def readConfig(self):
'''
Read VAMPzeros configuration parameters. Command line arguments overwrite the configurations in the toolspecific part.
'''
TIXIHandle = tixiLib.openTIXI(self.cpacsIn)
if self.args.d != None:
self.config['deviationAmplitude'] = float(self.args.d)
else:
devFactor = 0.0
devFactorStr = tixiLib.getText(TIXIHandle,'/cpacs/toolspecific/vampZero/toolSettings/deviationAmplitude')
if devFactorStr != None:
devFactor = float(devFactorStr)
self.config['deviationAmplitude'] = devFactor
# read configuration for extended output
self.config['extendedOutput'] = True
extendedOutput = tixiLib.getText(TIXIHandle,'/cpacs/toolspecific/vampZero/toolSettings/extendedOutput')
if extendedOutput in ('False', 'false', '0.0', '0.', '0'):
self.config['extendedOutput'] = False
# read sensitivity configuration
self.config['calcSensitivities'] = False
calcSensitivities = tixiLib.getText(TIXIHandle,'/cpacs/toolspecific/vampZero/toolSettings/calcSensitivities')
if calcSensitivities in ('True', 'true', '1.0', '1.', '1'):
self.config['calcSensitivities'] = True
# read not converging behavior
self.config['notConvergingAction'] = 'exit'
not_converging_action = tixiLib.getText(TIXIHandle,'/cpacs/toolspecific/vampZero/toolSettings/notConvergingAction')
if not_converging_action in ('exit', 'copyInput', 'errorXML'):
self.config['notConvergingAction'] = not_converging_action
tixiLib.closeXML(TIXIHandle)
def cpacsImport(self,
path='.\\cpacs.xml',
TIXIHandle=None,
TIGLHandle=None):
'''
imports the value for thrust00 for the current engine out of TWDat
'''
if not TIXIHandle:
TIXIHandle = openTIXI(path)
if checkElement(TIXIHandle,
'/cpacs/vehicles/engines/engine/analysis/thrust00'):
self.thrust00 = eval(
getText(TIXIHandle,
'/cpacs/vehicles/engines/engine/analysis/thrust00'))
self.importSuccess()
else:
self.importError()
if checkElement(TIXIHandle, '/cpacs/vehicles/engines/engine/name'):
name = getText(TIXIHandle, '/cpacs/vehicles/engines/engine/name')
if name.find('scaled') != -1:
self.originalScaling = eval(name.split()[-1])
self.log.info(
"VAMPzero TIXI: imported previous scaling factor from TWDat: %s"
% self.originalScaling)
else:
self.originalScaling = 1.
else:
self.importError()
def cpacsImport(self, path='.\\cpacs.xml', TIXIHandle=None, TIGLHandle=None):
'''
imports the values for summed up Nose and Main Landing Gear and set value to fix
.. todo::
cpacsImport mLandingGear this is out dated since LGDesign does not apply to CPACS 1.4
'''
if not TIXIHandle:
TIXIHandle = openTIXI(path)
error = 0
if checkElement(TIXIHandle,
'/cpacs/vehicles/aircraft/model/analyses/massBreakdown/landingGear/mainGears/mainGear/totalMass/mass'):
self.mMainGear = eval(getText(TIXIHandle,
'/cpacs/vehicles/aircraft/model/analyses/massBreakdown/landingGear/mainGears/mainGear/totalMass/mass'))
else:
error = 1
if checkElement(TIXIHandle,
'/cpacs/vehicles/aircraft/model/analyses/massBreakdown/landingGear/noseGears/noseGear/totalMass/mass'):
self.mNoseGear = eval(getText(TIXIHandle,
'/cpacs/vehicles/aircraft/model/analyses/massBreakdown/landingGear/noseGears/noseGear/totalMass/mass'))
else:
error = 1
if not error:
self.setValueFix(2 * self.mMainGear + self.mNoseGear)
self.importSuccess()
else:
self.importError()
def cpacsImport(self, path='.\\cpacs.xml', TIXIHandle=None, TIGLHandle=None):
'''
Overwrites the parameter's cpacsImport method! Will get
the value for cDMINoffset from a CPACS aeroPerformanceMap.
