def Activated(self):
print("-----------------Wing Wizard-----------------")
selection = FreeCADGui.Selection.getSelectionEx()
if selection :
base = FreeCAD.ActiveDocument.getObject((selection[0].ObjectName))
PanelTable=[]
editor = WingEditorPanel()
editor.setupUi()
r = editor.form.exec_()
if r:
for row_number in range(editor.form.PanelTable.rowCount()):
rowData=[]
#create Panel
for col_number in range(10):#int(editor.form.PanelTable.columnCount())):
rowData.append(editor.form.PanelTable.item(row_number,col_number).text())
PanelTable.append(rowData)
_panelInput=PanelTable
_ribs=[]
_position=0
_PanelLength=[]
profil=[]
b=[]
#for i in range(0,obj.NberOfPanel) :
for i in range(0,editor.form.PanelTable.rowCount()) :
_row=_panelInput[i]
profil.append(_row[2])
_PanelLength.append(float(_row[4]))
# Add Rib Root
_ribs.append(FreeCAD.ActiveDocument.addObject("Part::FeaturePython","RibRoot_"+str(i)))
#WingRibs(obj,_profil,_nacagene,_nacaNbrPoint,_chord,_x,_y,_z,_xrot,_yrot,_zrot,_thickness=0,_useSpline = True,_finite_TE = False,_splitSpline = False):
#def (obj,_profil,_nacagene,_nacaNbrPoint,_chord,_x,_y,_z,_xrot,_yrot,_zrot,_rot=0,_thickness=0,_useSpline = True,_finite_TE = False,_splitSpline = False):
WingRib(_ribs[i*2],_row[2],False,0,_row[3],_row[6],_position,_row[8],0,0,0)
#FreeCAD.ActiveDocument.recompute()
ViewProviderWingRib(_ribs[i*2].ViewObject)
# Add Rib tip
_position=_position+float(_row[5])
_ribs.append(FreeCAD.ActiveDocument.addObject("Part::FeaturePython","RibTip_"+str(i)))
WingRib(_ribs[i*2+1],_row[2],False,0,_row[4],_row[7],_position,_row[9],0,0,0)
#FreeCAD.ActiveDocument.recompute()
ViewProviderWingRib(_ribs[i*2+1].ViewObject)
# Add wing panel
obj=FreeCAD.ActiveDocument.addObject("Part::FeaturePython","WingPanel")
#WingPanel(obj, _rootRib ,_tipRib ,_rootChord=200,_tipChord=100,_panelLength=100,_tipTwist=0,_dihedral=0)
WingPanel(obj,_ribs[i*2],_ribs[i*2+1],_row[3],_row[4],_position,0,0)
ViewProviderPanel(obj.ViewObject)
FreeCAD.ActiveDocument.recompute()
obj.ViewObject.hide()
#add to Wing
if selection : #selection==None :
if not base.WingPanels :
base.WingPanels=obj
else :
b=base.WingPanels
b.append(obj)
base.WingPanels=b
def Activated(self):
print("---------------------------------------")
print("-----------------Panel-----------------")
print("---------------------------------------")
selection = FreeCADGui.Selection.getSelectionEx()
if selection:
base = FreeCAD.ActiveDocument.getObject((selection[0].ObjectName))
#---------------------création des nervures temporaires
_rootRib = FreeCAD.ActiveDocument.addObject("Part::FeaturePython",
"RibRoot_")
WingRib(
_rootRib,
"/Users/fredericnivoix/Library/Preferences/FreeCAD/Mod/AirPlaneDesign/wingribprofil/naca/naca2412.dat",
False, 0, 200, 0, 0, 0, 0, 0, 0)
ViewProviderWingRib(_rootRib.ViewObject)
_tipRib = FreeCAD.ActiveDocument.addObject("Part::FeaturePython",
"RibTip_")
WingRib(
_tipRib,
"/Users/fredericnivoix/Library/Preferences/FreeCAD/Mod/AirPlaneDesign/wingribprofil/naca/naca2412.dat",
False, 0, 200, 0, 500, 0, 0, 0, 0)
ViewProviderWingRib(_tipRib.ViewObject)
FreeCAD.ActiveDocument.recompute()
#----------
#obj=FreeCAD.ActiveDocument.addObject("App::DocumentObjectGroupPython","WingPanel")
obj = FreeCAD.ActiveDocument.addObject("Part::FeaturePython",
"WingPanel")
WingPanel(obj, _rootRib, _tipRib, 200, 100, 100, 0, 0)
ViewProviderPanel(obj.ViewObject)
b = []
if selection: #selection==None :
if not base.WingPanels:
base.WingPanels = obj
else:
b = base.WingPanels
b.append(obj)
base.WingPanels = b
#if selection : #selection ==None:
# if not base.Group :
# base.Group=obj
# else :
# b=base.Group
# b.append(obj)
# base.Group=b
FreeCAD.ActiveDocument.recompute()
FreeCAD.Gui.activeDocument().activeView().viewAxonometric()
FreeCAD.Gui.SendMsgToActiveView("ViewFit")
def scaleByBoundbox(shape, boundbox, doScaleXYZ, copy=True):
basebbox = shape.BoundBox
#basebbox=[1.0,1.0,1.0]
scalevec = Vector(1, 1, 1)
if doScaleXYZ[0] and basebbox.XLength > epsilon:
scalevec.x = boundbox.XLength / basebbox.XLength
