diff --git a/requirements.txt b/requirements.txt
index ebf1ff5c9c85eb5f24336bdb0d21e0f0ca384d12..4f4ab5838748fa63eb598afca49c3f6cd8148ef6 100644
--- a/requirements.txt
+++ b/requirements.txt
@@ -7,5 +7,6 @@ pytest
xlrd
h5py
pandas
+tables
future
diff --git a/wetb/fatigue_tools/fatigue.py b/wetb/fatigue_tools/fatigue.py
index e26089ce4f5c6717651908ac1e35ef918d52fb9b..bde2d087b59a418c8fa6040f5a3c126e9330277b 100644
--- a/wetb/fatigue_tools/fatigue.py
+++ b/wetb/fatigue_tools/fatigue.py
@@ -70,7 +70,6 @@ def eq_load(signals, no_bins=46, m=[3, 4, 6, 8, 10, 12], neq=1, rainflow_func=ra
return [[np.nan] * len(np.atleast_1d(m))] * len(np.atleast_1d(neq))
-
def eq_load_and_cycles(signals, no_bins=46, m=[3, 4, 6, 8, 10, 12], neq=[10 ** 6, 10 ** 7, 10 ** 8], rainflow_func=rainflow_windap):
"""Calculate combined fatigue equivalent load
@@ -109,7 +108,6 @@ def eq_load_and_cycles(signals, no_bins=46, m=[3, 4, 6, 8, 10, 12], neq=[10 ** 6
return eq_loads, cycles, ampl_bin_mean, ampl_bin_edges
-
def cycle_matrix(signals, ampl_bins=10, mean_bins=10, rainflow_func=rainflow_windap):
"""Markow load cycle matrix
@@ -132,7 +130,8 @@ def cycle_matrix(signals, ampl_bins=10, mean_bins=10, rainflow_func=rainflow_win
Returns
-------
cycles : ndarray, shape(ampl_bins, mean_bins)
- A bi-dimensional histogram of load cycles(full cycles). Amplitudes are histogrammed along the first dimension and mean values are histogrammed along the second dimension.
+ A bi-dimensional histogram of load cycles(full cycles). Amplitudes are\
+ histogrammed along the first dimension and mean values are histogrammed along the second dimension.
ampl_bin_mean : ndarray, shape(ampl_bins,)
The average cycle amplitude of the bins
ampl_edges : ndarray, shape(ampl_bins+1,)
diff --git a/wetb/fatigue_tools/rainflowcounting/rfc_hist.py b/wetb/fatigue_tools/rainflowcounting/rfc_hist.py
deleted file mode 100644
index 65d3c00945c8f97f731af59972c4a8b2f55a7b25..0000000000000000000000000000000000000000
--- a/wetb/fatigue_tools/rainflowcounting/rfc_hist.py
+++ /dev/null
@@ -1,53 +0,0 @@
-from __future__ import division
-from __future__ import unicode_literals
-from __future__ import print_function
-from __future__ import absolute_import
-from future import standard_library
-standard_library.install_aliases()
-import numpy as np
-def rfc_hist(sig_rf, nrbins=46):
- """Histogram of rainflow counted cycles
-
- hist, bin_edges, bin_avg = rfc_hist(sig, nrbins=46)
-
- Divide the rainflow counted cycles of a signal into equally spaced bins.
-
- Created on Wed Feb 16 16:53:18 2011
- @author: David Verelst
- Modified 10.10.2011 by Mads M Pedersen to elimintate __copy__ and __eq__
-
- Parameters
- ----------
- sig_rf : array-like
- As output by rfc_astm or rainflow
-
- nrbins : int, optional
- Divide the rainflow counted amplitudes in a number of equally spaced
- bins.
-
- Returns
- -------
- hist : array-like
- Counted rainflow cycles per bin, has nrbins elements
-
- bin_edges : array-like
- Edges of the bins, has nrbins+1 elements.
-
- bin_avg : array-like
- Average rainflow cycle amplitude per bin, has nrbins elements.
- """
-
- rf_half = sig_rf
-
- # the Matlab approach is to divide into 46 bins
- bin_edges = np.linspace(0, 1, num=nrbins + 1) * rf_half.max()
- hist = np.histogram(rf_half, bins=bin_edges)[0]
- # calculate the average per bin
- hist_sum = np.histogram(rf_half, weights=rf_half, bins=bin_edges)[0]
- # replace zeros with one, to avoid 0/0
- hist_ = hist.copy()
- hist_[(hist == 0).nonzero()] = 1.0
- # since the sum is also 0, the avg remains zero for those whos hist is zero
- bin_avg = hist_sum / hist_
-
- return hist, bin_edges, bin_avg
diff --git a/wetb/hawc2/Hawc2io.py b/wetb/hawc2/Hawc2io.py
index 2ec8deff39bf036f1879869ac3121dce1b5ecbb6..ac8d28c8d43327f10373873b4521febfaf041434 100644
--- a/wetb/hawc2/Hawc2io.py
+++ b/wetb/hawc2/Hawc2io.py
@@ -90,8 +90,8 @@ class ReadHawc2(object):
Name = []; Unit = []; Description = [];
for i in range(0, self.NrCh):
temp = str(Lines[i + 12][12:43]); Name.append(temp.strip())
- temp = str(Lines[i + 12][43:48]); Unit.append(temp.strip())
- temp = str(Lines[i + 12][49:]); Description.append(temp.strip())
+ temp = str(Lines[i + 12][43:54]); Unit.append(temp.strip())
+ temp = str(Lines[i + 12][54:-1]); Description.append(temp.strip())
self.ChInfo = [Name, Unit, Description]
# if binary file format, scaling factors are read
if Format.lower() == 'binary':
diff --git a/wetb/prepost/Simulations.py b/wetb/prepost/Simulations.py
index dabfe334c84990e5c682a01f753e021b49df7440..164aa1866638be0fce68b42f14bddeb9f5db2f35 100755
--- a/wetb/prepost/Simulations.py
+++ b/wetb/prepost/Simulations.py
@@ -795,7 +795,7 @@ def prepare_launch(iter_dict, opt_tags, master, variable_tag_func,
launch(cases, runmethod=runmethod, verbose=verbose, check_log=check_log,
copyback_turb=copyback_turb, qsub=qsub, wine_appendix=wine_appendix,
windows_nr_cpus=windows_nr_cpus, short_job_names=short_job_names,
- pbs_fname_appendix=pbs_fname_appendix)
+ pbs_fname_appendix=pbs_fname_appendix, silent=silent)
return cases
@@ -1030,10 +1030,10 @@ def launch(cases, runmethod='local', verbose=False, copyback_turb=True,
elif runmethod in ['jess','gorm']:
# create the pbs object
pbs = PBS(cases, server=runmethod, short_job_names=short_job_names,
- pbs_fname_appendix=pbs_fname_appendix, qsub=qsub)
+ pbs_fname_appendix=pbs_fname_appendix, qsub=qsub,
+ verbose=verbose, silent=silent)
pbs.wine_appendix = wine_appendix
pbs.copyback_turb = copyback_turb
- pbs.verbose = verbose
pbs.pbs_out_dir = pbs_out_dir
pbs.create()
elif runmethod == 'local':
@@ -1851,8 +1851,8 @@ class PBS(object):
such as the turbulence file and folder, htc folder and others
"""
- def __init__(self, cases, server='gorm', qsub='time',
- pbs_fname_appendix=True, short_job_names=True):
+ def __init__(self, cases, server='gorm', qsub='time', silent=False,
+ pbs_fname_appendix=True, short_job_names=True, verbose=False):
"""
Define the settings here. This should be done outside, but how?
In a text file, paramters list or first create the object and than set
@@ -1882,7 +1882,8 @@ class PBS(object):
"""
self.server = server
- self.verbose = True
+ self.verbose = verbose
+ self.silent = silent
# if server == 'thyra':
# self.maxcpu = 4
@@ -2182,7 +2183,8 @@ class PBS(object):
ended = True
# print progress:
replace = ((i/self.maxcpu), (i_tot/self.maxcpu), self.walltime)
- print('pbs script %3i/%i walltime=%s' % replace)
+ if not self.silent:
+ print('pbs script %3i/%i walltime=%s' % replace)
count2 += 1
i += 1
@@ -2196,7 +2198,8 @@ class PBS(object):
self.ending(pbs_path)
# progress printing
replace = ( (i/self.maxcpu), (i_tot/self.maxcpu), self.walltime )
- print('pbs script %3i/%i walltime=%s, partially loaded' % replace)
+ if not self.silent:
+ print('pbs script %3i/%i walltime=%s, partially loaded' % replace)
# print 'pbs progress, script '+format(i/self.maxcpu,'2.0f')\
# + '/' + format(i_tot/self.maxcpu, '2.0f') \
# + ' partially loaded...'
@@ -2451,7 +2454,8 @@ class PBS(object):
cases_fail = {}
- print('checking if all log and result files are present...', end='')
+ if not self.silent:
+ print('checking if all log and result files are present...', end='')
# check for each case if we have results and a log file
for cname, case in cases.items():
@@ -2473,7 +2477,8 @@ class PBS(object):
if size_sel < 5 or size_dat < 5:
cases_fail[cname] = copy.copy(cases[cname])
- print('done!')
+ if not self.silent:
+ print('done!')
# length will be zero if there are no failures
return cases_fail
@@ -3828,7 +3833,7 @@ class Cases(object):
save=True, m=[3, 4, 6, 8, 10, 12], neq=None, no_bins=46,
ch_fatigue={}, update=False, add_sensor=None,
chs_resultant=[], i0=0, i1=-1, saveinterval=1000,
- csv=True, suffix=None, fatigue_cycles=False, A=None,
+ csv=True, suffix=None, A=None,
ch_wind=None, save_new_sigs=False, xlsx=False):
"""
Calculate statistics and save them in a pandas dataframe. Save also
@@ -3851,10 +3856,6 @@ class Cases(object):
needs to be calculated. When set to None, ch_fatigue = ch_sel,
and hence all channels will have a fatigue analysis.