Does a monkey patch as it replaces cDMINoffset.calc with cDMINoffset.calcLiLi
.. todo::
cpacsImport cDMINoffset catch error if cfy is unequal zero
'''
try:
if not TIXIHandle:
TIXIHandle = openTIXI(path)
self.refArea = eval(getText(TIXIHandle, '/cpacs/vehicles/aircraft/model/reference/area'))
self.CfxList = getList(TIXIHandle, '/cpacs/vehicles/aircraft/model/analyses/aeroPerformanceMap/cfx')
self.CfzList = getList(TIXIHandle, '/cpacs/vehicles/aircraft/model/analyses/aeroPerformanceMap/cfz')
self.CfyList = getList(TIXIHandle, '/cpacs/vehicles/aircraft/model/analyses/aeroPerformanceMap/cfy')
self.AOAList = getList(TIXIHandle,
'/cpacs/vehicles/aircraft/model/analyses/aeroPerformanceMap/angleOfAttack')
self.AOYList = getList(TIXIHandle, '/cpacs/vehicles/aircraft/model/analyses/aeroPerformanceMap/angleOfYaw')
self.machList = getList(TIXIHandle, '/cpacs/vehicles/aircraft/model/analyses/aeroPerformanceMap/machNumber')
self.reList = getList(TIXIHandle,
'/cpacs/vehicles/aircraft/model/analyses/aeroPerformanceMap/reynoldsNumber')
if self.CfxList:
self.calc = self.calcLiLi
self.monkeyPatch('LiftingLine')
except:
self.importError()
def cpacsImport(self,
path='.\\cpacs.xml',
TIXIHandle=None,
TIGLHandle=None):
'''
Imports the values for the primary wing structure and applies formula to calculate mWing
Value is set to FIX, but a correction factor is applied to get secondary wing mass from
the imported primary wing structure mass.
:Source: Analytical Fuselage and Wing Weight Estimation of Transport Aircraft, M. D. Ardema, M. C. Chambers, A. P. Patron, A. S. Hahn, H. Miura, M. D. Moore, NASA Technical Memorandum 110392, 1996, p. 22 eq. 109
'''
if not TIXIHandle:
TIXIHandle = openTIXI(path)
error = 0
if checkElement(
TIXIHandle,
'/cpacs/vehicles/aircraft/model/analyses/massBreakdown/mOEM/mEM/mStructure/mWingsStructure/mWingStructure[1]/massDescription/mass'
):
self.mWingPrimary = eval(
getText(
TIXIHandle,
'/cpacs/vehicles/aircraft/model/analyses/massBreakdown/mOEM/mEM/mStructure/mWingsStructure/mWingStructure[1]/massDescription/mass'
))
else:
error = 1
if error == 0 and self.mWingPrimary is not None:
self.setValueFix(2. * self.mWingPrimary)
self.importSuccess()
else:
self.importError()
def cpacsImport(self, path='.\\cpacs.xml', TIXIHandle=None, TIGLHandle=None):
'''
TIXI and TIGL Handle should be given, to save some valueable time
Imports self.cpacsPath from path
Input Values will be set to 'fix'
'''
if not TIXIHandle:
TIXIHandle = openTIXI(path)
if self.getCpacsPath() != '':
retVal = getText(TIXIHandle, self.getCpacsPath())
if retVal is not None and retVal is not '':
try:
self.setValueFix(eval(retVal))
self.importSuccess()
# This may occur if UID or other strings will be imported
except NameError:
self.setValueFix(retVal)
self.importSuccess()
except SyntaxError:
self.setValueFix(retVal)
self.importSuccess()
else:
self.importError()
def cpacsImport(self,
path='.\\cpacs.xml',
TIXIHandle=None,
TIGLHandle=None):
'''
'''
if not TIXIHandle:
TIXIHandle = openTIXI(path)
error = 0
if checkElement(
TIXIHandle,
'/cpacs/vehicles/aircraft/model/analyses/massBreakdown/mOEM/mEM/mStructure/mWingsStructure/mWingStructure[3]/massDescription/mass'
):
self.mWingPrimary = eval(
getText(
TIXIHandle,
'/cpacs/vehicles/aircraft/model/analyses/massBreakdown/mOEM/mEM/mStructure/mWingsStructure/mWingStructure[3]/massDescription/mass'
))
else:
error = 1
if error == 0 and self.mWingPrimary is not None:
self.setValueFix(self.mWingPrimary * 2.)
self.importSuccess()
else:
self.importError()
def cpacsImport(self, path=".\\cpacs.xml", TIXIHandle=None, TIGLHandle=None):
"""
Imports the values for the primary wing structure and applies formula to calculate mWing
Value is set to FIX, but a correction factor is applied to get secondary wing mass from
the imported primary wing structure mass.
