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):
'''
Overwrites the parameters cpacsImport method!
Will get the value for dfus 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'):
lastSegment = getFuselageSegmentCount(TIGLHandle)
dmax = 0.
for i in range(lastSegment):
diameter = getFuselageDiameter(TIGLHandle, i + 1, 1.)
if diameter > dmax:
dmax = diameter
self.setValueFix(dmax)
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 dfus 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'):
lastSegment = getFuselageSegmentCount(TIGLHandle)
dmax = 0.
for i in range(lastSegment):
diameter = getFuselageDiameter(TIGLHandle, i+1,1.)
if diameter > dmax:
dmax = diameter
self.setValueFix(dmax)
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()