- fatigue_cycles : Boolean, default=False
- If True, the cycle matrix, or sum( n_i*S_i^m ), is calculated. If
- set to False, the 1Hz equivalent load is calculated.
-
chs_resultant
add_sensor
@@ -4168,12 +4169,13 @@ class Cases(object):
signal = self.sig[:,chi]
if neq is None:
neq = float(case['[duration]'])
- if not fatigue_cycles:
- eq = self.res.calc_fatigue(signal, no_bins=no_bins,
- neq=neq, m=m)
- else:
- eq = self.res.cycle_matrix(signal, no_bins=no_bins, m=m)
+
+ eq = self.res.calc_fatigue(signal, no_bins=no_bins,
+ neq=neq, m=m)
+
+ # save in the fatigue results
fatigue[ch_id] = {}
+ fatigue[ch_id]['neq'] = neq
# when calc_fatigue succeeds, we should have as many items
# as in m
if len(eq) == len(m):
@@ -4188,6 +4190,7 @@ class Cases(object):
for m_ in m:
tag = 'm=%2.01f' % m_
tags_fatigue.append(tag)
+ tags_fatigue.append('neq')
# -----------------------------------------------------------------
# define the pandas data frame dict on first run
@@ -4408,10 +4411,10 @@ class Cases(object):
raise(e)
return df_dict2
- def fatigue_lifetime(self, dfs, neq, res_dir='res/', fh_lst=None, years=20.,
+ def fatigue_lifetime(self, dfs, neq_life, res_dir='res/', fh_lst=None,
dlc_folder="dlc%s_iec61400-1ed3/", extra_cols=[],
save=False, update=False, csv=False, new_sim_id=False,
- xlsx=False):
+ xlsx=False, years=20.0):
"""
Cacluate the fatigue over a selection of cases and indicate how many
hours each case contributes to its life time.
@@ -4427,7 +4430,7 @@ class Cases(object):
should only hold the results of one standard organized DLC (one
turbine, one inflow case).
- neq : float
+ neq_life : float
Reference number of cycles. Usually, neq is either set to 10e6,
10e7 or 10e8.
@@ -4543,12 +4546,17 @@ class Cases(object):
# values of the identifier columns for each case. We do this
# in case the original dfs holds multiple DLC cases.
dict_Leq[col].append(sel_sort[col].unique()[0])
+
+ # R_eq is usually expressed as the 1Hz equivalent load
+ neq_1hz = sel_sort['neq'].values
+
for m in ms:
- # sel_sort[m] holds the cycle_matrices for each of the DLC
+ # sel_sort[m] holds the equivalent loads for each of the DLC
# cases: such all the different wind speeds for dlc1.2
- R_eq = (sel_sort[m].values*np.array(hours)).sum()
+ R_eq_mod = np.power(sel_sort[m].values, m) * neq_1hz
+ tmp = (R_eq_mod*np.array(hours)).sum()
# the effective Leq for each of the material constants
- dict_Leq[m].append(math.pow(R_eq/neq, 1.0/float(m[2:])))
+ dict_Leq[m].append(math.pow(tmp/neq_life, 1.0/float(m[2:])))
# the following is twice as slow:
# [i*j for (i,j) in zip(sel_sort[m].values.tolist(),hours)]
diff --git a/wetb/prepost/dlcdefs.py b/wetb/prepost/dlcdefs.py
index ce8dbc144de91964c096119bf9f4e63159aa1574..747e775320bb335f4f80eaed9063400ff4c4ca81 100644
--- a/wetb/prepost/dlcdefs.py
+++ b/wetb/prepost/dlcdefs.py
@@ -46,7 +46,7 @@ def configure_dirs(verbose=False):
raise ValueError('Could not find master file in htc/_master')
MASTERFILE = master
P_MASTERFILE = os.path.join(P_SOURCE, 'htc%s_master%s' % (os.sep, os.sep))
- POST_DIR = os.path.join(p_run_root, PROJECT, 'python-prepost-data%s' % os.sep)
+ POST_DIR = os.path.join(p_run_root, PROJECT, 'prepost-data%s' % os.sep)
if verbose:
print('='*79)
@@ -240,7 +240,7 @@ def tags_defaults(master):
def excel_stabcon(proot, fext='xlsx', pignore=None, sheet=0,
- pinclude=None):
+ pinclude=None, silent=False):
"""
Read all MS Excel files that hold load case definitions according to
the team STABCON definitions. Save each case in a list according to the
@@ -272,16 +272,20 @@ def excel_stabcon(proot, fext='xlsx', pignore=None, sheet=0,
first sheet (index=0) is taken.
"""
- print('looking for DLC spreadsheet definitions at:')
- print(proot)
+ if not silent:
+ print('looking for DLC spreadsheet definitions at:')
+ print(proot)
df_list = misc.read_excel_files(proot, fext=fext, pignore=pignore,
- sheet=sheet, pinclude=pinclude)
+ sheet=sheet, pinclude=pinclude,
+ silent=silent)
- print('found %i Excel file(s), ' % len(df_list), end='')
+ if not silent:
+ print('found %i Excel file(s), ' % len(df_list), end='')
k = 0
for df in df_list:
k += len(df)
- print('in which a total of %s cases are defined.' % k)
+ if not silent:
+ print('in which a total of %s cases are defined.' % k)
opt_tags = []
diff --git a/wetb/prepost/dlctemplate.py b/wetb/prepost/dlctemplate.py
index 39d1b00a850dfd6b11ce3bb95c3ba5a39732c572..b6240f46840503754662d6b80b23c03bee436105 100755
--- a/wetb/prepost/dlctemplate.py
+++ b/wetb/prepost/dlctemplate.py
@@ -164,7 +164,7 @@ def variable_tag_func(master, case_id_short=False):
### PRE- POST
# =============================================================================
-def launch_dlcs_excel(sim_id):
+def launch_dlcs_excel(sim_id, silent=False):
"""
Launch load cases defined in Excel files
"""
@@ -175,9 +175,10 @@ def launch_dlcs_excel(sim_id):
# see if a htc/DLCs dir exists
dlcs_dir = os.path.join(P_SOURCE, 'htc', 'DLCs')
if os.path.exists(dlcs_dir):
- opt_tags = dlcdefs.excel_stabcon(dlcs_dir)
+ opt_tags = dlcdefs.excel_stabcon(dlcs_dir, silent=silent)
else:
- opt_tags = dlcdefs.excel_stabcon(os.path.join(P_SOURCE, 'htc'))
+ opt_tags = dlcdefs.excel_stabcon(os.path.join(P_SOURCE, 'htc'),
+ silent=silent)
if len(opt_tags) < 1:
raise ValueError('There are is not a single case defined. Make sure '
@@ -200,7 +201,8 @@ def launch_dlcs_excel(sim_id):
# runmethod = 'local-script'
# runmethod = 'windows-script'
# runmethod = 'jess'
- master = master_tags(sim_id, runmethod=runmethod)
+ master = master_tags(sim_id, runmethod=runmethod, silent=silent,
+ verbose=False)
master.tags['[sim_id]'] = sim_id
master.output_dirs.append('[Case folder]')
master.output_dirs.append('[Case id.]')
@@ -219,7 +221,8 @@ def launch_dlcs_excel(sim_id):
write_htc=True, runmethod=runmethod, verbose=False,
copyback_turb=True, msg='', update_cases=False,
ignore_non_unique=False, run_only_new=False,
- pbs_fname_appendix=False, short_job_names=False)
+ pbs_fname_appendix=False, short_job_names=False,
+ silent=silent)
def launch_param(sim_id):
@@ -264,10 +267,10 @@ def launch_param(sim_id):
def post_launch(sim_id, statistics=True, rem_failed=True, check_logs=True,
force_dir=False, update=False, saveinterval=2000, csv=False,
- fatigue_cycles=False, m=[1, 3, 4, 5, 6, 8, 10, 12, 14],
- neq=1e6, no_bins=46, years=20.0, fatigue=True, nn_twb=1,
- nn_twt=20, nn_blr=4, A=None, save_new_sigs=False,
- envelopeturbine=False, envelopeblade=False, save_iter=False):
+ m=[1, 3, 4, 5, 6, 8, 10, 12, 14], neq=1e6, no_bins=46,
+ years=20.0, fatigue=True, nn_twb=1, nn_twt=20, nn_blr=4, A=None,
+ save_new_sigs=False, envelopeturbine=False, envelopeblade=False,
+ save_iter=False, AEP=False):
# =========================================================================
# check logfiles, results files, pbs output files
@@ -339,12 +342,12 @@ def post_launch(sim_id, statistics=True, rem_failed=True, check_logs=True,
df_stats = cc.statistics(calc_mech_power=True, i0=i0, i1=i1,
tags=tags, add_sensor=add, ch_fatigue=None,
update=update, saveinterval=saveinterval,
- suffix=suffix, fatigue_cycles=fatigue_cycles,
+ suffix=suffix, save_new_sigs=save_new_sigs,
csv=csv, m=m, neq=neq, no_bins=no_bins,
- chs_resultant=chs_resultant, A=A,
- save_new_sigs=save_new_sigs)
+ chs_resultant=chs_resultant, A=A)
# annual energy production
- df_AEP = cc.AEP(df_stats, csv=csv, update=update, save=True)
+ if AEP:
+ df_AEP = cc.AEP(df_stats, csv=csv, update=update, save=True)
if envelopeblade:
ch_list = []
@@ -395,6 +398,9 @@ if __name__ == '__main__':
dest='stats', help='calculate statistics')
parser.add_argument('--fatigue', action='store_true', default=False,
dest='fatigue', help='calculate Leq for a full DLC')
+ parser.add_argument('--AEP', action='store_true', default=False,
+ dest='AEP', help='calculate AEP, requires '
+ 'htc/DLCs/dlc_config.xlsx')
parser.add_argument('--csv', action='store_true', default=False,
dest='csv', help='Save data also as csv file')
parser.add_argument('--years', type=float, default=20.0, action='store',
@@ -429,24 +435,26 @@ if __name__ == '__main__':
