1P]
+; Drivetrain damper
+ constant 38 0.0 ; Proportional gain of active DT damper [Nm/(rad/s)], requires frequency in input 10
+; Over speed
+ constant 39 25.0 ; Overspeed percentage before initiating turbine controller alarm (shut-down) [%]
+; Additional non-linear pitch control term (not used when all zero)
+ constant 40 0.0 ; Err0 [rad/s]
+ constant 41 0.0 ; ErrDot0 [rad/s^2]
+ constant 42 0.0 ; PitNonLin1 [rad/s]
+; Storm control command
+ constant 43 28.0 ; Wind speed 'Vstorm' above which derating of rotor speed is used [m/s]
+ constant 44 28.0 ; Cut-out wind speed (only used for derating of rotor speed in storm) [m/s]
+; Safety system parameters
+ constant 45 25.0 ; Overspeed percentage before initiating safety system alarm (shut-down) [%]
+ constant 46 1.5 ; Max low-pass filtered tower top acceleration level [m/s^2] - max in DLC 1.3=1.1 m/s^2
+; Turbine parameter
+ constant 47 205.8 ; Nominal rotor diameter [m]
+; Parameters for rotor inertia reduction in variable speed region
+ constant 48 0.0 ; Proportional gain on rotor acceleration in variable speed region [Nm/(rad/s^2)] (not used when zero)
+; Parameters for alternative partial load controller with PI regulated TSR tracking
+ constant 49 0.0 ; Optimal tip speed ratio [-] (only used when K=constant 11 = 0 otherwise Qg=K*Omega^2 is used)
+; Parameters for adding aerodynamic drivetrain damping on gain scheduling
+ constant 50 0.0 ; Proportional gain of aerodynamic DT damping [Nm/(rad/s)]
+ constant 51 0.0 ; Coefficient of linear term in aerodynamic DT damping scheduling, KK1 [deg]
+ constant 52 0.0 ; Coefficient of quadratic term in aerodynamic DT damping scheduling, KK2 [deg^2]
+ end init ;
+;
+ begin output ;
+ general time ; [s]
+ constraint bearing1 shaft_rot 1 only 2 ; Drivetrain speed [rad/s]
+ constraint bearing2 pitch1 1 only 1; [rad]
+ constraint bearing2 pitch2 1 only 1; [rad]
+ constraint bearing2 pitch3 1 only 1; [rad]
+ wind free_wind 1 0.0 0.0 -127 ; Global coordinates at hub height
+ dll inpvec 2 2 ; Elec. power from generator servo .dll
+ dll inpvec 2 8 ; Grid state flag from generator servo .dll
+ mbdy state acc tower 10 1.0 global only 1 ; Tower top x-acceleration [m/s^2]
+ mbdy state acc tower 10 1.0 global only 2 ; Tower top y-acceleration [m/s^2]
+ end output;
+ end type2_dll;
+;
+ begin type2_dll;
+ name generator_servo ;
+ filename ./control/generator_servo.dll ;
+ dll_subroutine_init init_generator_servo ;
+ dll_subroutine_update update_generator_servo ;
+ arraysizes_init 7 1 ;
+ arraysizes_update 4 8 ;
+ begin init ;
+ constant 1 20.0 ; Frequency of 2nd order servo model of generator-converter system [Hz]
+ constant 2 0.9 ; Damping ratio 2nd order servo model of generator-converter system [-]
+ constant 3 15.6E+06 ; Maximum allowable LSS torque (pull-out torque) [Nm]
+ constant 4 0.94 ; Generator efficiency [-]
+ constant 5 1.0 ; Gearratio [-]
+ constant 6 0.0 ; Time for half value in softstart of torque [s]
+ constant 7 5000 ; Time for grid loss [s]
+ end init ;
+;
+ begin output;
+ general time ; Time [s]
+ dll inpvec 1 1 ; Electrical torque reference [Nm]
+ constraint bearing1 shaft_rot 1 only 2; Generator LSS speed [rad/s]
+ mbdy momentvec shaft 1 1 shaft only 3 ; Shaft moment [kNm] (Qshaft)
+ end output;
+;
+ begin actions;
+ mbdy moment_int shaft 1 -3 shaft towertop 2 ; Generator LSS torque [Nm]
+ end actions;
+ end type2_dll;
+;
+ begin type2_dll;
+ name mech_brake ;
+ filename ./control/mech_brake.dll ;
+ dll_subroutine_init init_mech_brake ;
+ dll_subroutine_update update_mech_brake ;
+ arraysizes_init 7 1 ;
+ arraysizes_update 4 6 ;
+ begin init ;
+ constant 1 5225.35 ; Fully deployed maximum brake torque [Nm] (0.6*max torque)
+ constant 2 100.0 ; Parameter alpha used in Q = tanh(omega*alpha), typically 1e2/Omega_nom
+ constant 3 0.5 ; Delay time for before brake starts to deploy [s]
+ constant 4 0.74 ; Time for brake to become fully deployed [s]
+ end init ;
+;
+ begin output;
+ general time ; Time [s]
+ constraint bearing1 shaft_rot 1 only 2 ; Generator LSS speed [rad/s]
+ dll inpvec 1 25 ; Command to deploy mechanical disc brake [0,1]
+ end output;
+;
+ begin actions;
+ mbdy moment_int shaft 1 -3 shaft towertop 2 ; Generator LSS torque [Nm]
+ end actions;
+ end type2_dll;
+;
+ begin type2_dll;
+ name servo_with_limits ;
+ filename ./control/servo_with_limits.dll ;
+ dll_subroutine_init init_servo_with_limits ;
+ dll_subroutine_update update_servo_with_limits ;
+ arraysizes_init 10 1 ;
+ arraysizes_update 5 9 ;
+ begin init ;
+ constant 1 3 ; Number of blades [-]
+ constant 2 1.0 ; Frequency of 2nd order servo model of pitch system [Hz]
+ constant 3 0.7 ; Damping ratio 2nd order servo model of pitch system [-]
+ constant 4 10.0 ; Max. pitch speed [deg/s]
+ constant 5 15.0 ; Max. pitch acceleration [deg/s^2]
+ constant 6 -5.0 ; Min. pitch angle [deg]
+ constant 7 90.0 ; Max. pitch angle [deg]
+ constant 8 5000 ; Time for pitch runaway [s]
+ constant 9 -1 ; Time for stuck blade 1 [s]
+ constant 10 0 ; Angle of stuck blade 1 [deg]
+ end init ;
+ begin output;
+ general time ; Time [s]
+ dll inpvec 1 2 ; Pitch1 demand angle [rad]
+ dll inpvec 1 3 ; Pitch2 demand angle [rad]
+ dll inpvec 1 4 ; Pitch3 demand angle [rad]
+ dll inpvec 1 26 ; Flag for emergency pitch stop [0=off/1=on]
+ end output;
+;
+ begin actions;
+ constraint bearing2 angle pitch1 ; Angle pitch1 bearing [rad]
+ constraint bearing2 angle pitch2 ; Angle pitch2 bearing [rad]
+ constraint bearing2 angle pitch3 ; Angle pitch3 bearing [rad]
+ end actions;
+ end type2_dll;
+;
+; --- DLL for tower-blade tip distance -- ;
+ begin type2_dll;
+ name disttowtip ;
+ filename ./control/towclearsens.dll ;
+ dll_subroutine_init initialize ;
+ dll_subroutine_update update ;
+ arraysizes_init 1 1 ;
+ arraysizes_update 12 4 ;
+ begin init ;
+ constant 1 3.87 ; Tower radius close to downward blade tip [m]
+ end init ;
+ begin output;
+ mbdy state pos tower 5 0.00 global ; [1,2,3]. Tower position: 24.58 m
+ mbdy state pos blade1 26 1.0 global ; [4,5,6]
+ mbdy state pos blade2 26 1.0 global ; [7,8,9]
+ mbdy state pos blade3 26 1.0 global ; [10,11,12]
+ end output;
+ end type2_dll;
+end dll;
+;
+;----------------------------------------------------------------------------------------------------------------------------------------------------------------
+;
+begin output;
+ filename ./res/dlc01_demos/dlc01_steady_wsp10_noturb ;
+ time 20 40 ;
+ data_format hawc_binary;
+ buffer 1 ;
+;
+ general time;
+ constraint bearing1 shaft_rot 2; angle and angle velocity
+ constraint bearing2 pitch1 5; angle and angle velocity
+ constraint bearing2 pitch2 5; angle and angle velocity
+ constraint bearing2 pitch3 5; angle and angle velocity
+ aero omega ;
+ aero torque;
+ aero power;
+ aero thrust;
+ wind free_wind 1 0.0 0.0 -127; local wind at fixed position: coo (1=global,2=non-rotation rotor coo.), pos x, pos y, pos z
+ ; non rotating coordinates shaft tip: equivalent to stationary hub in BLADED
+ mbdy momentvec shaft 3 2 shaft_nonrotate # non rotating shaft tip ;
+ mbdy forcevec shaft 3 2 shaft_nonrotate # non rotating shaft tip ;
+ ; Moments:
+ mbdy momentvec tower 1 1 tower # tower base ;
+ mbdy momentvec tower 19 2 tower # tower yaw bearing ;
+ mbdy momentvec shaft 4 1 shaft # main bearing ;
+ mbdy momentvec blade1 3 2 blade1 # blade 1 root ;
+ mbdy momentvec blade2 3 2 blade2 # blade 2 root ;
+ mbdy momentvec blade3 3 2 blade3 # blade 3 root ;
+ ; blade 2,3 root section loads
+ mbdy momentvec blade2 3 2 local # blade 2 section root;
+ mbdy momentvec blade3 3 2 local # blade 3 section root;
+ ; blade 1 sectional loads in local coordinates
+ mbdy momentvec blade1 2 2 local # blade 1 section;
+ mbdy momentvec blade1 3 2 local # blade 1 section root;
+ mbdy momentvec blade1 4 2 local # blade 1 section;
+ mbdy momentvec blade1 5 2 local # blade 1 section;
+ mbdy momentvec blade1 6 2 local # blade 1 section;
+ mbdy momentvec blade1 7 2 local # blade 1 section;
+ mbdy momentvec blade1 8 2 local # blade 1 section;
+ mbdy momentvec blade1 9 2 local # blade 1 section;
+ mbdy momentvec blade1 10 2 local # blade 1 section;
+ mbdy momentvec blade1 11 2 local # blade 1 section;
+ mbdy momentvec blade1 12 2 local # blade 1 section;
+ mbdy momentvec blade1 13 2 local # blade 1 section;
+ mbdy momentvec blade1 14 2 local # blade 1 section;
+ mbdy momentvec blade1 15 2 local # blade 1 section;
+ mbdy momentvec blade1 16 2 local # blade 1 section;
+ mbdy momentvec blade1 17 2 local # blade 1 section;
+ mbdy momentvec blade1 18 2 local # blade 1 section;
+ mbdy momentvec blade1 19 2 local # blade 1 section;
+ mbdy momentvec blade1 20 2 local # blade 1 section;
+ mbdy momentvec blade1 21 2 local # blade 1 section;
+ mbdy momentvec blade1 22 2 local # blade 1 section;
+ mbdy momentvec blade1 23 2 local # blade 1 section;
+ mbdy momentvec blade1 24 2 local # blade 1 section;
+ mbdy momentvec blade1 25 2 local # blade 1 section;
+ mbdy momentvec blade1 26 2 local # blade 1 section;
+ ; blade root out and in of plane forces
+ mbdy momentvec blade1 3 2 hub1 # blade 1 root ;
+ mbdy momentvec blade2 3 2 hub2 # blade 2 root ;
+ mbdy momentvec blade3 3 2 hub3 # blade 3 root ;
+; mbdy momentvec blade1 14 1 local # blade 1 50% local e coo ;
+; mbdy momentvec blade2 14 1 local # blade 2 50% local e coo ;
+; mbdy momentvec blade3 14 1 local # blade 3 50% local e coo ;
+ ; Displacements and accellerations
+ mbdy state pos tower 19 1.0 global only 1 # Tower top FA displ;
+ mbdy state pos tower 19 1.0 global only 2 # Tower top SS displ;
+ mbdy state acc tower 19 1.0 global only 1 # Tower top FA acc;
+ mbdy state acc tower 19 1.0 global only 2 # Tower top SS acc;
+;
+ mbdy state pos blade1 26 1.0 global # gl blade 1 tip pos ;
+ mbdy state pos blade2 26 1.0 global # gl blade 2 tip pos ;
+ mbdy state pos blade3 26 1.0 global # gl blade 3 tip pos ;
+ mbdy state pos blade1 26 1.0 blade1 # blade 1 tip pos ;
+ mbdy state pos blade2 26 1.0 blade2 # blade 2 tip pos ;
+ mbdy state pos blade3 26 1.0 blade3 # blade 3 tip pos ;
+;
+ mbdy state pos tower 5 0.00 global ; [1,2,3]. Tower position: 24.58 m
+;
+ ; elastic twist (torsional deformation) along the blade
+ aero tors_ang 1 45.56;
+ aero tors_ang 1 59.19;
+ aero tors_ang 1 70.87;
+ aero tors_ang 1 80.61;
+ aero tors_ang 1 84.50;
+ aero tors_ang 1 88.40;
+ aero tors_ang 1 92.29;
+ aero tors_ang 1 96.19;
+ aero tors_ang 1 98.13;
+ aero tors_ang 1 100.08; tip
+;
+; - Monitor Aerodynamics - ;
+ aero windspeed 3 1 1 72.5;
+ aero alfa 1 72.5;
+ aero alfa 2 72.5;
+ aero alfa 3 72.5;
+ aero cl 1 72.5;
+ aero cl 2 72.5;
+ aero cl 3 72.5;
+ aero cd 1 72.5;
+ aero cd 2 72.5;
+ aero cd 3 72.5;
+; - Main Controller -
+; Output to controller
+ ; dll outvec 1 1 # time;
+ ; dll outvec 1 2 # slow speed shaft rad/s;
+ ; dll outvec 1 3 # pitch angle 1;
+ ; dll outvec 1 4 # pitch angle 2;
+ ; dll outvec 1 5 # pitch angle 3;
+ ; dll outvec 1 6 # WSP_x_global;
+ ; dll outvec 1 7 # WSP_y_global;
+ ; dll outvec 1 8 # WSP_z_global;
+ ; dll outvec 1 9 # Elec. pwr ;
+ ; dll outvec 1 10 # Grid flag ;
+; Input from controller
+ dll inpvec 1 1 # Generator torque reference [Nm] ;
+ dll inpvec 1 2 # Pitch angle reference of blade 1 [rad] ;
+ dll inpvec 1 3 # Pitch angle reference of blade 2 [rad] ;
+ dll inpvec 1 4 # Pitch angle reference of blade 3 [rad] ;
+ ; dll inpvec 1 5 # Power reference [W] ;
+ ; dll inpvec 1 6 # Filtered wind speed [m/s] ;
+ ; dll inpvec 1 7 # Filtered rotor speed [rad/s];
+ ; dll inpvec 1 8 # Filtered rotor speed error for torque [rad/s];
+ ; dll inpvec 1 9 # Bandpass filtered rotor speed [rad/s];
+ ; dll inpvec 1 10 # Proportional term of torque contr. [Nm] ;
+ ; dll inpvec 1 11 # Integral term of torque controller [Nm] ;
+ ; dll inpvec 1 12 # Minimum limit of torque [Nm] ;
+ ; dll inpvec 1 13 # Maximum limit of torque [Nm] ;
+ dll inpvec 1 14 # Torque limit switch based on pitch [-] ;
+ ; dll inpvec 1 15 # Filtered rotor speed error for pitch [rad/s];
+ ; dll inpvec 1 16 # Power error for pitch [W] ;
+ ; dll inpvec 1 17 # Proportional term of pitch controller [rad] ;
+ ; dll inpvec 1 18 # Integral term of pitch controller [rad] ;
+ ; dll inpvec 1 19 # Minimum limit of pitch [rad] ;
+ ; dll inpvec 1 20 # Maximum limit of pitch [rad] ;
+ dll inpvec 1 21 # Torque reference from DT dammper [Nm] ;
+ dll inpvec 1 22 # Status signal [-] ;
+ ; dll inpvec 1 23 # Total added pitch rate [rad/s] ;
+ dll inpvec 1 24 # Filtered Mean pitch for gain sch [rad] ;
+ dll inpvec 1 25 # Flag for mechnical brake [0=off/1=on] ;
+ dll inpvec 1 26 # Flag for emergency pitch stop [0=off/1=on] ;
+ dll inpvec 1 27 # LP filtered acceleration level [m/s^2] ;
+; ; Output to generator model
+ ; dll outvec 2 1 # time ;
+ ; dll outvec 2 2 # Electrical torque reference [Nm] ;
+ ; dll outvec 2 3 # omega LSS ;
+; Input from generator model
+ dll inpvec 2 1 # Mgen LSS [Nm];
+ dll inpvec 2 2 # Pelec W ;
+ dll inpvec 2 3 # Mframe ;
+ dll inpvec 2 4 # Mgen HSS ;
+ dll inpvec 2 5 # Generator Pmech kW ;
+ dll inpvec 2 6 # Filtered Gen speed ;
+ dll inpvec 2 7 # Resulting Eff ;
+ dll inpvec 2 8 # Grid flag ;
+; Output to mechanical brake
+ dll inpvec 3 1 # Brake torque [Nm] ;
+; ; Input from mechanical brake
+ ; dll outvec 3 1 # Time [s] ;
+ ; dll outvec 3 2 # Generator LSS speed [rad/s] ;
+ ; dll outvec 3 3 # Deploy brake ;
+; ; Output to pitch servo
+ ; dll outvec 4 1 # time;
+ ; dll outvec 4 2 # pitchref 1;
+ ; dll outvec 4 3 # pitchref 2;
+ ; dll outvec 4 4 # pitchref 3;
+ ; dll outvec 4 5 # Emerg. stop;
+; Input from pitch servo
+ dll inpvec 4 1 # pitch 1;
+ dll inpvec 4 2 # pitch 2;
+ dll inpvec 4 3 # pitch 3;
+; Check tower clearence
+ dll inpvec 5 1 # Bltip tow min d [m];
+; general constant 1.0 ; constant 1.0 - to mesure activity of flap in terms of displacement
+; - Check on flap control:
+ ; ; - From flap controller: -
+ ; dll type2_dll cyclic_flap_controller inpvec 1 # Ref flap signal bl 1 [deg] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 2 # Ref flap signal bl 2 [deg] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 3 # Ref flap signal bl 3 [deg] ;
+ ; ; - Mbc values
+ ; dll type2_dll cyclic_flap_controller inpvec 4 # momvec mbc cos [kNm] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 5 # momvec mbc sin [kNm] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 6 # momvec mbc filt cos [kNm] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 7 # momvec mbc filt sin [kNm] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 8 # flap mbc cos [deg] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 9 # flap mbc sin [deg] ;
+ ; ; - Check Gains - ;
+ ; dll type2_dll cyclic_flap_controller inpvec 10 # lead angle [deg] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 11 # scaling on rat pow [-] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 12 # actual kp [deg/kNm] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 13 # actual ki [deg/kNms] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 14 # actual kd [deg s/kNm] ;
+ ; ; - Actual deflections -
+ ; aero beta 1 1 ;
+ ; aero beta 2 1 ;
+ ; aero beta 3 1 ;
+ ; ; - Mbc values
+ ; dll type2_dll cyclic_flap_controller inpvec 4 # momvec mbc cos [kNm] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 5 # momvec mbc sin [kNm] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 6 # momvec mbc filt cos [kNm] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 7 # momvec mbc filt sin [kNm] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 8 # flap mbc cos [deg] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 9 # flap mbc sin [deg] ;
+end output;
+;
+exit;
diff --git a/wetb/prepost/tests/data/demo_dlc/ref/htc/dlc01_demos/dlc01_steady_wsp8_noturb.htc b/wetb/prepost/tests/data/demo_dlc/ref/htc/dlc01_demos/dlc01_steady_wsp8_noturb.htc
new file mode 100644
index 00000000..94abe5e1
--- /dev/null
+++ b/wetb/prepost/tests/data/demo_dlc/ref/htc/dlc01_demos/dlc01_steady_wsp8_noturb.htc
@@ -0,0 +1,850 @@
+;this version was at some point based on: Avatar_10MW_RWT version 1, 06-08-14, Anyd
+begin simulation;
+ time_stop 40;
+ solvertype 1 ; (newmark)
+ on_no_convergence continue ;
+; convergence_limits 1E3 1.0 1E-7 ;
+ logfile ./logfiles/dlc01_demos/dlc01_steady_wsp8_noturb.log ;
+ begin newmark;
+ deltat 0.02;
+ end newmark;
+end simulation;
+;
+;----------------------------------------------------------------------------------------------------------------------------------------------------------------
