def createFuselageSections(parent, nose,cabin,tail, dfus, strUID, strName, strDescr):
'''
Used for generation of fuselage Sections.
Creates all the sections given through myRQSi.
@author: Jonas Jepsen
@param parent: fuselageType object, Sections-object will be added here
@param confList: cross Sections from PrADO for section configurations
@param strUID: UID of Sections [string]
@param strName: Name of Sections [string]
@param strDescr: Description of Sections [string]
'''
mySections = fuselageSectionsType()
# countAll counts the total amount of cross sections for this fuselage
countAll = 0
for cs in nose:
countAll += 1
# create Section
createFuselageSection(mySections, dfus, cs, 'Circle', strUID+'_Sec'+str(countAll), strName+'_Sec'+str(countAll), strDescr+'_Sec'+str(countAll))
for cs in cabin:
countAll += 1
# create Section
createFuselageSection(mySections, dfus, cs, 'Circle', strUID+'_Sec'+str(countAll), strName+'_Sec'+str(countAll), strDescr+'_Sec'+str(countAll))
for cs in tail:
countAll += 1
# create Section
createFuselageSection(mySections, dfus, cs, 'Circle', strUID+'_Sec'+str(countAll), strName+'_Sec'+str(countAll), strDescr+'_Sec'+str(countAll))
parent.set_sections(mySections)
def createFuselage(CPACSObj, id, dfus, lnose, lcabin, ltail, LoD=0):
# just for now
if LoD==FUSE_LOD.NONE:
return
cpacsPath = '/cpacs/vehicles/aircraft/model/fuselages/fuselage[' + id + ']'
# the next line is the one to use later on
#cpacsPath = '/cpacs/vehicles/aircraft/model[model]/fuselages/fuselage[' + self.id + ']'
# gets a list of all wing elements
myFuse = getObjfromXpath(CPACSObj,cpacsPath)
strUID = myFuse.get_uID()
myUID = strUID
myName = stringBaseType(valueOf_=id)
myDescr = stringBaseType(valueOf_=strUID)
myFuse.set_uID(myUID)
myFuse.set_name(myName)
myFuse.set_description(myDescr)
createTransformation(myFuse, 'absGlobal',0.,0.,0.)
if LoD==FUSE_LOD.A320:
nose = list(NOSE)
cabin = list(CABIN)
tail = list(TAIL)
# remove double values
cabin.pop(0)
tail.pop(0)
# sections will be created, all existing sections will be deleted
createFuselageSections(myFuse, nose,cabin,tail, dfus, strUID, strUID, strUID)
createFuselagePositionings(myFuse, nose,cabin,tail, lnose,lcabin,ltail, strUID, strUID)
createFuselageSegments(myFuse, strUID, len(nose)+len(cabin)+len(tail)-1)
elif LoD==FUSE_LOD.ZYL:
# sections will be created, all existing sections will be deleted
mySections = fuselageSectionsType()
#calc fuselage radius
#rfus = dfus/2.
# make fuselage configuration data [x_rel,z-dist,height/2,width/2]]
fuseConf = [0.,0.,0.5,0.5]
createFuselageSection(mySections, dfus, fuseConf, 'Circle', strUID+'_Sec1', strUID+'_Sec1', strUID+'_Sec1')
createFuselageSection(mySections, dfus, fuseConf, 'Circle', strUID+'_Sec2', strUID+'_Sec2', strUID+'_Sec2')
createFuselageSection(mySections, dfus, fuseConf, 'Circle', strUID+'_Sec3', strUID+'_Sec3', strUID+'_Sec3')
createFuselageSection(mySections, dfus, fuseConf, 'Circle', strUID+'_Sec4', strUID+'_Sec4', strUID+'_Sec4')
myFuse.set_sections(mySections)
myPositionings = positioningsType()
createPositioning(myPositionings,str(id) + '_Pos1',None, str(id) + '_Sec1',0.,90.,0.,id + '_Pos1')
createPositioning(myPositionings,str(id) + '_Pos2',str(id) + '_Sec1',str(id) + '_Sec2',lnose,90.,0,id + '_Pos2')
createPositioning(myPositionings,str(id) + '_Pos3',str(id) + '_Sec2',str(id) + '_Sec3',lcabin,90.,0,id + '_Pos3')
createPositioning(myPositionings,str(id) + '_Pos4',str(id) + '_Sec3',str(id) + '_Sec4',ltail,90.,0,id + '_Pos4')
myFuse.set_positionings(myPositionings)
createFuselageSegments(myFuse, strUID, 3)
def createFuselageSections(parent, nose, cabin, tail, dfus, strUID, strName,
strDescr):
'''
Used for generation of fuselage Sections.