# --plots, --report, --...
# -------------------------------------------------------------------------
-# # manually configure all the dirs
-# p_root_remote = '/mnt/hawc2sim'
-# p_root_local = '/home/dave/DTU/Projects/AVATAR/'
+# # 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 = '/mnt/hawc2sim/'
+# p_root_local = '/mnt/hawc2sim/'
# # project name, sim_id, master file name
-# PROJECT = 'DTU10MW'
-# sim_id = 'C0014'
-# MASTERFILE = 'dtu10mw_master_C0014.htc'
+# PROJECT = 'demo'
+# sim_id = 'A0001'
+# MASTERFILE = 'dtu10mw_avatar_master_A0001.htc'
# # MODEL SOURCES, exchanche file sources
# P_RUN = os.path.join(p_root_remote, PROJECT, sim_id+'/')
-# P_SOURCE = os.path.join(p_root_local, PROJECT)
+# P_SOURCE = os.path.join(p_root_local, PROJECT, sim_id)
# # location of the master file
-# P_MASTERFILE = os.path.join(p_root_local, PROJECT, 'htc', '_master/')
+# P_MASTERFILE = os.path.join(p_root_local, PROJECT, sim_id, 'htc', '_master/')
# # location of the pre and post processing data
-# POST_DIR = os.path.join(p_root_remote, PROJECT, 'python-prepost-data/')
+# POST_DIR = os.path.join(p_root_remote, PROJECT, sim_id, 'prepost-data/')
# force_dir = P_RUN
# launch_dlcs_excel(sim_id)
# post_launch(sim_id, check_logs=True, update=False, force_dir=force_dir,
-# saveinterval=2000, csv=False)
+# saveinterval=2000, csv=True, fatigue_cycles=True, fatigue=False)
# -------------------------------------------------------------------------
# create HTC files and PBS launch scripts (*.p)
@@ -458,7 +466,7 @@ if __name__ == '__main__':
post_launch(sim_id, check_logs=opt.check_logs, update=False,
force_dir=P_RUN, saveinterval=2000, csv=opt.csv,
statistics=opt.stats, years=opt.years, neq=opt.neq,
- fatigue=opt.fatigue, fatigue_cycles=True, A=opt.rotarea,
+ fatigue=opt.fatigue, A=opt.rotarea, AEP=opt.AEP,
no_bins=opt.no_bins, nn_blr=opt.nn_blr, nn_twt=opt.nn_twt,
save_new_sigs=opt.save_new_sigs, save_iter=False,
envelopeturbine=opt.envelopeturbine,
diff --git a/wetb/prepost/misc.py b/wetb/prepost/misc.py
index 441e20c1c500c7ca879e3eb22e95ec404545e068..0c1ab9b0d9c3b95738847d0c5d7127027d453d43 100644
--- a/wetb/prepost/misc.py
+++ b/wetb/prepost/misc.py
@@ -678,7 +678,7 @@ def to_lower_case(proot):
os.rename(root, new)
def read_excel_files(proot, fext='xlsx', pignore=None, sheet=0,
- pinclude=None):
+ pinclude=None, silent=False):
"""
Read recursively all MS Excel files with extension "fext". Only the
default name for the first sheet (Sheet1) of the Excel file is considered.
@@ -726,14 +726,17 @@ def read_excel_files(proot, fext='xlsx', pignore=None, sheet=0,
# if it does contain pignore, ingore the dlc
if pignore is not None and f_target.find(pignore) > -1:
continue
- print(f_target, end='')
+ if not silent:
+ print(f_target, end='')
try:
xl = pd.ExcelFile(f_target)
df = xl.parse(sheet)
df_list[f_target.replace('.'+fext, '')] = df
- print(': sucesfully included %i case(s)' % len(df))
+ if not silent:
+ print(': sucesfully included %i case(s)' % len(df))
except:
- print(' XXXXX ERROR COULD NOT READ')
+ if not silent:
+ print(' XXXXX ERROR COULD NOT READ')
return df_list
diff --git a/wetb/prepost/tests/data/demo_dlc/ref/control/minimal_demo_file.txt b/wetb/prepost/tests/data/demo_dlc/ref/control/minimal_demo_file.txt
new file mode 100644
index 0000000000000000000000000000000000000000..8db2621539988442dd84f09006b47d9b6ed08690
--- /dev/null
+++ b/wetb/prepost/tests/data/demo_dlc/ref/control/minimal_demo_file.txt
@@ -0,0 +1 @@
+just one demo line
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 0000000000000000000000000000000000000000..8db2621539988442dd84f09006b47d9b6ed08690
--- /dev/null
+++ b/wetb/prepost/tests/data/demo_dlc/ref/data/minimal_demo_file.txt
@@ -0,0 +1 @@
+just one demo line
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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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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 0000000000000000000000000000000000000000..6e956f80d62257709ddd129408b8d77305da4339
--- /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 0000000000000000000000000000000000000000..c54c20d0df50daf94a80962feaefcd924123559f
--- /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 0000000000000000000000000000000000000000..94abe5e13faf4dbd2ffcf86f0bb95df884a573a8
--- /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 0000000000000000000000000000000000000000..537e8ef73085b26598c46f2986c11fc8ad738464
--- /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 0000000000000000000000000000000000000000..1bc115f781b7821f729e97bddcf49683bb623c20
--- /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 0000000000000000000000000000000000000000..640e5c20ec09f6f50b5a6002586bd030b96604c9
--- /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 0000000000000000000000000000000000000000..a9d5ef524b9feddbadd7df3e08d7873cc39fe96d
--- /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/remote.pkl b/wetb/prepost/tests/data/demo_dlc/ref/prepost/remote.pkl
new file mode 100644
index 0000000000000000000000000000000000000000..424870abe4d235d40b0bc86884127247ace71cde
Binary files /dev/null and b/wetb/prepost/tests/data/demo_dlc/ref/prepost/remote.pkl differ
diff --git a/wetb/prepost/tests/data/demo_dlc/ref/prepost/remote_tags.txt b/wetb/prepost/tests/data/demo_dlc/ref/prepost/remote_tags.txt
new file mode 100644
index 0000000000000000000000000000000000000000..21c9f3dd8e9452763faab41e0e8920e87c22a63d
--- /dev/null
+++ b/wetb/prepost/tests/data/demo_dlc/ref/prepost/remote_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] : []
+
+-------------------------------------------------------------------------------
+ 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] : []
+
+-------------------------------------------------------------------------------
+ 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] : []
diff --git a/wetb/prepost/tests/data/demo_dlc/source/control/minimal_demo_file.txt b/wetb/prepost/tests/data/demo_dlc/source/control/minimal_demo_file.txt
new file mode 100644
index 0000000000000000000000000000000000000000..8db2621539988442dd84f09006b47d9b6ed08690
--- /dev/null
+++ b/wetb/prepost/tests/data/demo_dlc/source/control/minimal_demo_file.txt
@@ -0,0 +1 @@
+just one demo line
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 0000000000000000000000000000000000000000..8db2621539988442dd84f09006b47d9b6ed08690
--- /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
new file mode 100644
index 0000000000000000000000000000000000000000..60fe434ad3dc15cf5e1dd1977c630107c611ac55
Binary files /dev/null and b/wetb/prepost/tests/data/demo_dlc/source/demo_dlc_remote.zip differ
diff --git a/wetb/prepost/tests/data/demo_dlc/source/htc/DLCs/dlc01_demos.xlsx b/wetb/prepost/tests/data/demo_dlc/source/htc/DLCs/dlc01_demos.xlsx
new file mode 100755
index 0000000000000000000000000000000000000000..1f4c2311367ccea9d06f57db32793e8948f0e959
Binary files /dev/null and b/wetb/prepost/tests/data/demo_dlc/source/htc/DLCs/dlc01_demos.xlsx differ
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 0000000000000000000000000000000000000000..6e956f80d62257709ddd129408b8d77305da4339
--- /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 0000000000000000000000000000000000000000..61628546afc1110717316b1ec79f6269a2926fc5
--- /dev/null
+++ b/wetb/prepost/tests/test_Simulations.py
@@ -0,0 +1,69 @@
+'''
+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
+import pickle
+
+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 = 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, tmpl.PROJECT, 'remote/')
+ tmpl.P_SOURCE = os.path.join(p_root, tmpl.PROJECT, 'source/')
+ # location of the master file
+ tmpl.P_MASTERFILE = os.path.join(p_root, tmpl.PROJECT,
+ 'source', 'htc', '_master/')
+ # location of the pre and post processing data
+ tmpl.POST_DIR = os.path.join(p_root, tmpl.PROJECT, 'remote',
+ 'prepost/')
+ tmpl.force_dir = tmpl.P_RUN
+ tmpl.launch_dlcs_excel('remote', silent=True)
+
+ # we can not check-in empty dirs in git
+ for subdir in ['control', 'data', 'htc', 'pbs_in']:
+ remote = os.path.join(p_root, tmpl.PROJECT, 'remote', subdir)
+ ref = os.path.join(p_root, tmpl.PROJECT, 'ref', subdir)
