def test_open(self):
t = Tixi()
self.assertRaises(TixiException, t.open, "____HOPEFULLY_THIS_FILE_NAME_DOES_NOT_EXIST~~~~") #OPEN_FAILED
self.assertRaises(TixiException, t.open, os.path.join("TestData", "illformed.xml")) #NOT_WELL_FORMED
t.open(os.path.join("TestData", "in.xml"))
self.assertTrue(t._handle.value != -1)
t.close()
def __init__(self):
super(MainWindow, self).__init__()
self.setWindowTitle('Main Window')
tixi = Tixi()
# tixi.open(conf.path_cpacs_simple)
# tixi.open(Config.path_cpacs_D150_3)
tixi.openDocument(Config.path_cpacs_simple)
#tixi.openDocument(conf.path_cpacs_A320_Wing)
#self.tixi.schemaValidateFromFile(cpacs_scheme)
tigl = Tigl()
try:
tigl.open(tixi,"")
except TiglException as err:
print ('Error opening tigl document: ', err.__str__())
xml_editor = EditorWindow(tixi, Config.path_cpacs_simple)
ogl_editor = MainWidget(tixi, tigl)
dockWidgets = [('xml editor', xml_editor), ('ogl editor', ogl_editor)]
xml_editor.updateAction.triggered.connect(ogl_editor.updateView)
for (name, widget) in dockWidgets :
self.addSimpleWidget(name, widget)
def test_multiple_tixis(self):
''' Check if we can handle several loaded DLLs and CPACS at the same time. '''
a = Tixi()
b = Tixi()
self.assertNotEqual(a._handle, b._handle)
a.open(os.path.join("TestData", "in.xml"))
b.open(os.path.join("TestData", "in.xml"))
self.assertNotEqual(a._handle, b._handle)
a.close()
b.close()
def __init__(self, parent = None):
super(MainWidget, self).__init__(parent)
self.tixi = Tixi()
self.tigl = Tigl()
self.loadFile(Config.path_cpacs_A320_Fuse, Config.path_cpacs_21_schema)
buttonAirf = QtGui.QPushButton("airfoil")
buttonFuse = QtGui.QPushButton("fuselage")
grid = QtGui.QGridLayout()
grid.addWidget(buttonAirf, 0,0)
grid.addWidget(buttonFuse, 0,1)
self.setWindowTitle('Profile-Editor-Widget')
self.setLayout(grid)
self.resize(560,520)
# fuse or airfoil window
self.window = None
# actions
buttonAirf.clicked.connect(self.fire_AirfoilMainWidget)
buttonFuse.clicked.connect(self.fire_FuselageMainWidget)
def test_validation_and_export(self):
t = Tixi()
t.open(os.path.join("TestData", "valid_CPACS_dokumentiert.xml"))
c = t.exportDocumentAsString()
self.assertTrue(c != None and c != "")
header = '<?xml version="1.0" encoding="UTF-8"?>'
self.assertTrue(c.startswith(header))
t.schemaValidateFromFile(
os.path.join("TestData", "valid_cpacs_schema.xsd"))
schema = 'invalid'
self.assertRaises(TixiException, t.schemaValidateFromString,
schema) #OPEN_SCHEMA_FAILED
schema = '<?xml version="1.0" encoding="UTF-8"?>\\n<?xml-stylesheet href="xs3p.xsl" type="text/xsl"?>\\n<xsd:schema xmlns:xsd="http://www.w3.org/2001/XMLSchema" xmlns="http://www.w3.org/1999/xhtml" targetNamespace="http://www.w3.org/1999/xhtml" elementFormDefault="qualified" attributeFormDefault="unqualified">\\n</xsd:schema>' # TODO
self.assertRaises(TixiException, t.schemaValidateFromString,
schema) #NOT_SCHEMA_COMPLIANT
t.close()
def test_validation_and_export(self):
t = Tixi()
t.open(os.path.join("TestData", "valid_CPACS_dokumentiert.xml"))
c = t.exportDocumentAsString()
self.assertTrue(c != None and c != "")
header = '<?xml version="1.0" encoding="UTF-8"?>'
self.assertTrue(c.startswith(header))
t.schemaValidateFromFile(os.path.join("TestData", "valid_cpacs_schema.xsd"))
schema = 'invalid'
self.assertRaises(TixiException, t.schemaValidateFromString, schema) #OPEN_SCHEMA_FAILED
schema = '<?xml version="1.0" encoding="UTF-8"?>\\n<?xml-stylesheet href="xs3p.xsl" type="text/xsl"?>\\n<xsd:schema xmlns:xsd="http://www.w3.org/2001/XMLSchema" xmlns="http://www.w3.org/1999/xhtml" targetNamespace="http://www.w3.org/1999/xhtml" elementFormDefault="qualified" attributeFormDefault="unqualified">\\n</xsd:schema>' # TODO
self.assertRaises(TixiException, t.schemaValidateFromString, schema) #NOT_SCHEMA_COMPLIANT
t.close()
def test(self):
# lxml test
try:
root = etree.Element("root")
print (root.tag)
print ("lxml ok")
except ImportError :
print ("import error lxml")
# matplot test
try:
figure = Figure(figsize=(5,4), dpi=100)
plot = figure.add_subplot(111)
canvas = FigureCanvas(figure)
print ("matplotlib ok")
except ImportError :
print ("import error matplotlib")
# tixi, tigl
try:
tixi = Tixi()
tixi.openDocument("toolOutput.xml")
print ("tixi ok")
except TixiException :
print ("import error Tixi")
try:
tigl = Tigl()
tigl.open(tixi,"")
print ("tigl ok")
except TixiException :
print ("import error Tigl")
try:
np.arange(10000000)
print ("numpy ok")
except TixiException :
print ("import error numpy")
def test_open(self):
t = Tixi()
self.assertRaises(
TixiException, t.open,
"____HOPEFULLY_THIS_FILE_NAME_DOES_NOT_EXIST~~~~") #OPEN_FAILED
self.assertRaises(TixiException, t.open,
os.path.join("TestData",
"illformed.xml")) #NOT_WELL_FORMED
t.open(os.path.join("TestData", "in.xml"))
self.assertTrue(t._handle.value != -1)
t.close()
def __init__(self, parent=None):
super(Plotter_LC, self).__init__(parent)
self.tixi = Tixi()
self.tixi.open(Config.path_cpacs_lc_ref)
self.buttonBox = QtGui.QDialogButtonBox()
self.buttonBox.addButton(QtGui.QDialogButtonBox.Ok)
self.buttonBox.addButton(QtGui.QDialogButtonBox.Reset)
self.buttonBox.addButton(QtGui.QDialogButtonBox.Cancel)
self.plot_widget = PlotWidget("LC")
self.comboBoxLoadCases = QtGui.QComboBox()
self.fillComboBoxLoadCases()
self.fire_LoadCaseChanged(0)
self.grid = QtGui.QGridLayout()
self.grid.addWidget(self.comboBoxLoadCases, 0,0)
self.grid.addWidget(self.plot_widget, 1, 0)
# set the layout
layout = QtGui.QGridLayout()
layout.addLayout(self.grid, 0,0,1,3)
layout.addWidget(self.buttonBox, 5, 0, 1,3)
widget = QtGui.QWidget()
widget.setLayout(layout)
self.setCentralWidget(widget)
# ===============================================================================================
# actions
# ===============================================================================================
self.comboBoxLoadCases.currentIndexChanged.connect(self.fire_LoadCaseChanged)
self.buttonBox.button(QtGui.QDialogButtonBox.Ok).clicked.connect(self.close)
self.buttonBox.button(QtGui.QDialogButtonBox.Reset).clicked.connect(self.close)
self.buttonBox.button(QtGui.QDialogButtonBox.Cancel).clicked.connect(self.close)
def test_open_http(self):
t = Tixi()
t.openHttp("http://www.w3schools.com/XML/note.xml")
t.close()
def test_open_string(self):
t = Tixi()
cpacs = '<?xml version="1.0"?><cpacs><header><version>1.2.3</version></header></cpacs>'
t.openString(cpacs)
t.close()
def test_vector_array(self):
t = Tixi()
t.open(os.path.join("TestData", "vectorcount.xml"))
self.assertEquals(t.getVectorSize("/a/aeroPerformanceMap/cfx"), 32)
#v = t.getFloatVector("/a/aeroPerformanceMap/cfx", 32)
#print v[0], v[1], v[-1]
#1 2 118
t.close()
# manual creation of vector
t.create('doc')
t.addFloatVector('/doc', 'myvec', range(100,130), 30, "%g")
size = t.getVectorSize('/doc/myvec')
self.assertEquals(size, 30)
v = t.getFloatVector('/doc/myvec', 30)
self.assertEquals(v, tuple(range(100,130)))
t.close()
t.open(os.path.join("TestData", "arraytests.xml"))
self.assertEquals(t.getArrayDimensions("/root/aeroPerformanceMap"), 4)
self.assertEquals(t.getArrayDimensionSizes("/root/aeroPerformanceMap", 4), ((1, 2, 3, 8), 48))
self.assertEquals(t.getArrayDimensionNames("/root/aeroPerformanceMap", 4), ("machNumber", "reynoldsNumber", "angleOfYaw", "angleOfAttack"))