Creates all the sections given through myRQSi.
@author: Jonas Jepsen
@param parent: fuselageType object, Sections-object will be added here
@param confList: cross Sections from PrADO for section configurations
@param strUID: UID of Sections [string]
@param strName: Name of Sections [string]
@param strDescr: Description of Sections [string]
'''
mySections = fuselageSectionsType()
# countAll counts the total amount of cross sections for this fuselage
countAll = 0
for cs in nose:
countAll += 1
# create Section
createFuselageSection(mySections, dfus, cs, 'Circle',
strUID + '_Sec' + str(countAll),
strName + '_Sec' + str(countAll),
strDescr + '_Sec' + str(countAll))
for cs in cabin:
countAll += 1
# create Section
createFuselageSection(mySections, dfus, cs, 'Circle',
strUID + '_Sec' + str(countAll),
strName + '_Sec' + str(countAll),
strDescr + '_Sec' + str(countAll))
for cs in tail:
countAll += 1
# create Section
createFuselageSection(mySections, dfus, cs, 'Circle',
strUID + '_Sec' + str(countAll),
strName + '_Sec' + str(countAll),
strDescr + '_Sec' + str(countAll))
parent.set_sections(mySections)
def createFuselage(CPACSObj, id, dfus, lnose, lcabin, ltail, LoD=0):
# just for now
if LoD == FUSE_LOD.NONE:
return
cpacsPath = '/cpacs/vehicles/aircraft/model/fuselages/fuselage[' + id + ']'
# the next line is the one to use later on
#cpacsPath = '/cpacs/vehicles/aircraft/model[model]/fuselages/fuselage[' + self.id + ']'
# gets a list of all wing elements
myFuse = getObjfromXpath(CPACSObj, cpacsPath)
strUID = myFuse.get_uID()
myUID = strUID
myName = stringBaseType(None, None, None, id)
myDescr = stringBaseType(None, None, None, strUID)
myFuse.set_uID(myUID)
myFuse.set_name(myName)
myFuse.set_description(myDescr)
createTransformation(myFuse, 'absGlobal', 0., 0., 0.)
if LoD == FUSE_LOD.A320:
nose = list(NOSE)
cabin = list(CABIN)
tail = list(TAIL)
# remove double values
cabin.pop(0)
tail.pop(0)
# sections will be created, all existing sections will be deleted
createFuselageSections(myFuse, nose, cabin, tail, dfus, strUID, strUID,
strUID)
createFuselagePositionings(myFuse, nose, cabin, tail, lnose, lcabin,
ltail, strUID, strUID)
createFuselageSegments(myFuse, strUID,
len(nose) + len(cabin) + len(tail) - 1)
elif LoD == FUSE_LOD.ZYL:
# sections will be created, all existing sections will be deleted
mySections = fuselageSectionsType()
#calc fuselage radius
#rfus = dfus/2.
# make fuselage configuration data [x_rel,z-dist,height/2,width/2]]
fuseConf = [0., 0., 0.5, 0.5]
createFuselageSection(mySections, dfus, fuseConf, 'Circle',
strUID + '_Sec1', strUID + '_Sec1',
strUID + '_Sec1')
createFuselageSection(mySections, dfus, fuseConf, 'Circle',
strUID + '_Sec2', strUID + '_Sec2',
strUID + '_Sec2')
createFuselageSection(mySections, dfus, fuseConf, 'Circle',
strUID + '_Sec3', strUID + '_Sec3',
strUID + '_Sec3')
createFuselageSection(mySections, dfus, fuseConf, 'Circle',
strUID + '_Sec4', strUID + '_Sec4',
strUID + '_Sec4')
myFuse.set_sections(mySections)
myPositionings = positioningsType()
createPositioning(myPositionings,
str(id) + '_Pos1', None,
str(id) + '_Sec1', 0., 90., 0., id + '_Pos1')
createPositioning(myPositionings,
str(id) + '_Pos2',
str(id) + '_Sec1',
str(id) + '_Sec2', lnose, 90., 0, id + '_Pos2')
createPositioning(myPositionings,
str(id) + '_Pos3',
str(id) + '_Sec2',
str(id) + '_Sec3', lcabin, 90., 0, id + '_Pos3')
createPositioning(myPositionings,
str(id) + '_Pos4',
str(id) + '_Sec3',
str(id) + '_Sec4', ltail, 90., 0, id + '_Pos4')
myFuse.set_positionings(myPositionings)
createFuselageSegments(myFuse, strUID, 3)