+ 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)
+
+ # for the pickled file we can just read it
+ remote = os.path.join(p_root, tmpl.PROJECT, 'remote', 'prepost')
+ ref = os.path.join(p_root, tmpl.PROJECT, 'ref', 'prepost')
+ cmp = filecmp.cmp(os.path.join(remote, 'remote_tags.txt'),
+ os.path.join(ref, 'remote_tags.txt'), shallow=False)
+ self.assertTrue(cmp)
+# with open(os.path.join(remote, 'remote.pkl'), 'rb') as FILE:
+# pkl_remote = pickle.load(FILE)
+# with open(os.path.join(ref, 'remote.pkl'), 'rb') as FILE:
+# pkl_ref = pickle.load(FILE)
+# self.assertTrue(pkl_remote == pkl_ref)
+
+
+if __name__ == "__main__":
+ unittest.main()
diff --git a/wetb/prepost/windIO.py b/wetb/prepost/windIO.py
index 5c38c195d772b9eb74eba2f86c53c504060572ae..170e6e1d8f943ec3fa02b87556b3cb3774b65774 100755
--- a/wetb/prepost/windIO.py
+++ b/wetb/prepost/windIO.py
@@ -17,10 +17,6 @@ from future import standard_library
standard_library.install_aliases()
from builtins import object
- # always devide as floats
-
-#print(*objects, sep=' ', end='\n', file=sys.stdout)
-
__author__ = 'David Verelst'
__license__ = 'GPL'
__version__ = '0.5'
@@ -32,24 +28,20 @@ import math
from time import time
import codecs
-import scipy
import scipy.integrate as integrate
-import array
import numpy as np
import pandas as pd
-#import sympy
-
# misc is part of prepost, which is available on the dtu wind gitlab server:
# https://gitlab.windenergy.dtu.dk/dave/prepost
from wetb.prepost import misc
# wind energy python toolbox, available on the dtu wind redmine server:
# http://vind-redmine.win.dtu.dk/projects/pythontoolbox/repository/show/fatigue_tools
-from wetb.fatigue_tools.rainflowcounting.rainflowcount import rainflow_astm as rainflow_astm
-from wetb.fatigue_tools.rainflowcounting.rfc_hist import rfc_hist as rfc_hist
+from wetb.hawc2.Hawc2io import ReadHawc2
+from wetb.fatigue_tools.fatigue import eq_load
-class LoadResults(object):
+class LoadResults(ReadHawc2):
"""Read a HAWC2 result data file
Usage:
@@ -126,215 +118,34 @@ class LoadResults(object):
self.file_path = file_path
# remove .log, .dat, .sel extensions who might be accedental left
- if file_name[-4:] in ['.htc','.sel','.dat','.log']:
+ if file_name[-4:] in ['.htc', '.sel', '.dat', '.log']:
file_name = file_name[:-4]
-
+ # FIXME: since HAWC2 will always have lower case output files, convert
+ # any wrongly used upper case letters to lower case here
self.file_name = file_name
- self.read_sel()
- # create for any supported channel the
- # continue if the file has been succesfully read
- if self.error_msg == 'none':
- # load the channel id's and scale factors
- self.scale_factors = self.data_sel()
- # with the sel file loaded, we have all the channel names to
- # squeeze into a more consistant naming scheme
- self._unified_channel_names()
- # only read when asked for
- if readdata:
- # if there is sel file but it is empty or whatever else
- # FilType will not exists
- try:
- # read the binary file
- if self.FileType == 'BINARY':
- self.read_bin(self.scale_factors, usecols=usecols)
- # read the ASCII file
- elif self.FileType == 'ASCII':
- self.read_ascii(usecols=usecols)
- else:
- print('='*79)
- print('unknown file type: ' + self.FileType)
- print('='*79)
- self.error_msg = 'error: unknown file type'
- self.sig = []
- except:
- print('='*79)
- print('couldn\'t determine FileType')
- print('='*79)
- self.error_msg = 'error: no file type'
- self.sig = []
+ FileName = os.path.join(self.file_path, self.file_name)
- if self.debug:
- stop = time() - start
- print('time to load HAWC2 file:', stop, 's')
+ ReadOnly = 0 if readdata else 1
+ super(LoadResults, self).__init__(FileName, ReadOnly=ReadOnly)
+ self.FileType = self.FileFormat[6:]
+ self.N = int(self.NrSc)
+ self.Nch = int(self.NrCh)
+ self.ch_details = np.ndarray(shape=(self.Nch, 3), dtype='<U100')
+ for ic in range(self.Nch):
+ self.ch_details[ic, 0] = self.ChInfo[0][ic]
+ self.ch_details[ic, 1] = self.ChInfo[1][ic]
+ self.ch_details[ic, 2] = self.ChInfo[2][ic]
- def read_sel(self):
- # anticipate error on file reading
- try:
- # open file, read and close
- go_sel = os.path.join(self.file_path, self.file_name + '.sel')
- FILE = opent(go_sel, "r")
- self.lines = FILE.readlines()
- FILE.close()
- self.error_msg = 'none'
-
- # error message if the file does not exists
- except:
- # print(26*' ' + 'ERROR'
- print(50*'=')
- print(self.file_path)
- print(self.file_name + '.sel could not be found')
- print(50*'=')
- self.error_msg = 'error: file not found'
-
- def data_sel(self):
-
- # scan through all the lines in the file
- line_nr = 1
- # channel counter for ch_details
- ch = 0
- for line in self.lines:
- # on line 9 we can read following paramaters:
- if line_nr == 9:
- # remove the end of line character
- line = line.replace('\n','').replace('\r', '')
-
- settings = line.split(' ')
- # delete all empty string values
- for k in range(settings.count('')):
- settings.remove('')
-
- # and assign proper values with correct data type
- self.N = int(settings[0])
- self.Nch = int(settings[1])
- self.Time = float(settings[2])
- self.FileType = settings[3]
- self.Freq = self.N/self.Time
-
- # prepare list variables
- self.ch_details = np.ndarray(shape=(self.Nch,3),dtype='<U100')
- # it seems that float64 reeds the data correctly from the file
- scale_factors = scipy.zeros(self.Nch, dtype='Float64')
- #self.scale_factors_dec = scipy.zeros(self.Nch, dtype='f8')
- i = 0
-
- # starting from line 13, we have the channels info
- if line_nr > 12:
- # read the signal details
- if line_nr < 13 + self.Nch:
- # remove leading and trailing whitespaces from line parts
- self.ch_details[ch,0] = str(line[12:43]).strip() # chID
- self.ch_details[ch,1] = str(line[43:54]).strip() # chUnits
- self.ch_details[ch,2] = str(line[54:-1]).strip() # chDescr
- ch += 1
- # read the signal scale parameters for binary format
- elif line_nr > 14 + self.Nch:
- scale_factors[i] = line
- # print(scale_factors[i]
- #self.scale_factors_dec[i] = D.Decimal(line)
- i = i + 1
- # stop going through the lines if at the end of the file
- if line_nr == 2*self.Nch + 14:
- self.scale_factors = scale_factors
-
- if self.debug:
- print('N ', self.N)
- print('Nch ', self.Nch)
- print('Time ', self.Time)
- print('FileType', self.FileType)
- print('Freq ', self.Freq)
- print('scale_factors', scale_factors.shape)
-
- return scale_factors
- break
+ ChVec = [] if usecols is None else usecols
- # counting the line numbers
- line_nr = line_nr + 1
+ self._unified_channel_names()
+ if readdata:
+ self.sig = super(LoadResults, self).__call__(ChVec=ChVec)
- def read(self, usecols=False):
- """
- This whole LoadResults needs to be refactered because it is crap.
- Keep the old ones for backwards compatibility
- """
-
- if self.FileType == 'ASCII':
- self.read_ascii(usecols=usecols)
- elif self.FileType == 'BINARY':
- self.read_bin(self.scale_factors, usecols=usecols)
-
- def read_bin(self, scale_factors, usecols=False):
- if not usecols:
- usecols = list(range(0, self.Nch))
- fid = open(os.path.join(self.file_path, self.file_name) + '.dat', 'rb')
- self.sig = np.zeros( (self.N, len(usecols)) )
- for j, i in enumerate(usecols):
- fid.seek(i*self.N*2,0)
- self.sig[:,j] = np.fromfile(fid, 'int16', self.N)*scale_factors[i]
-
- def read_bin_old(self, scale_factors):
- # if there is an error reading the binary file (for instance if empty)
- try:
- # read the binary file
- go_binary = os.path.join(self.file_path, self.file_name) + '.dat'
- FILE = open(go_binary, mode='rb')
-
- # create array, put all the binary elements as one long chain in it
- binvalues = array.array('h')
- binvalues.fromfile(FILE, self.N * self.Nch)
- FILE.close()
- # convert now to a structured numpy array
- # sig = np.array(binvalues, np.float)
-# sig = np.array(binvalues)
- # this is faster! the saved bin values are only of type int16
- sig = np.array(binvalues, dtype='int16')
-
- if self.debug: print(self.N, self.Nch, sig.shape)
-
-# sig = np.reshape(sig, (self.Nch, self.N))
-# # apperently Nch and N had to be reversed to read it correctly
-# # is this because we are reading a Fortran array with Python C
-# # code? so now transpose again so we have sig(time, channel)
-# sig = np.transpose(sig)
-