:Source: Analytical Fuselage and Wing Weight Estimation of Transport Aircraft, M. D. Ardema, M. C. Chambers, A. P. Patron, A. S. Hahn, H. Miura, M. D. Moore, NASA Technical Memorandum 110392, 1996, p. 22 eq. 109
"""
if not TIXIHandle:
TIXIHandle = openTIXI(path)
error = 0
if checkElement(
TIXIHandle,
"/cpacs/vehicles/aircraft/model/analyses/massBreakdown/mOEM/mEM/mStructure/mWingsStructure/mWingStructure[1]/massDescription/mass",
):
self.mWingPrimary = eval(
getText(
TIXIHandle,
"/cpacs/vehicles/aircraft/model/analyses/massBreakdown/mOEM/mEM/mStructure/mWingsStructure/mWingStructure[1]/massDescription/mass",
)
)
else:
error = 1
if error == 0 and self.mWingPrimary is not None:
self.setValueFix(self.mWingPrimary)
self.importSuccess()
else:
self.importError()
def cpacsImport(self,
path='.\\cpacs.xml',
TIXIHandle=None,
TIGLHandle=None):
'''
TIXI and TIGL Handle should be given, to save some valueable time
Imports self.cpacsPath from path
Input Values will be set to 'fix'
'''
if not TIXIHandle:
TIXIHandle = openTIXI(path)
if self.getCpacsPath() != '':
retVal = getText(TIXIHandle, self.getCpacsPath())
if retVal is not None and retVal is not '':
try:
self.setValueFix(eval(retVal))
self.importSuccess()
# This may occur if UID or other strings will be imported
except NameError:
self.setValueFix(retVal)
self.importSuccess()
except SyntaxError:
self.setValueFix(retVal)
self.importSuccess()
else:
self.importError()
def cpacsImport(self,
path='.\\cpacs.xml',
TIXIHandle=None,
TIGLHandle=None):
'''
imports the values for summed up Nose and Main Landing Gear and set value to fix
.. todo::
cpacsImport mLandingGear this is out dated since LGDesign does not apply to CPACS 1.4
'''
if not TIXIHandle:
TIXIHandle = openTIXI(path)
error = 0
if checkElement(
TIXIHandle,
'/cpacs/vehicles/aircraft/model/analyses/massBreakdown/landingGear/mainGears/mainGear/totalMass/mass'
):
self.mMainGear = eval(
getText(
TIXIHandle,
'/cpacs/vehicles/aircraft/model/analyses/massBreakdown/landingGear/mainGears/mainGear/totalMass/mass'
))
else:
error = 1
if checkElement(
TIXIHandle,
'/cpacs/vehicles/aircraft/model/analyses/massBreakdown/landingGear/noseGears/noseGear/totalMass/mass'
):
self.mNoseGear = eval(
getText(
TIXIHandle,
'/cpacs/vehicles/aircraft/model/analyses/massBreakdown/landingGear/noseGears/noseGear/totalMass/mass'
))
else:
error = 1
if not error:
self.setValueFix(2 * self.mMainGear + self.mNoseGear)
self.importSuccess()
else:
self.importError()
def cpacsImport(self,
path='.\\cpacs.xml',
TIXIHandle=None,
TIGLHandle=None):
'''
Overwrites the parameter's cpacsImport method!
