def cpacsImport(self,
path='.\\cpacs.xml',
TIXIHandle=None,
TIGLHandle=None):
'''
Overwrites the parameters cpacsImport method!
Will get the value for lfus from CPACS via TIGL functions
'''
if not TIXIHandle:
TIXIHandle = openTIXI(path)
if not TIGLHandle:
TIGLHandle = openTIGL(TIXIHandle,
self.parent.aircraft.modelUID.getValue())
if checkElement(TIXIHandle,
'/cpacs/vehicles/aircraft/model/fuselages/fuselage'):
# get First Point from the Fuselage
x1, y1, z1 = getFuselagePoint(TIGLHandle, 1, 0., 0.)
lastSegment = getFuselageSegmentCount(TIGLHandle)
x2, y2, z2 = getFuselagePoint(TIGLHandle, lastSegment, 1., 0.)
self.setValueFix(x2 - x1)
self.importSuccess()
else:
self.importError()
def cpacsImport(self,
path='.\\cpacs.xml',
TIXIHandle=None,
TIGLHandle=None):
'''
Retrieves the xRoot coordinate from TIGL. It will go for the main fuselage. The first sections x coordinate is read at eta and zeta
equal 0.
'''
if not TIXIHandle:
TIXIHandle = openTIXI(path)
if not TIGLHandle:
TIGLHandle = openTIGL(TIXIHandle,
self.parent.aircraft.modelUID.getValue())
if checkElement(TIXIHandle,
'/cpacs/vehicles/aircraft/model/fuselages/fuselage'):
self.log.debug('Importing fuselage x position...')
try:
# fuselage index is implicitly set to 1 in TIGL/tigl.py
x1, _, _ = getFuselagePoint(TIGLHandle, 1, 0, 0)
except Exception as e:
self.log.warning(str(e))
self.log.debug('Importing fuselage x position... {}'.format(x1))
self.setValueFix(x1)
self.importSuccess()
else:
self.importError()
def cpacsImport(self, path='.\\cpacs.xml', TIXIHandle=None, TIGLHandle=None):
'''
Overwrites the parameters cpacsImport method!
Will get the value for lfus from CPACS via TIGL functions
'''
if not TIXIHandle:
TIXIHandle = openTIXI(path)
if not TIGLHandle:
TIGLHandle = openTIGL(TIXIHandle, self.parent.aircraft.modelUID.getValue())
if checkElement(TIXIHandle, '/cpacs/vehicles/aircraft/model/fuselages/fuselage'):
# get First Point from the Fuselage
x1, y1, z1 = getFuselagePoint(TIGLHandle, 1, 0., 0.)
lastSegment = getFuselageSegmentCount(TIGLHandle)
x2, y2, z2 = getFuselagePoint(TIGLHandle, lastSegment, 1., 0.)
self.setValueFix(x2 - x1)
self.importSuccess()
else:
self.importError()
def cpacsImport(self, path='.\\cpacs.xml', TIXIHandle=None, TIGLHandle=None):
'''
Retrieves the xRoot coordinate from TIGL. It will go for the main fuselage. The first sections x coordinate is read at eta and zeta
equal 0.
'''
if not TIXIHandle:
TIXIHandle = openTIXI(path)
if not TIGLHandle:
TIGLHandle = openTIGL(TIXIHandle, self.parent.aircraft.modelUID.getValue())
if checkElement(TIXIHandle, '/cpacs/vehicles/aircraft/model/fuselages/fuselage'):
self.log.debug('Importing fuselage x position...')
try:
# fuselage index is implicitly set to 1 in TIGL/tigl.py
x1, _, _ = getFuselagePoint(TIGLHandle, 1, 0, 0)
except Exception as e:
self.log.warning(str(e))
self.log.debug('Importing fuselage x position... {}'.format(x1))
self.setValueFix(x1)
self.importSuccess()
else:
self.importError()