# print t.getArrayDimensionValues("/root/aeroPerformanceMap", 0) 1.0
# print t.getArrayDimensionValues("/root/aeroPerformanceMap", 2) 0 5 10
self.assertEquals(t.getArrayParameters("/root/aeroPerformanceMap"), 7)
# print t.getArrayParameterNames("/root/aeroPerformanceMap") ("cfx", "cfy", "cfz", "cmx", "cmy", "cmz", "def")
# print t.getArray("/root/aeroPerformanceMap", "cmx") None
# print t.getArrayValue(arr, "/root/aeroPerformanceMap", "angleOfAttack")
#8
#print t.getArrayElementNames("/root/aeroPerformanceMap", "vector")
#print t.getArrayElementNames("/root/aeroPerformanceMap", "array")
t.getArrayElementCount("/root/aeroPerformanceMap","array")
t.createElement("/root", "p1")
t.addPoint("/root/p1", 1, 2, 3, None)
self.assertEquals(t.getPoint("/root/p1"), (1.0, 2.0, 3.0))
self.assertEquals(t.xPathEvaluateNodeNumber("/root/aeroPerformanceMap"), 1)
t.close()
t.open(os.path.join("TestData", "in.xml"))
self.assertEquals(t.xPathExpressionGetTextByIndex("/plane/wings/wing/centerOfGravity/x", 2), "30.0")
t.close()
t.open(os.path.join("TestData", "uid_correct.xml"))
t.uIDCheckDuplicates()
t.uIDCheckExists("schlumpf")
t.close()
t.open(os.path.join("TestData", "uid_duplicated.xml"))
self.assertRaises(TixiException, t.uIDCheckDuplicates) #UID_NOT_UNIQUE
class Plotter(QtGui.QMainWindow):
def __init__(self, path, parent=None):
super(Plotter, self).__init__(parent)
self.tixi = Tixi()
t = self.tixi.open(Config.path_cpacs_pm_ref)
self.pathPerMap = "/cpacs/vehicles/aircraft/model[1]/analyses/aeroPerformanceMap"
self.path_specific = path
self.buttonBox = QtGui.QDialogButtonBox()
self.buttonBox.addButton(QtGui.QDialogButtonBox.Ok)
self.buttonBox.addButton(QtGui.QDialogButtonBox.Reset)
self.buttonBox.addButton(QtGui.QDialogButtonBox.Cancel)
self.comboBoxXAxis = QtGui.QComboBox()
self.comboBoxXAxis.addItem("machNumber")
self.comboBoxXAxis.addItem("reynoldsNumber")
self.comboBoxXAxis.addItem("angleOfYaw")
self.comboBoxXAxis.addItem("angleOfAttack")
self.comboBoxPlotPnt = QtGui.QComboBox()
self.comboBoxPlotPnt.addItem("curve")
self.comboBoxPlotPnt.addItem("points")
self.labelXAxis = QtGui.QLabel("set x-axis")
self.labelDisplay = QtGui.QLabel("display")
self.labelMachNum = QtGui.QLabel("machNumber")
self.labelReynoldsNum = QtGui.QLabel("reynoldsNumber")
self.labelAngleOfYaw = QtGui.QLabel("angleOfYaw")
self.labelAngleOfAtt = QtGui.QLabel("angleOfAttack")
self.listMachNum = QtGui.QListWidget()
self.listReynoldsNum = QtGui.QListWidget()
self.listAngleOfYaw = QtGui.QListWidget()
self.listAngleOfAtt = QtGui.QListWidget()
#self.comboBoxXAxis.setCurrentIndex(0)
self.__hidePlotLists(True, False, False, False)
self.__fillPlotLists(self.pathPerMap)
self.grid = QtGui.QGridLayout()
self.grid.addWidget(self.labelXAxis, 0,0,1,3)
self.grid.addWidget(self.labelDisplay, 0,3)
self.grid.addWidget(self.comboBoxXAxis, 1,0,1,3)
self.grid.addWidget(self.comboBoxPlotPnt, 1,3)
self.grid.addWidget(self.labelMachNum, 2,0)
self.grid.addWidget(self.listMachNum, 3,0)
self.grid.addWidget(self.labelReynoldsNum, 2,1)
self.grid.addWidget(self.listReynoldsNum, 3,1)
self.grid.addWidget(self.labelAngleOfYaw, 2,2)
self.grid.addWidget(self.listAngleOfYaw, 3,2)
self.grid.addWidget(self.labelAngleOfAtt, 2,3)
self.grid.addWidget(self.listAngleOfAtt, 3,3)
# set the layout
layout = QtGui.QGridLayout()
layout.addLayout(self.grid, 0,0,1,3)
layout.addWidget(self.buttonBox, 5, 0, 1,3)
widget = QtGui.QWidget()
widget.setLayout(layout)
self.setCentralWidget(widget)
# ===============================================================================================
# actions
# ===============================================================================================
self.comboBoxXAxis.currentIndexChanged.connect(self.fire_XAxisChanged)
self.buttonBox.button(QtGui.QDialogButtonBox.Ok).clicked.connect(self.plot)
self.buttonBox.button(QtGui.QDialogButtonBox.Reset).clicked.connect(self.reset)
self.buttonBox.button(QtGui.QDialogButtonBox.Cancel).clicked.connect(self.close)
def addSimpleWidget(self, name, widget):
dock = QtGui.QDockWidget(name)
dock.setWidget(widget)
dock.setMinimumWidth(100)
dock.setMinimumHeight(300)
dock.setAllowedAreas(QtCore.Qt.AllDockWidgetAreas)
dock.setFeatures(QtGui.QDockWidget.DockWidgetClosable |
QtGui.QDockWidget.DockWidgetMovable |
QtGui.QDockWidget.DockWidgetFloatable)
self.addDockWidget(QtCore.Qt.BottomDockWidgetArea, dock)
return dock
def fire_XAxisChanged(self, idx):
self.reset()
self.__setPlotListVisibility(idx == 0, idx == 1, idx == 2, idx == 3)
def plot(self):
# get current selection
x_axis_idx = self.comboBoxXAxis.currentIndex()
mach_idx = self.listMachNum.currentRow()
reyn_idx = self.listReynoldsNum.currentRow()
yaw_idx = self.listAngleOfYaw.currentRow()
att_idx = self.listAngleOfAtt.currentRow()
# find x-axis array ; stop one selection missed
if x_axis_idx == 0 :
x_axis = self.getMachNumberVector(self.pathPerMap)
elif x_axis_idx == 1 :
x_axis = self.getReynoldsNumberVector(self.pathPerMap)
elif x_axis_idx == 2 :
x_axis = self.getAngleOfYawVector(self.pathPerMap)
elif x_axis_idx == 3 :
x_axis = self.getAngleOfAttackVector(self.pathPerMap)
# set display option
displayOpt = 'go' if self.comboBoxPlotPnt.currentText() == "points" else ""
# get values for tixiGetArrayValue
((cnt_mach, cnt_reyn, cnt_angleYaw, cnt_angleAtt), size) = self.tixi.getArrayDimensionSizes(self.pathPerMap, 4)
dimSize = [cnt_mach, cnt_reyn, cnt_angleYaw, cnt_angleAtt]
dimPos = [mach_idx, reyn_idx, yaw_idx, att_idx]
dims = self.tixi.getArrayDimensions(self.pathPerMap)
for widget in self.plotWidgets:
array = self.getCoefficientArray(self.path_specific, widget.getTitle(), size)
widget.setXLabel(self.comboBoxXAxis.currentText())
widget.updatePlot(array, dimSize, dimPos, dims, x_axis, x_axis_idx ,self.tixi, self.pathPerMap, displayOpt)
def reset(self):
for widget in self.plotWidgets:
widget.updateReset()
def __fillPlotLists(self, path):
for item in self.getMachNumberVector(path) :
self.listMachNum.addItem(str(item))
for item in self.getReynoldsNumberVector(path) :
self.listReynoldsNum.addItem(str(item))
for item in self.getAngleOfYawVector(path) :
self.listAngleOfYaw.addItem(str(item))
for item in self.getAngleOfAttackVector(path) :
self.listAngleOfAtt.addItem(str(item))
def getAngleOfYawVector(self, path):
return self.tixi.getFloatVector(path + "/angleOfYaw", self.tixi.getVectorSize(path + "/angleOfYaw"))
def getAngleOfAttackVector(self, path):
return self.tixi.getFloatVector(path + "/angleOfAttack", self.tixi.getVectorSize(path + "/angleOfAttack"))
def getReynoldsNumberVector(self, path):
return self.tixi.getFloatVector(path + "/reynoldsNumber", self.tixi.getVectorSize(path + "/reynoldsNumber"))
def getMachNumberVector(self, path):
return self.tixi.getFloatVector(path + "/machNumber", self.tixi.getVectorSize(path + "/machNumber"))
def getCoefficientArray(self, path, child, num):
return self.tixi.getArray(path , child, num)
def __hidePlotLists(self, flag_mach, flag_reyn, flag_yaw, flag_att):
self.__setPlotListVisibility(flag_mach, flag_reyn, flag_yaw, flag_att)
def __setPlotListVisibility(self, flag_mach, flag_reyn, flag_yaw, flag_att):
self.labelMachNum.setHidden(flag_mach)
self.labelReynoldsNum.setHidden(flag_reyn)
self.labelAngleOfYaw.setHidden(flag_yaw)
self.labelAngleOfAtt.setHidden(flag_att)
self.listMachNum.setHidden(flag_mach)
self.listReynoldsNum.setHidden(flag_reyn)
self.listAngleOfYaw.setHidden(flag_yaw)
self.listAngleOfAtt.setHidden(flag_att)
def test_elements(self):
t = Tixi()