- # reshape the array to 2D and transpose (Fortran to C array)
- sig = sig.reshape((self.Nch, self.N)).T
-
- # create diagonal vector of size (Nch,Nch)
- dig = np.diag(scale_factors)
- # now all rows of column 1 are multiplied with dig(1,1)
- sig = np.dot(sig,dig)
- self.sig = sig
- # 'file name;' + 'lnr;msg;'*(len(MsgList)) + '\n'
- except:
- self.sig = []
- self.error_msg = 'error: reading binary file failed'
- print('========================================================')
- print(self.error_msg)
- print(self.file_path)
- print(self.file_name)
- print('========================================================')
-
- def read_ascii(self, usecols=None):
+ if self.debug:
+ stop = time() - start
+ print('time to load HAWC2 file:', stop, 's')
- try:
- go_ascii = os.path.join(self.file_path, self.file_name) + '.dat'
-# self.sig = np.genfromtxt(go_ascii)
- self.sig = np.loadtxt(go_ascii, usecols=usecols)
-# self.sig = np.fromfile(go_ascii, dtype=np.float32, sep=' ')
-# self.sig = self.sig.reshape((self.N, self.Nch))
- except:
- self.sig = []
- self.error_msg = 'error: reading ascii file failed'
- print('========================================================')
- print(self.error_msg)
- print(self.file_path)
- print(self.file_name)
- print('========================================================')
-
-# print '========================================================'
-# print 'ASCII reading not implemented yet'
-# print '========================================================'
-# self.sig = []
-# self.error_msg = 'error: ASCII reading not implemented yet'
def reformat_sig_details(self):
"""Change HAWC2 output description of the channels short descriptive
@@ -345,7 +156,7 @@ class LoadResults(object):
# CONFIGURATION: mappings between HAWC2 and short good output:
change_list = []
- change_list.append( ['original','new improved'] )
+ change_list.append( ['original', 'new improved'] )
# change_list.append( ['Mx coo: hub1','blade1 root bending: flap'] )
# change_list.append( ['My coo: hub1','blade1 root bending: edge'] )
@@ -359,41 +170,41 @@ class LoadResults(object):
# change_list.append( ['My coo: hub3','blade3 root bending: edge'] )
# change_list.append( ['Mz coo: hub3','blade3 root bending: torsion'] )
- change_list.append( ['Mx coo: blade1','blade1 flap'] )
- change_list.append( ['My coo: blade1','blade1 edge'] )
- change_list.append( ['Mz coo: blade1','blade1 torsion'] )
+ change_list.append(['Mx coo: blade1', 'blade1 flap'])
+ change_list.append(['My coo: blade1', 'blade1 edge'])
+ change_list.append(['Mz coo: blade1', 'blade1 torsion'])
- change_list.append( ['Mx coo: blade2','blade2 flap'] )
- change_list.append( ['My coo: blade2','blade2 edge'] )
- change_list.append( ['Mz coo: blade2','blade2 torsion'] )
+ change_list.append(['Mx coo: blade2', 'blade2 flap'])
+ change_list.append(['My coo: blade2', 'blade2 edge'])
+ change_list.append(['Mz coo: blade2', 'blade2 torsion'])
- change_list.append( ['Mx coo: blade3','blade3 flap'] )
- change_list.append( ['My coo: blade3','blade3 edeg'] )
- change_list.append( ['Mz coo: blade3','blade3 torsion'] )
+ change_list.append(['Mx coo: blade3', 'blade3 flap'])
+ change_list.append(['My coo: blade3', 'blade3 edeg'])
+ change_list.append(['Mz coo: blade3', 'blade3 torsion'])
- change_list.append( ['Mx coo: hub1','blade1 out-of-plane'] )
- change_list.append( ['My coo: hub1','blade1 in-plane'] )
- change_list.append( ['Mz coo: hub1','blade1 torsion'] )
+ change_list.append(['Mx coo: hub1', 'blade1 out-of-plane'])
+ change_list.append(['My coo: hub1', 'blade1 in-plane'])
+ change_list.append(['Mz coo: hub1', 'blade1 torsion'])
- change_list.append( ['Mx coo: hub2','blade2 out-of-plane'] )
- change_list.append( ['My coo: hub2','blade2 in-plane'] )
- change_list.append( ['Mz coo: hub2','blade2 torsion'] )
+ change_list.append(['Mx coo: hub2', 'blade2 out-of-plane'])
+ change_list.append(['My coo: hub2', 'blade2 in-plane'])
+ change_list.append(['Mz coo: hub2', 'blade2 torsion'])
- change_list.append( ['Mx coo: hub3','blade3 out-of-plane'] )
- change_list.append( ['My coo: hub3','blade3 in-plane'] )
- change_list.append( ['Mz coo: hub3','blade3 torsion'] )
+ change_list.append(['Mx coo: hub3', 'blade3 out-of-plane'])
+ change_list.append(['My coo: hub3', 'blade3 in-plane'])
+ change_list.append(['Mz coo: hub3', 'blade3 torsion'])
# this one will create a false positive for tower node nr1
- change_list.append( ['Mx coo: tower','tower top momemt FA'] )
- change_list.append( ['My coo: tower','tower top momemt SS'] )
- change_list.append( ['Mz coo: tower','yaw-moment'] )
+ change_list.append(['Mx coo: tower', 'tower top momemt FA'])
+ change_list.append(['My coo: tower', 'tower top momemt SS'])
+ change_list.append(['Mz coo: tower', 'yaw-moment'])
- change_list.append( ['Mx coo: chasis','chasis momemt FA'] )
- change_list.append( ['My coo: chasis','yaw-moment chasis'] )
- change_list.append( ['Mz coo: chasis','chasis moment SS'] )
+ change_list.append(['Mx coo: chasis', 'chasis momemt FA'])
+ change_list.append(['My coo: chasis', 'yaw-moment chasis'])
+ change_list.append(['Mz coo: chasis', 'chasis moment SS'])
- change_list.append( ['DLL inp 2: 2','tower clearance'] )
+ change_list.append(['DLL inp 2: 2', 'tower clearance'])
- self.ch_details_new = np.ndarray(shape=(self.Nch,3),dtype='<U100')
+ self.ch_details_new = np.ndarray(shape=(self.Nch, 3), dtype='<U100')
# approach: look for a specific description and change it.
# This approach is slow, but will not fail if the channel numbers change
@@ -401,10 +212,10 @@ class LoadResults(object):
for ch in range(self.Nch):
# the change_list will always be slower, so this loop will be
# inside the bigger loop of all channels
- self.ch_details_new[ch,:] = self.ch_details[ch,:]
+ self.ch_details_new[ch, :] = self.ch_details[ch, :]
for k in range(len(change_list)):
- if change_list[k][0] == self.ch_details[ch,0]:
- self.ch_details_new[ch,0] = change_list[k][1]
+ if change_list[k][0] == self.ch_details[ch, 0]:
+ self.ch_details_new[ch, 0] = change_list[k][1]
# channel description should be unique, so delete current
# entry and stop looking in the change list
del change_list[k]
@@ -483,7 +294,7 @@ class LoadResults(object):
# some channel ID's are unique, use them
ch_unique = set(['Omega', 'Ae rot. torque', 'Ae rot. power',
- 'Ae rot. thrust', 'Time', 'Azi 1'])
+ 'Ae rot. thrust', 'Time', 'Azi 1'])
ch_aero = set(['Cl', 'Cd', 'Alfa', 'Vrel', 'Tors_e', 'Alfa'])
ch_aerogrid = set(['a_grid', 'am_grid'])
@@ -492,13 +303,13 @@ class LoadResults(object):
# 'component', 'pos', 'coord', 'sensortype', 'radius',
# 'blade_nr', 'units', 'output_type', 'io_nr', 'io', 'dll',
# 'azimuth', 'flap_nr'])
- df_dict = {col:[] for col in self.cols}
+ df_dict = {col: [] for col in self.cols}
df_dict['ch_name'] = []
# scan through all channels and see which can be converted
# to sensible unified name
for ch in range(self.Nch):
- items = self.ch_details[ch,2].split(' ')
+ items = self.ch_details[ch, 2].split(' ')
# remove empty values in the list
items = misc.remove_items(items, '')
@@ -511,24 +322,24 @@ class LoadResults(object):
# -----------------------------------------------------------------
# check for all the unique channel descriptions
if self.ch_details[ch,0].strip() in ch_unique:
- tag = self.ch_details[ch,0].strip()
+ tag = self.ch_details[ch, 0].strip()
channelinfo = {}
- channelinfo['units'] = self.ch_details[ch,1]
- channelinfo['sensortag'] = self.ch_details[ch,2]
+ channelinfo['units'] = self.ch_details[ch, 1]
+ channelinfo['sensortag'] = self.ch_details[ch, 2]
channelinfo['chi'] = ch
# -----------------------------------------------------------------
# or in the long description:
# 0 1 2 3 4 5 6 and up
# MomentMz Mbdy:blade nodenr: 5 coo: blade TAG TEXT
- elif self.ch_details[ch,2].startswith('MomentM'):
+ elif self.ch_details[ch, 2].startswith('MomentM'):
coord = items[5]
bodyname = items[1].replace('Mbdy:', '')
# set nodenr to sortable way, include leading zeros
# node numbers start with 0 at the root
nodenr = '%03i' % int(items[3])
# skip the attached the component
- #sensortype = items[0][:-2]
+ # sensortype = items[0][:-2]
# or give the sensor type the same name as in HAWC2
sensortype = 'momentvec'
component = items[0][-1:len(items[0])]