+begin new_htc_structure;
+;--------------------------------------------------------------------------------------------------
+; beam_output_file_name ./res_eigen/dlc01_demos/dlc01_steady_wsp8_noturb/dlc01_steady_wsp8_noturb_beam.dat;
+; body_output_file_name ./res_eigen/dlc01_demos/dlc01_steady_wsp8_noturb/dlc01_steady_wsp8_noturb_body.dat;
+; struct_inertia_output_file_name ./res_eigen/dlc01_demos/dlc01_steady_wsp8_noturb/dlc01_steady_wsp8_noturb_struct.dat;
+; body_eigenanalysis_file_name ./res_eigen/dlc01_demos/dlc01_steady_wsp8_noturb/dlc01_steady_wsp8_noturb_body_eigen.dat;
+; structure_eigenanalysis_file_name ./res_eigen/dlc01_demos/dlc01_steady_wsp8_noturb/dlc01_steady_wsp8_noturb_strc_eigen.dat;
+;---------------------------------------------------------------------------------------------------
+ begin main_body; tower 123.6m
+ name tower ;
+ type timoschenko ;
+ nbodies 3 ;
+ node_distribution c2_def ;
+ damping_posdef 0 0 0 4.7E-03 4.7E-03 4.3E-04 ; tuned by Anyd 12/8/14
+ begin timoschenko_input;
+ filename ./data/AVATAR_10MW_RWT_tower_st.dat;
+ set 1 1 ;
+ end timoschenko_input;
+ begin c2_def; Definition of centerline (main_body coordinates)
+ nsec 20;
+ sec 1 0 0 0.000 0 ; x,y,z,twist
+ sec 2 0 0 -12.293 0 ;
+ sec 3 0 0 -12.294 0 ;
+ sec 4 0 0 -24.585 0 ;
+ sec 5 0 0 -24.586 0 ;
+ sec 6 0 0 -36.878 0 ;
+ sec 7 0 0 -36.879 0 ;
+ sec 8 0 0 -49.171 0 ;
+ sec 9 0 0 -49.172 0 ;
+ sec 10 0 0 -61.463 0 ;
+ sec 11 0 0 -61.464 0 ;
+ sec 12 0 0 -73.756 0 ;
+ sec 13 0 0 -73.757 0 ;
+ sec 14 0 0 -86.049 0 ;
+ sec 15 0 0 -86.050 0 ;
+ sec 16 0 0 -98.341 0 ;
+ sec 17 0 0 -98.342 0 ;
+ sec 18 0 0 -110.634 0 ;
+ sec 19 0 0 -110.635 0 ;
+ sec 20 0 0 -123.600 0 ;
+ end c2_def ;
+ end main_body;
+;
+ begin main_body;
+ name towertop ;
+ type timoschenko ;
+ nbodies 1 ;
+ node_distribution c2_def ;
+ damping_posdef 7.50E-03 7.40E-03 7.00E-03 7.00E-03 7.00E-03 7.00E-03 ; "changed by Anyd
+ concentrated_mass 2.0 0.0 2.6870E+00 3.0061E-01 4.4604E+05 4.1060E+06 4.1060E+05 4.1060E+06 ; Nacel
+ begin timoschenko_input;
+ filename ./data/DTU_10MW_RWT_Towertop_st.dat ;
+ set 1 2 ;
+ end timoschenko_input;
+ begin c2_def; Definition of centerline (main_body coordinates)
+ nsec 2;
+ sec 1 0.0 0.0 0.0 0.0 ; x,y,z,twist
+ sec 2 0.0 0.0 -2.75 0.0 ;
+ end c2_def ;
+ end main_body;
+;
+ begin main_body;
+ name shaft ;
+ type timoschenko ;
+ nbodies 1 ;
+ node_distribution c2_def ;
+; damping_posdef 8.00E-3 8.00E-03 8.00E-02 4.65E-04 4.65E-04 2.38E-02 ; "tuned by Anyd 22/2/13
+ damping_posdef 0.0 0.0 3.983E-03 4.65E-04 4.65E-04 3.983E-03 ; "tuned by Anyd 23/5/13 to 31.45 l
+ concentrated_mass 1.0 0.0 0.0 0.0 0.0 0.0 0.0 3.751E+06 ; generator equivalent slow shaft "re_tu
+ concentrated_mass 5.0 0.0 0.0 0.0 1.0552E+05 0.0 0.0 3.257E+05 ; hub mass and inertia; "re_tuned
+ begin timoschenko_input;
+ filename ./data/DTU_10MW_RWT_Shaft_st.dat ;
+ set 1 1 ;
+ end timoschenko_input;
+ begin c2_def; Definition of centerline (main_body coordinates)
+ nsec 5;
+ sec 1 0.0 0.0 0.0 0.0 ; Tower top x,y,z,twist
+ sec 2 0.0 0.0 1.5 0.0 ;
+ sec 3 0.0 0.0 3.0 0.0 ;
+ sec 4 0.0 0.0 4.4 0.0 ; Main bearing
+ sec 5 0.0 0.0 7.1 0.0 ; Rotor centre
+ end c2_def ;
+ end main_body;
+;
+ begin main_body;
+ name shaft_nonrotate ;
+ type timoschenko ;
+ nbodies 1 ;
+ node_distribution c2_def ;
+ damping_posdef 0.00E+00 0.00E+00 0.00E+00 1.0E-01 1.0E-01 1.0E-01 ;
+ begin timoschenko_input;
+ filename ./data/DTU_10MW_RWT_Shaft_st.dat ;
+ set 1 3; dummy light and stiff structure
+ end timoschenko_input;
+ begin c2_def;
+ nsec 2;
+ sec 1 0.0 0.0 0.0 0.0 ;
+ sec 2 0.0 0.0 0.1 0.0 ;
+ end c2_def;
+ end main_body;
+;
+ begin main_body;
+ name hub1 ;
+ type timoschenko ;
+ nbodies 1 ;
+ node_distribution c2_def ;
+ damping_posdef 2.00E-05 2.00E-05 2.00E-04 3.00E-06 3.00E-06 2.00E-05;
+ begin timoschenko_input;
+ filename ./data/DTU_10MW_RWT_Hub_st.dat ;
+ set 1 2 ;
+ end timoschenko_input;
+ begin c2_def; Definition of centerline (main_body coordinates)
+ nsec 2;
+ sec 1 0.0 0.0 0.0 0.0 ; x,y,z,twist
+ sec 2 0.0 0.0 2.8 0.0 ;
+ end c2_def ;
+ end main_body;
+;
+ begin main_body;
+ name hub2 ;
+ copy_main_body hub1;
+ end main_body;
+;
+ begin main_body;
+ name hub3 ;
+ copy_main_body hub1 ;
+ end main_body;
+;
+ begin main_body;
+ name blade1 ;
+ type timoschenko ;
+ nbodies 10 ;
+ node_distribution c2_def;
+; damping_posdef 0.0 0.0 0.0 2.5e-3 8.9e-4 3.2e-4 ; "Tuned by Anyd"
+; damping_posdef 0.0 0.0 0.0 1.5e-3 2.45e-3 3.2e-4 ; " 3% damping tuned by Anyd 20/02/12 unable to
+; damping_posdef 0.0 0.0 0.0 2.1e-3 1.9e-3 1.3e-4 ; " 3% damping tuned by Anyd 15/08/14 rev2
+ damping_posdef 0.0 0.0 0.0 1.68e-3 2.25e-3 1.0e-4 ; " 3% damping tuned by Anyd 16/12/14
+ begin timoschenko_input ;
+ filename ./data/AVATAR_10MW_RWT_Blade_st.dat ;
+ set 1 9 ;
+ end timoschenko_input;
+ begin c2_def;
+ nsec 27 ;
+ sec 1 -0.001 -0.001 0.000 -17.280 ;
+ sec 2 -0.005 -0.001 2.220 -17.280 ;
+ sec 3 -0.006 -0.000 4.440 -17.280 ;
+ sec 4 -0.086 0.022 6.660 -17.280 ;
+ sec 5 -0.231 0.069 11.039 -17.273 ;
+ sec 6 -0.447 0.121 15.418 -16.441 ;
+ sec 7 -0.690 0.161 19.797 -14.613 ;
+ sec 8 -0.812 0.162 24.176 -12.578 ;
+ sec 9 -0.891 0.158 28.555 -10.588 ;
+ sec 10 -0.865 0.124 32.934 -9.070 ;
+ sec 11 -0.833 0.112 37.313 -8.224 ;
+ sec 12 -0.797 0.102 41.692 -7.688 ;
+ sec 13 -0.760 0.093 46.071 -7.205 ;
+ sec 14 -0.721 0.083 50.450 -6.749 ;
+ sec 15 -0.683 0.075 54.829 -6.288 ;
+ sec 16 -0.644 0.066 59.208 -5.838 ;
+ sec 17 -0.606 0.058 63.587 -5.401 ;
+ sec 18 -0.567 0.050 67.966 -4.982 ;
+ sec 19 -0.529 0.044 72.345 -4.640 ;
+ sec 20 -0.492 0.037 76.724 -4.380 ;
+ sec 21 -0.456 0.032 81.103 -4.144 ;
+ sec 22 -0.422 0.026 85.482 -3.914 ;
+ sec 23 -0.392 0.021 89.861 -3.685 ;
+ sec 24 -0.346 0.014 94.240 -3.460 ;
+ sec 25 -0.307 0.010 96.190 -3.350 ;
+ sec 26 -0.249 0.005 98.130 -3.250 ;
+ sec 27 -0.089 0.006 100.080 -3.140 ;
+ end c2_def ;
+ end main_body;
+;
+ begin main_body;
+ name blade2 ;
+ copy_main_body blade1;
+ end main_body;
+;
+ begin main_body;
+ name blade3 ;
+ copy_main_body blade1 ;
+ end main_body;
+;-------------------------------------------------------------------------------------------------------------------------------
+;
+ begin orientation;
+ begin base;
+ body tower;
+ inipos 0.0 0.0 0.0 ; initial position of node 1
+ body_eulerang 0.0 0.0 0.0;
+ end base;
+;
+ begin relative;
+ body1 tower last;
+ body2 towertop 1;
+ body2_eulerang 0.0 0.0 0.0;
+ end relative;
+;
+ begin relative;
+ body1 towertop last;
+ body2 shaft 1;
+ body2_eulerang 90.0 0.0 0.0;
+ body2_eulerang 5.0 0.0 0.0; 5 deg tilt angle
+ body2_eulerang 0.0 0.0 0;
+ mbdy2_ini_rotvec_d1 0.0 0.0 -1.0 0.5 ; mbdy2_ini_rotvec_d1 0.0 0.0 -1.0 0.5;
+ end relative;
+;
+ begin relative; dummy non rotating hub coordinates
+ body1 towertop last;
+ body2 shaft_nonrotate 1;
+ body2_eulerang 90.0 0.0 0.0;
+ body2_eulerang 5.0 0.0 0.0; same 5 deg tilt angle as real shaft
+ end relative;
+;
+ begin relative;
+ body1 shaft last;
+ body2 hub1 1;
+ body2_eulerang -90.0 0.0 0.0;
+ body2_eulerang 0.0 180.0 0.0;
+ body2_eulerang 2.5 0.0 0.0; 2.5deg cone angle
+ end relative;
+;
+ begin relative;
+ body1 shaft last;
+ body2 hub2 1;
+ body2_eulerang -90.0 0.0 0.0;
+ body2_eulerang 0.0 60.0 0.0;
+ body2_eulerang 2.5 0.0 0.0; 2.5deg cone angle
+ end relative;
+;
+ begin relative;
+ body1 shaft last;
+ body2 hub3 1;
+ body2_eulerang -90.0 0.0 0.0;
+ body2_eulerang 0.0 -60.0 0.0;
+ body2_eulerang 2.5 0.0 0.0; 2.5deg cone angle
+ end relative;
+;
+ begin relative;
+ body1 hub1 last;
+ body2 blade1 1;
+ body2_eulerang 0.0 0.0 0;
+ end relative;
+;
+ begin relative;
+ body1 hub2 last;
+ body2 blade2 1;
+ body2_eulerang 0.0 0.0 0.0;
+ end relative;
+;
+ begin relative;
+ body1 hub3 last;
+ body2 blade3 1;
+ body2_eulerang 0.0 0.0 0.0;
+ end relative;
+;
+ end orientation;
+;-------------------------------------------------------------------------------------------------------------------------------
+begin constraint;
+;
+ begin fix0; fixed to ground in translation and rotation of node 1
+ body tower;
+ end fix0;
+;
+ begin fix1;
+ body1 tower last ;
+ body2 towertop 1;
+ end fix1;
+;
+ begin bearing1; free bearing
+ name shaft_rot;
+ body1 towertop last;
+ body2 shaft 1;
+ bearing_vector 2 0.0 0.0 -1.0; x=coo (0=global.1=body1.2=body2) vector in body2 coordinates where the free rotation is present
+ end bearing1;
+;
+; begin bearing3; free bearing
+; name shaft_rot;
+; body1 towertop last;
+; body2 shaft 1;
+; bearing_vector 2 0.0 0.0 -1.0; x=coo (0=global.1=body1.2=body2) vector in body2 coordinates where the free rotation is present
+; omegas 0.0 ;
+; end bearing3;
+;
+ begin fix1;
+ body1 tower last ;
+ body2 shaft_nonrotate 1;
+ end fix1;
+;
+ begin fix1;
+ body1 shaft last ;
+ body2 hub1 1;
+ end fix1;
+;
+ begin fix1;
+ body1 shaft last ;
+ body2 hub2 1;
+ end fix1;
+;
+ begin fix1;
+ body1 shaft last ;
+ body2 hub3 1;
+ end fix1;
+;
+ begin bearing2;
+ name pitch1;
+ body1 hub1 last;
+ body2 blade1 1;
+ bearing_vector 2 0.0 0.0 -1.0;
+ end bearing2;
+;
+ begin bearing2;
+ name pitch2;
+ body1 hub2 last;
+ body2 blade2 1;
+ bearing_vector 2 0.0 0.0 -1.0;
+ end bearing2;
+;
+ begin bearing2;
+ name pitch3;
+ body1 hub3 last;
+ body2 blade3 1;
+ bearing_vector 2 0.0 0.0 -1.0;
+ end bearing2;
+end constraint;
+;
+end new_htc_structure;
+;----------------------------------------------------------------------------------------------------------------------------------------------------------------
+begin wind ;
+ density 1.225 ;
+ wsp 8 ;
+ tint 0.232 ;
+ horizontal_input 1 ;
+ windfield_rotations 0 8.0 0.0 ; yaw, tilt (positive=upflow=wind coming from below), rotation
+ center_pos0 0.0 0.0 -127 ; hub heigth
+ shear_format 3 0 ;
+ turb_format 0 ; 0=none, 1=mann,2=flex
+ tower_shadow_method 3 ; 0=none, 1=potential flow, 2=jet
+ scale_time_start 20 ;
+ wind_ramp_factor 0.0 20 1.0 1.0 ;
+ ; iec_gust ;
+;
+; wind_ramp_abs 400.0 401.0 0.0 1.0 ; wsp. after the step: 5.0
+; wind_ramp_abs 501.0 502.0 0.0 1.0 ; wsp. after the step: 6.0
+; wind_ramp_abs 602.0 603.0 0.0 1.0 ; wsp. after the step: 7.0
+; wind_ramp_abs 703.0 704.0 0.0 1.0 ; wsp. after the step: 8.0
+; wind_ramp_abs 804.0 805.0 0.0 1.0 ; wsp. after the step: 9.0
+; wind_ramp_abs 905.0 906.0 0.0 1.0 ; wsp. after the step: 10.0
+; wind_ramp_abs 1006.0 1007.0 0.0 1.0 ; wsp. after the step: 11.0
+; wind_ramp_abs 1107.0 1108.0 0.0 1.0 ; wsp. after the step: 12.0
+; wind_ramp_abs 1208.0 1209.0 0.0 1.0 ; wsp. after the step: 13.0
+; wind_ramp_abs 1309.0 1310.0 0.0 1.0 ; wsp. after the step: 14.0
+; wind_ramp_abs 1410.0 1411.0 0.0 1.0 ; wsp. after the step: 15.0
+; wind_ramp_abs 1511.0 1512.0 0.0 1.0 ; wsp. after the step: 16.0
+; wind_ramp_abs 1612.0 1613.0 0.0 1.0 ; wsp. after the step: 17.0
+; wind_ramp_abs 1713.0 1714.0 0.0 1.0 ; wsp. after the step: 18.0
+; wind_ramp_abs 1814.0 1815.0 0.0 1.0 ; wsp. after the step: 19.0
+; wind_ramp_abs 1915.0 1916.0 0.0 1.0 ; wsp. after the step: 20.0
+; wind_ramp_abs 2016.0 2017.0 0.0 1.0 ; wsp. after the step: 21.0
+; wind_ramp_abs 2117.0 2118.0 0.0 1.0 ; wsp. after the step: 22.0
+; wind_ramp_abs 2218.0 2219.0 0.0 1.0 ; wsp. after the step: 23.0
+; wind_ramp_abs 2319.0 2320.0 0.0 1.0 ; wsp. after the step: 24.0
+; wind_ramp_abs 2420.0 2421.0 0.0 1.0 ; wsp. after the step: 25.0
+ ;
+; wind_ramp_abs 400.0 2200.0 0.0 21.0 ; wsp. after the step: 25.0
+; wind_ramp_abs 2400.0 4200.0 0.0 -21.0 ; wsp. after the step: 25.0
+ ;
+ begin mann ;
+ create_turb_parameters 29.4 1.0 3.9 0 1.0 ; L, alfaeps, gamma, seed, highfrq compensation
+ filename_u ./turb/noneu.bin ;
+ filename_v ./turb/nonev.bin ;
+ filename_w ./turb/nonew.bin ;
+ box_dim_u 8192 0.0390625 ;
+ box_dim_v 32 7.5;
+ box_dim_w 32 7.5;
+ std_scaling 1.0 0.7 0.5 ;
+ end mann ;
+;
+ begin tower_shadow_potential_2;
+ tower_mbdy_link tower;
+ nsec 2;
+ radius 0.0 4.15 ;
+ radius 123.6 2.75 ; (radius)
+ end tower_shadow_potential_2;
+end wind;
+;
+begin aerodrag ;
+ begin aerodrag_element ;
+ mbdy_name tower;
+ aerodrag_sections uniform 10 ;
+ nsec 2 ;
+ sec 0.0 0.6 8.3 ; tower bottom
+ sec 123.6 0.6 5.5 ; tower top (diameter)
+ end aerodrag_element;
+;
+ begin aerodrag_element ; Nacelle drag side
+ mbdy_name shaft;
+ aerodrag_sections uniform 2 ;
+ nsec 2 ;
+ sec 0.0 0.8 10.0 ;
+ sec 7.01 0.8 10.0 ;
+ end aerodrag_element;
+end aerodrag;
+;
+begin aero ;
+ nblades 3;
+ hub_vec shaft -3 ; rotor rotation vector (normally shaft composant directed from pressure to sustion side)
+ link 1 mbdy_c2_def blade1;
+ link 2 mbdy_c2_def blade2;
+ link 3 mbdy_c2_def blade3;
+ ae_filename ./data/AVATAR_10MW_RWT_ae.dat ;
+ pc_filename ./data/AVATAR_10MW_RWT_pc_hama_v1.dat ;
+ induction_method 1 ; 0=none, 1=normal
+ aerocalc_method 1 ; 0=ingen aerodynamic, 1=med aerodynamic
+ aero_distribution ae_file 1 ;
+ ae_sets 1 1 1;
+ tiploss_method 1 ; 0=none, 1=prandtl
+ dynstall_method 2 ; 0=none, 1=stig øye method,2=mhh method
+;
+; ; --- Flaps --- ;
+ ; begin dynstall_ateflap ;
+ ; Ais 0.165 0.335 0.0 ;
+ ; Bis 0.0455 0.30 0.30 ;
+ ; flap 59.5925 85.5023 ./data/Flap_dturwt1_Thk24.ds ; Flap Sec: 1
+ ; end dynstall_ateflap;
+end aero ;
+;-------------------------------------------------------------------------------------------------
+begin dll;
+;
+ begin type2_dll;
+ name risoe_controller ;
+ filename ./control/risoe_controller.dll ;
+ dll_subroutine_init init_regulation ;
+ dll_subroutine_update update_regulation ;
+ arraysizes_init 52 1 ;
+ arraysizes_update 12 100 ;
+ begin init ;
+ ; Overall parameters
+ constant 1 10000.0 ; Rated power [kW]
+ constant 2 0.628 ; Minimum rotor speed [rad/s]
+ constant 3 1.005 ; Rated rotor speed [rad/s]
+ constant 4 15.6E+06 ; Maximum allowable generator torque [Nm]
+ 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 'wpdata.n', where n=int(theta_min)
+ 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 9 0.7 ; Damping ratio of speed filter [-]
+ constant 10 1.64 ; Frequency of free-free DT torsion mode [Hz], if zero no notch filter used
+ ; Partial load control parameters
+ constant 11 0.9648030e+07 ; 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 1.047610E+08 ; Proportional gain of torque controller [Nm/(rad/s)]
+ constant 13 0.153367E+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, 2=constant torque]
+ constant 16 0.762489 ; Proportional gain of pitch controller [rad/(rad/s)]
+ constant 17 0.224086 ; Integral gain of pitch controller [rad/rad]
+ constant 18 0.0 ; Differential gain of pitch controller [rad/(rad/s^2)]
+ constant 19 0.4e-9 ; Proportional power error gain [rad/W]
+ constant 20 0.4e-9 ; Integral power error gain [rad/(Ws)]
+ constant 21 10.6824 ; Coefficient of linear term in aerodynamic gain scheduling, KK1 [deg]
+ constant 22 601.25499 ; 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
+ constant 24 -1 ; Cut-in time [s]
+ constant 25 1.0 ; Time delay for soft start of torque [1/1P]
+; Cut-out simulation parameters
+ constant 26 -1 ; Cut-out time [s]
+ constant 27 5.0 ; Time constant for linear torque cut-out [s]
+ constant 28 1 ; Stop type [1=normal, 2=emergency]
+ constant 29 1.0 ; Time delay for pitch stop after shut-down signal [s]
+ constant 30 3 ; Maximum pitch velocity during initial period of stop [deg/s]
+ constant 31 3.0 ; Time period of initial pitch stop phase [s] (maintains pitch speed specified in constant 30)
+ constant 32 4 ; Maximum pitch velocity during final phase of stop [deg/s]
+; Expert parameters (keep default values unless otherwise given)
+ constant 33 2.0 ; Lower angle above lowest minimum pitch angle for switch [deg]
+ constant 34 2.0 ; Upper angle above lowest minimum pitch angle for switch [deg], if equal then hard switch
+ constant 35 95.0 ; Ratio between filtered speed and reference speed for fully open torque limits [%]
+ constant 36 2.0 ; Time constant of 1st order filter on wind speed used for minimum pitch [1/1P]
+ constant 37 1.0 ; Time constant of 1st order filter on pitch angle used for gain scheduling [1/1P]
+; Drivetrain damper
+ constant 38 0.0 ; Proportional gain of active DT damper [Nm/(rad/s)], requires frequency in input 10
+; Over speed
+ constant 39 25.0 ; Overspeed percentage before initiating turbine controller alarm (shut-down) [%]
+; Additional non-linear pitch control term (not used when all zero)
+ constant 40 0.0 ; Err0 [rad/s]
+ constant 41 0.0 ; ErrDot0 [rad/s^2]
+ constant 42 0.0 ; PitNonLin1 [rad/s]