t.open(os.path.join("TestData", "in.xml"))
self.assertEqual(t.getTextElement("/plane/name"), "Junkers JU 52")
t.updateTextElement("/plane/name", "D150")
self.assertEqual(t.getTextElement("/plane/name"), "D150")
t.addTextElement("/plane", "name", "B747")
self.assertEqual(t.getTextElement("/plane/name[2]"), "B747")
self.assertEqual(t.getIntegerElement("/plane/numberOfPassengers"), 57)
t.addIntegerElement("/plane", "nop", 123456, None)
self.assertEqual(t.getIntegerElement("/plane/nop"), 123456)
self.assertEqual(
t.getDoubleElement("/plane/wings[1]/wing[1]/centerOfGravity/x"),
30.0)
t.addDoubleElement("/plane/wings/wing[1]", "cog", 123.456, None)
self.assertEqual(t.getDoubleElement("/plane/wings/wing[1]/cog"),
123.456)
self.assertFalse(t.getBooleanElement("/plane/bool/aBool2"))
self.assertTrue(t.getBooleanElement("/plane/bool/aBool1b"))
self.assertFalse(t.checkElement("/plane/xx")) #ELEMENT_NOT_FOUND
t.createElement("/plane", "xx")
t.checkElement("/plane/xx")
self.assertEquals(t.getTextElement("/plane/xx"), "")
t.updateTextElement("/plane/xx", "value")
self.assertEquals(t.getTextElement("/plane/xx"), "value")
t.removeElement("/plane/xx")
self.assertEqual(t.checkElement("/plane/xx"), False)
self.assertRaises(TixiException, t.getTextElement,
"/plane/xx") #ELEMENT_NOT_FOUND
def test_multiple_tixis(self):
''' Check if we can handle several loaded DLLs and CPACS at the same time. '''
a = Tixi()
b = Tixi()
self.assertNotEqual(a._handle, b._handle)
a.open(os.path.join("TestData", "in.xml"))
b.open(os.path.join("TestData", "in.xml"))
self.assertNotEqual(a._handle, b._handle)
a.close()
b.close()
def __init__(self, parent=None):
super(Plotter_ControlSurfaces, self).__init__(parent)
self.tixi = Tixi()
self.tixi.open(Config.path_cpacs_pm_ref)
self.buttonBox = QtGui.QDialogButtonBox()
self.buttonBox.addButton(QtGui.QDialogButtonBox.Ok)
self.buttonBox.addButton(QtGui.QDialogButtonBox.Reset)
self.buttonBox.addButton(QtGui.QDialogButtonBox.Cancel)
self.comboBoxXAxis = QtGui.QComboBox()
self.comboBoxXAxis.addItem("machNumber")
self.comboBoxXAxis.addItem("reynoldsNumber")
self.comboBoxXAxis.addItem("angleOfYaw")
self.comboBoxXAxis.addItem("angleOfAttack")
self.comboBoxXAxis.addItem("relDeflection")
self.comboBoxPlotPnt = QtGui.QComboBox()
self.comboBoxPlotPnt.addItem("curve")
self.comboBoxPlotPnt.addItem("points")
self.comboBoxCtrlSurUID = QtGui.QComboBox()
self.labelCtrlSurUID = QtGui.QLabel("controlSurfaceUID")
self.labelXAxis = QtGui.QLabel("set x-axis")
self.labelDisplay = QtGui.QLabel("display")
self.labelMachNum = QtGui.QLabel("machNumber")
self.labelReynoldsNum = QtGui.QLabel("reynoldsNumber")
self.labelAngleOfYaw = QtGui.QLabel("angleOfYaw")
self.labelAngleOfAtt = QtGui.QLabel("angleOfAttack")
self.labelRelDefl = QtGui.QLabel("relDeflection")
self.listMachNum = QtGui.QListWidget()
self.listReynoldsNum = QtGui.QListWidget()
self.listAngleOfYaw = QtGui.QListWidget()
self.listAngleOfAtt = QtGui.QListWidget()
self.listRelDefl = QtGui.QListWidget()
self.hidePlotLists(True, False, False, False, False)
self.fillPlotLists("/cpacs/vehicles/aircraft/model[1]/analyses/aeroPerformanceMap")
self.grid = QtGui.QGridLayout()
self.grid.addWidget(self.labelCtrlSurUID, 0, 0, 1, 5)
self.grid.addWidget(self.comboBoxCtrlSurUID,1,0, 1, 5)
self.grid.addWidget(self.labelXAxis, 2,0,1,3)
self.grid.addWidget(self.labelDisplay, 2,3,1,2)
self.grid.addWidget(self.comboBoxXAxis, 3,0,1,3)
self.grid.addWidget(self.comboBoxPlotPnt, 3,3,1,2)
self.grid.addWidget(self.labelMachNum, 4,0)
self.grid.addWidget(self.listMachNum, 5,0)
self.grid.addWidget(self.labelReynoldsNum, 4,1)
self.grid.addWidget(self.listReynoldsNum, 5,1)
self.grid.addWidget(self.labelAngleOfYaw, 4,2)
self.grid.addWidget(self.listAngleOfYaw, 5,2)
self.grid.addWidget(self.labelAngleOfAtt, 4,3)
self.grid.addWidget(self.listAngleOfAtt, 5,3)
self.grid.addWidget(self.labelRelDefl, 4,4)
self.grid.addWidget(self.listRelDefl, 5,4)
# set the layout
layout = QtGui.QGridLayout()
layout.addLayout(self.grid, 0,0,1,3)
layout.addWidget(self.buttonBox, 5, 0, 1,3)
widget = QtGui.QWidget()
widget.setLayout(layout)
self.setCentralWidget(widget)
# add observer
self.plotWidgets = [PlotWidget("dcfx"), PlotWidget("dcfy"), PlotWidget("dcfz"), PlotWidget("dcmx"), PlotWidget("dcmy"), PlotWidget("dcmz")]
self.dockList = []
for widget in self.plotWidgets :
dock = self.addSimpleWidget(widget.getTitle(), widget)
insertIndex = len(self.dockList) - 1
self.dockList.insert(insertIndex, dock)
if len(self.dockList) > 1:
for index in range(0, len(self.dockList) - 1):
self.tabifyDockWidget(self.dockList[index],
self.dockList[index + 1])
self.dockList[0].raise_()
self.nextindex = 1
# ===============================================================================================
# actions
# ===============================================================================================
self.comboBoxXAxis.currentIndexChanged.connect(self.fire_XAxisChanged)
self.comboBoxCtrlSurUID.currentIndexChanged.connect(self.fire_CtrlSurfacesChanged)
self.buttonBox.button(QtGui.QDialogButtonBox.Ok).clicked.connect(self.plot)
self.buttonBox.button(QtGui.QDialogButtonBox.Reset).clicked.connect(self.reset)
self.buttonBox.button(QtGui.QDialogButtonBox.Cancel).clicked.connect(self.close)
class Plotter_LC(QtGui.QMainWindow):
def __init__(self, parent=None):
super(Plotter_LC, self).__init__(parent)
self.tixi = Tixi()
self.tixi.open(Config.path_cpacs_lc_ref)
self.buttonBox = QtGui.QDialogButtonBox()
self.buttonBox.addButton(QtGui.QDialogButtonBox.Ok)
self.buttonBox.addButton(QtGui.QDialogButtonBox.Reset)
self.buttonBox.addButton(QtGui.QDialogButtonBox.Cancel)
self.plot_widget = PlotWidget("LC")
self.comboBoxLoadCases = QtGui.QComboBox()
self.fillComboBoxLoadCases()
self.fire_LoadCaseChanged(0)
self.grid = QtGui.QGridLayout()
self.grid.addWidget(self.comboBoxLoadCases, 0,0)
self.grid.addWidget(self.plot_widget, 1, 0)
# set the layout
layout = QtGui.QGridLayout()
layout.addLayout(self.grid, 0,0,1,3)
layout.addWidget(self.buttonBox, 5, 0, 1,3)
widget = QtGui.QWidget()
widget.setLayout(layout)
self.setCentralWidget(widget)
# ===============================================================================================
# actions
# ===============================================================================================
self.comboBoxLoadCases.currentIndexChanged.connect(self.fire_LoadCaseChanged)
self.buttonBox.button(QtGui.QDialogButtonBox.Ok).clicked.connect(self.close)
self.buttonBox.button(QtGui.QDialogButtonBox.Reset).clicked.connect(self.close)
self.buttonBox.button(QtGui.QDialogButtonBox.Cancel).clicked.connect(self.close)
def fire_LoadCaseChanged(self, idx):
uid = self.comboBoxLoadCases.currentText()
path = '/cpacs/vehicles/aircraft/model[1]/analyses/loadAnalysis/loadCases/flightLoadCase[@uID="' + uid + '"]'
x_axis, y_axis = self.getPlotPointValues(path)
self.plot_widget.plot.clear()
self.plot_widget.plot.grid(True)
self.plot_widget.simplePlot(x_axis, y_axis)
def fillComboBoxLoadCases(self):
path_lc = "/cpacs/vehicles/aircraft/model[1]/analyses/loadAnalysis/loadCases"
for idx_lc in range(1, self.tixi.getNumberOfChilds(path_lc) + 1) :
tmp_path = path_lc + "/flightLoadCase[" + str(idx_lc) + "]"
self.comboBoxLoadCases.addItem( self.tixi.getTextAttribute(tmp_path,"uID") )
def getPlotPointValues(self, path):
"""...
Args:
path (String): path to specific flightLoadCase
Returns:
...