@@ -540,7 +351,7 @@ class LoadResults(object):
# and tag it
pos = 'node-%s' % nodenr
- tagitems = (coord,bodyname,pos,sensortype,component)
+ tagitems = (coord, bodyname, pos, sensortype, component)
tag = '%s-%s-%s-%s-%s' % tagitems
# save all info in the dict
channelinfo = {}
@@ -551,17 +362,17 @@ class LoadResults(object):
channelinfo['component'] = component
channelinfo['chi'] = ch
channelinfo['sensortag'] = sensortag
- channelinfo['units'] = self.ch_details[ch,1]
+ channelinfo['units'] = self.ch_details[ch, 1]
# -----------------------------------------------------------------
# 0 1 2 3 4 5 6 7 and up
# Force Fx Mbdy:blade nodenr: 2 coo: blade TAG TEXT
- elif self.ch_details[ch,2].startswith('Force'):
+ elif self.ch_details[ch, 2].startswith('Force'):
coord = items[6]
bodyname = items[2].replace('Mbdy:', '')
nodenr = '%03i' % int(items[4])
# skipe the attached the component
- #sensortype = items[0]
+ # sensortype = items[0]
# or give the sensor type the same name as in HAWC2
sensortype = 'forcevec'
component = items[1][1]
@@ -572,7 +383,7 @@ class LoadResults(object):
# and tag it
pos = 'node-%s' % nodenr
- tagitems = (coord,bodyname,pos,sensortype,component)
+ tagitems = (coord, bodyname, pos, sensortype, component)
tag = '%s-%s-%s-%s-%s' % tagitems
# save all info in the dict
channelinfo = {}
@@ -583,7 +394,7 @@ class LoadResults(object):
channelinfo['component'] = component
channelinfo['chi'] = ch
channelinfo['sensortag'] = sensortag
- channelinfo['units'] = self.ch_details[ch,1]
+ channelinfo['units'] = self.ch_details[ch, 1]
# -----------------------------------------------------------------
# 0 1 2 3 4 5 6 7 8
@@ -604,7 +415,7 @@ class LoadResults(object):
# skip the attached the component
#sensortype = ''.join(items[0:2])
# or give the sensor type the same name as in HAWC2
- tmp = self.ch_details[ch,0].split(' ')
+ tmp = self.ch_details[ch, 0].split(' ')
sensortype = tmp[0]
if sensortype.startswith('State'):
sensortype += ' ' + tmp[1]
@@ -616,7 +427,7 @@ class LoadResults(object):
# and tag it
pos = 'elem-%s-zrel-%s' % (elementnr, zrel)
- tagitems = (coord,bodyname,pos,sensortype,component)
+ tagitems = (coord, bodyname, pos, sensortype, component)
tag = '%s-%s-%s-%s-%s' % tagitems
# save all info in the dict
channelinfo = {}
@@ -627,7 +438,7 @@ class LoadResults(object):
channelinfo['component'] = component
channelinfo['chi'] = ch
channelinfo['sensortag'] = sensortag
- channelinfo['units'] = self.ch_details[ch,1]
+ channelinfo['units'] = self.ch_details[ch, 1]
# -----------------------------------------------------------------
# DLL CONTROL I/O
@@ -645,17 +456,17 @@ class LoadResults(object):
# description case 3
# 0 1 2 4
# hawc_dll :echo outvec : 1
- elif self.ch_details[ch,0].startswith('DLL'):
+ elif self.ch_details[ch, 0].startswith('DLL'):
# case 3
if items[1][0] == ':echo':
# hawc_dll named case (case 3) is polluted with colons
- items = self.ch_details[ch,2].replace(':','')
+ items = self.ch_details[ch,2].replace(':', '')
items = items.split(' ')
items = misc.remove_items(items, '')
dll = items[1]
io = items[2]
io_nr = items[3]
- tag = 'DLL-%s-%s-%s' % (dll,io,io_nr)
+ tag = 'DLL-%s-%s-%s' % (dll, io, io_nr)
sensortag = ''
# case 2: no reference to dll name
elif self.ch_details[ch,2].startswith('DLL'):
@@ -671,7 +482,7 @@ class LoadResults(object):
io = items[1]
io_nr = items[2]
sensortag = ' '.join(items[3:])
- tag = 'DLL-%s-%s-%s' % (dll,io,io_nr)
+ tag = 'DLL-%s-%s-%s' % (dll, io, io_nr)
# save all info in the dict
channelinfo = {}
@@ -680,19 +491,19 @@ class LoadResults(object):
channelinfo['io_nr'] = io_nr
channelinfo['chi'] = ch
channelinfo['sensortag'] = sensortag
- channelinfo['units'] = self.ch_details[ch,1]
+ channelinfo['units'] = self.ch_details[ch, 1]
# -----------------------------------------------------------------
# BEARING OUTPUS
# bea1 angle_speed rpm shaft_nacelle angle speed
- elif self.ch_details[ch,0].startswith('bea'):
- output_type = self.ch_details[ch,0].split(' ')[1]
+ elif self.ch_details[ch, 0].startswith('bea'):
+ output_type = self.ch_details[ch, 0].split(' ')[1]
bearing_name = items[0]
- units = self.ch_details[ch,1]
+ units = self.ch_details[ch, 1]
# there is no label option for the bearing output
# and tag it
- tag = 'bearing-%s-%s-%s' % (bearing_name,output_type,units)
+ tag = 'bearing-%s-%s-%s' % (bearing_name, output_type, units)
# save all info in the dict
channelinfo = {}
channelinfo['bearing_name'] = bearing_name
@@ -704,20 +515,20 @@ class LoadResults(object):
# AERO CL, CD, CM, VREL, ALFA, LIFT, DRAG, etc
# Cl, R= 0.5 deg Cl of blade 1 at radius 0.49
# Azi 1 deg Azimuth of blade 1
- elif self.ch_details[ch,0].split(',')[0] in ch_aero:
- dscr_list = self.ch_details[ch,2].split(' ')
+ elif self.ch_details[ch, 0].split(',')[0] in ch_aero:
+ dscr_list = self.ch_details[ch, 2].split(' ')
dscr_list = misc.remove_items(dscr_list, '')
- sensortype = self.ch_details[ch,0].split(',')[0]
+ sensortype = self.ch_details[ch, 0].split(',')[0]
radius = dscr_list[-1]
# is this always valid?
- blade_nr = self.ch_details[ch,2].split('blade ')[1][0]
+ blade_nr = self.ch_details[ch, 2].split('blade ')[1][0]
# sometimes the units for aero sensors are wrong!
- units = self.ch_details[ch,1]
+ units = self.ch_details[ch, 1]
# there is no label option
# and tag it
- tag = '%s-%s-%s' % (sensortype,blade_nr,radius)
+ tag = '%s-%s-%s' % (sensortype, blade_nr, radius)
# save all info in the dict
channelinfo = {}
channelinfo['sensortype'] = sensortype
@@ -729,14 +540,14 @@ class LoadResults(object):
# -----------------------------------------------------------------
# for the induction grid over the rotor
# a_grid, azi 0.00 r 1.74
- elif self.ch_details[ch,0].split(',')[0] in ch_aerogrid:
- items = self.ch_details[ch,0].split(',')
+ elif self.ch_details[ch, 0].split(',')[0] in ch_aerogrid:
+ items = self.ch_details[ch, 0].split(',')
sensortype = items[0]
items2 = items[1].split(' ')
items2 = misc.remove_items(items2, '')
azi = items2[1]
radius = items2[3]
- units = self.ch_details[ch,1]
+ units = self.ch_details[ch, 1]
# and tag it
tag = '%s-azi-%s-r-%s' % (sensortype,azi,radius)
# save all info in the dict
@@ -756,15 +567,15 @@ class LoadResults(object):
# Induc. Vy, blco, R= 1.4 // Induced wsp Vy of blade 1 at radius 1.37, local bl coo.
# Induc. Vz, glco, R= 1.4 // Induced wsp Vz of blade 1 at radius 1.37, global coo.
# Induc. Vx, rpco, R= 8.4 // Induced wsp Vx of blade 1 at radius 8.43, RP. coo.
- elif self.ch_details[ch,0].strip()[:5] == 'Induc':
- items = self.ch_details[ch,2].split(' ')
+ elif self.ch_details[ch, 0].strip()[:5] == 'Induc':
+ items = self.ch_details[ch, 2].split(' ')
items = misc.remove_items(items, '')
blade_nr = int(items[5])
radius = float(items[8].replace(',', ''))
- items = self.ch_details[ch,0].split(',')
+ items = self.ch_details[ch, 0].split(',')
coord = items[1].strip()
component = items[0][-2:]
- units = self.ch_details[ch,1]
+ units = self.ch_details[ch, 1]
# and tag it
rpl = (coord, blade_nr, component, radius)
tag = 'induc-%s-blade-%1i-%s-r-%03.02f' % rpl
@@ -787,8 +598,8 @@ class LoadResults(object):
# -----------------------------------------------------------------
# WATER SURFACE gl. coo, at gl. coo, x,y= 0.00, 0.00
- elif self.ch_details[ch,2].startswith('Water'):
- units = self.ch_details[ch,1]
+ elif self.ch_details[ch, 2].startswith('Water'):
+ units = self.ch_details[ch, 1]
# but remove the comma
x = items[-2][:-1]
@@ -806,10 +617,10 @@ class LoadResults(object):
# -----------------------------------------------------------------
# WIND SPEED
# WSP gl. coo.,Vx
- elif self.ch_details[ch,0].startswith('WSP gl.'):
- units = self.ch_details[ch,1]
- direction = self.ch_details[ch,0].split(',')[1]
- tmp = self.ch_details[ch,2].split('pos')[1]
+ elif self.ch_details[ch, 0].startswith('WSP gl.'):
+ units = self.ch_details[ch, 1]
+ direction = self.ch_details[ch, 0].split(',')[1]
+ tmp = self.ch_details[ch, 2].split('pos')[1]
x, y, z = tmp.split(',')
x, y, z = x.strip(), y.strip(), z.strip()
@@ -821,18 +632,16 @@ class LoadResults(object):
channelinfo['pos'] = (x, y, z)
channelinfo['units'] = units
channelinfo['chi'] = ch
- channelinfo['sensortype'] = 'windspeed'
- channelinfo['component'] = direction[1:]