+; Storm control command
+ constant 43 28.0 ; Wind speed 'Vstorm' above which derating of rotor speed is used [m/s]
+ constant 44 28.0 ; Cut-out wind speed (only used for derating of rotor speed in storm) [m/s]
+; Safety system parameters
+ constant 45 25.0 ; Overspeed percentage before initiating safety system alarm (shut-down) [%]
+ constant 46 1.5 ; Max low-pass filtered tower top acceleration level [m/s^2] - max in DLC 1.3=1.1 m/s^2
+; Turbine parameter
+ constant 47 205.8 ; Nominal rotor diameter [m]
+; Parameters for rotor inertia reduction in variable speed region
+ constant 48 0.0 ; Proportional gain on rotor acceleration in variable speed region [Nm/(rad/s^2)] (not used when zero)
+; Parameters for alternative partial load controller with PI regulated TSR tracking
+ constant 49 0.0 ; Optimal tip speed ratio [-] (only used when K=constant 11 = 0 otherwise Qg=K*Omega^2 is used)
+; Parameters for adding aerodynamic drivetrain damping on gain scheduling
+ constant 50 0.0 ; Proportional gain of aerodynamic DT damping [Nm/(rad/s)]
+ constant 51 0.0 ; Coefficient of linear term in aerodynamic DT damping scheduling, KK1 [deg]
+ constant 52 0.0 ; Coefficient of quadratic term in aerodynamic DT damping scheduling, KK2 [deg^2]
+ end init ;
+;
+ begin output ;
+ general time ; [s]
+ constraint bearing1 shaft_rot 1 only 2 ; Drivetrain speed [rad/s]
+ constraint bearing2 pitch1 1 only 1; [rad]
+ constraint bearing2 pitch2 1 only 1; [rad]
+ constraint bearing2 pitch3 1 only 1; [rad]
+ wind free_wind 1 0.0 0.0 -127 ; Global coordinates at hub height
+ dll inpvec 2 2 ; Elec. power from generator servo .dll
+ dll inpvec 2 8 ; Grid state flag from generator servo .dll
+ mbdy state acc tower 10 1.0 global only 1 ; Tower top x-acceleration [m/s^2]
+ mbdy state acc tower 10 1.0 global only 2 ; Tower top y-acceleration [m/s^2]
+ end output;
+ end type2_dll;
+;
+ begin type2_dll;
+ name generator_servo ;
+ filename ./control/generator_servo.dll ;
+ dll_subroutine_init init_generator_servo ;
+ dll_subroutine_update update_generator_servo ;
+ arraysizes_init 7 1 ;
+ arraysizes_update 4 8 ;
+ begin init ;
+ constant 1 20.0 ; Frequency of 2nd order servo model of generator-converter system [Hz]
+ constant 2 0.9 ; Damping ratio 2nd order servo model of generator-converter system [-]
+ constant 3 15.6E+06 ; Maximum allowable LSS torque (pull-out torque) [Nm]
+ constant 4 0.94 ; Generator efficiency [-]
+ constant 5 1.0 ; Gearratio [-]
+ constant 6 0.0 ; Time for half value in softstart of torque [s]
+ constant 7 5000 ; Time for grid loss [s]
+ end init ;
+;
+ begin output;
+ general time ; Time [s]
+ dll inpvec 1 1 ; Electrical torque reference [Nm]
+ constraint bearing1 shaft_rot 1 only 2; Generator LSS speed [rad/s]
+ mbdy momentvec shaft 1 1 shaft only 3 ; Shaft moment [kNm] (Qshaft)
+ end output;
+;
+ begin actions;
+ mbdy moment_int shaft 1 -3 shaft towertop 2 ; Generator LSS torque [Nm]
+ end actions;
+ end type2_dll;
+;
+ begin type2_dll;
+ name mech_brake ;
+ filename ./control/mech_brake.dll ;
+ dll_subroutine_init init_mech_brake ;
+ dll_subroutine_update update_mech_brake ;
+ arraysizes_init 7 1 ;
+ arraysizes_update 4 6 ;
+ begin init ;
+ constant 1 5225.35 ; Fully deployed maximum brake torque [Nm] (0.6*max torque)
+ constant 2 100.0 ; Parameter alpha used in Q = tanh(omega*alpha), typically 1e2/Omega_nom
+ constant 3 0.5 ; Delay time for before brake starts to deploy [s]
+ constant 4 0.74 ; Time for brake to become fully deployed [s]
+ end init ;
+;
+ begin output;
+ general time ; Time [s]
+ constraint bearing1 shaft_rot 1 only 2 ; Generator LSS speed [rad/s]
+ dll inpvec 1 25 ; Command to deploy mechanical disc brake [0,1]
+ end output;
+;
+ begin actions;
+ mbdy moment_int shaft 1 -3 shaft towertop 2 ; Generator LSS torque [Nm]
+ end actions;
+ end type2_dll;
+;
+ begin type2_dll;
+ name servo_with_limits ;
+ filename ./control/servo_with_limits.dll ;
+ dll_subroutine_init init_servo_with_limits ;
+ dll_subroutine_update update_servo_with_limits ;
+ arraysizes_init 10 1 ;
+ arraysizes_update 5 9 ;
+ begin init ;
+ constant 1 3 ; Number of blades [-]
+ constant 2 1.0 ; Frequency of 2nd order servo model of pitch system [Hz]
+ constant 3 0.7 ; Damping ratio 2nd order servo model of pitch system [-]
+ constant 4 10.0 ; Max. pitch speed [deg/s]
+ constant 5 15.0 ; Max. pitch acceleration [deg/s^2]
+ constant 6 -5.0 ; Min. pitch angle [deg]
+ constant 7 90.0 ; Max. pitch angle [deg]
+ constant 8 5000 ; Time for pitch runaway [s]
+ constant 9 -1 ; Time for stuck blade 1 [s]
+ constant 10 0 ; Angle of stuck blade 1 [deg]
+ end init ;
+ begin output;
+ general time ; Time [s]
+ dll inpvec 1 2 ; Pitch1 demand angle [rad]
+ dll inpvec 1 3 ; Pitch2 demand angle [rad]
+ dll inpvec 1 4 ; Pitch3 demand angle [rad]
+ dll inpvec 1 26 ; Flag for emergency pitch stop [0=off/1=on]
+ end output;
+;
+ begin actions;
+ constraint bearing2 angle pitch1 ; Angle pitch1 bearing [rad]
+ constraint bearing2 angle pitch2 ; Angle pitch2 bearing [rad]
+ constraint bearing2 angle pitch3 ; Angle pitch3 bearing [rad]
+ end actions;
+ end type2_dll;
+;
+; --- DLL for tower-blade tip distance -- ;
+ begin type2_dll;
+ name disttowtip ;
+ filename ./control/towclearsens.dll ;
+ dll_subroutine_init initialize ;
+ dll_subroutine_update update ;
+ arraysizes_init 1 1 ;
+ arraysizes_update 12 4 ;
+ begin init ;
+ constant 1 3.87 ; Tower radius close to downward blade tip [m]
+ end init ;
+ begin output;
+ mbdy state pos tower 5 0.00 global ; [1,2,3]. Tower position: 24.58 m
+ mbdy state pos blade1 26 1.0 global ; [4,5,6]
+ mbdy state pos blade2 26 1.0 global ; [7,8,9]
+ mbdy state pos blade3 26 1.0 global ; [10,11,12]
+ end output;
+ end type2_dll;
+end dll;
+;
+;----------------------------------------------------------------------------------------------------------------------------------------------------------------
+;
+begin output;
+ filename ./res/dlc01_demos/dlc01_steady_wsp8_noturb ;
+ time 20 40 ;
+ data_format hawc_binary;
+ buffer 1 ;
+;
+ general time;
+ constraint bearing1 shaft_rot 2; angle and angle velocity
+ constraint bearing2 pitch1 5; angle and angle velocity
+ constraint bearing2 pitch2 5; angle and angle velocity
+ constraint bearing2 pitch3 5; angle and angle velocity
+ aero omega ;
+ aero torque;
+ aero power;
+ aero thrust;
+ wind free_wind 1 0.0 0.0 -127; local wind at fixed position: coo (1=global,2=non-rotation rotor coo.), pos x, pos y, pos z
+ ; non rotating coordinates shaft tip: equivalent to stationary hub in BLADED
+ mbdy momentvec shaft 3 2 shaft_nonrotate # non rotating shaft tip ;
+ mbdy forcevec shaft 3 2 shaft_nonrotate # non rotating shaft tip ;
+ ; Moments:
+ mbdy momentvec tower 1 1 tower # tower base ;
+ mbdy momentvec tower 19 2 tower # tower yaw bearing ;
+ mbdy momentvec shaft 4 1 shaft # main bearing ;
+ mbdy momentvec blade1 3 2 blade1 # blade 1 root ;
+ mbdy momentvec blade2 3 2 blade2 # blade 2 root ;
+ mbdy momentvec blade3 3 2 blade3 # blade 3 root ;
+ ; blade 2,3 root section loads
+ mbdy momentvec blade2 3 2 local # blade 2 section root;
+ mbdy momentvec blade3 3 2 local # blade 3 section root;
+ ; blade 1 sectional loads in local coordinates
+ mbdy momentvec blade1 2 2 local # blade 1 section;
+ mbdy momentvec blade1 3 2 local # blade 1 section root;
+ mbdy momentvec blade1 4 2 local # blade 1 section;
+ mbdy momentvec blade1 5 2 local # blade 1 section;
+ mbdy momentvec blade1 6 2 local # blade 1 section;
+ mbdy momentvec blade1 7 2 local # blade 1 section;
+ mbdy momentvec blade1 8 2 local # blade 1 section;
+ mbdy momentvec blade1 9 2 local # blade 1 section;
+ mbdy momentvec blade1 10 2 local # blade 1 section;
+ mbdy momentvec blade1 11 2 local # blade 1 section;
+ mbdy momentvec blade1 12 2 local # blade 1 section;
+ mbdy momentvec blade1 13 2 local # blade 1 section;
+ mbdy momentvec blade1 14 2 local # blade 1 section;
+ mbdy momentvec blade1 15 2 local # blade 1 section;
+ mbdy momentvec blade1 16 2 local # blade 1 section;
+ mbdy momentvec blade1 17 2 local # blade 1 section;
+ mbdy momentvec blade1 18 2 local # blade 1 section;
+ mbdy momentvec blade1 19 2 local # blade 1 section;
+ mbdy momentvec blade1 20 2 local # blade 1 section;
+ mbdy momentvec blade1 21 2 local # blade 1 section;
+ mbdy momentvec blade1 22 2 local # blade 1 section;
+ mbdy momentvec blade1 23 2 local # blade 1 section;
+ mbdy momentvec blade1 24 2 local # blade 1 section;
+ mbdy momentvec blade1 25 2 local # blade 1 section;
+ mbdy momentvec blade1 26 2 local # blade 1 section;
+ ; blade root out and in of plane forces
+ mbdy momentvec blade1 3 2 hub1 # blade 1 root ;
+ mbdy momentvec blade2 3 2 hub2 # blade 2 root ;
+ mbdy momentvec blade3 3 2 hub3 # blade 3 root ;
+; mbdy momentvec blade1 14 1 local # blade 1 50% local e coo ;
+; mbdy momentvec blade2 14 1 local # blade 2 50% local e coo ;
+; mbdy momentvec blade3 14 1 local # blade 3 50% local e coo ;
+ ; Displacements and accellerations
+ mbdy state pos tower 19 1.0 global only 1 # Tower top FA displ;
+ mbdy state pos tower 19 1.0 global only 2 # Tower top SS displ;
+ mbdy state acc tower 19 1.0 global only 1 # Tower top FA acc;
+ mbdy state acc tower 19 1.0 global only 2 # Tower top SS acc;
+;
+ mbdy state pos blade1 26 1.0 global # gl blade 1 tip pos ;
+ mbdy state pos blade2 26 1.0 global # gl blade 2 tip pos ;
+ mbdy state pos blade3 26 1.0 global # gl blade 3 tip pos ;
+ mbdy state pos blade1 26 1.0 blade1 # blade 1 tip pos ;
+ mbdy state pos blade2 26 1.0 blade2 # blade 2 tip pos ;
+ mbdy state pos blade3 26 1.0 blade3 # blade 3 tip pos ;
+;
+ mbdy state pos tower 5 0.00 global ; [1,2,3]. Tower position: 24.58 m
+;
+ ; elastic twist (torsional deformation) along the blade
+ aero tors_ang 1 45.56;
+ aero tors_ang 1 59.19;
+ aero tors_ang 1 70.87;
+ aero tors_ang 1 80.61;
+ aero tors_ang 1 84.50;
+ aero tors_ang 1 88.40;
+ aero tors_ang 1 92.29;
+ aero tors_ang 1 96.19;
+ aero tors_ang 1 98.13;
+ aero tors_ang 1 100.08; tip
+;
+; - Monitor Aerodynamics - ;
+ aero windspeed 3 1 1 72.5;
+ aero alfa 1 72.5;
+ aero alfa 2 72.5;
+ aero alfa 3 72.5;
+ aero cl 1 72.5;
+ aero cl 2 72.5;
+ aero cl 3 72.5;
+ aero cd 1 72.5;
+ aero cd 2 72.5;
+ aero cd 3 72.5;
+; - Main Controller -
+; Output to controller
+ ; dll outvec 1 1 # time;
+ ; dll outvec 1 2 # slow speed shaft rad/s;
+ ; dll outvec 1 3 # pitch angle 1;
+ ; dll outvec 1 4 # pitch angle 2;
+ ; dll outvec 1 5 # pitch angle 3;
+ ; dll outvec 1 6 # WSP_x_global;
+ ; dll outvec 1 7 # WSP_y_global;
+ ; dll outvec 1 8 # WSP_z_global;
+ ; dll outvec 1 9 # Elec. pwr ;
+ ; dll outvec 1 10 # Grid flag ;
+; Input from controller
+ dll inpvec 1 1 # Generator torque reference [Nm] ;
+ dll inpvec 1 2 # Pitch angle reference of blade 1 [rad] ;
+ dll inpvec 1 3 # Pitch angle reference of blade 2 [rad] ;
+ dll inpvec 1 4 # Pitch angle reference of blade 3 [rad] ;
+ ; dll inpvec 1 5 # Power reference [W] ;
+ ; dll inpvec 1 6 # Filtered wind speed [m/s] ;
+ ; dll inpvec 1 7 # Filtered rotor speed [rad/s];
+ ; dll inpvec 1 8 # Filtered rotor speed error for torque [rad/s];
+ ; dll inpvec 1 9 # Bandpass filtered rotor speed [rad/s];
+ ; dll inpvec 1 10 # Proportional term of torque contr. [Nm] ;
+ ; dll inpvec 1 11 # Integral term of torque controller [Nm] ;
+ ; dll inpvec 1 12 # Minimum limit of torque [Nm] ;
+ ; dll inpvec 1 13 # Maximum limit of torque [Nm] ;
+ dll inpvec 1 14 # Torque limit switch based on pitch [-] ;
+ ; dll inpvec 1 15 # Filtered rotor speed error for pitch [rad/s];
+ ; dll inpvec 1 16 # Power error for pitch [W] ;
+ ; dll inpvec 1 17 # Proportional term of pitch controller [rad] ;
+ ; dll inpvec 1 18 # Integral term of pitch controller [rad] ;
+ ; dll inpvec 1 19 # Minimum limit of pitch [rad] ;
+ ; dll inpvec 1 20 # Maximum limit of pitch [rad] ;
+ dll inpvec 1 21 # Torque reference from DT dammper [Nm] ;
+ dll inpvec 1 22 # Status signal [-] ;
+ ; dll inpvec 1 23 # Total added pitch rate [rad/s] ;
+ dll inpvec 1 24 # Filtered Mean pitch for gain sch [rad] ;
+ dll inpvec 1 25 # Flag for mechnical brake [0=off/1=on] ;
+ dll inpvec 1 26 # Flag for emergency pitch stop [0=off/1=on] ;
+ dll inpvec 1 27 # LP filtered acceleration level [m/s^2] ;
+; ; Output to generator model
+ ; dll outvec 2 1 # time ;
+ ; dll outvec 2 2 # Electrical torque reference [Nm] ;
+ ; dll outvec 2 3 # omega LSS ;
+; Input from generator model
+ dll inpvec 2 1 # Mgen LSS [Nm];
+ dll inpvec 2 2 # Pelec W ;
+ dll inpvec 2 3 # Mframe ;
+ dll inpvec 2 4 # Mgen HSS ;
+ dll inpvec 2 5 # Generator Pmech kW ;
+ dll inpvec 2 6 # Filtered Gen speed ;
+ dll inpvec 2 7 # Resulting Eff ;
+ dll inpvec 2 8 # Grid flag ;
+; Output to mechanical brake
+ dll inpvec 3 1 # Brake torque [Nm] ;
+; ; Input from mechanical brake
+ ; dll outvec 3 1 # Time [s] ;
+ ; dll outvec 3 2 # Generator LSS speed [rad/s] ;
+ ; dll outvec 3 3 # Deploy brake ;
+; ; Output to pitch servo
+ ; dll outvec 4 1 # time;
+ ; dll outvec 4 2 # pitchref 1;
+ ; dll outvec 4 3 # pitchref 2;
+ ; dll outvec 4 4 # pitchref 3;
+ ; dll outvec 4 5 # Emerg. stop;
+; Input from pitch servo
+ dll inpvec 4 1 # pitch 1;
+ dll inpvec 4 2 # pitch 2;
+ dll inpvec 4 3 # pitch 3;
+; Check tower clearence
+ dll inpvec 5 1 # Bltip tow min d [m];
+; general constant 1.0 ; constant 1.0 - to mesure activity of flap in terms of displacement
+; - Check on flap control:
+ ; ; - From flap controller: -
+ ; dll type2_dll cyclic_flap_controller inpvec 1 # Ref flap signal bl 1 [deg] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 2 # Ref flap signal bl 2 [deg] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 3 # Ref flap signal bl 3 [deg] ;
+ ; ; - Mbc values
+ ; dll type2_dll cyclic_flap_controller inpvec 4 # momvec mbc cos [kNm] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 5 # momvec mbc sin [kNm] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 6 # momvec mbc filt cos [kNm] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 7 # momvec mbc filt sin [kNm] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 8 # flap mbc cos [deg] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 9 # flap mbc sin [deg] ;
+ ; ; - Check Gains - ;
+ ; dll type2_dll cyclic_flap_controller inpvec 10 # lead angle [deg] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 11 # scaling on rat pow [-] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 12 # actual kp [deg/kNm] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 13 # actual ki [deg/kNms] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 14 # actual kd [deg s/kNm] ;
+ ; ; - Actual deflections -
+ ; aero beta 1 1 ;
+ ; aero beta 2 1 ;
+ ; aero beta 3 1 ;
+ ; ; - Mbc values
+ ; dll type2_dll cyclic_flap_controller inpvec 4 # momvec mbc cos [kNm] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 5 # momvec mbc sin [kNm] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 6 # momvec mbc filt cos [kNm] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 7 # momvec mbc filt sin [kNm] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 8 # flap mbc cos [deg] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 9 # flap mbc sin [deg] ;
+end output;
+;
+exit;
diff --git a/wetb/prepost/tests/data/demo_dlc/ref/htc/dlc01_demos/dlc01_steady_wsp9_noturb.htc b/wetb/prepost/tests/data/demo_dlc/ref/htc/dlc01_demos/dlc01_steady_wsp9_noturb.htc
new file mode 100644
index 00000000..537e8ef7
--- /dev/null
+++ b/wetb/prepost/tests/data/demo_dlc/ref/htc/dlc01_demos/dlc01_steady_wsp9_noturb.htc
@@ -0,0 +1,850 @@
+;this version was at some point based on: Avatar_10MW_RWT version 1, 06-08-14, Anyd
+begin simulation;
+ time_stop 40;
+ solvertype 1 ; (newmark)
+ on_no_convergence continue ;
+; convergence_limits 1E3 1.0 1E-7 ;
+ logfile ./logfiles/dlc01_demos/dlc01_steady_wsp9_noturb.log ;
+ begin newmark;
+ deltat 0.02;
+ end newmark;
+end simulation;
+;
+;----------------------------------------------------------------------------------------------------------------------------------------------------------------
+begin new_htc_structure;
+;--------------------------------------------------------------------------------------------------
+; beam_output_file_name ./res_eigen/dlc01_demos/dlc01_steady_wsp9_noturb/dlc01_steady_wsp9_noturb_beam.dat;
+; body_output_file_name ./res_eigen/dlc01_demos/dlc01_steady_wsp9_noturb/dlc01_steady_wsp9_noturb_body.dat;
+; struct_inertia_output_file_name ./res_eigen/dlc01_demos/dlc01_steady_wsp9_noturb/dlc01_steady_wsp9_noturb_struct.dat;