"""
xaxis = []
yaxis = []
path_wings = path + "/aeroLoads/wings"
for idx_wing in range(1, self.tixi.getNumberOfChilds(path_wings) + 1) :
path_segs = path_wings + "/wing[" + str(idx_wing) + "]/segments"
for idx_seg in range(1, self.tixi.getNumberOfChilds(path_segs) + 1) :
for idx_strip in range(1, self.tixi.getNamedChildrenCount(path_segs + "/segment[" + str(idx_seg) + "]", "strip") + 1) :
x = self.tixi.getDoubleElement(path_segs + "/segment[" + str(idx_seg) + "]/strip[" + str(idx_strip) + "]/reference/point/x")
y = self.tixi.getDoubleElement(path_segs + "/segment[" + str(idx_seg) + "]/strip[" + str(idx_strip) + "]/reference/point/y")
xaxis.append(x)
yaxis.append(y)
return xaxis, yaxis
class Plotter_ControlSurfaces(QtGui.QMainWindow):
def __init__(self, parent=None):
super(Plotter_ControlSurfaces, self).__init__(parent)
self.tixi = Tixi()
self.tixi.open(Config.path_cpacs_pm_ref)
self.buttonBox = QtGui.QDialogButtonBox()
self.buttonBox.addButton(QtGui.QDialogButtonBox.Ok)
self.buttonBox.addButton(QtGui.QDialogButtonBox.Reset)
self.buttonBox.addButton(QtGui.QDialogButtonBox.Cancel)
self.comboBoxXAxis = QtGui.QComboBox()
self.comboBoxXAxis.addItem("machNumber")
self.comboBoxXAxis.addItem("reynoldsNumber")
self.comboBoxXAxis.addItem("angleOfYaw")
self.comboBoxXAxis.addItem("angleOfAttack")
self.comboBoxXAxis.addItem("relDeflection")
self.comboBoxPlotPnt = QtGui.QComboBox()
self.comboBoxPlotPnt.addItem("curve")
self.comboBoxPlotPnt.addItem("points")
self.comboBoxCtrlSurUID = QtGui.QComboBox()
self.labelCtrlSurUID = QtGui.QLabel("controlSurfaceUID")
self.labelXAxis = QtGui.QLabel("set x-axis")
self.labelDisplay = QtGui.QLabel("display")
self.labelMachNum = QtGui.QLabel("machNumber")
self.labelReynoldsNum = QtGui.QLabel("reynoldsNumber")
self.labelAngleOfYaw = QtGui.QLabel("angleOfYaw")
self.labelAngleOfAtt = QtGui.QLabel("angleOfAttack")
self.labelRelDefl = QtGui.QLabel("relDeflection")
self.listMachNum = QtGui.QListWidget()
self.listReynoldsNum = QtGui.QListWidget()
self.listAngleOfYaw = QtGui.QListWidget()
self.listAngleOfAtt = QtGui.QListWidget()
self.listRelDefl = QtGui.QListWidget()
self.hidePlotLists(True, False, False, False, False)
self.fillPlotLists("/cpacs/vehicles/aircraft/model[1]/analyses/aeroPerformanceMap")
self.grid = QtGui.QGridLayout()
self.grid.addWidget(self.labelCtrlSurUID, 0, 0, 1, 5)
self.grid.addWidget(self.comboBoxCtrlSurUID,1,0, 1, 5)
self.grid.addWidget(self.labelXAxis, 2,0,1,3)
self.grid.addWidget(self.labelDisplay, 2,3,1,2)
self.grid.addWidget(self.comboBoxXAxis, 3,0,1,3)
self.grid.addWidget(self.comboBoxPlotPnt, 3,3,1,2)
self.grid.addWidget(self.labelMachNum, 4,0)
self.grid.addWidget(self.listMachNum, 5,0)
self.grid.addWidget(self.labelReynoldsNum, 4,1)
self.grid.addWidget(self.listReynoldsNum, 5,1)
self.grid.addWidget(self.labelAngleOfYaw, 4,2)
self.grid.addWidget(self.listAngleOfYaw, 5,2)
self.grid.addWidget(self.labelAngleOfAtt, 4,3)
self.grid.addWidget(self.listAngleOfAtt, 5,3)
self.grid.addWidget(self.labelRelDefl, 4,4)
self.grid.addWidget(self.listRelDefl, 5,4)
# set the layout
layout = QtGui.QGridLayout()
layout.addLayout(self.grid, 0,0,1,3)
layout.addWidget(self.buttonBox, 5, 0, 1,3)
widget = QtGui.QWidget()
widget.setLayout(layout)
self.setCentralWidget(widget)
# add observer
self.plotWidgets = [PlotWidget("dcfx"), PlotWidget("dcfy"), PlotWidget("dcfz"), PlotWidget("dcmx"), PlotWidget("dcmy"), PlotWidget("dcmz")]
self.dockList = []
for widget in self.plotWidgets :
dock = self.addSimpleWidget(widget.getTitle(), widget)
insertIndex = len(self.dockList) - 1
self.dockList.insert(insertIndex, dock)
if len(self.dockList) > 1:
for index in range(0, len(self.dockList) - 1):
self.tabifyDockWidget(self.dockList[index],
self.dockList[index + 1])
self.dockList[0].raise_()
self.nextindex = 1
# ===============================================================================================
# actions
# ===============================================================================================
self.comboBoxXAxis.currentIndexChanged.connect(self.fire_XAxisChanged)
self.comboBoxCtrlSurUID.currentIndexChanged.connect(self.fire_CtrlSurfacesChanged)
self.buttonBox.button(QtGui.QDialogButtonBox.Ok).clicked.connect(self.plot)
self.buttonBox.button(QtGui.QDialogButtonBox.Reset).clicked.connect(self.reset)
self.buttonBox.button(QtGui.QDialogButtonBox.Cancel).clicked.connect(self.close)
def addSimpleWidget(self, name, widget):
''' create dock widget and set it to main window'''
dock = QtGui.QDockWidget(name)
dock.setWidget(widget)
dock.setMinimumWidth(100)
dock.setMinimumHeight(300)
dock.setAllowedAreas(QtCore.Qt.AllDockWidgetAreas)
dock.setFeatures(QtGui.QDockWidget.DockWidgetClosable |
QtGui.QDockWidget.DockWidgetMovable |
QtGui.QDockWidget.DockWidgetFloatable)
self.addDockWidget(QtCore.Qt.BottomDockWidgetArea, dock)
return dock
def fire_XAxisChanged(self, idx):
'''sets all options if the x-axis was changed'''
self.reset()
self.hidePlotLists(idx == 0, idx == 1, idx == 2, idx == 3, idx == 4)
def fire_CtrlSurfacesChanged(self, idx):
'''sets all options if the controlSurface was changed'''
self.reset()
self.listRelDefl.clear()
for item in self.getRelDeflectionVector("/cpacs/vehicles/aircraft/model[1]/analyses/aeroPerformanceMap", self.comboBoxCtrlSurUID.currentText()):
self.listRelDefl.addItem(str(item))
def plot(self):
'''updates all observer plot widgets'''
path = "/cpacs/vehicles/aircraft/model[1]/analyses/aeroPerformanceMap"
x_axis_idx = self.comboBoxXAxis.currentIndex()
# indices of the lists
mach_idx = self.listMachNum.currentRow()
reyn_idx = self.listReynoldsNum.currentRow()
yaw_idx = self.listAngleOfYaw.currentRow()
att_idx = self.listAngleOfAtt.currentRow()
relDef_idx = self.listRelDefl.currentRow()
# get uid of chosen controlSurfaces
relDef_uid = self.comboBoxCtrlSurUID.currentText()
# determine x-axis
if x_axis_idx == 0 :
x_axis = self.getMachNumberVector(path)
elif x_axis_idx == 1 :
x_axis = self.getReynoldsNumberVector(path)
elif x_axis_idx == 2 :
x_axis = self.getAngleOfYawVector(path)
elif x_axis_idx == 3 :
x_axis = self.getAngleOfAttackVector(path)
elif x_axis_idx == 4 :
x_axis = self.getRelDeflectionVector(path, relDef_uid)
# dimSize == product over all sizes (for complete array size)
# cnt_mach, cnt_reyn, cnt_angleYaw, cnt_angleAtt) == size of coefficients
((cnt_mach, cnt_reyn, cnt_angleYaw, cnt_angleAtt), size) = self.tixi.getArrayDimensionSizes(path, 4)
# the same for controlSurface
((cnt_relDef,_), _) = self.tixi.getArrayDimensionSizes(path + "/controlSurfaces/controlSurface["
+ str(self.tixiGetIdxOfUID(relDef_uid)) + "]", 2)
# determine complete array size (including relDeflection)
size = size * cnt_relDef
# set drawing option
displayOpt = 'go' if self.comboBoxPlotPnt.currentText() == "points" else ""
dimPos = [mach_idx, reyn_idx, yaw_idx, att_idx, relDef_idx]
dimSize = [cnt_mach, cnt_reyn, cnt_angleYaw, cnt_angleAtt, cnt_relDef]
dims = 5 # self.tixi.getArrayDimensions(path + "/controlSurfaces/controlSurface[" + str(self.tixiGetIdxOfUID(relDef_uid)) + "]") + oben dims
# update all observer
for widget in self.plotWidgets:
# determine coefficient array
array = self.getCoefficientArray(path + "/controlSurfaces/controlSurface[1]", widget.getTitle(), size)
widget.setXLabel(self.comboBoxXAxis.currentText())
widget.updatePlot(array, dimSize, dimPos, dims, x_axis, x_axis_idx, self.tixi, path, displayOpt)
def reset(self):
'''resets all observer'''
for widget in self.plotWidgets:
widget.updateReset()
def tixiGetIdxOfUID(self, uID):
"""determines the index of a given controlSurface uID
Args:
uID (String): controlSurface uID
Returns:
the index of the controlSurface with the given uID
"""
path = "/cpacs/vehicles/aircraft/model[1]/analyses/aeroPerformanceMap/controlSurfaces"
for i in range(1, self.tixi.getNumberOfChilds(path) +1 ) :
tmp_uid = self.tixi.getTextElement(path + "/controlSurface[" + str(i) + "]/controlSurfaceUID")
if uID == tmp_uid :
return i
return None
def fillPlotLists(self, path):
"""fills the five list boxes
Args:
path (String): path to aeroPerformanceMap
"""
for item in self.getMachNumberVector(path) :
self.listMachNum.addItem(str(item))
for item in self.getReynoldsNumberVector(path) :
self.listReynoldsNum.addItem(str(item))
for item in self.getAngleOfYawVector(path) :
self.listAngleOfYaw.addItem(str(item))
for item in self.getAngleOfAttackVector(path) :
self.listAngleOfAtt.addItem(str(item))
for i in range(1, self.tixi.getNumberOfChilds(path + "/controlSurfaces") +1) :
uid = self.tixi.getTextElement(path + "/controlSurfaces/controlSurface[" + str(i) + "]/controlSurfaceUID")
self.comboBoxCtrlSurUID.addItem(uid)
if(i == 1): # pre-fill relDeflection list
for item in self.getRelDeflectionVector(path, uid):
self.listRelDefl.addItem(str(item))
def getAngleOfYawVector(self, path):
return self.tixi.getFloatVector(path + "/angleOfYaw", self.tixi.getVectorSize(path + "/angleOfYaw"))
def getAngleOfAttackVector(self, path):
return self.tixi.getFloatVector(path + "/angleOfAttack", self.tixi.getVectorSize(path + "/angleOfAttack"))
def getReynoldsNumberVector(self, path):
return self.tixi.getFloatVector(path + "/reynoldsNumber", self.tixi.getVectorSize(path + "/reynoldsNumber"))
def getMachNumberVector(self, path):
return self.tixi.getFloatVector(path + "/machNumber", self.tixi.getVectorSize(path + "/machNumber"))
def getRelDeflectionVector(self, path, uid):
"""returns relDeflection of a controlSurface given by a uid
Args:
path (String): path to aeroPerformanceMap
"""
for i in range(1, self.tixi.getNumberOfChilds(path) +1) :
_uid = self.tixi.getTextElement(path + "/controlSurfaces/controlSurface[" + str(i) + "]/controlSurfaceUID")
if(_uid == uid):
p = path + "/controlSurfaces/controlSurface[" + str(i) + "]/relDeflection"
return self.tixi.getFloatVector(p, self.tixi.getVectorSize(p))
return None
def getCoefficientArray(self, path, child, num):
"""returns the array of a given path, child node and element count
Args:
path (String): path to array
child (String): child node to array
num (int): count of elements
Returns:
the square root of n.