# WIND SPEED AT BLADE
# 0: WSP Vx, glco, R= 61.5
# 2: Wind speed Vx of blade 1 at radius 61.52, global coo.
- elif self.ch_details[ch,0].startswith('WSP V'):
- units = self.ch_details[ch,1].strip()
- direction = self.ch_details[ch,0].split(' ')[1].strip()
- blade_nr = self.ch_details[ch,2].split('blade')[1].strip()[:2]
- radius = self.ch_details[ch,2].split('radius')[1].split(',')[0]
- coord = self.ch_details[ch,2].split(',')[1].strip()
+ elif self.ch_details[ch, 0].startswith('WSP V'):
+ units = self.ch_details[ch, 1].strip()
+ direction = self.ch_details[ch, 0].split(' ')[1].strip()
+ blade_nr = self.ch_details[ch, 2].split('blade')[1].strip()[:2]
+ radius = self.ch_details[ch, 2].split('radius')[1].split(',')[0]
+ coord = self.ch_details[ch, 2].split(',')[1].strip()
radius = radius.strip()
blade_nr = blade_nr.strip()
@@ -851,11 +660,11 @@ class LoadResults(object):
# FLAP ANGLE
# 2: Flap angle for blade 3 flap number 1
- elif self.ch_details[ch,0][:7] == 'setbeta':
- units = self.ch_details[ch,1].strip()
- blade_nr = self.ch_details[ch,2].split('blade')[1].strip()
+ elif self.ch_details[ch, 0][:7] == 'setbeta':
+ units = self.ch_details[ch, 1].strip()
+ blade_nr = self.ch_details[ch, 2].split('blade')[1].strip()
blade_nr = blade_nr.split(' ')[0].strip()
- flap_nr = self.ch_details[ch,2].split(' ')[-1].strip()
+ flap_nr = self.ch_details[ch, 2].split(' ')[-1].strip()
radius = radius.strip()
blade_nr = blade_nr.strip()
@@ -917,7 +726,7 @@ class LoadResults(object):
for ch_name, channelinfo in self.ch_dict.items():
cols.update(set(channelinfo.keys()))
- df_dict = {col:[] for col in cols}
+ df_dict = {col: [] for col in cols}
df_dict['ch_name'] = []
for ch_name, channelinfo in self.ch_dict.items():
cols_ch = set(channelinfo.keys())
@@ -931,7 +740,6 @@ class LoadResults(object):
self.ch_df = pd.DataFrame(df_dict)
self.ch_df.set_index('chi', inplace=True)
-
def _data_window(self, nr_rev=None, time=None):
"""
Based on a time interval, create a proper slice object
@@ -977,7 +785,7 @@ class LoadResults(object):
i_range = int(self.Freq*time_range)
window = [0, time_range]
# in case the first datapoint is not at 0 seconds
- i_zero = int(self.sig[0,0]*self.Freq)
+ i_zero = int(self.sig[0, 0]*self.Freq)
slice_ = np.r_[i_zero:i_range+i_zero]
zoomtype = '_nrrev_' + format(nr_rev, '1.0f') + 'rev'
@@ -990,23 +798,23 @@ class LoadResults(object):
slice_ = np.r_[i_start:i_end]
window = [time[0], time[1]]
- zoomtype = '_zoom_%1.1f-%1.1fsec' % (time[0], time[1])
+ zoomtype = '_zoom_%1.1f-%1.1fsec' % (time[0], time[1])
return slice_, window, zoomtype, time_range
# TODO: general signal method, this is not HAWC2 specific, move out
- def calc_stats(self, sig, i0=0, i1=-1):
+ def calc_stats(self, sig, i0=0, i1=None):
stats = {}
# calculate the statistics values:
- stats['max'] = sig[i0:i1,:].max(axis=0)
- stats['min'] = sig[i0:i1,:].min(axis=0)
- stats['mean'] = sig[i0:i1,:].mean(axis=0)
- stats['std'] = sig[i0:i1,:].std(axis=0)
+ stats['max'] = sig[i0:i1, :].max(axis=0)
+ stats['min'] = sig[i0:i1, :].min(axis=0)
+ stats['mean'] = sig[i0:i1, :].mean(axis=0)
+ stats['std'] = sig[i0:i1, :].std(axis=0)
stats['range'] = stats['max'] - stats['min']
- stats['absmax'] = np.absolute(sig[i0:i1,:]).max(axis=0)
- stats['rms'] = np.sqrt(np.mean(sig[i0:i1,:]*sig[i0:i1,:], axis=0))
- stats['int'] = integrate.trapz(sig[i0:i1,:], x=sig[i0:i1,0], axis=0)
+ stats['absmax'] = np.absolute(sig[i0:i1, :]).max(axis=0)
+ stats['rms'] = np.sqrt(np.mean(sig[i0:i1, :]*sig[i0:i1, :], axis=0))
+ stats['int'] = integrate.trapz(sig[i0:i1, :], x=sig[i0:i1, 0], axis=0)
return stats
# TODO: general signal method, this is not HAWC2 specific, move out
@@ -1030,45 +838,7 @@ class LoadResults(object):
Damage equivalent loads for each m value.
"""
- try:
- sig_rf = rainflow_astm(signal)
- except (TypeError) as e:
- print(e)
- return []
-
- if len(sig_rf) < 1 and not sig_rf:
- return []
-
- hist_data, x, bin_avg = rfc_hist(sig_rf, no_bins)
- m = np.atleast_1d(m)
-
- eq = []
- for i in range(len(m)):
- eq.append(np.power(np.sum(0.5 * hist_data *\
- np.power(bin_avg, m[i])) / neq, 1. / m[i]))
- return eq
-
- # TODO: general signal method, this is not HAWC2 specific, move out
- def cycle_matrix(self, signal, no_bins=46, m=[3, 4, 6, 8, 10, 12]):
-
-# import fatigue_tools.fatigue as ft
-# cycles, ampl_bin_mean, ampl_bin_edges, mean_bin_mean, mean_edges \
-# = ft.cycle_matrix(signal, ampl_bins=no_bins, mean_bins=1,
-# rainflow_func=ft.rainflow_windap)
-# # in this case eq = sum( n_i*S_i^m )
-# return [np.sum(cycles * ampl_bin_mean ** _m) for _m in m]
-
- try:
- sig_rf = rainflow_astm(signal)
- except:
- return []
-
- if len(sig_rf) < 1 and not sig_rf:
- return []
-
- hist_data, x, bin_avg = rfc_hist(sig_rf, no_bins)
- m = np.atleast_1d(m)
- return [np.sum(0.5 * hist_data * bin_avg ** _m) for _m in m]
+ return eq_load(signal, no_bins=no_bins, m=m, neq=neq)[0]
def blade_deflection(self):
"""
@@ -1077,18 +847,18 @@ class LoadResults(object):
# select all the y deflection channels
db = misc.DictDB(self.ch_dict)
- db.search({'sensortype' : 'state pos', 'component' : 'z'})
+ db.search({'sensortype': 'state pos', 'component': 'z'})
# sort the keys and save the mean values to an array/list
chiz, zvals = [], []
for key in sorted(db.dict_sel.keys()):
- zvals.append(-self.sig[:,db.dict_sel[key]['chi']].mean())
+ zvals.append(-self.sig[:, db.dict_sel[key]['chi']].mean())
chiz.append(db.dict_sel[key]['chi'])
- db.search({'sensortype' : 'state pos', 'component' : 'y'})
+ db.search({'sensortype': 'state pos', 'component': 'y'})
# sort the keys and save the mean values to an array/list
chiy, yvals = [], []
for key in sorted(db.dict_sel.keys()):
- yvals.append(self.sig[:,db.dict_sel[key]['chi']].mean())
+ yvals.append(self.sig[:, db.dict_sel[key]['chi']].mean())
chiy.append(db.dict_sel[key]['chi'])
return np.array(zvals), np.array(yvals)
@@ -1113,7 +883,7 @@ class LoadResults(object):
# and save
print('saving...', end='')
- np.savetxt(fname, self.sig[:,list(map_sorting.keys())], fmt=fmt,
+ np.savetxt(fname, self.sig[:, list(map_sorting.keys())], fmt=fmt,
delimiter=delimiter, header=delimiter.join(header))
print(fname)
@@ -1170,26 +940,26 @@ def ReadEigenBody(fname, debug=False):
"""
- #Body data for body number : 3 with the name :nacelle
- #Results: fd [Hz] fn [Hz] log.decr [%]
- #Mode nr: 1: 1.45388E-21 1.74896E-03 6.28319E+02
+ # Body data for body number : 3 with the name :nacelle
+ # Results: fd [Hz] fn [Hz] log.decr [%]
+ # Mode nr: 1: 1.45388E-21 1.74896E-03 6.28319E+02
FILE = opent(fname)
lines = FILE.readlines()
FILE.close()
- df_dict = {'Fd_hz':[], 'Fn_hz':[], 'log_decr_pct':[], 'body':[]}
+ df_dict = {'Fd_hz': [], 'Fn_hz': [], 'log_decr_pct': [], 'body': []}
for i, line in enumerate(lines):
if debug: print('line nr: %5i' % i)
# identify for which body we will read the data
if line[:25] == 'Body data for body number':
body = line.split(':')[2].rstrip().lstrip()
# remove any annoying characters
- body = body.replace('\n','').replace('\r','')
+ body = body.replace('\n', '').replace('\r', '')
if debug: print('modes for body: %s' % body)
# identify mode number and read the eigenfrequencies
elif line[:8] == 'Mode nr:':
- linelist = line.replace('\n','').replace('\r','').split(':')
- #modenr = linelist[1].rstrip().lstrip()
+ linelist = line.replace('\n', '').replace('\r', '').split(':')
+ # modenr = linelist[1].rstrip().lstrip()
# text after Mode nr can be empty
try:
eigenmodes = linelist[2].rstrip().lstrip().split(' ')
@@ -1205,12 +975,12 @@ def ReadEigenBody(fname, debug=False):
for k in eigenmodes:
if len(k) > 1:
eigmod.append(k)
- #eigenmodes = eigmod
+ # eigenmodes = eigmod
else:
eigmod = eigenmodes
# remove any trailing spaces for each element
for k in range(len(eigmod)):
- eigmod[k] = float(eigmod[k])#.lstrip().rstrip()
+ eigmod[k] = float(eigmod[k]) #.lstrip().rstrip()
df_dict['body'].append(body)
df_dict['Fd_hz'].append(eigmod[0])
@@ -1260,16 +1030,16 @@ def ReadEigenStructure(file_path, file_name, debug=False, max_modes=500):
"""
- #0 Version ID : HAWC2MB 11.3
- #1 ___________________________________________________________________