+; body_eigenanalysis_file_name ./res_eigen/dlc01_demos/dlc01_steady_wsp9_noturb/dlc01_steady_wsp9_noturb_body_eigen.dat;
+; structure_eigenanalysis_file_name ./res_eigen/dlc01_demos/dlc01_steady_wsp9_noturb/dlc01_steady_wsp9_noturb_strc_eigen.dat;
+;---------------------------------------------------------------------------------------------------
+ begin main_body; tower 123.6m
+ name tower ;
+ type timoschenko ;
+ nbodies 3 ;
+ node_distribution c2_def ;
+ damping_posdef 0 0 0 4.7E-03 4.7E-03 4.3E-04 ; tuned by Anyd 12/8/14
+ begin timoschenko_input;
+ filename ./data/AVATAR_10MW_RWT_tower_st.dat;
+ set 1 1 ;
+ end timoschenko_input;
+ begin c2_def; Definition of centerline (main_body coordinates)
+ nsec 20;
+ sec 1 0 0 0.000 0 ; x,y,z,twist
+ sec 2 0 0 -12.293 0 ;
+ sec 3 0 0 -12.294 0 ;
+ sec 4 0 0 -24.585 0 ;
+ sec 5 0 0 -24.586 0 ;
+ sec 6 0 0 -36.878 0 ;
+ sec 7 0 0 -36.879 0 ;
+ sec 8 0 0 -49.171 0 ;
+ sec 9 0 0 -49.172 0 ;
+ sec 10 0 0 -61.463 0 ;
+ sec 11 0 0 -61.464 0 ;
+ sec 12 0 0 -73.756 0 ;
+ sec 13 0 0 -73.757 0 ;
+ sec 14 0 0 -86.049 0 ;
+ sec 15 0 0 -86.050 0 ;
+ sec 16 0 0 -98.341 0 ;
+ sec 17 0 0 -98.342 0 ;
+ sec 18 0 0 -110.634 0 ;
+ sec 19 0 0 -110.635 0 ;
+ sec 20 0 0 -123.600 0 ;
+ end c2_def ;
+ end main_body;
+;
+ begin main_body;
+ name towertop ;
+ type timoschenko ;
+ nbodies 1 ;
+ node_distribution c2_def ;
+ damping_posdef 7.50E-03 7.40E-03 7.00E-03 7.00E-03 7.00E-03 7.00E-03 ; "changed by Anyd
+ concentrated_mass 2.0 0.0 2.6870E+00 3.0061E-01 4.4604E+05 4.1060E+06 4.1060E+05 4.1060E+06 ; Nacel
+ begin timoschenko_input;
+ filename ./data/DTU_10MW_RWT_Towertop_st.dat ;
+ set 1 2 ;
+ end timoschenko_input;
+ begin c2_def; Definition of centerline (main_body coordinates)
+ nsec 2;
+ sec 1 0.0 0.0 0.0 0.0 ; x,y,z,twist
+ sec 2 0.0 0.0 -2.75 0.0 ;
+ end c2_def ;
+ end main_body;
+;
+ begin main_body;
+ name shaft ;
+ type timoschenko ;
+ nbodies 1 ;
+ node_distribution c2_def ;
+; damping_posdef 8.00E-3 8.00E-03 8.00E-02 4.65E-04 4.65E-04 2.38E-02 ; "tuned by Anyd 22/2/13
+ damping_posdef 0.0 0.0 3.983E-03 4.65E-04 4.65E-04 3.983E-03 ; "tuned by Anyd 23/5/13 to 31.45 l
+ concentrated_mass 1.0 0.0 0.0 0.0 0.0 0.0 0.0 3.751E+06 ; generator equivalent slow shaft "re_tu
+ concentrated_mass 5.0 0.0 0.0 0.0 1.0552E+05 0.0 0.0 3.257E+05 ; hub mass and inertia; "re_tuned
+ begin timoschenko_input;
+ filename ./data/DTU_10MW_RWT_Shaft_st.dat ;
+ set 1 1 ;
+ end timoschenko_input;
+ begin c2_def; Definition of centerline (main_body coordinates)
+ nsec 5;
+ sec 1 0.0 0.0 0.0 0.0 ; Tower top x,y,z,twist
+ sec 2 0.0 0.0 1.5 0.0 ;
+ sec 3 0.0 0.0 3.0 0.0 ;
+ sec 4 0.0 0.0 4.4 0.0 ; Main bearing
+ sec 5 0.0 0.0 7.1 0.0 ; Rotor centre
+ end c2_def ;
+ end main_body;
+;
+ begin main_body;
+ name shaft_nonrotate ;
+ type timoschenko ;
+ nbodies 1 ;
+ node_distribution c2_def ;
+ damping_posdef 0.00E+00 0.00E+00 0.00E+00 1.0E-01 1.0E-01 1.0E-01 ;
+ begin timoschenko_input;
+ filename ./data/DTU_10MW_RWT_Shaft_st.dat ;
+ set 1 3; dummy light and stiff structure
+ end timoschenko_input;
+ begin c2_def;
+ nsec 2;
+ sec 1 0.0 0.0 0.0 0.0 ;
+ sec 2 0.0 0.0 0.1 0.0 ;
+ end c2_def;
+ end main_body;
+;
+ begin main_body;
+ name hub1 ;
+ type timoschenko ;
+ nbodies 1 ;
+ node_distribution c2_def ;
+ damping_posdef 2.00E-05 2.00E-05 2.00E-04 3.00E-06 3.00E-06 2.00E-05;
+ begin timoschenko_input;
+ filename ./data/DTU_10MW_RWT_Hub_st.dat ;
+ set 1 2 ;
+ end timoschenko_input;
+ begin c2_def; Definition of centerline (main_body coordinates)
+ nsec 2;
+ sec 1 0.0 0.0 0.0 0.0 ; x,y,z,twist
+ sec 2 0.0 0.0 2.8 0.0 ;
+ end c2_def ;
+ end main_body;
+;
+ begin main_body;
+ name hub2 ;
+ copy_main_body hub1;
+ end main_body;
+;
+ begin main_body;
+ name hub3 ;
+ copy_main_body hub1 ;
+ end main_body;
+;
+ begin main_body;
+ name blade1 ;
+ type timoschenko ;
+ nbodies 10 ;
+ node_distribution c2_def;
+; damping_posdef 0.0 0.0 0.0 2.5e-3 8.9e-4 3.2e-4 ; "Tuned by Anyd"
+; damping_posdef 0.0 0.0 0.0 1.5e-3 2.45e-3 3.2e-4 ; " 3% damping tuned by Anyd 20/02/12 unable to
+; damping_posdef 0.0 0.0 0.0 2.1e-3 1.9e-3 1.3e-4 ; " 3% damping tuned by Anyd 15/08/14 rev2
+ damping_posdef 0.0 0.0 0.0 1.68e-3 2.25e-3 1.0e-4 ; " 3% damping tuned by Anyd 16/12/14
+ begin timoschenko_input ;
+ filename ./data/AVATAR_10MW_RWT_Blade_st.dat ;
+ set 1 9 ;
+ end timoschenko_input;
+ begin c2_def;
+ nsec 27 ;
+ sec 1 -0.001 -0.001 0.000 -17.280 ;
+ sec 2 -0.005 -0.001 2.220 -17.280 ;
+ sec 3 -0.006 -0.000 4.440 -17.280 ;
+ sec 4 -0.086 0.022 6.660 -17.280 ;
+ sec 5 -0.231 0.069 11.039 -17.273 ;
+ sec 6 -0.447 0.121 15.418 -16.441 ;
+ sec 7 -0.690 0.161 19.797 -14.613 ;
+ sec 8 -0.812 0.162 24.176 -12.578 ;
+ sec 9 -0.891 0.158 28.555 -10.588 ;
+ sec 10 -0.865 0.124 32.934 -9.070 ;
+ sec 11 -0.833 0.112 37.313 -8.224 ;
+ sec 12 -0.797 0.102 41.692 -7.688 ;
+ sec 13 -0.760 0.093 46.071 -7.205 ;
+ sec 14 -0.721 0.083 50.450 -6.749 ;
+ sec 15 -0.683 0.075 54.829 -6.288 ;
+ sec 16 -0.644 0.066 59.208 -5.838 ;
+ sec 17 -0.606 0.058 63.587 -5.401 ;
+ sec 18 -0.567 0.050 67.966 -4.982 ;
+ sec 19 -0.529 0.044 72.345 -4.640 ;
+ sec 20 -0.492 0.037 76.724 -4.380 ;
+ sec 21 -0.456 0.032 81.103 -4.144 ;
+ sec 22 -0.422 0.026 85.482 -3.914 ;
+ sec 23 -0.392 0.021 89.861 -3.685 ;
+ sec 24 -0.346 0.014 94.240 -3.460 ;
+ sec 25 -0.307 0.010 96.190 -3.350 ;
+ sec 26 -0.249 0.005 98.130 -3.250 ;
+ sec 27 -0.089 0.006 100.080 -3.140 ;
+ end c2_def ;
+ end main_body;
+;
+ begin main_body;
+ name blade2 ;
+ copy_main_body blade1;
+ end main_body;
+;
+ begin main_body;
+ name blade3 ;
+ copy_main_body blade1 ;
+ end main_body;
+;-------------------------------------------------------------------------------------------------------------------------------
+;
+ begin orientation;
+ begin base;
+ body tower;
+ inipos 0.0 0.0 0.0 ; initial position of node 1
+ body_eulerang 0.0 0.0 0.0;
+ end base;
+;
+ begin relative;
+ body1 tower last;
+ body2 towertop 1;
+ body2_eulerang 0.0 0.0 0.0;
+ end relative;
+;
+ begin relative;
+ body1 towertop last;
+ body2 shaft 1;
+ body2_eulerang 90.0 0.0 0.0;
+ body2_eulerang 5.0 0.0 0.0; 5 deg tilt angle
+ body2_eulerang 0.0 0.0 0;
+ mbdy2_ini_rotvec_d1 0.0 0.0 -1.0 0.5 ; mbdy2_ini_rotvec_d1 0.0 0.0 -1.0 0.5;
+ end relative;
+;
+ begin relative; dummy non rotating hub coordinates
+ body1 towertop last;
+ body2 shaft_nonrotate 1;
+ body2_eulerang 90.0 0.0 0.0;
+ body2_eulerang 5.0 0.0 0.0; same 5 deg tilt angle as real shaft
+ end relative;
+;
+ begin relative;
+ body1 shaft last;
+ body2 hub1 1;
+ body2_eulerang -90.0 0.0 0.0;
+ body2_eulerang 0.0 180.0 0.0;
+ body2_eulerang 2.5 0.0 0.0; 2.5deg cone angle
+ end relative;
+;
+ begin relative;
+ body1 shaft last;
+ body2 hub2 1;
+ body2_eulerang -90.0 0.0 0.0;
+ body2_eulerang 0.0 60.0 0.0;
+ body2_eulerang 2.5 0.0 0.0; 2.5deg cone angle
+ end relative;
+;
+ begin relative;
+ body1 shaft last;
+ body2 hub3 1;
+ body2_eulerang -90.0 0.0 0.0;
+ body2_eulerang 0.0 -60.0 0.0;
+ body2_eulerang 2.5 0.0 0.0; 2.5deg cone angle
+ end relative;
+;
+ begin relative;
+ body1 hub1 last;
+ body2 blade1 1;
+ body2_eulerang 0.0 0.0 0;
+ end relative;
+;
+ begin relative;
+ body1 hub2 last;
+ body2 blade2 1;
+ body2_eulerang 0.0 0.0 0.0;
+ end relative;
+;
+ begin relative;
+ body1 hub3 last;
+ body2 blade3 1;
+ body2_eulerang 0.0 0.0 0.0;
+ end relative;
+;
+ end orientation;
+;-------------------------------------------------------------------------------------------------------------------------------
+begin constraint;
+;
+ begin fix0; fixed to ground in translation and rotation of node 1
+ body tower;
+ end fix0;
+;
+ begin fix1;
+ body1 tower last ;
+ body2 towertop 1;
+ end fix1;
+;
+ begin bearing1; free bearing
+ name shaft_rot;
+ body1 towertop last;
+ body2 shaft 1;
+ bearing_vector 2 0.0 0.0 -1.0; x=coo (0=global.1=body1.2=body2) vector in body2 coordinates where the free rotation is present
+ end bearing1;
+;
+; begin bearing3; free bearing
+; name shaft_rot;
+; body1 towertop last;
+; body2 shaft 1;
+; bearing_vector 2 0.0 0.0 -1.0; x=coo (0=global.1=body1.2=body2) vector in body2 coordinates where the free rotation is present
+; omegas 0.0 ;
+; end bearing3;
+;
+ begin fix1;
+ body1 tower last ;
+ body2 shaft_nonrotate 1;
+ end fix1;
+;
+ begin fix1;
+ body1 shaft last ;
+ body2 hub1 1;
+ end fix1;
+;
+ begin fix1;
+ body1 shaft last ;
+ body2 hub2 1;
+ end fix1;
+;
+ begin fix1;
+ body1 shaft last ;
+ body2 hub3 1;
+ end fix1;
+;
+ begin bearing2;
+ name pitch1;
+ body1 hub1 last;
+ body2 blade1 1;
+ bearing_vector 2 0.0 0.0 -1.0;
+ end bearing2;
+;
+ begin bearing2;
+ name pitch2;
+ body1 hub2 last;
+ body2 blade2 1;
+ bearing_vector 2 0.0 0.0 -1.0;
+ end bearing2;
+;
+ begin bearing2;
+ name pitch3;
+ body1 hub3 last;
+ body2 blade3 1;
+ bearing_vector 2 0.0 0.0 -1.0;
+ end bearing2;
+end constraint;
+;
+end new_htc_structure;
+;----------------------------------------------------------------------------------------------------------------------------------------------------------------
+begin wind ;
+ density 1.225 ;
+ wsp 9 ;
+ tint 0.219555555556 ;
+ horizontal_input 1 ;
+ windfield_rotations 0 8.0 0.0 ; yaw, tilt (positive=upflow=wind coming from below), rotation
+ center_pos0 0.0 0.0 -127 ; hub heigth
+ shear_format 3 0 ;
+ turb_format 0 ; 0=none, 1=mann,2=flex
+ tower_shadow_method 3 ; 0=none, 1=potential flow, 2=jet
+ scale_time_start 20 ;
+ wind_ramp_factor 0.0 20 0.888888888889 1.0 ;
+ ; iec_gust ;
+;
+; wind_ramp_abs 400.0 401.0 0.0 1.0 ; wsp. after the step: 5.0
+; wind_ramp_abs 501.0 502.0 0.0 1.0 ; wsp. after the step: 6.0
+; wind_ramp_abs 602.0 603.0 0.0 1.0 ; wsp. after the step: 7.0
+; wind_ramp_abs 703.0 704.0 0.0 1.0 ; wsp. after the step: 8.0
+; wind_ramp_abs 804.0 805.0 0.0 1.0 ; wsp. after the step: 9.0
+; wind_ramp_abs 905.0 906.0 0.0 1.0 ; wsp. after the step: 10.0
+; wind_ramp_abs 1006.0 1007.0 0.0 1.0 ; wsp. after the step: 11.0
+; wind_ramp_abs 1107.0 1108.0 0.0 1.0 ; wsp. after the step: 12.0
+; wind_ramp_abs 1208.0 1209.0 0.0 1.0 ; wsp. after the step: 13.0
+; wind_ramp_abs 1309.0 1310.0 0.0 1.0 ; wsp. after the step: 14.0
+; wind_ramp_abs 1410.0 1411.0 0.0 1.0 ; wsp. after the step: 15.0
+; wind_ramp_abs 1511.0 1512.0 0.0 1.0 ; wsp. after the step: 16.0
+; wind_ramp_abs 1612.0 1613.0 0.0 1.0 ; wsp. after the step: 17.0
+; wind_ramp_abs 1713.0 1714.0 0.0 1.0 ; wsp. after the step: 18.0
+; wind_ramp_abs 1814.0 1815.0 0.0 1.0 ; wsp. after the step: 19.0
+; wind_ramp_abs 1915.0 1916.0 0.0 1.0 ; wsp. after the step: 20.0
+; wind_ramp_abs 2016.0 2017.0 0.0 1.0 ; wsp. after the step: 21.0
+; wind_ramp_abs 2117.0 2118.0 0.0 1.0 ; wsp. after the step: 22.0
+; wind_ramp_abs 2218.0 2219.0 0.0 1.0 ; wsp. after the step: 23.0
+; wind_ramp_abs 2319.0 2320.0 0.0 1.0 ; wsp. after the step: 24.0
+; wind_ramp_abs 2420.0 2421.0 0.0 1.0 ; wsp. after the step: 25.0
+ ;
+; wind_ramp_abs 400.0 2200.0 0.0 21.0 ; wsp. after the step: 25.0
+; wind_ramp_abs 2400.0 4200.0 0.0 -21.0 ; wsp. after the step: 25.0
+ ;
+ begin mann ;
+ create_turb_parameters 29.4 1.0 3.9 0 1.0 ; L, alfaeps, gamma, seed, highfrq compensation
+ filename_u ./turb/noneu.bin ;
+ filename_v ./turb/nonev.bin ;
+ filename_w ./turb/nonew.bin ;
+ box_dim_u 8192 0.0439453125 ;
+ box_dim_v 32 7.5;
+ box_dim_w 32 7.5;
+ std_scaling 1.0 0.7 0.5 ;
+ end mann ;
+;
+ begin tower_shadow_potential_2;
+ tower_mbdy_link tower;
+ nsec 2;
+ radius 0.0 4.15 ;
+ radius 123.6 2.75 ; (radius)
+ end tower_shadow_potential_2;
+end wind;
+;
+begin aerodrag ;
+ begin aerodrag_element ;
+ mbdy_name tower;
+ aerodrag_sections uniform 10 ;
+ nsec 2 ;
+ sec 0.0 0.6 8.3 ; tower bottom
+ sec 123.6 0.6 5.5 ; tower top (diameter)
+ end aerodrag_element;
+;
+ begin aerodrag_element ; Nacelle drag side
+ mbdy_name shaft;
+ aerodrag_sections uniform 2 ;
+ nsec 2 ;
+ sec 0.0 0.8 10.0 ;
+ sec 7.01 0.8 10.0 ;
+ end aerodrag_element;
+end aerodrag;
+;
+begin aero ;
+ nblades 3;
+ hub_vec shaft -3 ; rotor rotation vector (normally shaft composant directed from pressure to sustion side)
+ link 1 mbdy_c2_def blade1;
+ link 2 mbdy_c2_def blade2;
+ link 3 mbdy_c2_def blade3;
+ ae_filename ./data/AVATAR_10MW_RWT_ae.dat ;
+ pc_filename ./data/AVATAR_10MW_RWT_pc_hama_v1.dat ;
+ induction_method 1 ; 0=none, 1=normal
+ aerocalc_method 1 ; 0=ingen aerodynamic, 1=med aerodynamic
+ aero_distribution ae_file 1 ;
+ ae_sets 1 1 1;
+ tiploss_method 1 ; 0=none, 1=prandtl
+ dynstall_method 2 ; 0=none, 1=stig øye method,2=mhh method
+;
+; ; --- Flaps --- ;
+ ; begin dynstall_ateflap ;
+ ; Ais 0.165 0.335 0.0 ;
+ ; Bis 0.0455 0.30 0.30 ;
+ ; flap 59.5925 85.5023 ./data/Flap_dturwt1_Thk24.ds ; Flap Sec: 1
+ ; end dynstall_ateflap;
+end aero ;
+;-------------------------------------------------------------------------------------------------
+begin dll;
+;
+ begin type2_dll;
+ name risoe_controller ;
+ filename ./control/risoe_controller.dll ;
+ dll_subroutine_init init_regulation ;
+ dll_subroutine_update update_regulation ;
+ arraysizes_init 52 1 ;
+ arraysizes_update 12 100 ;
+ begin init ;
+ ; Overall parameters
+ constant 1 10000.0 ; Rated power [kW]
+ constant 2 0.628 ; Minimum rotor speed [rad/s]
+ constant 3 1.005 ; Rated rotor speed [rad/s]
+ constant 4 15.6E+06 ; Maximum allowable generator torque [Nm]
+ 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 'wpdata.n', where n=int(theta_min)
+ 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 9 0.7 ; Damping ratio of speed filter [-]
+ constant 10 1.64 ; Frequency of free-free DT torsion mode [Hz], if zero no notch filter used
+ ; Partial load control parameters
+ constant 11 0.9648030e+07 ; 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 1.047610E+08 ; Proportional gain of torque controller [Nm/(rad/s)]
+ constant 13 0.153367E+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, 2=constant torque]
+ constant 16 0.762489 ; Proportional gain of pitch controller [rad/(rad/s)]
+ constant 17 0.224086 ; Integral gain of pitch controller [rad/rad]
+ constant 18 0.0 ; Differential gain of pitch controller [rad/(rad/s^2)]
+ constant 19 0.4e-9 ; Proportional power error gain [rad/W]
+ constant 20 0.4e-9 ; Integral power error gain [rad/(Ws)]
+ constant 21 10.6824 ; Coefficient of linear term in aerodynamic gain scheduling, KK1 [deg]
+ constant 22 601.25499 ; 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
+ constant 24 -1 ; Cut-in time [s]
+ constant 25 1.0 ; Time delay for soft start of torque [1/1P]
+; Cut-out simulation parameters
+ constant 26 -1 ; Cut-out time [s]
+ constant 27 5.0 ; Time constant for linear torque cut-out [s]
+ constant 28 1 ; Stop type [1=normal, 2=emergency]
+ constant 29 1.0 ; Time delay for pitch stop after shut-down signal [s]
+ constant 30 3 ; Maximum pitch velocity during initial period of stop [deg/s]
+ constant 31 3.0 ; Time period of initial pitch stop phase [s] (maintains pitch speed specified in constant 30)
+ constant 32 4 ; Maximum pitch velocity during final phase of stop [deg/s]
+; Expert parameters (keep default values unless otherwise given)
+ constant 33 2.0 ; Lower angle above lowest minimum pitch angle for switch [deg]
+ constant 34 2.0 ; Upper angle above lowest minimum pitch angle for switch [deg], if equal then hard switch
+ constant 35 95.0 ; Ratio between filtered speed and reference speed for fully open torque limits [%]
+ constant 36 2.0 ; Time constant of 1st order filter on wind speed used for minimum pitch [1/1P]
+ constant 37 1.0 ; Time constant of 1st order filter on pitch angle used for gain scheduling [1/1P]
+; Drivetrain damper
+ constant 38 0.0 ; Proportional gain of active DT damper [Nm/(rad/s)], requires frequency in input 10
+; Over speed
+ constant 39 25.0 ; Overspeed percentage before initiating turbine controller alarm (shut-down) [%]
+; Additional non-linear pitch control term (not used when all zero)
+ constant 40 0.0 ; Err0 [rad/s]
+ constant 41 0.0 ; ErrDot0 [rad/s^2]
+ constant 42 0.0 ; PitNonLin1 [rad/s]
+; Storm control command
+ constant 43 28.0 ; Wind speed 'Vstorm' above which derating of rotor speed is used [m/s]
+ constant 44 28.0 ; Cut-out wind speed (only used for derating of rotor speed in storm) [m/s]
+; Safety system parameters
+ constant 45 25.0 ; Overspeed percentage before initiating safety system alarm (shut-down) [%]
+ constant 46 1.5 ; Max low-pass filtered tower top acceleration level [m/s^2] - max in DLC 1.3=1.1 m/s^2