Will get the value for the Oswald Factor from CPACS
It will be assumed that the aeroperformanceMap holds LiLi values
Does a monkey patch as it replaces oswald.calc with oswald.calcLiLi
.. todo::
cpacsImport oswald catch error if cfy is unequal zero
'''
try:
if not TIXIHandle:
TIXIHandle = openTIXI(path)
self.refArea = eval(
getText(TIXIHandle,
'/cpacs/vehicles/aircraft/model/reference/area'))
self.CfxList = getList(
TIXIHandle,
'/cpacs/vehicles/aircraft/model/analyses/aeroPerformanceMap/cfx'
)
self.CfzList = getList(
TIXIHandle,
'/cpacs/vehicles/aircraft/model/analyses/aeroPerformanceMap/cfz'
)
self.CfyList = getList(
TIXIHandle,
'/cpacs/vehicles/aircraft/model/analyses/aeroPerformanceMap/cfy'
)
self.AOAList = getList(
TIXIHandle,
'/cpacs/vehicles/aircraft/model/analyses/aeroPerformanceMap/angleOfAttack'
)
self.AOYList = getList(
TIXIHandle,
'/cpacs/vehicles/aircraft/model/analyses/aeroPerformanceMap/angleOfYaw'
)
self.machList = getList(
TIXIHandle,
'/cpacs/vehicles/aircraft/model/analyses/aeroPerformanceMap/machNumber'
)
self.reList = getList(
TIXIHandle,
'/cpacs/vehicles/aircraft/model/analyses/aeroPerformanceMap/reynoldsNumber'
)
if self.CfxList:
self.calc = self.calcLiLi
self.monkeyPatch('LiftingLine')
except:
self.importError()
def cpacsImport(self, path='.\\cpacs.xml', TIXIHandle=None, TIGLHandle=None):
'''
imports the value for thrust00 for the current engine out of TWDat
'''
if not TIXIHandle:
TIXIHandle = openTIXI(path)
if checkElement(TIXIHandle, '/cpacs/vehicles/engines/engine/analysis/thrust00'):
self.thrust00 = eval(getText(TIXIHandle, '/cpacs/vehicles/engines/engine/analysis/thrust00'))
self.importSuccess()
else:
self.importError()
if checkElement(TIXIHandle, '/cpacs/vehicles/engines/engine/name'):
name = getText(TIXIHandle, '/cpacs/vehicles/engines/engine/name')
if name.find('scaled') != -1:
self.originalScaling = eval(name.split()[-1])
self.log.info("VAMPzero TIXI: imported previous scaling factor from TWDat: %s" % self.originalScaling)
else:
self.originalScaling = 1.
else:
self.importError()
def readConfig(self):
'''
Read VAMPzeros configuration parameters. Command line arguments overwrite the configurations in the toolspecific part.
'''
TIXIHandle = tixiLib.openTIXI(self.cpacsIn)
if self.args.d != None:
self.config['deviationAmplitude'] = float(self.args.d)
else:
devFactor = 0.0
devFactorStr = tixiLib.getText(
TIXIHandle,
'/cpacs/toolspecific/vampZero/toolSettings/deviationAmplitude')
if devFactorStr != None:
devFactor = float(devFactorStr)
self.config['deviationAmplitude'] = devFactor
# read configuration for extended output
self.config['extendedOutput'] = True
extendedOutput = tixiLib.getText(
TIXIHandle,
'/cpacs/toolspecific/vampZero/toolSettings/extendedOutput')
if extendedOutput in ('False', 'false', '0.0', '0.', '0'):
self.config['extendedOutput'] = False
# read sensitivity configuration
self.config['calcSensitivities'] = False
calcSensitivities = tixiLib.getText(
TIXIHandle,
'/cpacs/toolspecific/vampZero/toolSettings/calcSensitivities')
if calcSensitivities in ('True', 'true', '1.0', '1.', '1'):
self.config['calcSensitivities'] = True
# read not converging behavior
self.config['notConvergingAction'] = 'exit'
not_converging_action = tixiLib.getText(
TIXIHandle,
'/cpacs/toolspecific/vampZero/toolSettings/notConvergingAction')
if not_converging_action in ('exit', 'copyInput', 'errorXML'):
self.config['notConvergingAction'] = not_converging_action