"""
return self.tixi.getArray(path, child, num)
# This function hides labels and plot lists.
def hidePlotLists(self, flag_mach, flag_reyn, flag_yaw, flag_att, flag_relDef):
"""hides labels and plot lists.
Args:
flag_mach (bool): hide label of machNumber and list of machNumber
flag_reyn (bool): hide label of reynoldNumber and list of reynoldNumber
flag_yaw (bool): hide label of angleOfYaw and list of angleOfYaw
flag_att (bool): hide label of angleOfAttack and list of angleOfAttack
flag_relDef (bool): hide label of relDeflection and list of relDeflection
"""
self.labelMachNum.setHidden(flag_mach)
self.labelReynoldsNum.setHidden(flag_reyn)
self.labelAngleOfYaw.setHidden(flag_yaw)
self.labelAngleOfAtt.setHidden(flag_att)
self.labelRelDefl.setHidden(flag_relDef)
self.listMachNum.setHidden(flag_mach)
self.listReynoldsNum.setHidden(flag_reyn)
self.listAngleOfYaw.setHidden(flag_yaw)
self.listAngleOfAtt.setHidden(flag_att)
self.listRelDefl.setHidden(flag_relDef)
def test_elements(self):
t = Tixi()
t.open(os.path.join("TestData", "in.xml"))
self.assertEqual(t.getTextElement("/plane/name"), "Junkers JU 52")
t.updateTextElement("/plane/name", "D150")
self.assertEqual(t.getTextElement("/plane/name"), "D150")
t.addTextElement("/plane", "name", "B747")
self.assertEqual(t.getTextElement("/plane/name[2]"), "B747")
self.assertEqual(t.getIntegerElement("/plane/numberOfPassengers"), 57)
t.addIntegerElement("/plane", "nop", 123456, None)
self.assertEqual(t.getIntegerElement("/plane/nop"), 123456)
self.assertEqual(t.getDoubleElement("/plane/wings[1]/wing[1]/centerOfGravity/x"), 30.0)
t.addDoubleElement("/plane/wings/wing[1]", "cog", 123.456, None)
self.assertEqual(t.getDoubleElement("/plane/wings/wing[1]/cog"), 123.456)
self.assertFalse(t.getBooleanElement("/plane/bool/aBool2"))
self.assertTrue(t.getBooleanElement("/plane/bool/aBool1b"))
self.assertFalse(t.checkElement("/plane/xx")) #ELEMENT_NOT_FOUND
t.createElement("/plane", "xx")
t.checkElement("/plane/xx")
self.assertEquals(t.getTextElement("/plane/xx"), "")
t.updateTextElement("/plane/xx", "value")
self.assertEquals(t.getTextElement("/plane/xx"), "value")
t.removeElement("/plane/xx")
self.assertEqual(t.checkElement("/plane/xx"),False)
self.assertRaises(TixiException, t.getTextElement, "/plane/xx") #ELEMENT_NOT_FOUND
def test_open_http(self):
t = Tixi()
t.openHttp("http://www.w3schools.com/XML/note.xml")
t.close()
def test_open_string(self):
t = Tixi()
cpacs = '<?xml version="1.0"?><cpacs><header><version>1.2.3</version></header></cpacs>'
t.openString(cpacs)
t.close()
def __init__(self, parent=None):
super(Plotter_DamingDerivates, self).__init__(parent)
self.tixi = Tixi()
self.tixi.open("../cpacs_files/outputfile_PM_Ref.xml")
self.buttonBox = QtGui.QDialogButtonBox()
self.buttonBox.addButton(QtGui.QDialogButtonBox.Ok)
self.buttonBox.addButton(QtGui.QDialogButtonBox.Reset)
self.buttonBox.addButton(QtGui.QDialogButtonBox.Cancel)
self.comboBoxXAxis = QtGui.QComboBox()
self.comboBoxXAxis.addItem("machNumber")
self.comboBoxXAxis.addItem("reynoldsNumber")
self.comboBoxXAxis.addItem("angleOfYaw")
self.comboBoxXAxis.addItem("angleOfAttack")
self.comboBoxPlotPnt = QtGui.QComboBox()
self.comboBoxPlotPnt.addItem("curve")
self.comboBoxPlotPnt.addItem("points")
self.labelXAxis = QtGui.QLabel("set x-axis")
self.labelDisplay = QtGui.QLabel("display")
self.labelMachNum = QtGui.QLabel("machNumber")
self.labelReynoldsNum = QtGui.QLabel("reynoldsNumber")
self.labelAngleOfYaw = QtGui.QLabel("angleOfYaw")
self.labelAngleOfAtt = QtGui.QLabel("angleOfAttack")
self.listMachNum = QtGui.QListWidget()
self.listReynoldsNum = QtGui.QListWidget()
self.listAngleOfYaw = QtGui.QListWidget()
self.listAngleOfAtt = QtGui.QListWidget()
self.__hidePlotLists(True, False, False, False)
self.__fillPlotLists("/cpacs/vehicles/aircraft/model[1]/analyses/aeroPerformanceMap")
self.grid = QtGui.QGridLayout()
self.grid.addWidget(self.labelXAxis, 0,0,1,3)
self.grid.addWidget(self.labelDisplay, 0,3)
self.grid.addWidget(self.comboBoxXAxis, 1,0,1,3)
self.grid.addWidget(self.comboBoxPlotPnt, 1,3)
self.grid.addWidget(self.labelMachNum, 2,0)
self.grid.addWidget(self.listMachNum, 3,0)
self.grid.addWidget(self.labelReynoldsNum, 2,1)
self.grid.addWidget(self.listReynoldsNum, 3,1)
self.grid.addWidget(self.labelAngleOfYaw, 2,2)
self.grid.addWidget(self.listAngleOfYaw, 3,2)
self.grid.addWidget(self.labelAngleOfAtt, 2,3)
self.grid.addWidget(self.listAngleOfAtt, 3,3)
# set the layout
layout = QtGui.QGridLayout()
layout.addLayout(self.grid, 0,0,1,3)
layout.addWidget(self.buttonBox, 5, 0, 1,3)
widget = QtGui.QWidget()
widget.setLayout(layout)
self.setCentralWidget(widget)
self.plotWidgets = [PlotWidget("dcfxdpstar"), PlotWidget("dcfxdqstar"), PlotWidget("dcfxdrstar"),
PlotWidget("dcfydpstar"), PlotWidget("dcfydqstar"), PlotWidget("dcfydrstar"),
PlotWidget("dcfzdpstar"), PlotWidget("dcfzdqstar"), PlotWidget("dcfzdrstar"),
PlotWidget("dcmxdpstar"), PlotWidget("dcmxdqstar"), PlotWidget("dcmxdrstar"),
PlotWidget("dcmydpstar"), PlotWidget("dcmydqstar"), PlotWidget("dcmydrstar"),
PlotWidget("dcmzdpstar"), PlotWidget("dcmzdqstar"), PlotWidget("dcmzdrstar")]
i = 0 ; l = len(self.plotWidgets) / 4
for widget in self.plotWidgets :
if i < l :
self.addSimpleWidget(widget, QtCore.Qt.LeftDockWidgetArea, True)
elif i < 2 * l :
self.addSimpleWidget(widget, QtCore.Qt.RightDockWidgetArea, True)
else :
self.addSimpleWidget(widget, QtCore.Qt.BottomDockWidgetArea, False)
i+=1
# ===============================================================================================
# actions
# ===============================================================================================
self.comboBoxXAxis.currentIndexChanged.connect(self.fire_XAxisChanged)
self.buttonBox.button(QtGui.QDialogButtonBox.Ok).clicked.connect(self.plot)
self.buttonBox.button(QtGui.QDialogButtonBox.Reset).clicked.connect(self.reset)
self.buttonBox.button(QtGui.QDialogButtonBox.Cancel).clicked.connect(self.close)
def test_create(self):
t = Tixi()
t.create("cpacs")
self.assertTrue(t._handle != -1)
t.close()
class MainWidget(QtGui.QWidget):
def __init__(self, parent = None):
super(MainWidget, self).__init__(parent)
self.tixi = Tixi()
self.tigl = Tigl()
self.loadFile(Config.path_cpacs_A320_Fuse, Config.path_cpacs_21_schema)
buttonAirf = QtGui.QPushButton("airfoil")
buttonFuse = QtGui.QPushButton("fuselage")
grid = QtGui.QGridLayout()
grid.addWidget(buttonAirf, 0,0)
grid.addWidget(buttonFuse, 0,1)
self.setWindowTitle('Profile-Editor-Widget')
self.setLayout(grid)
self.resize(560,520)
# fuse or airfoil window
self.window = None
# actions
buttonAirf.clicked.connect(self.fire_AirfoilMainWidget)
buttonFuse.clicked.connect(self.fire_FuselageMainWidget)
def loadFile(self, filePath, cpacsSchema):
"""loads a cpacs file with tixi and tigl.