+; Turbine parameter
+ constant 47 205.8 ; Nominal rotor diameter [m]
+; Parameters for rotor inertia reduction in variable speed region
+ constant 48 0.0 ; Proportional gain on rotor acceleration in variable speed region [Nm/(rad/s^2)] (not used when zero)
+; Parameters for alternative partial load controller with PI regulated TSR tracking
+ constant 49 0.0 ; Optimal tip speed ratio [-] (only used when K=constant 11 = 0 otherwise Qg=K*Omega^2 is used)
+; Parameters for adding aerodynamic drivetrain damping on gain scheduling
+ constant 50 0.0 ; Proportional gain of aerodynamic DT damping [Nm/(rad/s)]
+ constant 51 0.0 ; Coefficient of linear term in aerodynamic DT damping scheduling, KK1 [deg]
+ constant 52 0.0 ; Coefficient of quadratic term in aerodynamic DT damping scheduling, KK2 [deg^2]
+ end init ;
+;
+ begin output ;
+ general time ; [s]
+ constraint bearing1 shaft_rot 1 only 2 ; Drivetrain speed [rad/s]
+ constraint bearing2 pitch1 1 only 1; [rad]
+ constraint bearing2 pitch2 1 only 1; [rad]
+ constraint bearing2 pitch3 1 only 1; [rad]
+ wind free_wind 1 0.0 0.0 -127 ; Global coordinates at hub height
+ dll inpvec 2 2 ; Elec. power from generator servo .dll
+ dll inpvec 2 8 ; Grid state flag from generator servo .dll
+ mbdy state acc tower 10 1.0 global only 1 ; Tower top x-acceleration [m/s^2]
+ mbdy state acc tower 10 1.0 global only 2 ; Tower top y-acceleration [m/s^2]
+ end output;
+ end type2_dll;
+;
+ begin type2_dll;
+ name generator_servo ;
+ filename ./control/generator_servo.dll ;
+ dll_subroutine_init init_generator_servo ;
+ dll_subroutine_update update_generator_servo ;
+ arraysizes_init 7 1 ;
+ arraysizes_update 4 8 ;
+ begin init ;
+ constant 1 20.0 ; Frequency of 2nd order servo model of generator-converter system [Hz]
+ constant 2 0.9 ; Damping ratio 2nd order servo model of generator-converter system [-]
+ constant 3 15.6E+06 ; Maximum allowable LSS torque (pull-out torque) [Nm]
+ constant 4 0.94 ; Generator efficiency [-]
+ constant 5 1.0 ; Gearratio [-]
+ constant 6 0.0 ; Time for half value in softstart of torque [s]
+ constant 7 5000 ; Time for grid loss [s]
+ end init ;
+;
+ begin output;
+ general time ; Time [s]
+ dll inpvec 1 1 ; Electrical torque reference [Nm]
+ constraint bearing1 shaft_rot 1 only 2; Generator LSS speed [rad/s]
+ mbdy momentvec shaft 1 1 shaft only 3 ; Shaft moment [kNm] (Qshaft)
+ end output;
+;
+ begin actions;
+ mbdy moment_int shaft 1 -3 shaft towertop 2 ; Generator LSS torque [Nm]
+ end actions;
+ end type2_dll;
+;
+ begin type2_dll;
+ name mech_brake ;
+ filename ./control/mech_brake.dll ;
+ dll_subroutine_init init_mech_brake ;
+ dll_subroutine_update update_mech_brake ;
+ arraysizes_init 7 1 ;
+ arraysizes_update 4 6 ;
+ begin init ;
+ constant 1 5225.35 ; Fully deployed maximum brake torque [Nm] (0.6*max torque)
+ constant 2 100.0 ; Parameter alpha used in Q = tanh(omega*alpha), typically 1e2/Omega_nom
+ constant 3 0.5 ; Delay time for before brake starts to deploy [s]
+ constant 4 0.74 ; Time for brake to become fully deployed [s]
+ end init ;
+;
+ begin output;
+ general time ; Time [s]
+ constraint bearing1 shaft_rot 1 only 2 ; Generator LSS speed [rad/s]
+ dll inpvec 1 25 ; Command to deploy mechanical disc brake [0,1]
+ end output;
+;
+ begin actions;
+ mbdy moment_int shaft 1 -3 shaft towertop 2 ; Generator LSS torque [Nm]
+ end actions;
+ end type2_dll;
+;
+ begin type2_dll;
+ name servo_with_limits ;
+ filename ./control/servo_with_limits.dll ;
+ dll_subroutine_init init_servo_with_limits ;
+ dll_subroutine_update update_servo_with_limits ;
+ arraysizes_init 10 1 ;
+ arraysizes_update 5 9 ;
+ begin init ;
+ constant 1 3 ; Number of blades [-]
+ constant 2 1.0 ; Frequency of 2nd order servo model of pitch system [Hz]
+ constant 3 0.7 ; Damping ratio 2nd order servo model of pitch system [-]
+ constant 4 10.0 ; Max. pitch speed [deg/s]
+ constant 5 15.0 ; Max. pitch acceleration [deg/s^2]
+ constant 6 -5.0 ; Min. pitch angle [deg]
+ constant 7 90.0 ; Max. pitch angle [deg]
+ constant 8 5000 ; Time for pitch runaway [s]
+ constant 9 -1 ; Time for stuck blade 1 [s]
+ constant 10 0 ; Angle of stuck blade 1 [deg]
+ end init ;
+ begin output;
+ general time ; Time [s]
+ dll inpvec 1 2 ; Pitch1 demand angle [rad]
+ dll inpvec 1 3 ; Pitch2 demand angle [rad]
+ dll inpvec 1 4 ; Pitch3 demand angle [rad]
+ dll inpvec 1 26 ; Flag for emergency pitch stop [0=off/1=on]
+ end output;
+;
+ begin actions;
+ constraint bearing2 angle pitch1 ; Angle pitch1 bearing [rad]
+ constraint bearing2 angle pitch2 ; Angle pitch2 bearing [rad]
+ constraint bearing2 angle pitch3 ; Angle pitch3 bearing [rad]
+ end actions;
+ end type2_dll;
+;
+; --- DLL for tower-blade tip distance -- ;
+ begin type2_dll;
+ name disttowtip ;
+ filename ./control/towclearsens.dll ;
+ dll_subroutine_init initialize ;
+ dll_subroutine_update update ;
+ arraysizes_init 1 1 ;
+ arraysizes_update 12 4 ;
+ begin init ;
+ constant 1 3.87 ; Tower radius close to downward blade tip [m]
+ end init ;
+ begin output;
+ mbdy state pos tower 5 0.00 global ; [1,2,3]. Tower position: 24.58 m
+ mbdy state pos blade1 26 1.0 global ; [4,5,6]
+ mbdy state pos blade2 26 1.0 global ; [7,8,9]
+ mbdy state pos blade3 26 1.0 global ; [10,11,12]
+ end output;
+ end type2_dll;
+end dll;
+;
+;----------------------------------------------------------------------------------------------------------------------------------------------------------------
+;
+begin output;
+ filename ./res/dlc01_demos/dlc01_steady_wsp9_noturb ;
+ time 20 40 ;
+ data_format hawc_binary;
+ buffer 1 ;
+;
+ general time;
+ constraint bearing1 shaft_rot 2; angle and angle velocity
+ constraint bearing2 pitch1 5; angle and angle velocity
+ constraint bearing2 pitch2 5; angle and angle velocity
+ constraint bearing2 pitch3 5; angle and angle velocity
+ aero omega ;
+ aero torque;
+ aero power;
+ aero thrust;
+ wind free_wind 1 0.0 0.0 -127; local wind at fixed position: coo (1=global,2=non-rotation rotor coo.), pos x, pos y, pos z
+ ; non rotating coordinates shaft tip: equivalent to stationary hub in BLADED
+ mbdy momentvec shaft 3 2 shaft_nonrotate # non rotating shaft tip ;
+ mbdy forcevec shaft 3 2 shaft_nonrotate # non rotating shaft tip ;
+ ; Moments:
+ mbdy momentvec tower 1 1 tower # tower base ;
+ mbdy momentvec tower 19 2 tower # tower yaw bearing ;
+ mbdy momentvec shaft 4 1 shaft # main bearing ;
+ mbdy momentvec blade1 3 2 blade1 # blade 1 root ;
+ mbdy momentvec blade2 3 2 blade2 # blade 2 root ;
+ mbdy momentvec blade3 3 2 blade3 # blade 3 root ;
+ ; blade 2,3 root section loads
+ mbdy momentvec blade2 3 2 local # blade 2 section root;
+ mbdy momentvec blade3 3 2 local # blade 3 section root;
+ ; blade 1 sectional loads in local coordinates
+ mbdy momentvec blade1 2 2 local # blade 1 section;
+ mbdy momentvec blade1 3 2 local # blade 1 section root;
+ mbdy momentvec blade1 4 2 local # blade 1 section;
+ mbdy momentvec blade1 5 2 local # blade 1 section;
+ mbdy momentvec blade1 6 2 local # blade 1 section;
+ mbdy momentvec blade1 7 2 local # blade 1 section;
+ mbdy momentvec blade1 8 2 local # blade 1 section;
+ mbdy momentvec blade1 9 2 local # blade 1 section;
+ mbdy momentvec blade1 10 2 local # blade 1 section;
+ mbdy momentvec blade1 11 2 local # blade 1 section;
+ mbdy momentvec blade1 12 2 local # blade 1 section;
+ mbdy momentvec blade1 13 2 local # blade 1 section;
+ mbdy momentvec blade1 14 2 local # blade 1 section;
+ mbdy momentvec blade1 15 2 local # blade 1 section;
+ mbdy momentvec blade1 16 2 local # blade 1 section;
+ mbdy momentvec blade1 17 2 local # blade 1 section;
+ mbdy momentvec blade1 18 2 local # blade 1 section;
+ mbdy momentvec blade1 19 2 local # blade 1 section;
+ mbdy momentvec blade1 20 2 local # blade 1 section;
+ mbdy momentvec blade1 21 2 local # blade 1 section;
+ mbdy momentvec blade1 22 2 local # blade 1 section;
+ mbdy momentvec blade1 23 2 local # blade 1 section;
+ mbdy momentvec blade1 24 2 local # blade 1 section;
+ mbdy momentvec blade1 25 2 local # blade 1 section;
+ mbdy momentvec blade1 26 2 local # blade 1 section;
+ ; blade root out and in of plane forces
+ mbdy momentvec blade1 3 2 hub1 # blade 1 root ;
+ mbdy momentvec blade2 3 2 hub2 # blade 2 root ;
+ mbdy momentvec blade3 3 2 hub3 # blade 3 root ;
+; mbdy momentvec blade1 14 1 local # blade 1 50% local e coo ;
+; mbdy momentvec blade2 14 1 local # blade 2 50% local e coo ;
+; mbdy momentvec blade3 14 1 local # blade 3 50% local e coo ;
+ ; Displacements and accellerations
+ mbdy state pos tower 19 1.0 global only 1 # Tower top FA displ;
+ mbdy state pos tower 19 1.0 global only 2 # Tower top SS displ;
+ mbdy state acc tower 19 1.0 global only 1 # Tower top FA acc;
+ mbdy state acc tower 19 1.0 global only 2 # Tower top SS acc;
+;
+ mbdy state pos blade1 26 1.0 global # gl blade 1 tip pos ;
+ mbdy state pos blade2 26 1.0 global # gl blade 2 tip pos ;
+ mbdy state pos blade3 26 1.0 global # gl blade 3 tip pos ;
+ mbdy state pos blade1 26 1.0 blade1 # blade 1 tip pos ;
+ mbdy state pos blade2 26 1.0 blade2 # blade 2 tip pos ;
+ mbdy state pos blade3 26 1.0 blade3 # blade 3 tip pos ;
+;
+ mbdy state pos tower 5 0.00 global ; [1,2,3]. Tower position: 24.58 m
+;
+ ; elastic twist (torsional deformation) along the blade
+ aero tors_ang 1 45.56;
+ aero tors_ang 1 59.19;
+ aero tors_ang 1 70.87;
+ aero tors_ang 1 80.61;
+ aero tors_ang 1 84.50;
+ aero tors_ang 1 88.40;
+ aero tors_ang 1 92.29;
+ aero tors_ang 1 96.19;
+ aero tors_ang 1 98.13;
+ aero tors_ang 1 100.08; tip
+;
+; - Monitor Aerodynamics - ;
+ aero windspeed 3 1 1 72.5;
+ aero alfa 1 72.5;
+ aero alfa 2 72.5;
+ aero alfa 3 72.5;
+ aero cl 1 72.5;
+ aero cl 2 72.5;
+ aero cl 3 72.5;
+ aero cd 1 72.5;
+ aero cd 2 72.5;
+ aero cd 3 72.5;
+; - Main Controller -
+; Output to controller
+ ; dll outvec 1 1 # time;
+ ; dll outvec 1 2 # slow speed shaft rad/s;
+ ; dll outvec 1 3 # pitch angle 1;
+ ; dll outvec 1 4 # pitch angle 2;
+ ; dll outvec 1 5 # pitch angle 3;
+ ; dll outvec 1 6 # WSP_x_global;
+ ; dll outvec 1 7 # WSP_y_global;
+ ; dll outvec 1 8 # WSP_z_global;
+ ; dll outvec 1 9 # Elec. pwr ;
+ ; dll outvec 1 10 # Grid flag ;
+; Input from controller
+ dll inpvec 1 1 # Generator torque reference [Nm] ;
+ dll inpvec 1 2 # Pitch angle reference of blade 1 [rad] ;
+ dll inpvec 1 3 # Pitch angle reference of blade 2 [rad] ;
+ dll inpvec 1 4 # Pitch angle reference of blade 3 [rad] ;
+ ; dll inpvec 1 5 # Power reference [W] ;
+ ; dll inpvec 1 6 # Filtered wind speed [m/s] ;
+ ; dll inpvec 1 7 # Filtered rotor speed [rad/s];
+ ; dll inpvec 1 8 # Filtered rotor speed error for torque [rad/s];
+ ; dll inpvec 1 9 # Bandpass filtered rotor speed [rad/s];
+ ; dll inpvec 1 10 # Proportional term of torque contr. [Nm] ;
+ ; dll inpvec 1 11 # Integral term of torque controller [Nm] ;
+ ; dll inpvec 1 12 # Minimum limit of torque [Nm] ;
+ ; dll inpvec 1 13 # Maximum limit of torque [Nm] ;
+ dll inpvec 1 14 # Torque limit switch based on pitch [-] ;
+ ; dll inpvec 1 15 # Filtered rotor speed error for pitch [rad/s];
+ ; dll inpvec 1 16 # Power error for pitch [W] ;
+ ; dll inpvec 1 17 # Proportional term of pitch controller [rad] ;
+ ; dll inpvec 1 18 # Integral term of pitch controller [rad] ;
+ ; dll inpvec 1 19 # Minimum limit of pitch [rad] ;
+ ; dll inpvec 1 20 # Maximum limit of pitch [rad] ;
+ dll inpvec 1 21 # Torque reference from DT dammper [Nm] ;
+ dll inpvec 1 22 # Status signal [-] ;
+ ; dll inpvec 1 23 # Total added pitch rate [rad/s] ;
+ dll inpvec 1 24 # Filtered Mean pitch for gain sch [rad] ;
+ dll inpvec 1 25 # Flag for mechnical brake [0=off/1=on] ;
+ dll inpvec 1 26 # Flag for emergency pitch stop [0=off/1=on] ;
+ dll inpvec 1 27 # LP filtered acceleration level [m/s^2] ;
+; ; Output to generator model
+ ; dll outvec 2 1 # time ;
+ ; dll outvec 2 2 # Electrical torque reference [Nm] ;
+ ; dll outvec 2 3 # omega LSS ;
+; Input from generator model
+ dll inpvec 2 1 # Mgen LSS [Nm];
+ dll inpvec 2 2 # Pelec W ;
+ dll inpvec 2 3 # Mframe ;
+ dll inpvec 2 4 # Mgen HSS ;
+ dll inpvec 2 5 # Generator Pmech kW ;
+ dll inpvec 2 6 # Filtered Gen speed ;
+ dll inpvec 2 7 # Resulting Eff ;
+ dll inpvec 2 8 # Grid flag ;
+; Output to mechanical brake
+ dll inpvec 3 1 # Brake torque [Nm] ;
+; ; Input from mechanical brake
+ ; dll outvec 3 1 # Time [s] ;
+ ; dll outvec 3 2 # Generator LSS speed [rad/s] ;
+ ; dll outvec 3 3 # Deploy brake ;
+; ; Output to pitch servo
+ ; dll outvec 4 1 # time;
+ ; dll outvec 4 2 # pitchref 1;
+ ; dll outvec 4 3 # pitchref 2;
+ ; dll outvec 4 4 # pitchref 3;
+ ; dll outvec 4 5 # Emerg. stop;
+; Input from pitch servo
+ dll inpvec 4 1 # pitch 1;
+ dll inpvec 4 2 # pitch 2;
+ dll inpvec 4 3 # pitch 3;
+; Check tower clearence
+ dll inpvec 5 1 # Bltip tow min d [m];
+; general constant 1.0 ; constant 1.0 - to mesure activity of flap in terms of displacement
+; - Check on flap control:
+ ; ; - From flap controller: -
+ ; dll type2_dll cyclic_flap_controller inpvec 1 # Ref flap signal bl 1 [deg] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 2 # Ref flap signal bl 2 [deg] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 3 # Ref flap signal bl 3 [deg] ;
+ ; ; - Mbc values
+ ; dll type2_dll cyclic_flap_controller inpvec 4 # momvec mbc cos [kNm] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 5 # momvec mbc sin [kNm] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 6 # momvec mbc filt cos [kNm] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 7 # momvec mbc filt sin [kNm] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 8 # flap mbc cos [deg] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 9 # flap mbc sin [deg] ;
+ ; ; - Check Gains - ;
+ ; dll type2_dll cyclic_flap_controller inpvec 10 # lead angle [deg] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 11 # scaling on rat pow [-] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 12 # actual kp [deg/kNm] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 13 # actual ki [deg/kNms] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 14 # actual kd [deg s/kNm] ;
+ ; ; - Actual deflections -
+ ; aero beta 1 1 ;
+ ; aero beta 2 1 ;
+ ; aero beta 3 1 ;
+ ; ; - Mbc values
+ ; dll type2_dll cyclic_flap_controller inpvec 4 # momvec mbc cos [kNm] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 5 # momvec mbc sin [kNm] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 6 # momvec mbc filt cos [kNm] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 7 # momvec mbc filt sin [kNm] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 8 # flap mbc cos [deg] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 9 # flap mbc sin [deg] ;
+end output;
+;
+exit;
diff --git a/wetb/prepost/tests/data/demo_dlc/ref/pbs_in/dlc01_demos/dlc01_steady_wsp10_noturb.p b/wetb/prepost/tests/data/demo_dlc/ref/pbs_in/dlc01_demos/dlc01_steady_wsp10_noturb.p
new file mode 100644
index 00000000..1bc115f7
--- /dev/null
+++ b/wetb/prepost/tests/data/demo_dlc/ref/pbs_in/dlc01_demos/dlc01_steady_wsp10_noturb.p
@@ -0,0 +1,55 @@
+### Standard Output
+#PBS -N dlc01_steady_wsp10_noturb
+#PBS -o ./pbs_out/dlc01_demos/dlc01_steady_wsp10_noturb.out
+### Standard Error
+#PBS -e ./pbs_out/dlc01_demos/dlc01_steady_wsp10_noturb.err
+#PBS -W umask=003
+### Maximum wallclock time format HOURS:MINUTES:SECONDS
+#PBS -l walltime=04:00:00
+#PBS -l nodes=1:ppn=1
+### Queue name
+#PBS -q workq
+### Create scratch directory and copy data to it
+cd $PBS_O_WORKDIR
+echo "current working dir (pwd):"
+pwd
+cp -R ./demo_dlc_remote.zip /scratch/$USER/$PBS_JOBID
+
+
+echo ""
+echo "Execute commands on scratch nodes"
+cd /scratch/$USER/$PBS_JOBID
+pwd
+/usr/bin/unzip demo_dlc_remote.zip
+mkdir -p htc/dlc01_demos/
+mkdir -p res/dlc01_demos/
+mkdir -p logfiles/dlc01_demos/
+mkdir -p turb/
+cp -R $PBS_O_WORKDIR/htc/dlc01_demos/dlc01_steady_wsp10_noturb.htc ./htc/dlc01_demos/
+cp -R $PBS_O_WORKDIR/../turb/none*.bin turb/
+time WINEARCH=win32 WINEPREFIX=~/.wine32 wine hawc2-latest ./htc/dlc01_demos/dlc01_steady_wsp10_noturb.htc &
+### wait for jobs to finish
+wait
+echo ""
+echo "Copy back from scratch directory"
+cd /scratch/$USER/$PBS_JOBID
+mkdir -p $PBS_O_WORKDIR/res/dlc01_demos/
+mkdir -p $PBS_O_WORKDIR/logfiles/dlc01_demos/
+mkdir -p $PBS_O_WORKDIR/animation/
+mkdir -p $PBS_O_WORKDIR/../turb/
+cp -R res/dlc01_demos/. $PBS_O_WORKDIR/res/dlc01_demos/.