tixiLib.closeXML(TIXIHandle)
def cpacsImport(self, path='.\\cpacs.xml'):
'''
Looks for parameter.CPACSPath in CPACSFilse defined by Path
Transfers Value is possible
Input Values will be set to 'fix'
'''
self.log.info('')
self.log.info(
"##############################################################################"
)
self.log.info("VAMPzero CPACS Import from %s" % path)
self.log.info("trying to import and fix parameters")
self.log.info(
"##############################################################################"
)
TIXIHandle = openTIXI(path)
modelUID = getText(TIXIHandle,
'/cpacs/toolspecific/vampZero/aircraftModelUID')
if modelUID is None:
self.log.info(
"VAMPzero IMPORT: No modelUID specified in the toolspecific Block"
)
try:
modelUID = self.modelUID.getValue()
self.log.info("VAMPzero IMPORT: loaded modelUID from VAMPzero")
except AttributeError:
modelUID = None
self.log.info(
"VAMPzero IMPORT: could not load modelUID from VAMPzero")
if modelUID is not None:
TIGLHandle = openTIGL(TIXIHandle, modelUID)
if TIGLHandle is not None:
self.log.debug(
"VAMPzero IMPORT: Opened TIXI and TIGL in Component")
else:
TIGLHandle = None
self.log.debug(
"VAMPzero IMPORT: Opened only TIXI in Component as no modelUID was specified"
)
self.importer(path, TIXIHandle, TIGLHandle)
self.log.info("VAMPzero IMPORT: done.")
closeXML(TIXIHandle)
def cpacsImport(self, path='.\\cpacs.xml', TIXIHandle=None, TIGLHandle=None):
'''
'''
if not TIXIHandle:
TIXIHandle = openTIXI(path)
error = 0
if checkElement(TIXIHandle,
'/cpacs/vehicles/aircraft/model/analyses/massBreakdown/mOEM/mEM/mStructure/mWingsStructure/mWingStructure[3]/massDescription/mass'):
self.mWingPrimary = eval(getText(TIXIHandle,
'/cpacs/vehicles/aircraft/model/analyses/massBreakdown/mOEM/mEM/mStructure/mWingsStructure/mWingStructure[3]/massDescription/mass'))
else:
error = 1
if error == 0 and self.mWingPrimary is not None:
self.setValueFix(self.mWingPrimary * 2.)
self.importSuccess()
else:
self.importError()
def cpacsImport(self, path='.\\cpacs.xml'):
'''
Looks for parameter.CPACSPath in CPACSFilse defined by Path
Transfers Value is possible
Input Values will be set to 'fix'
'''
self.log.info('')
self.log.info("##############################################################################")
self.log.info("VAMPzero CPACS Import from %s" % path)
self.log.info("trying to import and fix parameters")
self.log.info("##############################################################################")
TIXIHandle = openTIXI(path)
modelUID = getText(TIXIHandle, '/cpacs/toolspecific/vampZero/aircraftModelUID')
if modelUID is None:
self.log.info("VAMPzero IMPORT: No modelUID specified in the toolspecific Block")
try:
modelUID = self.modelUID.getValue()
self.log.info("VAMPzero IMPORT: loaded modelUID from VAMPzero")
except AttributeError:
modelUID = None
self.log.info("VAMPzero IMPORT: could not load modelUID from VAMPzero")
if modelUID is not None:
TIGLHandle = openTIGL(TIXIHandle, modelUID)
if TIGLHandle is not None:
self.log.debug("VAMPzero IMPORT: Opened TIXI and TIGL in Component")
else:
TIGLHandle = None
self.log.debug("VAMPzero IMPORT: Opened only TIXI in Component as no modelUID was specified")
self.importer(path, TIXIHandle, TIGLHandle)
self.log.info("VAMPzero IMPORT: done.")
closeXML(TIXIHandle)
def cpacsImport(self,
path='.\\cpacs.xml',
TIXIHandle=None,
TIGLHandle=None):
'''
Overwrites the parameters cpacsImport method!