Args:
filePath (String): path to cpacs file
cpacsSchema (String): path to cpacs schema file
"""
try:
print filePath
self.tixi.openDocument(filePath)
self.tixi.schemaValidateFromFile(cpacsSchema)
try:
self.tigl.open(self.tixi,"")
except TiglException as e:
QtGui.QMessageBox.information(self, "Error", "TIGL: " + str(e.error))
except TixiException as e:
msgBox = QtGui.QMessageBox()
msgBox.setText('open file or exit application')
btnOpen = QtGui.QPushButton('open')
msgBox.addButton(btnOpen, QtGui.QMessageBox.YesRole)
btnExit = QtGui.QPushButton('exit')
msgBox.addButton(btnExit, QtGui.QMessageBox.NoRole)
if msgBox.exec_() == 0 :
(filePath,_) = QtGui.QFileDialog.getOpenFileName(self, 'Open file')
self.loadFile(filePath, cpacsSchema)
else:
sys.exit()
def getVectorX(self, prof_uid):
xpath = self.tixi.uIDGetXPath(prof_uid)
numX = self.tixi.getVectorSize(xpath + "/pointList/x")
return self.tixi.getFloatVector(xpath + "/pointList/x",numX)
def getVectorY(self, prof_uid):
xpath = self.tixi.uIDGetXPath(prof_uid)
numY = self.tixi.getVectorSize(xpath + "/pointList/y")
return self.tixi.getFloatVector(xpath + "/pointList/y",numY)
def getVectorZ(self, prof_uid):
xpath = self.tixi.uIDGetXPath(prof_uid)
numZ = self.tixi.getVectorSize(xpath + "/pointList/z")
return self.tixi.getFloatVector(xpath + "/pointList/z",numZ)
def createPointList(self, uID) :
"""creates a point list with profile points of given uID
Args:
uID (String): uID from cpacs profile
Returns:
lists of top and bottom profile points in format [ [x0,y0,z0] , [x1,y1,z1] , ... ]
"""
vecX = self.getVectorX(uID)
vecY = self.getVectorY(uID)
vecZ = self.getVectorZ(uID)
res = []
for i in range(len(vecX)) :
res.append([vecX[i], vecY[i], vecZ[i]])
return res
def fire_AirfoilMainWidget(self, uid='NACA0000'):
self.window = AirfoilMainWidget( Airfoil(uid, self.tigl, self.createPointList(uid)) )
def fire_FuselageMainWidget(self, uid='CircleProfile'):
self.window = FuselageMainWidget( Fuselage(uid, self.tigl, self.createPointList(uid)) )
def test_api(self):
t = Tixi()
self.assertEquals(t.version, t.getVersion())
t.create("root")
t.addDoubleElement("/root","myDouble",3.2,0)
t.addIntegerElement("/root","myInteger",6,None)
# Here starts the rest
t.addBooleanElement("/root","myBoolean",0)
t.updateDoubleElement("/root/myDouble",3.14159262,0)
t.updateIntegerElement("/root/myInteger",7,None)
t.updateBooleanElement("/root/myBoolean",1)
t.addTextElementAtIndex("/root","myNewTextElement","myText",2)
t.createElementAtIndex("/root","array",0)
t.addFloatVector("/root","myFloatVector",(0.0,1.1,2.2),3, "%g")
t.addExternalLink("/root","/externalLink",".xml")
t.addHeader("tool","version","author")
t.addCpacsHeader("name","creator","version","description","cpacsVersion")
t.usePrettyPrint(1)
t.uIDCheckLinks()
t.uIDSetToXPath("/root/myBoolean","booleanID")
self.assertEqual(t.uIDGetXPath("booleanID"),"/root/myBoolean")
#t.dTDValidate()
#t.xSLTransformationToFile()
t.save(os.path.join("TestData", "test_save.xml"))
t.close()
t.cleanup()
def test_attributes(self):
t = Tixi()
t.open(os.path.join("TestData", "in.xml"))
self.assertEquals(t.getTextAttribute("/plane/wings/wing[1]", "position"), "left")
self.assertEquals(t.getIntegerAttribute("/plane/wings", "numberOfWings"), 2)
t.addIntegerAttribute("/plane", "intattr", 324, None)
self.assertEquals(t.getIntegerAttribute("/plane", "intattr"), 324)
t.removeAttribute("/plane", "intattr")
self.assertEquals(t.getDoubleAttribute("/plane/coordinateOrigin", "scaling"), 1.3456)
self.assertFalse(t.checkAttribute("/plane", "doubleattr")) # ATTRIBUTE_NOT_FOUND \n
t.addDoubleAttribute("/plane", "doubleattr", 123.456, None)
t.checkAttribute("/plane", "doubleattr")
self.assertEquals(t.getDoubleAttribute("/plane", "doubleattr"), 123.456)
t.removeAttribute("/plane", "doubleattr")
t.addTextAttribute("/plane", "attr", "val")
self.assertEquals(t.getTextAttribute("/plane", "attr"), "val")
self.assertEquals(t.getNamedChildrenCount("/plane/wings", "wing"), 2)
t.addDoubleListWithAttributes("/plane", "list", "elem", "attr", [1., 2., 3.], None, ["a", "b", "c"], 3)
self.assertEquals(t.getTextAttribute("/plane/list/elem[1]", "attr"), "a")
self.assertEquals(t.getDoubleElement("/plane/list/elem[3]"), 3.0)
t.close()
def __init__(self, path, parent=None):
super(Plotter, self).__init__(parent)
self.tixi = Tixi()
t = self.tixi.open(Config.path_cpacs_pm_ref)
self.pathPerMap = "/cpacs/vehicles/aircraft/model[1]/analyses/aeroPerformanceMap"
self.path_specific = path
self.buttonBox = QtGui.QDialogButtonBox()
self.buttonBox.addButton(QtGui.QDialogButtonBox.Ok)
self.buttonBox.addButton(QtGui.QDialogButtonBox.Reset)
self.buttonBox.addButton(QtGui.QDialogButtonBox.Cancel)
self.comboBoxXAxis = QtGui.QComboBox()
self.comboBoxXAxis.addItem("machNumber")
self.comboBoxXAxis.addItem("reynoldsNumber")
self.comboBoxXAxis.addItem("angleOfYaw")
self.comboBoxXAxis.addItem("angleOfAttack")
self.comboBoxPlotPnt = QtGui.QComboBox()
self.comboBoxPlotPnt.addItem("curve")
self.comboBoxPlotPnt.addItem("points")
self.labelXAxis = QtGui.QLabel("set x-axis")
self.labelDisplay = QtGui.QLabel("display")
self.labelMachNum = QtGui.QLabel("machNumber")
self.labelReynoldsNum = QtGui.QLabel("reynoldsNumber")
self.labelAngleOfYaw = QtGui.QLabel("angleOfYaw")
self.labelAngleOfAtt = QtGui.QLabel("angleOfAttack")
self.listMachNum = QtGui.QListWidget()
self.listReynoldsNum = QtGui.QListWidget()
self.listAngleOfYaw = QtGui.QListWidget()
self.listAngleOfAtt = QtGui.QListWidget()
#self.comboBoxXAxis.setCurrentIndex(0)
self.__hidePlotLists(True, False, False, False)
self.__fillPlotLists(self.pathPerMap)
self.grid = QtGui.QGridLayout()
self.grid.addWidget(self.labelXAxis, 0,0,1,3)
self.grid.addWidget(self.labelDisplay, 0,3)
self.grid.addWidget(self.comboBoxXAxis, 1,0,1,3)
self.grid.addWidget(self.comboBoxPlotPnt, 1,3)
self.grid.addWidget(self.labelMachNum, 2,0)
self.grid.addWidget(self.listMachNum, 3,0)
self.grid.addWidget(self.labelReynoldsNum, 2,1)
self.grid.addWidget(self.listReynoldsNum, 3,1)
self.grid.addWidget(self.labelAngleOfYaw, 2,2)
self.grid.addWidget(self.listAngleOfYaw, 3,2)
self.grid.addWidget(self.labelAngleOfAtt, 2,3)
self.grid.addWidget(self.listAngleOfAtt, 3,3)
# set the layout
layout = QtGui.QGridLayout()
layout.addLayout(self.grid, 0,0,1,3)
layout.addWidget(self.buttonBox, 5, 0, 1,3)
widget = QtGui.QWidget()
widget.setLayout(layout)
self.setCentralWidget(widget)
# ===============================================================================================
# actions
# ===============================================================================================
self.comboBoxXAxis.currentIndexChanged.connect(self.fire_XAxisChanged)
self.buttonBox.button(QtGui.QDialogButtonBox.Ok).clicked.connect(self.plot)
self.buttonBox.button(QtGui.QDialogButtonBox.Reset).clicked.connect(self.reset)
self.buttonBox.button(QtGui.QDialogButtonBox.Cancel).clicked.connect(self.close)
def test_vector_array(self):
t = Tixi()
t.open(os.path.join("TestData", "vectorcount.xml"))
self.assertEquals(t.getVectorSize("/a/aeroPerformanceMap/cfx"), 32)
#v = t.getFloatVector("/a/aeroPerformanceMap/cfx", 32)
#print v[0], v[1], v[-1]
#1 2 118
t.close()
# manual creation of vector
t.create('doc')