+cp -R logfiles/dlc01_demos/. $PBS_O_WORKDIR/logfiles/dlc01_demos/.
+cp -R animation/. $PBS_O_WORKDIR/animation/.
+
+echo ""
+echo "COPY BACK TURB IF APPLICABLE"
+cd turb/
+for i in `ls *.bin`; do if [ -e $PBS_O_WORKDIR/../turb/$i ]; then echo "$i exists no copyback"; else echo "$i copyback"; cp $i $PBS_O_WORKDIR/../turb/; fi; done
+cd /scratch/$USER/$PBS_JOBID
+echo "END COPY BACK TURB"
+echo ""
+
+echo ""
+echo "following files are on the node (find .):"
+find .
+exit
diff --git a/wetb/prepost/tests/data/demo_dlc/ref/pbs_in/dlc01_demos/dlc01_steady_wsp8_noturb.p b/wetb/prepost/tests/data/demo_dlc/ref/pbs_in/dlc01_demos/dlc01_steady_wsp8_noturb.p
new file mode 100644
index 00000000..640e5c20
--- /dev/null
+++ b/wetb/prepost/tests/data/demo_dlc/ref/pbs_in/dlc01_demos/dlc01_steady_wsp8_noturb.p
@@ -0,0 +1,55 @@
+### Standard Output
+#PBS -N dlc01_steady_wsp8_noturb
+#PBS -o ./pbs_out/dlc01_demos/dlc01_steady_wsp8_noturb.out
+### Standard Error
+#PBS -e ./pbs_out/dlc01_demos/dlc01_steady_wsp8_noturb.err
+#PBS -W umask=003
+### Maximum wallclock time format HOURS:MINUTES:SECONDS
+#PBS -l walltime=04:00:00
+#PBS -l nodes=1:ppn=1
+### Queue name
+#PBS -q workq
+### Create scratch directory and copy data to it
+cd $PBS_O_WORKDIR
+echo "current working dir (pwd):"
+pwd
+cp -R ./demo_dlc_remote.zip /scratch/$USER/$PBS_JOBID
+
+
+echo ""
+echo "Execute commands on scratch nodes"
+cd /scratch/$USER/$PBS_JOBID
+pwd
+/usr/bin/unzip demo_dlc_remote.zip
+mkdir -p htc/dlc01_demos/
+mkdir -p res/dlc01_demos/
+mkdir -p logfiles/dlc01_demos/
+mkdir -p turb/
+cp -R $PBS_O_WORKDIR/htc/dlc01_demos/dlc01_steady_wsp8_noturb.htc ./htc/dlc01_demos/
+cp -R $PBS_O_WORKDIR/../turb/none*.bin turb/
+time WINEARCH=win32 WINEPREFIX=~/.wine32 wine hawc2-latest ./htc/dlc01_demos/dlc01_steady_wsp8_noturb.htc &
+### wait for jobs to finish
+wait
+echo ""
+echo "Copy back from scratch directory"
+cd /scratch/$USER/$PBS_JOBID
+mkdir -p $PBS_O_WORKDIR/res/dlc01_demos/
+mkdir -p $PBS_O_WORKDIR/logfiles/dlc01_demos/
+mkdir -p $PBS_O_WORKDIR/animation/
+mkdir -p $PBS_O_WORKDIR/../turb/
+cp -R res/dlc01_demos/. $PBS_O_WORKDIR/res/dlc01_demos/.
+cp -R logfiles/dlc01_demos/. $PBS_O_WORKDIR/logfiles/dlc01_demos/.
+cp -R animation/. $PBS_O_WORKDIR/animation/.
+
+echo ""
+echo "COPY BACK TURB IF APPLICABLE"
+cd turb/
+for i in `ls *.bin`; do if [ -e $PBS_O_WORKDIR/../turb/$i ]; then echo "$i exists no copyback"; else echo "$i copyback"; cp $i $PBS_O_WORKDIR/../turb/; fi; done
+cd /scratch/$USER/$PBS_JOBID
+echo "END COPY BACK TURB"
+echo ""
+
+echo ""
+echo "following files are on the node (find .):"
+find .
+exit
diff --git a/wetb/prepost/tests/data/demo_dlc/ref/pbs_in/dlc01_demos/dlc01_steady_wsp9_noturb.p b/wetb/prepost/tests/data/demo_dlc/ref/pbs_in/dlc01_demos/dlc01_steady_wsp9_noturb.p
new file mode 100644
index 00000000..a9d5ef52
--- /dev/null
+++ b/wetb/prepost/tests/data/demo_dlc/ref/pbs_in/dlc01_demos/dlc01_steady_wsp9_noturb.p
@@ -0,0 +1,55 @@
+### Standard Output
+#PBS -N dlc01_steady_wsp9_noturb
+#PBS -o ./pbs_out/dlc01_demos/dlc01_steady_wsp9_noturb.out
+### Standard Error
+#PBS -e ./pbs_out/dlc01_demos/dlc01_steady_wsp9_noturb.err
+#PBS -W umask=003
+### Maximum wallclock time format HOURS:MINUTES:SECONDS
+#PBS -l walltime=04:00:00
+#PBS -l nodes=1:ppn=1
+### Queue name
+#PBS -q workq
+### Create scratch directory and copy data to it
+cd $PBS_O_WORKDIR
+echo "current working dir (pwd):"
+pwd
+cp -R ./demo_dlc_remote.zip /scratch/$USER/$PBS_JOBID
+
+
+echo ""
+echo "Execute commands on scratch nodes"
+cd /scratch/$USER/$PBS_JOBID
+pwd
+/usr/bin/unzip demo_dlc_remote.zip
+mkdir -p htc/dlc01_demos/
+mkdir -p res/dlc01_demos/
+mkdir -p logfiles/dlc01_demos/
+mkdir -p turb/
+cp -R $PBS_O_WORKDIR/htc/dlc01_demos/dlc01_steady_wsp9_noturb.htc ./htc/dlc01_demos/
+cp -R $PBS_O_WORKDIR/../turb/none*.bin turb/
+time WINEARCH=win32 WINEPREFIX=~/.wine32 wine hawc2-latest ./htc/dlc01_demos/dlc01_steady_wsp9_noturb.htc &
+### wait for jobs to finish
+wait
+echo ""
+echo "Copy back from scratch directory"
+cd /scratch/$USER/$PBS_JOBID
+mkdir -p $PBS_O_WORKDIR/res/dlc01_demos/
+mkdir -p $PBS_O_WORKDIR/logfiles/dlc01_demos/
+mkdir -p $PBS_O_WORKDIR/animation/
+mkdir -p $PBS_O_WORKDIR/../turb/
+cp -R res/dlc01_demos/. $PBS_O_WORKDIR/res/dlc01_demos/.
+cp -R logfiles/dlc01_demos/. $PBS_O_WORKDIR/logfiles/dlc01_demos/.
+cp -R animation/. $PBS_O_WORKDIR/animation/.
+
+echo ""
+echo "COPY BACK TURB IF APPLICABLE"
+cd turb/
+for i in `ls *.bin`; do if [ -e $PBS_O_WORKDIR/../turb/$i ]; then echo "$i exists no copyback"; else echo "$i copyback"; cp $i $PBS_O_WORKDIR/../turb/; fi; done
+cd /scratch/$USER/$PBS_JOBID
+echo "END COPY BACK TURB"
+echo ""
+
+echo ""
+echo "following files are on the node (find .):"
+find .
+exit
diff --git a/wetb/prepost/tests/data/demo_dlc/ref/prepost/A0001.pkl b/wetb/prepost/tests/data/demo_dlc/ref/prepost/A0001.pkl
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diff --git a/wetb/prepost/tests/data/demo_dlc/ref/prepost/A0001_tags.txt b/wetb/prepost/tests/data/demo_dlc/ref/prepost/A0001_tags.txt
new file mode 100755
index 00000000..6de32e2b
--- /dev/null
+++ b/wetb/prepost/tests/data/demo_dlc/ref/prepost/A0001_tags.txt
@@ -0,0 +1,178 @@
+
+
+===============================================================================
+ iter_dict
+===============================================================================
+ [empty] : [False]
+
+===============================================================================
+ opt_tags
+===============================================================================
+
+-------------------------------------------------------------------------------
+ opt_tags set
+-------------------------------------------------------------------------------
+ [Case folder] : dlc01_demos
+ [Case id.] : dlc01_steady_wsp8_noturb
+ [Cut-in time] : -1
+ [Cut-out time] : -1
+ [DLC] : 01
+ [Dyn stall] : 2
+ [Free shaft rot] : True
+ [G_A] : True
+ [G_T] : True
+ [G_phi0] : True
+ [G_t0] : True
+ [Grid loss time] : 5000
+ [Induction] : 1
+ [Pitch 1 DLC22b] : 0
+ [Pitvel 1] : 3
+ [Pitvel 2] : 4
+ [Rotor azimuth] : 0
+ [Rotor locked] : False
+ [Stop type] : 1
+ [TI] : 0.232
+ [Time pitch runaway] : 5000
+ [Time stuck DLC22b] : -1
+ [Turb base name] : none
+ [Windspeed] : 8
+ [case_id] : dlc01_steady_wsp8_noturb
+ [data_dir] : data/
+ [dis_setbeta] : True
+ [duration] : 20.0
+ [gust] : False
+ [gust_type] : True
+ [htc_dir] : htc/dlc01_demos/
+ [init_wr] : 0.5
+ [iter_dir] : iter/dlc01_demos/
+ [log_dir] : logfiles/dlc01_demos/
+ [out_format] : hawc_binary
+ [pbs_in_dir] : pbs_in/dlc01_demos/
+ [pbs_out_dir] : pbs_out/dlc01_demos/
+ [res_dir] : res/dlc01_demos/
+ [shear_exp] : 0
+ [staircase] : False
+ [t flap on] : -1
+ [t0] : 20
+ [time stop] : 40
+ [time_stop] : 40
+ [tu_model] : 0
+ [tu_seed] : 0
+ [turb_base_name] : none
+ [turb_dx] : 0.0390625
+ [wdir] : 0
+ [windramp] : False
+ [wsp factor] : 1.0
+ [zip_root_files] : ['pbs_in_file_cache.txt', 'A0001_ErrorLog.csv']
+
+-------------------------------------------------------------------------------
+ opt_tags set
+-------------------------------------------------------------------------------
+ [Case folder] : dlc01_demos
+ [Case id.] : dlc01_steady_wsp9_noturb
+ [Cut-in time] : -1
+ [Cut-out time] : -1
+ [DLC] : 01
+ [Dyn stall] : 2
+ [Free shaft rot] : True
+ [G_A] : True
+ [G_T] : True
+ [G_phi0] : True
+ [G_t0] : True
+ [Grid loss time] : 5000
+ [Induction] : 1
+ [Pitch 1 DLC22b] : 0
+ [Pitvel 1] : 3
+ [Pitvel 2] : 4
+ [Rotor azimuth] : 0
+ [Rotor locked] : False
+ [Stop type] : 1
+ [TI] : 0.219555555556
+ [Time pitch runaway] : 5000
+ [Time stuck DLC22b] : -1
+ [Turb base name] : none
+ [Windspeed] : 9
+ [case_id] : dlc01_steady_wsp9_noturb
+ [data_dir] : data/
+ [dis_setbeta] : True
+ [duration] : 20.0
+ [gust] : False
+ [gust_type] : True
+ [htc_dir] : htc/dlc01_demos/
+ [init_wr] : 0.5
+ [iter_dir] : iter/dlc01_demos/
+ [log_dir] : logfiles/dlc01_demos/
+ [out_format] : hawc_binary
+ [pbs_in_dir] : pbs_in/dlc01_demos/
+ [pbs_out_dir] : pbs_out/dlc01_demos/
+ [res_dir] : res/dlc01_demos/
+ [shear_exp] : 0
+ [staircase] : False
+ [t flap on] : -1
+ [t0] : 20
+ [time stop] : 40
+ [time_stop] : 40
+ [tu_model] : 0
+ [tu_seed] : 0
+ [turb_base_name] : none
+ [turb_dx] : 0.0439453125
+ [wdir] : 0
+ [windramp] : False
+ [wsp factor] : 0.888888888889
+ [zip_root_files] : ['pbs_in_file_cache.txt', 'A0001_ErrorLog.csv']
+
+-------------------------------------------------------------------------------
+ opt_tags set
+-------------------------------------------------------------------------------
+ [Case folder] : dlc01_demos
+ [Case id.] : dlc01_steady_wsp10_noturb
+ [Cut-in time] : -1
+ [Cut-out time] : -1
+ [DLC] : 01
+ [Dyn stall] : 2
+ [Free shaft rot] : True
+ [G_A] : True
+ [G_T] : True
+ [G_phi0] : True
+ [G_t0] : True
+ [Grid loss time] : 5000
+ [Induction] : 1
+ [Pitch 1 DLC22b] : 0
+ [Pitvel 1] : 3
+ [Pitvel 2] : 4
+ [Rotor azimuth] : 0
+ [Rotor locked] : False
+ [Stop type] : 1
+ [TI] : 0.2096
+ [Time pitch runaway] : 5000
+ [Time stuck DLC22b] : -1
+ [Turb base name] : none
+ [Windspeed] : 10
+ [case_id] : dlc01_steady_wsp10_noturb
+ [data_dir] : data/
+ [dis_setbeta] : True
+ [duration] : 20.0
+ [gust] : False
+ [gust_type] : True
+ [htc_dir] : htc/dlc01_demos/
+ [init_wr] : 0.5
+ [iter_dir] : iter/dlc01_demos/
+ [log_dir] : logfiles/dlc01_demos/
+ [out_format] : hawc_binary
+ [pbs_in_dir] : pbs_in/dlc01_demos/
+ [pbs_out_dir] : pbs_out/dlc01_demos/
+ [res_dir] : res/dlc01_demos/
+ [shear_exp] : 0
+ [staircase] : False
+ [t flap on] : -1
+ [t0] : 20
+ [time stop] : 40
+ [time_stop] : 40
+ [tu_model] : 0
+ [tu_seed] : 0
+ [turb_base_name] : none
+ [turb_dx] : 0.048828125
+ [wdir] : 0
+ [windramp] : False
+ [wsp factor] : 0.8
+ [zip_root_files] : ['pbs_in_file_cache.txt', 'A0001_ErrorLog.csv']
diff --git a/wetb/prepost/tests/data/demo_dlc/source/data/minimal_demo_file.txt b/wetb/prepost/tests/data/demo_dlc/source/data/minimal_demo_file.txt
new file mode 100644
index 00000000..8db26215
--- /dev/null
+++ b/wetb/prepost/tests/data/demo_dlc/source/data/minimal_demo_file.txt
@@ -0,0 +1 @@
+just one demo line
diff --git a/wetb/prepost/tests/data/demo_dlc/source/demo_dlc_remote.zip b/wetb/prepost/tests/data/demo_dlc/source/demo_dlc_remote.zip
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diff --git a/wetb/prepost/tests/data/demo_dlc/source/htc/_master/demo_dlc_master_A0001.htc b/wetb/prepost/tests/data/demo_dlc/source/htc/_master/demo_dlc_master_A0001.htc
new file mode 100755
index 00000000..6e956f80
--- /dev/null
+++ b/wetb/prepost/tests/data/demo_dlc/source/htc/_master/demo_dlc_master_A0001.htc
@@ -0,0 +1,850 @@
+;this version was at some point based on: Avatar_10MW_RWT version 1, 06-08-14, Anyd
+begin simulation;
+ time_stop [time stop];
+ solvertype 1 ; (newmark)
+ on_no_convergence continue ;
+; convergence_limits 1E3 1.0 1E-7 ;
+ logfile ./logfiles/[Case folder]/[Case id.].log ;
+ begin newmark;
+ deltat 0.02;
+ end newmark;
+end simulation;
+;
+;----------------------------------------------------------------------------------------------------------------------------------------------------------------
+begin new_htc_structure;
+;--------------------------------------------------------------------------------------------------
+[staircase] beam_output_file_name ./res_eigen/[Case folder]/[Case id.]/[Case id.]_beam.dat;
+[staircase] body_output_file_name ./res_eigen/[Case folder]/[Case id.]/[Case id.]_body.dat;
+[staircase] struct_inertia_output_file_name ./res_eigen/[Case folder]/[Case id.]/[Case id.]_struct.dat;
+[staircase] body_eigenanalysis_file_name ./res_eigen/[Case folder]/[Case id.]/[Case id.]_body_eigen.dat;
+[staircase] structure_eigenanalysis_file_name ./res_eigen/[Case folder]/[Case id.]/[Case id.]_strc_eigen.dat;
+;---------------------------------------------------------------------------------------------------
+ begin main_body; tower 123.6m
+ name tower ;
+ type timoschenko ;
+ nbodies 3 ;
+ node_distribution c2_def ;
+ damping_posdef 0 0 0 4.7E-03 4.7E-03 4.3E-04 ; tuned by Anyd 12/8/14
+ begin timoschenko_input;
+ filename ./data/AVATAR_10MW_RWT_tower_st.dat;
+ set 1 1 ;
+ end timoschenko_input;
+ begin c2_def; Definition of centerline (main_body coordinates)
+ nsec 20;
+ sec 1 0 0 0.000 0 ; x,y,z,twist
+ sec 2 0 0 -12.293 0 ;
+ sec 3 0 0 -12.294 0 ;
+ sec 4 0 0 -24.585 0 ;
+ sec 5 0 0 -24.586 0 ;
+ sec 6 0 0 -36.878 0 ;
+ sec 7 0 0 -36.879 0 ;
+ sec 8 0 0 -49.171 0 ;
+ sec 9 0 0 -49.172 0 ;
+ sec 10 0 0 -61.463 0 ;
+ sec 11 0 0 -61.464 0 ;
+ sec 12 0 0 -73.756 0 ;
+ sec 13 0 0 -73.757 0 ;
+ sec 14 0 0 -86.049 0 ;
+ sec 15 0 0 -86.050 0 ;
+ sec 16 0 0 -98.341 0 ;
+ sec 17 0 0 -98.342 0 ;
+ sec 18 0 0 -110.634 0 ;
+ sec 19 0 0 -110.635 0 ;
+ sec 20 0 0 -123.600 0 ;
+ end c2_def ;
+ end main_body;
+;
+ begin main_body;
+ name towertop ;
+ type timoschenko ;
+ nbodies 1 ;
+ node_distribution c2_def ;
+ damping_posdef 7.50E-03 7.40E-03 7.00E-03 7.00E-03 7.00E-03 7.00E-03 ; "changed by Anyd
+ concentrated_mass 2.0 0.0 2.6870E+00 3.0061E-01 4.4604E+05 4.1060E+06 4.1060E+05 4.1060E+06 ; Nacel
+ begin timoschenko_input;
+ filename ./data/DTU_10MW_RWT_Towertop_st.dat ;
+ set 1 2 ;
+ end timoschenko_input;
+ begin c2_def; Definition of centerline (main_body coordinates)
+ nsec 2;
+ sec 1 0.0 0.0 0.0 0.0 ; x,y,z,twist
+ sec 2 0.0 0.0 -2.75 0.0 ;
+ end c2_def ;
+ end main_body;
+;
+ begin main_body;
+ name shaft ;
+ type timoschenko ;
+ nbodies 1 ;
+ node_distribution c2_def ;
+; damping_posdef 8.00E-3 8.00E-03 8.00E-02 4.65E-04 4.65E-04 2.38E-02 ; "tuned by Anyd 22/2/13
+ damping_posdef 0.0 0.0 3.983E-03 4.65E-04 4.65E-04 3.983E-03 ; "tuned by Anyd 23/5/13 to 31.45 l
+ concentrated_mass 1.0 0.0 0.0 0.0 0.0 0.0 0.0 3.751E+06 ; generator equivalent slow shaft "re_tu
+ concentrated_mass 5.0 0.0 0.0 0.0 1.0552E+05 0.0 0.0 3.257E+05 ; hub mass and inertia; "re_tuned
+ begin timoschenko_input;
+ filename ./data/DTU_10MW_RWT_Shaft_st.dat ;
+ set 1 1 ;
+ end timoschenko_input;
+ begin c2_def; Definition of centerline (main_body coordinates)
+ nsec 5;
+ sec 1 0.0 0.0 0.0 0.0 ; Tower top x,y,z,twist
+ sec 2 0.0 0.0 1.5 0.0 ;
+ sec 3 0.0 0.0 3.0 0.0 ;
+ sec 4 0.0 0.0 4.4 0.0 ; Main bearing
+ sec 5 0.0 0.0 7.1 0.0 ; Rotor centre
+ end c2_def ;
+ end main_body;
+;
+ begin main_body;
+ name shaft_nonrotate ;
+ type timoschenko ;
+ nbodies 1 ;
+ node_distribution c2_def ;
+ damping_posdef 0.00E+00 0.00E+00 0.00E+00 1.0E-01 1.0E-01 1.0E-01 ;
+ begin timoschenko_input;
+ filename ./data/DTU_10MW_RWT_Shaft_st.dat ;
+ set 1 3; dummy light and stiff structure
+ end timoschenko_input;
+ begin c2_def;
+ nsec 2;
+ sec 1 0.0 0.0 0.0 0.0 ;
+ sec 2 0.0 0.0 0.1 0.0 ;
+ end c2_def;
+ end main_body;
+;
+ begin main_body;
+ name hub1 ;
+ type timoschenko ;
+ nbodies 1 ;
+ node_distribution c2_def ;
+ damping_posdef 2.00E-05 2.00E-05 2.00E-04 3.00E-06 3.00E-06 2.00E-05;
+ begin timoschenko_input;
+ filename ./data/DTU_10MW_RWT_Hub_st.dat ;
+ set 1 2 ;
+ end timoschenko_input;
+ begin c2_def; Definition of centerline (main_body coordinates)
+ nsec 2;
+ sec 1 0.0 0.0 0.0 0.0 ; x,y,z,twist
+ sec 2 0.0 0.0 2.8 0.0 ;