Imports the enginePerformanceMap
This method replaces the initial calc method by calcCPACS
sfcCR will not be set fix because ongoing interpolation is necessary to find
the correct values
'''
if not TIXIHandle:
TIXIHandle = openTIXI(path)
if checkElement(
TIXIHandle,
'/cpacs/vehicles/engines/engine[last()]/analysis/performanceMaps/performanceMap'
):
# Get performanceMap from CPACS
Tmap = getText(
TIXIHandle,
"/cpacs/vehicles/engines/engine[last()]/analysis/performanceMaps/performanceMap/thrust"
).split(';')
Mamap = getText(
TIXIHandle,
"/cpacs/vehicles/engines/engine[last()]/analysis/performanceMaps/performanceMap/machNumber"
).split(';')
FLmap = getText(
TIXIHandle,
"/cpacs/vehicles/engines/engine[last()]/analysis/performanceMaps/performanceMap/flightLevel"
).split(';')
mDotmap = getText(
TIXIHandle,
"/cpacs/vehicles/engines/engine[last()]/analysis/performanceMaps/performanceMap/mDotFuel"
).split(';')
#Pop Last entries because of garbage
FLmap.pop()
mDotmap.pop()
Tmap.pop()
Mamap.pop()
#Conversion
FLmap = [float(val) for val in FLmap]
Mamap = [float(val) for val in Mamap]
Tmap = [float(val) for val in Tmap]
mDotmap = [float(val) for val in mDotmap]
#Dummies
maList = []
flList = []
thList = []
#Go Through complete Data Set
for i in range(len(FLmap)):
thList.append([Tmap[i - 1], mDotmap[i - 1]])
if Mamap[i] != Mamap[i - 1]:
maList.append([Mamap[i - 1], thList])
thList = []
if FLmap[i] != FLmap[i - 1]:
flList.append([FLmap[i - 1], maList])
maList = []
# Final List of List of List for the engine deck
self.TList = flList
#set calcTWDat as the new Calculation method
self.calc = self.calcCPACS
self.monkeyPatch('CPACS')
else:
self.importError()
def cpacsImport(self, path='.\\cpacs.xml', TIXIHandle=None, TIGLHandle=None):
'''
Overwrites the parameters cpacsImport method!
Imports the enginePerformanceMap
This method replaces the initial calc method by calcCPACS
sfcCR will not be set fix because ongoing interpolation is necessary to find
the correct values
'''
if not TIXIHandle:
TIXIHandle = openTIXI(path)
if checkElement(TIXIHandle, '/cpacs/vehicles/engines/engine[last()]/analysis/performanceMaps/performanceMap'):
# Get performanceMap from CPACS
Tmap = getText(TIXIHandle,
"/cpacs/vehicles/engines/engine[last()]/analysis/performanceMaps/performanceMap/thrust").split(
';')
Mamap = getText(TIXIHandle,
"/cpacs/vehicles/engines/engine[last()]/analysis/performanceMaps/performanceMap/machNumber").split(
';')
FLmap = getText(TIXIHandle,
"/cpacs/vehicles/engines/engine[last()]/analysis/performanceMaps/performanceMap/flightLevel").split(
';')
mDotmap = getText(TIXIHandle,
"/cpacs/vehicles/engines/engine[last()]/analysis/performanceMaps/performanceMap/mDotFuel").split(
';')
#Pop Last entries because of garbage
FLmap.pop()
mDotmap.pop()
Tmap.pop()
Mamap.pop()
#Conversion
FLmap = [float(val) for val in FLmap]
Mamap = [float(val) for val in Mamap]
Tmap = [float(val) for val in Tmap]
mDotmap = [float(val) for val in mDotmap]
#Dummies
maList = []
flList = []
thList = []
#Go Through complete Data Set
for i in range(len(FLmap)):
thList.append([Tmap[i - 1], mDotmap[i - 1]])
if Mamap[i] != Mamap[i - 1]:
maList.append([Mamap[i - 1], thList])
thList = []
if FLmap[i] != FLmap[i - 1]:
flList.append([FLmap[i - 1], maList])
maList = []
# Final List of List of List for the engine deck
self.TList = flList
#set calcTWDat as the new Calculation method
self.calc = self.calcCPACS
self.monkeyPatch('CPACS')
else:
self.importError()
def importGUI(myAircraft,path):
'''
This is an import routine for simple input from the tool-specific part of a
CPACS file. This also reads all information that can be generated by the
simple GUI available in the binary version of VAMPzero
It takes an *aircraft* as input. This is necessary to set the values in
the aircraft according to the information given in *path*. Usually
*path* is specified as ./ToolInput/toolInput.xml
'''
log = zeroLogger('General')
log.info('')
log.info("##############################################################################")
log.info('VAMPzero GUI: importing GUI Values from: %s'%path)
log.info("reading toolspecific/GUI inputs")
log.info("##############################################################################")
myAircraft.modelUID.cpacsImport(path)
if myAircraft.modelUID.getValue() != '':
log.info('VAMPzero GUI: Running with: %s as modelUID.'%myAircraft.modelUID.getValue())
else:
log.warning('VAMPzero GUI: No valid information for modelUID!')