t.addFloatVector('/doc', 'myvec', range(100, 130), 30, "%g")
size = t.getVectorSize('/doc/myvec')
self.assertEquals(size, 30)
v = t.getFloatVector('/doc/myvec', 30)
self.assertEquals(v, tuple(range(100, 130)))
t.close()
t.open(os.path.join("TestData", "arraytests.xml"))
self.assertEquals(t.getArrayDimensions("/root/aeroPerformanceMap"), 4)
self.assertEquals(
t.getArrayDimensionSizes("/root/aeroPerformanceMap", 4),
((1, 2, 3, 8), 48))
self.assertEquals(
t.getArrayDimensionNames("/root/aeroPerformanceMap", 4),
("machNumber", "reynoldsNumber", "angleOfYaw", "angleOfAttack"))
# print t.getArrayDimensionValues("/root/aeroPerformanceMap", 0) 1.0
# print t.getArrayDimensionValues("/root/aeroPerformanceMap", 2) 0 5 10
self.assertEquals(t.getArrayParameters("/root/aeroPerformanceMap"), 7)
# print t.getArrayParameterNames("/root/aeroPerformanceMap") ("cfx", "cfy", "cfz", "cmx", "cmy", "cmz", "def")
# print t.getArray("/root/aeroPerformanceMap", "cmx") None
# print t.getArrayValue(arr, "/root/aeroPerformanceMap", "angleOfAttack")
#8
#print t.getArrayElementNames("/root/aeroPerformanceMap", "vector")
#print t.getArrayElementNames("/root/aeroPerformanceMap", "array")
t.getArrayElementCount("/root/aeroPerformanceMap", "array")
t.createElement("/root", "p1")
t.addPoint("/root/p1", 1, 2, 3, None)
self.assertEquals(t.getPoint("/root/p1"), (1.0, 2.0, 3.0))
self.assertEquals(
t.xPathEvaluateNodeNumber("/root/aeroPerformanceMap"), 1)
t.close()
t.open(os.path.join("TestData", "in.xml"))
self.assertEquals(
t.xPathExpressionGetTextByIndex(
"/plane/wings/wing/centerOfGravity/x", 2), "30.0")
t.close()
t.open(os.path.join("TestData", "uid_correct.xml"))
t.uIDCheckDuplicates()
t.uIDCheckExists("schlumpf")
t.close()
t.open(os.path.join("TestData", "uid_duplicated.xml"))
self.assertRaises(TixiException, t.uIDCheckDuplicates) #UID_NOT_UNIQUE
def python_demo(filename):
tixi = Tixi()
tigl = Tigl()
# open cpacs xml with tixi
try:
tixi.open(filename)
except:
print 'Error opening cpacs file with TiXI'
return
# enable logging of errors and warnings into file
tigl.logSetFileEnding('txt')
tigl.logSetTimeInFilenameEnabled(TiglBoolean.TIGL_FALSE)
tigl.logToFileEnabled('demolog')
# open cpacs with tigl
try:
tigl.open(tixi, '')
except:
print 'Error opening cpacs file with TiGL'
return
# query number of wings and fuselages and their names
nWings = tigl.getWingCount()
nFuselages = tigl.getFuselageCount()
for i in range(1,nWings+1):
wingUID = tigl.wingGetUID(i)
print 'Wing %d name: %s' % (i, wingUID)
for i in range(1,nFuselages+1):
fuselageUID = tigl.fuselageGetUID(i)
print 'Fuselage %d name: %s' % (i, fuselageUID)
# query point on the upper wing surface
if nWings > 0:
(x,y,z) = tigl.wingGetUpperPoint(1, 1, 0.5, 0.5)
print 'Point on upper wing surface of wing 1/segment 1: (x,y,z) = (%g, %g, %g)' %(x, y, z)
# compute intersection of wing with a x-z plane
if nWings > 0:
wingUID = tigl.wingGetUID(1)
# do the intersection with a plane at p = (0,0.5,0) and normal vector n = (0,1,0)
int_id = tigl.intersectWithPlane(wingUID, 0, 0.5, 0, 0, 1, 0)
# get number of intersection wires
nlines = tigl.intersectGetLineCount(int_id)
# query points on the first line
if nlines > 0:
zeta = 0.
print '\nIntersection points of a plane with first wing:'
while zeta < 1:
(x,y,z) = tigl.intersectGetPoint(int_id, 1, zeta)
print 'zeta = %g\tp=(%g, %g, %g)' % (zeta, x, y, z)
zeta = zeta + 0.1
print
# Export geometry to iges file
print 'Exporting geometry to igesexport.igs'
tigl.exportIGES('igesexport.igs')
tigl.logToFileDisabled()
tigl.close()
tixi.close()
tixi.cleanup()
def test_api(self):
t = Tixi()
self.assertEquals(t.version, t.getVersion())
t.create("root")
t.addDoubleElement("/root", "myDouble", 3.2, 0)
t.addIntegerElement("/root", "myInteger", 6, None)
# Here starts the rest
t.addBooleanElement("/root", "myBoolean", 0)
t.updateDoubleElement("/root/myDouble", 3.14159262, 0)
t.updateIntegerElement("/root/myInteger", 7, None)
t.updateBooleanElement("/root/myBoolean", 1)
t.addTextElementAtIndex("/root", "myNewTextElement", "myText", 2)
t.createElementAtIndex("/root", "array", 0)
t.addFloatVector("/root", "myFloatVector", (0.0, 1.1, 2.2), 3, "%g")
t.addExternalLink("/root", "/externalLink", ".xml")
t.addHeader("tool", "version", "author")
t.addCpacsHeader("name", "creator", "version", "description",
"cpacsVersion")
t.usePrettyPrint(1)
t.uIDCheckLinks()
t.uIDSetToXPath("/root/myBoolean", "booleanID")
self.assertEqual(t.uIDGetXPath("booleanID"), "/root/myBoolean")
#t.dTDValidate()
#t.xSLTransformationToFile()
t.save(os.path.join("TestData", "test_save.xml"))
t.close()
t.cleanup()
class Plotter_DamingDerivates(QtGui.QMainWindow):
def __init__(self, parent=None):
super(Plotter_DamingDerivates, self).__init__(parent)
self.tixi = Tixi()
self.tixi.open("../cpacs_files/outputfile_PM_Ref.xml")
self.buttonBox = QtGui.QDialogButtonBox()
self.buttonBox.addButton(QtGui.QDialogButtonBox.Ok)
self.buttonBox.addButton(QtGui.QDialogButtonBox.Reset)
self.buttonBox.addButton(QtGui.QDialogButtonBox.Cancel)
self.comboBoxXAxis = QtGui.QComboBox()
self.comboBoxXAxis.addItem("machNumber")
self.comboBoxXAxis.addItem("reynoldsNumber")
self.comboBoxXAxis.addItem("angleOfYaw")
self.comboBoxXAxis.addItem("angleOfAttack")
self.comboBoxPlotPnt = QtGui.QComboBox()
self.comboBoxPlotPnt.addItem("curve")
self.comboBoxPlotPnt.addItem("points")
self.labelXAxis = QtGui.QLabel("set x-axis")
self.labelDisplay = QtGui.QLabel("display")
self.labelMachNum = QtGui.QLabel("machNumber")
self.labelReynoldsNum = QtGui.QLabel("reynoldsNumber")
self.labelAngleOfYaw = QtGui.QLabel("angleOfYaw")
self.labelAngleOfAtt = QtGui.QLabel("angleOfAttack")
self.listMachNum = QtGui.QListWidget()
self.listReynoldsNum = QtGui.QListWidget()
self.listAngleOfYaw = QtGui.QListWidget()
self.listAngleOfAtt = QtGui.QListWidget()
self.__hidePlotLists(True, False, False, False)
self.__fillPlotLists("/cpacs/vehicles/aircraft/model[1]/analyses/aeroPerformanceMap")
self.grid = QtGui.QGridLayout()
self.grid.addWidget(self.labelXAxis, 0,0,1,3)
self.grid.addWidget(self.labelDisplay, 0,3)
self.grid.addWidget(self.comboBoxXAxis, 1,0,1,3)
self.grid.addWidget(self.comboBoxPlotPnt, 1,3)
self.grid.addWidget(self.labelMachNum, 2,0)
self.grid.addWidget(self.listMachNum, 3,0)
self.grid.addWidget(self.labelReynoldsNum, 2,1)
self.grid.addWidget(self.listReynoldsNum, 3,1)
self.grid.addWidget(self.labelAngleOfYaw, 2,2)
self.grid.addWidget(self.listAngleOfYaw, 3,2)
self.grid.addWidget(self.labelAngleOfAtt, 2,3)
self.grid.addWidget(self.listAngleOfAtt, 3,3)
# set the layout
layout = QtGui.QGridLayout()
layout.addLayout(self.grid, 0,0,1,3)
layout.addWidget(self.buttonBox, 5, 0, 1,3)
widget = QtGui.QWidget()
widget.setLayout(layout)
self.setCentralWidget(widget)
self.plotWidgets = [PlotWidget("dcfxdpstar"), PlotWidget("dcfxdqstar"), PlotWidget("dcfxdrstar"),
PlotWidget("dcfydpstar"), PlotWidget("dcfydqstar"), PlotWidget("dcfydrstar"),
PlotWidget("dcfzdpstar"), PlotWidget("dcfzdqstar"), PlotWidget("dcfzdrstar"),
PlotWidget("dcmxdpstar"), PlotWidget("dcmxdqstar"), PlotWidget("dcmxdrstar"),
PlotWidget("dcmydpstar"), PlotWidget("dcmydqstar"), PlotWidget("dcmydrstar"),
PlotWidget("dcmzdpstar"), PlotWidget("dcmzdqstar"), PlotWidget("dcmzdrstar")]