+ end c2_def ;
+ end main_body;
+;
+ begin main_body;
+ name hub2 ;
+ copy_main_body hub1;
+ end main_body;
+;
+ begin main_body;
+ name hub3 ;
+ copy_main_body hub1 ;
+ end main_body;
+;
+ begin main_body;
+ name blade1 ;
+ type timoschenko ;
+ nbodies 10 ;
+ node_distribution c2_def;
+; damping_posdef 0.0 0.0 0.0 2.5e-3 8.9e-4 3.2e-4 ; "Tuned by Anyd"
+; damping_posdef 0.0 0.0 0.0 1.5e-3 2.45e-3 3.2e-4 ; " 3% damping tuned by Anyd 20/02/12 unable to
+; damping_posdef 0.0 0.0 0.0 2.1e-3 1.9e-3 1.3e-4 ; " 3% damping tuned by Anyd 15/08/14 rev2
+ damping_posdef 0.0 0.0 0.0 1.68e-3 2.25e-3 1.0e-4 ; " 3% damping tuned by Anyd 16/12/14
+ begin timoschenko_input ;
+ filename ./data/AVATAR_10MW_RWT_Blade_st.dat ;
+ set 1 9 ;
+ end timoschenko_input;
+ begin c2_def;
+ nsec 27 ;
+ sec 1 -0.001 -0.001 0.000 -17.280 ;
+ sec 2 -0.005 -0.001 2.220 -17.280 ;
+ sec 3 -0.006 -0.000 4.440 -17.280 ;
+ sec 4 -0.086 0.022 6.660 -17.280 ;
+ sec 5 -0.231 0.069 11.039 -17.273 ;
+ sec 6 -0.447 0.121 15.418 -16.441 ;
+ sec 7 -0.690 0.161 19.797 -14.613 ;
+ sec 8 -0.812 0.162 24.176 -12.578 ;
+ sec 9 -0.891 0.158 28.555 -10.588 ;
+ sec 10 -0.865 0.124 32.934 -9.070 ;
+ sec 11 -0.833 0.112 37.313 -8.224 ;
+ sec 12 -0.797 0.102 41.692 -7.688 ;
+ sec 13 -0.760 0.093 46.071 -7.205 ;
+ sec 14 -0.721 0.083 50.450 -6.749 ;
+ sec 15 -0.683 0.075 54.829 -6.288 ;
+ sec 16 -0.644 0.066 59.208 -5.838 ;
+ sec 17 -0.606 0.058 63.587 -5.401 ;
+ sec 18 -0.567 0.050 67.966 -4.982 ;
+ sec 19 -0.529 0.044 72.345 -4.640 ;
+ sec 20 -0.492 0.037 76.724 -4.380 ;
+ sec 21 -0.456 0.032 81.103 -4.144 ;
+ sec 22 -0.422 0.026 85.482 -3.914 ;
+ sec 23 -0.392 0.021 89.861 -3.685 ;
+ sec 24 -0.346 0.014 94.240 -3.460 ;
+ sec 25 -0.307 0.010 96.190 -3.350 ;
+ sec 26 -0.249 0.005 98.130 -3.250 ;
+ sec 27 -0.089 0.006 100.080 -3.140 ;
+ end c2_def ;
+ end main_body;
+;
+ begin main_body;
+ name blade2 ;
+ copy_main_body blade1;
+ end main_body;
+;
+ begin main_body;
+ name blade3 ;
+ copy_main_body blade1 ;
+ end main_body;
+;-------------------------------------------------------------------------------------------------------------------------------
+;
+ begin orientation;
+ begin base;
+ body tower;
+ inipos 0.0 0.0 0.0 ; initial position of node 1
+ body_eulerang 0.0 0.0 0.0;
+ end base;
+;
+ begin relative;
+ body1 tower last;
+ body2 towertop 1;
+ body2_eulerang 0.0 0.0 0.0;
+ end relative;
+;
+ begin relative;
+ body1 towertop last;
+ body2 shaft 1;
+ body2_eulerang 90.0 0.0 0.0;
+ body2_eulerang 5.0 0.0 0.0; 5 deg tilt angle
+ body2_eulerang 0.0 0.0 [Rotor azimuth];
+[Free shaft rot] mbdy2_ini_rotvec_d1 0.0 0.0 -1.0 [init_wr] ; mbdy2_ini_rotvec_d1 0.0 0.0 -1.0 [init_wr];
+ end relative;
+;
+ begin relative; dummy non rotating hub coordinates
+ body1 towertop last;
+ body2 shaft_nonrotate 1;
+ body2_eulerang 90.0 0.0 0.0;
+ body2_eulerang 5.0 0.0 0.0; same 5 deg tilt angle as real shaft
+ end relative;
+;
+ begin relative;
+ body1 shaft last;
+ body2 hub1 1;
+ body2_eulerang -90.0 0.0 0.0;
+ body2_eulerang 0.0 180.0 0.0;
+ body2_eulerang 2.5 0.0 0.0; 2.5deg cone angle
+ end relative;
+;
+ begin relative;
+ body1 shaft last;
+ body2 hub2 1;
+ body2_eulerang -90.0 0.0 0.0;
+ body2_eulerang 0.0 60.0 0.0;
+ body2_eulerang 2.5 0.0 0.0; 2.5deg cone angle
+ end relative;
+;
+ begin relative;
+ body1 shaft last;
+ body2 hub3 1;
+ body2_eulerang -90.0 0.0 0.0;
+ body2_eulerang 0.0 -60.0 0.0;
+ body2_eulerang 2.5 0.0 0.0; 2.5deg cone angle
+ end relative;
+;
+ begin relative;
+ body1 hub1 last;
+ body2 blade1 1;
+ body2_eulerang 0.0 0.0 0;
+ end relative;
+;
+ begin relative;
+ body1 hub2 last;
+ body2 blade2 1;
+ body2_eulerang 0.0 0.0 0.0;
+ end relative;
+;
+ begin relative;
+ body1 hub3 last;
+ body2 blade3 1;
+ body2_eulerang 0.0 0.0 0.0;
+ end relative;
+;
+ end orientation;
+;-------------------------------------------------------------------------------------------------------------------------------
+begin constraint;
+;
+ begin fix0; fixed to ground in translation and rotation of node 1
+ body tower;
+ end fix0;
+;
+ begin fix1;
+ body1 tower last ;
+ body2 towertop 1;
+ end fix1;
+;
+[Free shaft rot] begin bearing1; free bearing
+[Free shaft rot] name shaft_rot;
+[Free shaft rot] body1 towertop last;
+[Free shaft rot] body2 shaft 1;
+[Free shaft rot] bearing_vector 2 0.0 0.0 -1.0; x=coo (0=global.1=body1.2=body2) vector in body2 coordinates where the free rotation is present
+[Free shaft rot] end bearing1;
+;
+[Rotor locked] begin bearing3; free bearing
+[Rotor locked] name shaft_rot;
+[Rotor locked] body1 towertop last;
+[Rotor locked] body2 shaft 1;
+[Rotor locked] bearing_vector 2 0.0 0.0 -1.0; x=coo (0=global.1=body1.2=body2) vector in body2 coordinates where the free rotation is present
+[Rotor locked] omegas 0.0 ;
+[Rotor locked] end bearing3;
+;
+ begin fix1;
+ body1 tower last ;
+ body2 shaft_nonrotate 1;
+ end fix1;
+;
+ begin fix1;
+ body1 shaft last ;
+ body2 hub1 1;
+ end fix1;
+;
+ begin fix1;
+ body1 shaft last ;
+ body2 hub2 1;
+ end fix1;
+;
+ begin fix1;
+ body1 shaft last ;
+ body2 hub3 1;
+ end fix1;
+;
+ begin bearing2;
+ name pitch1;
+ body1 hub1 last;
+ body2 blade1 1;
+ bearing_vector 2 0.0 0.0 -1.0;
+ end bearing2;
+;
+ begin bearing2;
+ name pitch2;
+ body1 hub2 last;
+ body2 blade2 1;
+ bearing_vector 2 0.0 0.0 -1.0;
+ end bearing2;
+;
+ begin bearing2;
+ name pitch3;
+ body1 hub3 last;
+ body2 blade3 1;
+ bearing_vector 2 0.0 0.0 -1.0;
+ end bearing2;
+end constraint;
+;
+end new_htc_structure;
+;----------------------------------------------------------------------------------------------------------------------------------------------------------------
+begin wind ;
+ density 1.225 ;
+ wsp [Windspeed] ;
+ tint [TI] ;
+ horizontal_input 1 ;
+ windfield_rotations [wdir] 8.0 0.0 ; yaw, tilt (positive=upflow=wind coming from below), rotation
+ center_pos0 0.0 0.0 -127 ; hub heigth
+ shear_format 3 [shear_exp] ;
+ turb_format [tu_model] ; 0=none, 1=mann,2=flex
+ tower_shadow_method 3 ; 0=none, 1=potential flow, 2=jet
+ scale_time_start [t0] ;
+ wind_ramp_factor 0.0 [t0] [wsp factor] 1.0 ;
+ [gust] iec_gust [gust_type] [G_A] [G_phi0] [G_t0] [G_T] ;
+;
+[staircase] wind_ramp_abs 400.0 401.0 0.0 1.0 ; wsp. after the step: 5.0
+[staircase] wind_ramp_abs 501.0 502.0 0.0 1.0 ; wsp. after the step: 6.0
+[staircase] wind_ramp_abs 602.0 603.0 0.0 1.0 ; wsp. after the step: 7.0
+[staircase] wind_ramp_abs 703.0 704.0 0.0 1.0 ; wsp. after the step: 8.0
+[staircase] wind_ramp_abs 804.0 805.0 0.0 1.0 ; wsp. after the step: 9.0
+[staircase] wind_ramp_abs 905.0 906.0 0.0 1.0 ; wsp. after the step: 10.0
+[staircase] wind_ramp_abs 1006.0 1007.0 0.0 1.0 ; wsp. after the step: 11.0
+[staircase] wind_ramp_abs 1107.0 1108.0 0.0 1.0 ; wsp. after the step: 12.0
+[staircase] wind_ramp_abs 1208.0 1209.0 0.0 1.0 ; wsp. after the step: 13.0
+[staircase] wind_ramp_abs 1309.0 1310.0 0.0 1.0 ; wsp. after the step: 14.0
+[staircase] wind_ramp_abs 1410.0 1411.0 0.0 1.0 ; wsp. after the step: 15.0
+[staircase] wind_ramp_abs 1511.0 1512.0 0.0 1.0 ; wsp. after the step: 16.0
+[staircase] wind_ramp_abs 1612.0 1613.0 0.0 1.0 ; wsp. after the step: 17.0
+[staircase] wind_ramp_abs 1713.0 1714.0 0.0 1.0 ; wsp. after the step: 18.0
+[staircase] wind_ramp_abs 1814.0 1815.0 0.0 1.0 ; wsp. after the step: 19.0
+[staircase] wind_ramp_abs 1915.0 1916.0 0.0 1.0 ; wsp. after the step: 20.0
+[staircase] wind_ramp_abs 2016.0 2017.0 0.0 1.0 ; wsp. after the step: 21.0
+[staircase] wind_ramp_abs 2117.0 2118.0 0.0 1.0 ; wsp. after the step: 22.0
+[staircase] wind_ramp_abs 2218.0 2219.0 0.0 1.0 ; wsp. after the step: 23.0
+[staircase] wind_ramp_abs 2319.0 2320.0 0.0 1.0 ; wsp. after the step: 24.0
+[staircase] wind_ramp_abs 2420.0 2421.0 0.0 1.0 ; wsp. after the step: 25.0
+ ;
+[windramp] wind_ramp_abs 400.0 2200.0 0.0 21.0 ; wsp. after the step: 25.0
+[windramp] wind_ramp_abs 2400.0 4200.0 0.0 -21.0 ; wsp. after the step: 25.0
+ ;
+ begin mann ;
+ create_turb_parameters 29.4 1.0 3.9 [tu_seed] 1.0 ; L, alfaeps, gamma, seed, highfrq compensation
+ filename_u ./[turb_dir][Turb base name]u.bin ;
+ filename_v ./[turb_dir][Turb base name]v.bin ;
+ filename_w ./[turb_dir][Turb base name]w.bin ;
+ box_dim_u 8192 [turb_dx] ;
+ box_dim_v 32 7.5;
+ box_dim_w 32 7.5;
+ std_scaling 1.0 0.7 0.5 ;
+ end mann ;
+;
+ begin tower_shadow_potential_2;
+ tower_mbdy_link tower;
+ nsec 2;
+ radius 0.0 4.15 ;
+ radius 123.6 2.75 ; (radius)
+ end tower_shadow_potential_2;
+end wind;
+;
+begin aerodrag ;
+ begin aerodrag_element ;
+ mbdy_name tower;
+ aerodrag_sections uniform 10 ;
+ nsec 2 ;
+ sec 0.0 0.6 8.3 ; tower bottom
+ sec 123.6 0.6 5.5 ; tower top (diameter)
+ end aerodrag_element;
+;
+ begin aerodrag_element ; Nacelle drag side
+ mbdy_name shaft;
+ aerodrag_sections uniform 2 ;
+ nsec 2 ;
+ sec 0.0 0.8 10.0 ;
+ sec 7.01 0.8 10.0 ;
+ end aerodrag_element;
+end aerodrag;
+;
+begin aero ;
+ nblades 3;
+ hub_vec shaft -3 ; rotor rotation vector (normally shaft composant directed from pressure to sustion side)
+ link 1 mbdy_c2_def blade1;
+ link 2 mbdy_c2_def blade2;
+ link 3 mbdy_c2_def blade3;
+ ae_filename ./data/AVATAR_10MW_RWT_ae.dat ;
+ pc_filename ./data/AVATAR_10MW_RWT_pc_hama_v1.dat ;
+ induction_method [Induction] ; 0=none, 1=normal
+ aerocalc_method 1 ; 0=ingen aerodynamic, 1=med aerodynamic
+ aero_distribution ae_file 1 ;
+ ae_sets 1 1 1;
+ tiploss_method 1 ; 0=none, 1=prandtl
+ dynstall_method [Dyn stall] ; 0=none, 1=stig øye method,2=mhh method
+;
+; ; --- Flaps --- ;
+ ; begin dynstall_ateflap ;
+ ; Ais 0.165 0.335 0.0 ;
+ ; Bis 0.0455 0.30 0.30 ;
+ ; flap 59.5925 85.5023 ./data/Flap_dturwt1_Thk24.ds ; Flap Sec: 1
+ ; end dynstall_ateflap;
+end aero ;
+;-------------------------------------------------------------------------------------------------
+begin dll;
+;
+ begin type2_dll;
+ name risoe_controller ;
+ filename ./control/risoe_controller.dll ;
+ dll_subroutine_init init_regulation ;
+ dll_subroutine_update update_regulation ;
+ arraysizes_init 52 1 ;
+ arraysizes_update 12 100 ;
+ begin init ;
+ ; Overall parameters
+ constant 1 10000.0 ; Rated power [kW]
+ constant 2 0.628 ; Minimum rotor speed [rad/s]
+ constant 3 1.005 ; Rated rotor speed [rad/s]
+ constant 4 15.6E+06 ; Maximum allowable generator torque [Nm]
+ 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 'wpdata.n', where n=int(theta_min)
+ 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 9 0.7 ; Damping ratio of speed filter [-]
+ constant 10 1.64 ; Frequency of free-free DT torsion mode [Hz], if zero no notch filter used
+ ; Partial load control parameters
+ constant 11 0.9648030e+07 ; 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 1.047610E+08 ; Proportional gain of torque controller [Nm/(rad/s)]
+ constant 13 0.153367E+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, 2=constant torque]
+ constant 16 0.762489 ; Proportional gain of pitch controller [rad/(rad/s)]
+ constant 17 0.224086 ; Integral gain of pitch controller [rad/rad]
+ constant 18 0.0 ; Differential gain of pitch controller [rad/(rad/s^2)]
+ constant 19 0.4e-9 ; Proportional power error gain [rad/W]
+ constant 20 0.4e-9 ; Integral power error gain [rad/(Ws)]
+ constant 21 10.6824 ; Coefficient of linear term in aerodynamic gain scheduling, KK1 [deg]
+ constant 22 601.25499 ; 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
+ constant 24 [Cut-in time] ; Cut-in time [s]
+ constant 25 1.0 ; Time delay for soft start of torque [1/1P]
+; Cut-out simulation parameters
+ constant 26 [Cut-out time] ; Cut-out time [s]
+ constant 27 5.0 ; Time constant for linear torque cut-out [s]
+ constant 28 [Stop type] ; Stop type [1=normal, 2=emergency]
+ constant 29 1.0 ; Time delay for pitch stop after shut-down signal [s]
+ constant 30 [Pitvel 1] ; Maximum pitch velocity during initial period of stop [deg/s]
+ constant 31 3.0 ; Time period of initial pitch stop phase [s] (maintains pitch speed specified in constant 30)
+ constant 32 [Pitvel 2] ; Maximum pitch velocity during final phase of stop [deg/s]
+; Expert parameters (keep default values unless otherwise given)
+ constant 33 2.0 ; Lower angle above lowest minimum pitch angle for switch [deg]
+ constant 34 2.0 ; Upper angle above lowest minimum pitch angle for switch [deg], if equal then hard switch
+ constant 35 95.0 ; Ratio between filtered speed and reference speed for fully open torque limits [%]
+ constant 36 2.0 ; Time constant of 1st order filter on wind speed used for minimum pitch [1/1P]
+ constant 37 1.0 ; Time constant of 1st order filter on pitch angle used for gain scheduling [1/1P]
+; Drivetrain damper
+ constant 38 0.0 ; Proportional gain of active DT damper [Nm/(rad/s)], requires frequency in input 10
+; Over speed
+ constant 39 25.0 ; Overspeed percentage before initiating turbine controller alarm (shut-down) [%]
+; Additional non-linear pitch control term (not used when all zero)
+ constant 40 0.0 ; Err0 [rad/s]
+ constant 41 0.0 ; ErrDot0 [rad/s^2]
+ constant 42 0.0 ; PitNonLin1 [rad/s]
+; Storm control command
+ constant 43 28.0 ; Wind speed 'Vstorm' above which derating of rotor speed is used [m/s]
+ constant 44 28.0 ; Cut-out wind speed (only used for derating of rotor speed in storm) [m/s]
+; Safety system parameters
+ constant 45 25.0 ; Overspeed percentage before initiating safety system alarm (shut-down) [%]
+ constant 46 1.5 ; Max low-pass filtered tower top acceleration level [m/s^2] - max in DLC 1.3=1.1 m/s^2
+; Turbine parameter
+ constant 47 205.8 ; Nominal rotor diameter [m]
+; Parameters for rotor inertia reduction in variable speed region
+ constant 48 0.0 ; Proportional gain on rotor acceleration in variable speed region [Nm/(rad/s^2)] (not used when zero)
+; Parameters for alternative partial load controller with PI regulated TSR tracking
+ constant 49 0.0 ; Optimal tip speed ratio [-] (only used when K=constant 11 = 0 otherwise Qg=K*Omega^2 is used)
+; Parameters for adding aerodynamic drivetrain damping on gain scheduling
+ constant 50 0.0 ; Proportional gain of aerodynamic DT damping [Nm/(rad/s)]
+ constant 51 0.0 ; Coefficient of linear term in aerodynamic DT damping scheduling, KK1 [deg]
+ constant 52 0.0 ; Coefficient of quadratic term in aerodynamic DT damping scheduling, KK2 [deg^2]
+ end init ;
+;
+ begin output ;
+ general time ; [s]
+ constraint bearing1 shaft_rot 1 only 2 ; Drivetrain speed [rad/s]
+ constraint bearing2 pitch1 1 only 1; [rad]
+ constraint bearing2 pitch2 1 only 1; [rad]
+ constraint bearing2 pitch3 1 only 1; [rad]
+ wind free_wind 1 0.0 0.0 -127 ; Global coordinates at hub height
+ dll inpvec 2 2 ; Elec. power from generator servo .dll
+ dll inpvec 2 8 ; Grid state flag from generator servo .dll
+ mbdy state acc tower 10 1.0 global only 1 ; Tower top x-acceleration [m/s^2]
+ mbdy state acc tower 10 1.0 global only 2 ; Tower top y-acceleration [m/s^2]
+ end output;
+ end type2_dll;
+;
+ begin type2_dll;
+ name generator_servo ;
+ filename ./control/generator_servo.dll ;
+ dll_subroutine_init init_generator_servo ;
+ dll_subroutine_update update_generator_servo ;
+ arraysizes_init 7 1 ;
+ arraysizes_update 4 8 ;
+ begin init ;