TIXIHandle = openTIXI(path)
cpacsVal = c_char_p()
top = "/cpacs/toolspecific/vampZero/components/"
##Component#############################################################
countC = 1
while 1==1:
pathC = top+'component['+str(countC)+']'
if checkElement(TIXIHandle,pathC):
nameC = getText(TIXIHandle, pathC+'/name')
if nameC:
log.debug('VAMPzero GUI: importing for component: %s'%nameC)
else:
break
##Discipline#############################################################
countD = 1
while 1==1:
pathD = pathC+'/disciplines/discipline['+str(countD)+']'
if checkElement(TIXIHandle,pathD):
##Parameter#############################################################
countP = 1
while 1==1:
pathP = pathD+'/parameters/parameter['+str(countP)+']'
if checkElement(TIXIHandle,pathP):
nameP = getText(TIXIHandle,pathP+'/name')
valueP = getText(TIXIHandle,pathP+'/value')
factorP = getText(TIXIHandle,pathP+'/factor')
statusP = getText(TIXIHandle,pathP+'/status')
exportP = getText(TIXIHandle,pathP+'/exportTS')
setParameter(myAircraft, nameC, nameP, valueP, factorP, statusP, exportP)
countP += 1
else:
break
countD += 1
else:
break
countC += 1
else:
break
def importGUI(myAircraft, path):
'''
This is an import routine for simple input from the tool-specific part of a
CPACS file. This also reads all information that can be generated by the
simple GUI available in the binary version of VAMPzero
It takes an *aircraft* as input. This is necessary to set the values in
the aircraft according to the information given in *path*. Usually
*path* is specified as ./ToolInput/toolInput.xml
'''
log = zeroLogger('General')
log.info('')
log.info(
"##############################################################################"
)
log.info('VAMPzero GUI: importing GUI Values from: %s' % path)
log.info("reading toolspecific/GUI inputs")
log.info(
"##############################################################################"
)
myAircraft.modelUID.cpacsImport(path)
if myAircraft.modelUID.getValue() != '':
log.info('VAMPzero GUI: Running with: %s as modelUID.' %
myAircraft.modelUID.getValue())
else:
log.warning('VAMPzero GUI: No valid information for modelUID!')
TIXIHandle = openTIXI(path)
cpacsVal = c_char_p()
top = "/cpacs/toolspecific/vampZero/components/"
##Component#############################################################
countC = 1
while 1 == 1:
pathC = top + 'component[' + str(countC) + ']'
if checkElement(TIXIHandle, pathC):
nameC = getText(TIXIHandle, pathC + '/name')
if nameC:
log.debug('VAMPzero GUI: importing for component: %s' % nameC)
else:
break
##Discipline#############################################################
countD = 1
while 1 == 1:
pathD = pathC + '/disciplines/discipline[' + str(countD) + ']'
if checkElement(TIXIHandle, pathD):
##Parameter#############################################################
countP = 1
while 1 == 1:
pathP = pathD + '/parameters/parameter[' + str(
countP) + ']'
if checkElement(TIXIHandle, pathP):
nameP = getText(TIXIHandle, pathP + '/name')
valueP = getText(TIXIHandle, pathP + '/value')
factorP = getText(TIXIHandle, pathP + '/factor')
statusP = getText(TIXIHandle, pathP + '/status')
exportP = getText(TIXIHandle, pathP + '/exportTS')
setParameter(myAircraft, nameC, nameP, valueP,
factorP, statusP, exportP)
countP += 1
else:
break
countD += 1
else:
break
countC += 1
else:
break