i = 0 ; l = len(self.plotWidgets) / 4
for widget in self.plotWidgets :
if i < l :
self.addSimpleWidget(widget, QtCore.Qt.LeftDockWidgetArea, True)
elif i < 2 * l :
self.addSimpleWidget(widget, QtCore.Qt.RightDockWidgetArea, True)
else :
self.addSimpleWidget(widget, QtCore.Qt.BottomDockWidgetArea, False)
i+=1
# ===============================================================================================
# actions
# ===============================================================================================
self.comboBoxXAxis.currentIndexChanged.connect(self.fire_XAxisChanged)
self.buttonBox.button(QtGui.QDialogButtonBox.Ok).clicked.connect(self.plot)
self.buttonBox.button(QtGui.QDialogButtonBox.Reset).clicked.connect(self.reset)
self.buttonBox.button(QtGui.QDialogButtonBox.Cancel).clicked.connect(self.close)
def addSimpleWidget(self,widget, dockWidgetArea, flag_side):
dock = QtGui.QDockWidget()
dock.setWidget(widget)
if flag_side :
dock.setMinimumWidth(100)
dock.setMinimumHeight(100)
else:
dock.setMinimumWidth(100)
dock.setMinimumHeight(100)
dock.setAllowedAreas(dockWidgetArea)
dock.setFeatures(QtGui.QDockWidget.DockWidgetClosable |
QtGui.QDockWidget.DockWidgetMovable |
QtGui.QDockWidget.DockWidgetFloatable)
self.addDockWidget(dockWidgetArea, dock)
def fire_XAxisChanged(self, idx):
self.reset()
self.__setPlotListVisibility(idx == 0, idx == 1, idx == 2, idx == 3)
def plot(self):
x_axis_idx = self.comboBoxXAxis.currentIndex()
mach_idx = self.listMachNum.currentRow()
reyn_idx = self.listReynoldsNum.currentRow()
yaw_idx = self.listAngleOfYaw.currentRow()
att_idx = self.listAngleOfAtt.currentRow()
path = "/cpacs/vehicles/aircraft/model[1]/analyses/aeroPerformanceMap"
if x_axis_idx == 0 :
x_axis = self.getMachNumberVector(path)
elif x_axis_idx == 1 :
x_axis = self.getReynoldsNumberVector(path)
elif x_axis_idx == 2 :
x_axis = self.getAngleOfYawVector(path)
elif x_axis_idx == 3 :
x_axis = self.getAngleOfAttackVector(path)
((mach, reyn, angleYaw, angleAtt), dimSize) = self.tixi.getArrayDimensionSizes(path, 4)
display = self.comboBoxPlotPnt.currentText()
displayOpt = 'go' if display == "points" else ""
for widget in self.plotWidgets:
array = self.getCoefficientArray(path + "/dampingDerivatives/positiveRates", widget.getTitle(), dimSize)
widget.setXLabel(self.comboBoxXAxis.currentText())
widget.updatePlot(self.tixi, x_axis_idx, mach_idx, reyn_idx, yaw_idx, att_idx, mach, reyn, angleYaw, angleAtt, x_axis, array, path, displayOpt)
def reset(self):
for widget in self.plotWidgets:
widget.updateReset()
def __fillPlotLists(self, path):
for item in self.getMachNumberVector(path) :
self.listMachNum.addItem(str(item))
for item in self.getReynoldsNumberVector(path) :
self.listReynoldsNum.addItem(str(item))
for item in self.getAngleOfYawVector(path) :
self.listAngleOfYaw.addItem(str(item))
for item in self.getAngleOfAttackVector(path) :
self.listAngleOfAtt.addItem(str(item))
def getAngleOfYawVector(self, path):
return self.tixi.getFloatVector(path + "/angleOfYaw", self.tixi.getVectorSize(path + "/angleOfYaw"))
def getAngleOfAttackVector(self, path):
return self.tixi.getFloatVector(path + "/angleOfAttack", self.tixi.getVectorSize(path + "/angleOfAttack"))
def getReynoldsNumberVector(self, path):
return self.tixi.getFloatVector(path + "/reynoldsNumber", self.tixi.getVectorSize(path + "/reynoldsNumber"))
def getMachNumberVector(self, path):
return self.tixi.getFloatVector(path + "/machNumber", self.tixi.getVectorSize(path + "/machNumber"))
def getCoefficientArray(self, path, child, num):
return self.tixi.getArray(path, child, num)
def __hidePlotLists(self, flag_mach, flag_reyn, flag_yaw, flag_att):
self.__setPlotListVisibility(flag_mach, flag_reyn, flag_yaw, flag_att)
def __setPlotListVisibility(self, flag_mach, flag_reyn, flag_yaw, flag_att):
self.labelMachNum.setHidden(flag_mach)
self.labelReynoldsNum.setHidden(flag_reyn)
self.labelAngleOfYaw.setHidden(flag_yaw)
self.labelAngleOfAtt.setHidden(flag_att)
self.listMachNum.setHidden(flag_mach)
self.listReynoldsNum.setHidden(flag_reyn)
self.listAngleOfYaw.setHidden(flag_yaw)
self.listAngleOfAtt.setHidden(flag_att)
def test_create(self):
t = Tixi()
t.create("cpacs")
self.assertTrue(t._handle != -1)
t.close()
def test_attributes(self):
t = Tixi()
t.open(os.path.join("TestData", "in.xml"))
self.assertEquals(
t.getTextAttribute("/plane/wings/wing[1]", "position"), "left")
self.assertEquals(
t.getIntegerAttribute("/plane/wings", "numberOfWings"), 2)
t.addIntegerAttribute("/plane", "intattr", 324, None)
self.assertEquals(t.getIntegerAttribute("/plane", "intattr"), 324)
t.removeAttribute("/plane", "intattr")
self.assertEquals(
t.getDoubleAttribute("/plane/coordinateOrigin", "scaling"), 1.3456)
self.assertFalse(t.checkAttribute(
"/plane", "doubleattr")) # ATTRIBUTE_NOT_FOUND \n
t.addDoubleAttribute("/plane", "doubleattr", 123.456, None)
t.checkAttribute("/plane", "doubleattr")
self.assertEquals(t.getDoubleAttribute("/plane", "doubleattr"),
123.456)
t.removeAttribute("/plane", "doubleattr")
t.addTextAttribute("/plane", "attr", "val")
self.assertEquals(t.getTextAttribute("/plane", "attr"), "val")
self.assertEquals(t.getNamedChildrenCount("/plane/wings", "wing"), 2)
t.addDoubleListWithAttributes("/plane", "list", "elem", "attr",
[1., 2., 3.], None, ["a", "b", "c"], 3)
self.assertEquals(t.getTextAttribute("/plane/list/elem[1]", "attr"),
"a")
self.assertEquals(t.getDoubleElement("/plane/list/elem[3]"), 3.0)
t.close()
def python_demo(filename):
tixi = Tixi()
tigl = Tigl()
# open cpacs xml with tixi
try:
tixi.open(filename)
except:
print 'Error opening cpacs file with TiXI'
return
# enable logging of errors and warnings into file
tigl.logSetFileEnding('txt')
tigl.logSetTimeInFilenameEnabled(TiglBoolean.TIGL_FALSE)
tigl.logToFileEnabled('demolog')
# open cpacs with tigl
try:
tigl.open(tixi, '')
except:
print 'Error opening cpacs file with TiGL'
return
# query number of wings and fuselages and their names
nWings = tigl.getWingCount()
nFuselages = tigl.getFuselageCount()
for i in range(1, nWings + 1):
wingUID = tigl.wingGetUID(i)
print 'Wing %d name: %s' % (i, wingUID)
for i in range(1, nFuselages + 1):
fuselageUID = tigl.fuselageGetUID(i)
print 'Fuselage %d name: %s' % (i, fuselageUID)
# query point on the upper wing surface
if nWings > 0:
(x, y, z) = tigl.wingGetUpperPoint(1, 1, 0.5, 0.5)
print 'Point on upper wing surface of wing 1/segment 1: (x,y,z) = (%g, %g, %g)' % (
x, y, z)
# compute intersection of wing with a x-z plane
if nWings > 0:
wingUID = tigl.wingGetUID(1)
# do the intersection with a plane at p = (0,0.5,0) and normal vector n = (0,1,0)
int_id = tigl.intersectWithPlane(wingUID, 0, 0.5, 0, 0, 1, 0)
# get number of intersection wires
nlines = tigl.intersectGetLineCount(int_id)
# query points on the first line
if nlines > 0:
zeta = 0.
print '\nIntersection points of a plane with first wing:'
while zeta < 1:
(x, y, z) = tigl.intersectGetPoint(int_id, 1, zeta)
print 'zeta = %g\tp=(%g, %g, %g)' % (zeta, x, y, z)
zeta = zeta + 0.1
print
# Export geometry to iges file
print 'Exporting geometry to igesexport.igs'
tigl.exportIGES('igesexport.igs')
tigl.logToFileDisabled()
tigl.close()
tixi.close()
tixi.cleanup()