+ constant 1 20.0 ; Frequency of 2nd order servo model of generator-converter system [Hz]
+ constant 2 0.9 ; Damping ratio 2nd order servo model of generator-converter system [-]
+ constant 3 15.6E+06 ; Maximum allowable LSS torque (pull-out torque) [Nm]
+ constant 4 0.94 ; Generator efficiency [-]
+ constant 5 1.0 ; Gearratio [-]
+ constant 6 0.0 ; Time for half value in softstart of torque [s]
+ constant 7 [Grid loss time] ; Time for grid loss [s]
+ end init ;
+;
+ begin output;
+ general time ; Time [s]
+ dll inpvec 1 1 ; Electrical torque reference [Nm]
+ constraint bearing1 shaft_rot 1 only 2; Generator LSS speed [rad/s]
+ mbdy momentvec shaft 1 1 shaft only 3 ; Shaft moment [kNm] (Qshaft)
+ end output;
+;
+ begin actions;
+ mbdy moment_int shaft 1 -3 shaft towertop 2 ; Generator LSS torque [Nm]
+ end actions;
+ end type2_dll;
+;
+ begin type2_dll;
+ name mech_brake ;
+ filename ./control/mech_brake.dll ;
+ dll_subroutine_init init_mech_brake ;
+ dll_subroutine_update update_mech_brake ;
+ arraysizes_init 7 1 ;
+ arraysizes_update 4 6 ;
+ begin init ;
+ constant 1 5225.35 ; Fully deployed maximum brake torque [Nm] (0.6*max torque)
+ constant 2 100.0 ; Parameter alpha used in Q = tanh(omega*alpha), typically 1e2/Omega_nom
+ constant 3 0.5 ; Delay time for before brake starts to deploy [s]
+ constant 4 0.74 ; Time for brake to become fully deployed [s]
+ end init ;
+;
+ begin output;
+ general time ; Time [s]
+ constraint bearing1 shaft_rot 1 only 2 ; Generator LSS speed [rad/s]
+ dll inpvec 1 25 ; Command to deploy mechanical disc brake [0,1]
+ end output;
+;
+ begin actions;
+ mbdy moment_int shaft 1 -3 shaft towertop 2 ; Generator LSS torque [Nm]
+ end actions;
+ end type2_dll;
+;
+ begin type2_dll;
+ name servo_with_limits ;
+ filename ./control/servo_with_limits.dll ;
+ dll_subroutine_init init_servo_with_limits ;
+ dll_subroutine_update update_servo_with_limits ;
+ arraysizes_init 10 1 ;
+ arraysizes_update 5 9 ;
+ begin init ;
+ constant 1 3 ; Number of blades [-]
+ constant 2 1.0 ; Frequency of 2nd order servo model of pitch system [Hz]
+ constant 3 0.7 ; Damping ratio 2nd order servo model of pitch system [-]
+ constant 4 10.0 ; Max. pitch speed [deg/s]
+ constant 5 15.0 ; Max. pitch acceleration [deg/s^2]
+ constant 6 -5.0 ; Min. pitch angle [deg]
+ constant 7 90.0 ; Max. pitch angle [deg]
+ constant 8 [Time pitch runaway] ; Time for pitch runaway [s]
+ constant 9 [Time stuck DLC22b] ; Time for stuck blade 1 [s]
+ constant 10 [Pitch 1 DLC22b] ; Angle of stuck blade 1 [deg]
+ end init ;
+ begin output;
+ general time ; Time [s]
+ dll inpvec 1 2 ; Pitch1 demand angle [rad]
+ dll inpvec 1 3 ; Pitch2 demand angle [rad]
+ dll inpvec 1 4 ; Pitch3 demand angle [rad]
+ dll inpvec 1 26 ; Flag for emergency pitch stop [0=off/1=on]
+ end output;
+;
+ begin actions;
+ constraint bearing2 angle pitch1 ; Angle pitch1 bearing [rad]
+ constraint bearing2 angle pitch2 ; Angle pitch2 bearing [rad]
+ constraint bearing2 angle pitch3 ; Angle pitch3 bearing [rad]
+ end actions;
+ end type2_dll;
+;
+; --- DLL for tower-blade tip distance -- ;
+ begin type2_dll;
+ name disttowtip ;
+ filename ./control/towclearsens.dll ;
+ dll_subroutine_init initialize ;
+ dll_subroutine_update update ;
+ arraysizes_init 1 1 ;
+ arraysizes_update 12 4 ;
+ begin init ;
+ constant 1 3.87 ; Tower radius close to downward blade tip [m]
+ end init ;
+ begin output;
+ mbdy state pos tower 5 0.00 global ; [1,2,3]. Tower position: 24.58 m
+ mbdy state pos blade1 26 1.0 global ; [4,5,6]
+ mbdy state pos blade2 26 1.0 global ; [7,8,9]
+ mbdy state pos blade3 26 1.0 global ; [10,11,12]
+ end output;
+ end type2_dll;
+end dll;
+;
+;----------------------------------------------------------------------------------------------------------------------------------------------------------------
+;
+begin output;
+ filename ./res/[Case folder]/[Case id.] ;
+ time [t0] [time stop] ;
+ data_format [out_format];
+ buffer 1 ;
+;
+ general time;
+ constraint bearing1 shaft_rot 2; angle and angle velocity
+ constraint bearing2 pitch1 5; angle and angle velocity
+ constraint bearing2 pitch2 5; angle and angle velocity
+ constraint bearing2 pitch3 5; angle and angle velocity
+ aero omega ;
+ aero torque;
+ aero power;
+ aero thrust;
+ wind free_wind 1 0.0 0.0 -127; local wind at fixed position: coo (1=global,2=non-rotation rotor coo.), pos x, pos y, pos z
+ ; non rotating coordinates shaft tip: equivalent to stationary hub in BLADED
+ mbdy momentvec shaft 3 2 shaft_nonrotate # non rotating shaft tip ;
+ mbdy forcevec shaft 3 2 shaft_nonrotate # non rotating shaft tip ;
+ ; Moments:
+ mbdy momentvec tower 1 1 tower # tower base ;
+ mbdy momentvec tower 19 2 tower # tower yaw bearing ;
+ mbdy momentvec shaft 4 1 shaft # main bearing ;
+ mbdy momentvec blade1 3 2 blade1 # blade 1 root ;
+ mbdy momentvec blade2 3 2 blade2 # blade 2 root ;
+ mbdy momentvec blade3 3 2 blade3 # blade 3 root ;
+ ; blade 2,3 root section loads
+ mbdy momentvec blade2 3 2 local # blade 2 section root;
+ mbdy momentvec blade3 3 2 local # blade 3 section root;
+ ; blade 1 sectional loads in local coordinates
+ mbdy momentvec blade1 2 2 local # blade 1 section;
+ mbdy momentvec blade1 3 2 local # blade 1 section root;
+ mbdy momentvec blade1 4 2 local # blade 1 section;
+ mbdy momentvec blade1 5 2 local # blade 1 section;
+ mbdy momentvec blade1 6 2 local # blade 1 section;
+ mbdy momentvec blade1 7 2 local # blade 1 section;
+ mbdy momentvec blade1 8 2 local # blade 1 section;
+ mbdy momentvec blade1 9 2 local # blade 1 section;
+ mbdy momentvec blade1 10 2 local # blade 1 section;
+ mbdy momentvec blade1 11 2 local # blade 1 section;
+ mbdy momentvec blade1 12 2 local # blade 1 section;
+ mbdy momentvec blade1 13 2 local # blade 1 section;
+ mbdy momentvec blade1 14 2 local # blade 1 section;
+ mbdy momentvec blade1 15 2 local # blade 1 section;
+ mbdy momentvec blade1 16 2 local # blade 1 section;
+ mbdy momentvec blade1 17 2 local # blade 1 section;
+ mbdy momentvec blade1 18 2 local # blade 1 section;
+ mbdy momentvec blade1 19 2 local # blade 1 section;
+ mbdy momentvec blade1 20 2 local # blade 1 section;
+ mbdy momentvec blade1 21 2 local # blade 1 section;
+ mbdy momentvec blade1 22 2 local # blade 1 section;
+ mbdy momentvec blade1 23 2 local # blade 1 section;
+ mbdy momentvec blade1 24 2 local # blade 1 section;
+ mbdy momentvec blade1 25 2 local # blade 1 section;
+ mbdy momentvec blade1 26 2 local # blade 1 section;
+ ; blade root out and in of plane forces
+ mbdy momentvec blade1 3 2 hub1 # blade 1 root ;
+ mbdy momentvec blade2 3 2 hub2 # blade 2 root ;
+ mbdy momentvec blade3 3 2 hub3 # blade 3 root ;
+; mbdy momentvec blade1 14 1 local # blade 1 50% local e coo ;
+; mbdy momentvec blade2 14 1 local # blade 2 50% local e coo ;
+; mbdy momentvec blade3 14 1 local # blade 3 50% local e coo ;
+ ; Displacements and accellerations
+ mbdy state pos tower 19 1.0 global only 1 # Tower top FA displ;
+ mbdy state pos tower 19 1.0 global only 2 # Tower top SS displ;
+ mbdy state acc tower 19 1.0 global only 1 # Tower top FA acc;
+ mbdy state acc tower 19 1.0 global only 2 # Tower top SS acc;
+;
+ mbdy state pos blade1 26 1.0 global # gl blade 1 tip pos ;
+ mbdy state pos blade2 26 1.0 global # gl blade 2 tip pos ;
+ mbdy state pos blade3 26 1.0 global # gl blade 3 tip pos ;
+ mbdy state pos blade1 26 1.0 blade1 # blade 1 tip pos ;
+ mbdy state pos blade2 26 1.0 blade2 # blade 2 tip pos ;
+ mbdy state pos blade3 26 1.0 blade3 # blade 3 tip pos ;
+;
+ mbdy state pos tower 5 0.00 global ; [1,2,3]. Tower position: 24.58 m
+;
+ ; elastic twist (torsional deformation) along the blade
+ aero tors_ang 1 45.56;
+ aero tors_ang 1 59.19;
+ aero tors_ang 1 70.87;
+ aero tors_ang 1 80.61;
+ aero tors_ang 1 84.50;
+ aero tors_ang 1 88.40;
+ aero tors_ang 1 92.29;
+ aero tors_ang 1 96.19;
+ aero tors_ang 1 98.13;
+ aero tors_ang 1 100.08; tip
+;
+; - Monitor Aerodynamics - ;
+ aero windspeed 3 1 1 72.5;
+ aero alfa 1 72.5;
+ aero alfa 2 72.5;
+ aero alfa 3 72.5;
+ aero cl 1 72.5;
+ aero cl 2 72.5;
+ aero cl 3 72.5;
+ aero cd 1 72.5;
+ aero cd 2 72.5;
+ aero cd 3 72.5;
+; - Main Controller -
+; Output to controller
+ ; dll outvec 1 1 # time;
+ ; dll outvec 1 2 # slow speed shaft rad/s;
+ ; dll outvec 1 3 # pitch angle 1;
+ ; dll outvec 1 4 # pitch angle 2;
+ ; dll outvec 1 5 # pitch angle 3;
+ ; dll outvec 1 6 # WSP_x_global;
+ ; dll outvec 1 7 # WSP_y_global;
+ ; dll outvec 1 8 # WSP_z_global;
+ ; dll outvec 1 9 # Elec. pwr ;
+ ; dll outvec 1 10 # Grid flag ;
+; Input from controller
+ dll inpvec 1 1 # Generator torque reference [Nm] ;
+ dll inpvec 1 2 # Pitch angle reference of blade 1 [rad] ;
+ dll inpvec 1 3 # Pitch angle reference of blade 2 [rad] ;
+ dll inpvec 1 4 # Pitch angle reference of blade 3 [rad] ;
+ ; dll inpvec 1 5 # Power reference [W] ;
+ ; dll inpvec 1 6 # Filtered wind speed [m/s] ;
+ ; dll inpvec 1 7 # Filtered rotor speed [rad/s];
+ ; dll inpvec 1 8 # Filtered rotor speed error for torque [rad/s];
+ ; dll inpvec 1 9 # Bandpass filtered rotor speed [rad/s];
+ ; dll inpvec 1 10 # Proportional term of torque contr. [Nm] ;
+ ; dll inpvec 1 11 # Integral term of torque controller [Nm] ;
+ ; dll inpvec 1 12 # Minimum limit of torque [Nm] ;
+ ; dll inpvec 1 13 # Maximum limit of torque [Nm] ;
+ dll inpvec 1 14 # Torque limit switch based on pitch [-] ;
+ ; dll inpvec 1 15 # Filtered rotor speed error for pitch [rad/s];
+ ; dll inpvec 1 16 # Power error for pitch [W] ;
+ ; dll inpvec 1 17 # Proportional term of pitch controller [rad] ;
+ ; dll inpvec 1 18 # Integral term of pitch controller [rad] ;
+ ; dll inpvec 1 19 # Minimum limit of pitch [rad] ;
+ ; dll inpvec 1 20 # Maximum limit of pitch [rad] ;
+ dll inpvec 1 21 # Torque reference from DT dammper [Nm] ;
+ dll inpvec 1 22 # Status signal [-] ;
+ ; dll inpvec 1 23 # Total added pitch rate [rad/s] ;
+ dll inpvec 1 24 # Filtered Mean pitch for gain sch [rad] ;
+ dll inpvec 1 25 # Flag for mechnical brake [0=off/1=on] ;
+ dll inpvec 1 26 # Flag for emergency pitch stop [0=off/1=on] ;
+ dll inpvec 1 27 # LP filtered acceleration level [m/s^2] ;
+; ; Output to generator model
+ ; dll outvec 2 1 # time ;
+ ; dll outvec 2 2 # Electrical torque reference [Nm] ;
+ ; dll outvec 2 3 # omega LSS ;
+; Input from generator model
+ dll inpvec 2 1 # Mgen LSS [Nm];
+ dll inpvec 2 2 # Pelec W ;
+ dll inpvec 2 3 # Mframe ;
+ dll inpvec 2 4 # Mgen HSS ;
+ dll inpvec 2 5 # Generator Pmech kW ;
+ dll inpvec 2 6 # Filtered Gen speed ;
+ dll inpvec 2 7 # Resulting Eff ;
+ dll inpvec 2 8 # Grid flag ;
+; Output to mechanical brake
+ dll inpvec 3 1 # Brake torque [Nm] ;
+; ; Input from mechanical brake
+ ; dll outvec 3 1 # Time [s] ;
+ ; dll outvec 3 2 # Generator LSS speed [rad/s] ;
+ ; dll outvec 3 3 # Deploy brake ;
+; ; Output to pitch servo
+ ; dll outvec 4 1 # time;
+ ; dll outvec 4 2 # pitchref 1;
+ ; dll outvec 4 3 # pitchref 2;
+ ; dll outvec 4 4 # pitchref 3;
+ ; dll outvec 4 5 # Emerg. stop;
+; Input from pitch servo
+ dll inpvec 4 1 # pitch 1;
+ dll inpvec 4 2 # pitch 2;
+ dll inpvec 4 3 # pitch 3;
+; Check tower clearence
+ dll inpvec 5 1 # Bltip tow min d [m];
+; general constant 1.0 ; constant 1.0 - to mesure activity of flap in terms of displacement
+; - Check on flap control:
+ ; ; - From flap controller: -
+ ; dll type2_dll cyclic_flap_controller inpvec 1 # Ref flap signal bl 1 [deg] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 2 # Ref flap signal bl 2 [deg] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 3 # Ref flap signal bl 3 [deg] ;
+ ; ; - Mbc values
+ ; dll type2_dll cyclic_flap_controller inpvec 4 # momvec mbc cos [kNm] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 5 # momvec mbc sin [kNm] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 6 # momvec mbc filt cos [kNm] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 7 # momvec mbc filt sin [kNm] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 8 # flap mbc cos [deg] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 9 # flap mbc sin [deg] ;
+ ; ; - Check Gains - ;
+ ; dll type2_dll cyclic_flap_controller inpvec 10 # lead angle [deg] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 11 # scaling on rat pow [-] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 12 # actual kp [deg/kNm] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 13 # actual ki [deg/kNms] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 14 # actual kd [deg s/kNm] ;
+ ; ; - Actual deflections -
+ ; [dis_setbeta] aero beta 1 1 ;
+ ; [dis_setbeta] aero beta 2 1 ;
+ ; [dis_setbeta] aero beta 3 1 ;
+ ; ; - Mbc values
+ ; dll type2_dll cyclic_flap_controller inpvec 4 # momvec mbc cos [kNm] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 5 # momvec mbc sin [kNm] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 6 # momvec mbc filt cos [kNm] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 7 # momvec mbc filt sin [kNm] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 8 # flap mbc cos [deg] ;
+ ; dll type2_dll cyclic_flap_controller inpvec 9 # flap mbc sin [deg] ;
+end output;
+;
+exit;
diff --git a/wetb/prepost/tests/test_Simulations.py b/wetb/prepost/tests/test_Simulations.py
new file mode 100644
index 00000000..f4c9cfa4
--- /dev/null
+++ b/wetb/prepost/tests/test_Simulations.py
@@ -0,0 +1,55 @@
+'''
+Created on 05/11/2015
+
+@author: MMPE
+'''
+from __future__ import unicode_literals
+from __future__ import print_function
+from __future__ import division
+from __future__ import absolute_import
+from future import standard_library
+standard_library.install_aliases()
+
+import unittest
+import os
+import filecmp
+
+from wetb.prepost import dlctemplate as tmpl
+
+
+class TestGenerateInputs(unittest.TestCase):
+
+ def setUp(self):
+ self.basepath = os.path.dirname(__file__)
+
+ def test_launch_dlcs_excel(self):
+ # manually configure paths, HAWC2 model root path is then constructed as
+ # p_root_remote/PROJECT/sim_id, and p_root_local/PROJECT/sim_id
+ # adopt accordingly when you have configured your directories differently
+ p_root_remote = os.path.join(self.basepath, 'data/')
+ p_root_local = os.path.join(self.basepath, 'data/')
+ # project name, sim_id, master file name
+ tmpl.PROJECT = 'demo_dlc'
+ tmpl.MASTERFILE = 'demo_dlc_master_A0001.htc'
+ # MODEL SOURCES, exchanche file sources
+ tmpl.P_RUN = os.path.join(p_root_remote, tmpl.PROJECT, 'remote/')
+ tmpl.P_SOURCE = os.path.join(p_root_local, tmpl.PROJECT, 'source/')
+ # location of the master file
+ tmpl.P_MASTERFILE = os.path.join(p_root_local, tmpl.PROJECT,
+ 'source', 'htc', '_master/')
+ # location of the pre and post processing data
+ tmpl.POST_DIR = os.path.join(p_root_remote, tmpl.PROJECT, 'remote',
+ 'prepost/')
+ tmpl.force_dir = tmpl.P_RUN
+ tmpl.launch_dlcs_excel('remote', silent=True)
+
+ remote = os.path.join(p_root_remote, tmpl.PROJECT, 'remote')
+ ref = os.path.join(p_root_remote, tmpl.PROJECT, 'ref')
+ cmp = filecmp.dircmp(remote, ref)
+ self.assertTrue(len(cmp.diff_files)==0)
+ self.assertTrue(len(cmp.right_only)==0)
+ self.assertTrue(len(cmp.left_only)==0)
+
+
+if __name__ == "__main__":
+ unittest.main()
--
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