- #2 Structure eigenanalysis output
- #3 ___________________________________________________________________
- #4 Time : 13:46:59
- #5 Date : 28:11.2012
- #6 ___________________________________________________________________
- #7 Results: fd [Hz] fn [Hz] log.decr [%]
- #8 Mode nr: 1: 3.58673E+00 3.58688E+00 5.81231E+00
- # Mode nr:294: 0.00000E+00 6.72419E+09 6.28319E+02
+ # 0 Version ID : HAWC2MB 11.3
+ # 1 ___________________________________________________________________
+ # 2 Structure eigenanalysis output
+ # 3 ___________________________________________________________________
+ # 4 Time : 13:46:59
+ # 5 Date : 28:11.2012
+ # 6 ___________________________________________________________________
+ # 7 Results: fd [Hz] fn [Hz] log.decr [%]
+ # 8 Mode nr: 1: 3.58673E+00 3.58688E+00 5.81231E+00
+ # Mode nr:294: 0.00000E+00 6.72419E+09 6.28319E+02
FILE = opent(os.path.join(file_path, file_name))
lines = FILE.readlines()
@@ -1280,12 +1050,12 @@ def ReadEigenStructure(file_path, file_name, debug=False, max_modes=500):
# we now the number of modes by having the number of lines
nrofmodes = len(lines) - header_lines
- modes_arr = np.ndarray((3,nrofmodes))
+ modes_arr = np.ndarray((3, nrofmodes))
for i, line in enumerate(lines):
if i > max_modes:
# cut off the unused rest
- modes_arr = modes_arr[:,:i]
+ modes_arr = modes_arr[:, :i]
break
# ignore the header
@@ -1294,9 +1064,9 @@ def ReadEigenStructure(file_path, file_name, debug=False, max_modes=500):
# split up mode nr from the rest
parts = line.split(':')
- #modenr = int(parts[1])
+ # modenr = int(parts[1])
# get fd, fn and damping, but remove all empty items on the list
- modes_arr[:,i-header_lines]=misc.remove_items(parts[2].split(' '),'')
+ modes_arr[:, i-header_lines]=misc.remove_items(parts[2].split(' '), '')
return modes_arr
@@ -1430,7 +1200,7 @@ class UserWind(object):
t1 = np.exp(-math.sqrt(z_h / h_ME))
t2 = (z - z_h) / math.sqrt(z_h * h_ME)
- t3 = ( 1.0 - (z-z_h)/(2.0*math.sqrt(z_h*h_ME)) - (z-z_h)/(4.0*z_h) )
+ t3 = (1.0 - (z-z_h)/(2.0*math.sqrt(z_h*h_ME)) - (z-z_h)/(4.0*z_h))
return a_phi * t1 * t2 * t3
@@ -1479,9 +1249,9 @@ class UserWind(object):
# assert np.allclose(np.abs(u), np.abs(u2))
# assert np.allclose(np.abs(v), np.abs(v2))
- u_full = u[:,np.newaxis] + np.zeros((3,))[np.newaxis,:]
- v_full = v[:,np.newaxis] + np.zeros((3,))[np.newaxis,:]
- w_full = np.zeros((nr_vert,nr_hor))
+ u_full = u[:, np.newaxis] + np.zeros((3,))[np.newaxis, :]
+ v_full = v[:, np.newaxis] + np.zeros((3,))[np.newaxis, :]
+ w_full = np.zeros((nr_vert, nr_hor))
return u_full, v_full, w_full, x, z
@@ -1517,10 +1287,10 @@ class UserWind(object):
w_comp = np.genfromtxt(fname, skiprows=3+2+nr_vert*2,
skip_footer=i-3-3-nr_vert*3)
v_coord = np.genfromtxt(fname, skiprows=3+3+nr_vert*3,
- skip_footer=i-3-3-nr_vert*3-3)
+ skip_footer=i-3-3-nr_vert*3-3)
w_coord = np.genfromtxt(fname, skiprows=3+3+nr_vert*3+4,
- skip_footer=i-k)
- phi_deg = np.arctan(v_comp[:,0]/u_comp[:,0])*180.0/np.pi
+ skip_footer=i-k)
+ phi_deg = np.arctan(v_comp[:, 0]/u_comp[:, 0])*180.0/np.pi
return u_comp, v_comp, w_comp, v_coord, w_coord, phi_deg
@@ -1554,10 +1324,10 @@ class UserWind(object):
np.savetxt(fid, w, fmt=fmt_uvw, delimiter=' ')
h2 = b'# v coordinates (along the horizontal, nr_hor, 0 rotor center)'
fid.write(b'%s\n' % h2)
- np.savetxt(fid, v_coord.reshape((v_coord.size,1)), fmt=fmt_coord)
+ np.savetxt(fid, v_coord.reshape((v_coord.size, 1)), fmt=fmt_coord)
h3 = b'# w coordinates (zero is at ground level, height, nr_hor)'
fid.write(b'%s\n' % h3)
- np.savetxt(fid, w_coord.reshape((w_coord.size,1)), fmt=fmt_coord)
+ np.savetxt(fid, w_coord.reshape((w_coord.size, 1)), fmt=fmt_coord)
class WindProfiles(object):
@@ -1679,9 +1449,9 @@ class Turbulence(object):
# mean velocity components at the center of the box
v1, v2 = (shape[1]/2)-1, shape[1]/2
w1, w2 = (shape[2]/2)-1, shape[2]/2
- ucent = (u[:,v1,w1] + u[:,v1,w2] + u[:,v2,w1] + u[:,v2,w2]) / 4.0
- vcent = (v[:,v1,w1] + v[:,v1,w2] + v[:,v2,w1] + v[:,v2,w2]) / 4.0
- wcent = (w[:,v1,w1] + w[:,v1,w2] + w[:,v2,w1] + w[:,v2,w2]) / 4.0
+ ucent = (u[:, v1, w1] + u[:, v1, w2] + u[:, v2, w1] + u[:, v2, w2]) / 4.0
+ vcent = (v[:, v1, w1] + v[:, v1, w2] + v[:, v2, w1] + v[:, v2, w2]) / 4.0
+ wcent = (w[:, v1, w1] + w[:, v1, w2] + w[:, v2, w1] + w[:, v2, w2]) / 4.0
# FIXME: where is this range 351:7374 coming from?? The original script
# considered a box of lenght 8192
@@ -1707,9 +1477,9 @@ class Turbulence(object):
iv = np.zeros(shape)
iw = np.zeros(shape)
- iu[:,:,:] = (u - umean)/ustd*1000.0
- iv[:,:,:] = (v - vmean)/vstd*1000.0
- iw[:,:,:] = (w - wmean)/wstd*1000.0
+ iu[:, :, :] = (u - umean)/ustd*1000.0
+ iv[:, :, :] = (v - vmean)/vstd*1000.0
+ iw[:, :, :] = (w - wmean)/wstd*1000.0
# because MATLAB and Octave do a round when casting from float to int,
# and Python does a floor, we have to round first
@@ -1741,33 +1511,33 @@ class Turbulence(object):
iu, iv, iw = self.convert2bladed(fpath, basename, shape=shape)
fid = open(fpath + basename + '.wnd', 'wb')
- fid.write(struct.pack('h', R1)) # R1
- fid.write(struct.pack('h', R2)) # R2
- fid.write(struct.pack('i', turb)) # Turb
- fid.write(struct.pack('f', 999)) # Lat
- fid.write(struct.pack('f', 999)) # rough
- fid.write(struct.pack('f', 999)) # refh
- fid.write(struct.pack('f', longti)) # LongTi
- fid.write(struct.pack('f', latti)) # LatTi
- fid.write(struct.pack('f', vertti)) # VertTi
- fid.write(struct.pack('f', dv)) # VertGpSpace
- fid.write(struct.pack('f', dw)) # LatGpSpace
- fid.write(struct.pack('f', du)) # LongGpSpace
- fid.write(struct.pack('i', shape[0]/2)) # HalfAlong
- fid.write(struct.pack('f', mean_ws)) # meanWS
- fid.write(struct.pack('f', 999.)) # VertLongComp
- fid.write(struct.pack('f', 999.)) # LatLongComp
- fid.write(struct.pack('f', 999.)) # LongLongComp
- fid.write(struct.pack('i', 999)) # Int
- fid.write(struct.pack('i', seed)) # Seed
- fid.write(struct.pack('i', shape[1])) # VertGpNum
- fid.write(struct.pack('i', shape[2])) # LatGpNum
- fid.write(struct.pack('f', 999)) # VertLatComp
- fid.write(struct.pack('f', 999)) # LatLatComp
- fid.write(struct.pack('f', 999)) # LongLatComp
- fid.write(struct.pack('f', 999)) # VertVertComp
- fid.write(struct.pack('f', 999)) # LatVertComp
- fid.write(struct.pack('f', 999)) # LongVertComp
+ fid.write(struct.pack('h', R1)) # R1
+ fid.write(struct.pack('h', R2)) # R2
+ fid.write(struct.pack('i', turb)) # Turb
+ fid.write(struct.pack('f', 999)) # Lat
+ fid.write(struct.pack('f', 999)) # rough
+ fid.write(struct.pack('f', 999)) # refh
+ fid.write(struct.pack('f', longti)) # LongTi
+ fid.write(struct.pack('f', latti)) # LatTi
+ fid.write(struct.pack('f', vertti)) # VertTi
+ fid.write(struct.pack('f', dv)) # VertGpSpace
+ fid.write(struct.pack('f', dw)) # LatGpSpace
+ fid.write(struct.pack('f', du)) # LongGpSpace
+ fid.write(struct.pack('i', shape[0]/2)) # HalfAlong
+ fid.write(struct.pack('f', mean_ws)) # meanWS
+ fid.write(struct.pack('f', 999.)) # VertLongComp
+ fid.write(struct.pack('f', 999.)) # LatLongComp
+ fid.write(struct.pack('f', 999.)) # LongLongComp
+ fid.write(struct.pack('i', 999)) # Int
+ fid.write(struct.pack('i', seed)) # Seed
+ fid.write(struct.pack('i', shape[1])) # VertGpNum
+ fid.write(struct.pack('i', shape[2])) # LatGpNum
+ fid.write(struct.pack('f', 999)) # VertLatComp
+ fid.write(struct.pack('f', 999)) # LatLatComp
+ fid.write(struct.pack('f', 999)) # LongLatComp
+ fid.write(struct.pack('f', 999)) # VertVertComp
+ fid.write(struct.pack('f', 999)) # LatVertComp
+ fid.write(struct.pack('f', 999)) # LongVertComp
# fid.flush()
# bladed2 = np.ndarray((shape[0], shape[2], shape[1], 3), dtype=np.int16)
@@ -1783,9 +1553,9 @@ class Turbulence(object):
# re-arrange array for bladed format
bladed = np.ndarray((shape[0], shape[2], shape[1], 3), dtype=np.int16)
- bladed[:,:,:,0] = iu[:,::-1,:]
- bladed[:,:,:,1] = iv[:,::-1,:]
- bladed[:,:,:,2] = iw[:,::-1,:]
+ bladed[:, :, :, 0] = iu[:, ::-1, :]
+ bladed[:, :, :, 1] = iv[:, ::-1, :]
+ bladed[:, :, :, 2] = iw[:, ::-1, :]
bladed_swap_view = bladed.swapaxes(1,2)
bladed_swap_view.tofile(fid, format='%int16')