if doScaleXYZ[1] and basebbox.YLength > epsilon:
scalevec.y = boundbox.YLength / basebbox.YLength
if doScaleXYZ[2] and basebbox.ZLength > epsilon:
scalevec.z = boundbox.ZLength / basebbox.ZLength
scalevec.x = boundbox.XLength
scalevec.y = boundbox.YLength
scalevec.z = boundbox.ZLength
if scalevec.x < epsilon:
if doScaleXYZ[0]:
scalevec.x = epsilon
else:
scalevec.x = 1
if scalevec.y < epsilon:
if doScaleXYZ[1]:
scalevec.y = epsilon
else:
scalevec.y = 1
if scalevec.z < epsilon:
if doScaleXYZ[2]:
scalevec.z = epsilon
else:
scalevec.z = 1
_rib = FreeCAD.ActiveDocument.addObject("Part::FeaturePython", "Rib00")
print("Scale in scaleByBoundbox")
print(scalevec)
WingRib(
_rib,
"/Users/fredericnivoix/Library/Preferences/FreeCAD/Mod/AirPlaneDesign/wingribprofil/naca/naca2412.dat",
False, 0, scalevec.x, 0, 0, 0, 0, 0, 0)
ViewProviderWingRib(_rib.ViewObject)
_rib.Placement = shape.Placement
#dolly = scale(shape, scalevec, basebbox.Center, copy)
#dolly.Placement = shape.Placement
if doScaleXYZ[0]:
_rib.Placement.Base.x += boundbox.XMin - basebbox.XMin * scalevec.x
if doScaleXYZ[1]:
_rib.Placement.Base.y += boundbox.YMin - basebbox.YMin * scalevec.y
if doScaleXYZ[2]:
_rib.Placement.Base.z += boundbox.ZMin - basebbox.ZMin * scalevec.z
return _rib #dolly
def createRib(self, obj, chord, posvec, direction, rotaxis, angle):
#basebbox = obj.RootRib.Shape.BoundBox,basepl = obj.RootRib.Placement, print("Create Rib new release")
#bbox = CurvedShapes.boundbox_from_intersect(obj.Hullcurves, posvec, direction, self.doScaleXYZ)
FreeCAD.Console.PrintMessage("------------ createRib ------------\n")
#if not bbox:
# FreeCAD.Console.PrintMessage("------------ not bbox ------------\n")
# return None
_rib = FreeCAD.ActiveDocument.addObject("Part::FeaturePython", "Rib")
#calcul du facteur d'échelle de la nervure
#x,y,z,scalex,scaley,scalez=scaleByBoundbox2(obj.Base.Shape, bbox, self.doScaleXYZsum )
#(obj,_profil,_nacagene,_nacaNbrPoint,_chord,_x,_y,_z,_xrot,_yrot,_zrot,_thickness=0,_useSpline = True,_finite_TE = False,_splitSpline = False)
#(self, obj,_profil,_nacagene,_nacaNbrPoint,_chord,_x,_y,_z,_xrot,_yrot,_zrot,_rot=0,_thickness=0,_useSpline = True,_finite_TE = False,_splitSpline = False)
#FreeCAD.Console.PrintMessage("------------ createRib.posvec:"+str(posvec)+ " ------------\n")
#FreeCAD.Console.PrintMessage("------------ createRib.rotaxis:"+str(rotaxis)+ " ------------\n")
#FreeCAD.Console.PrintMessage("------------ createRib.angle"+str(angle)+ " ------------\n")
#FreeCAD.Console.PrintMessage("------------ createRib.scalex"+str(scalex)+ " ------------\n")
#FreeCAD.Console.PrintMessage("------------ createRib.scaley"+str(scaley)+ " ------------\n")
#FreeCAD.Console.PrintMessage("------------ createRib.scalez"+str(scalez)+ " ------------\n")
if obj.Base.NacaProfil == "":
WingRib(
_rib,
obj.Base.RibProfil,
"",
obj.Base.NacaNbrPoint,
chord,
posvec.x,
posvec.y,
posvec.z,
rotaxis.x,
rotaxis.y,
rotaxis.
z, #obj.Base.Placement.Rotation.Axis.x,obj.Base.Placement.Rotation.Axis.y, obj.Base.Placement.Rotation.Axis.z,
angle, #math.degrees(obj.Base.Placement.Rotation.Angle),
0,
obj.Base.useSpline,
obj.Base.finite_TE,
obj.Base.splitSpline)
else:
WingRib(
_rib,
obj.Base.RibProfil,
True,
obj.Base.NacaNbrPoint,
chord,
posvec.x,
posvec.y,
posvec.z,
rotaxis.x,
rotaxis.y,
rotaxis.
z, #obj.Base.Placement.Rotation.Axis.x,obj.Base.Placement.Rotation.Axis.y, obj.Base.Placement.Rotation.Axis.z,
angle, #math.degrees(obj.Base.Placement.Rotation.Angle),
0,
obj.Base.useSpline,
obj.Base.finite_TE,
obj.Base.splitSpline)
#obj.addProperty("App::PropertyString","NacaProfil","NacaProfil",QtCore.QT_TRANSLATE_NOOP("App::Property","Naca Profil")).NacaProfil=""
ViewProviderWingRib(_rib.ViewObject)
return _rib
def __init__(self, obj, _NberOfPanel, _panelInput):
'''Add some custom properties to our box feature'''
obj.Proxy = self
obj.addProperty("App::PropertyInteger", "NberOfPanel", "WingPanel",
"Number of Panel").NberOfPanel = _NberOfPanel
obj.addProperty("App::PropertyLinkList", "Rib", "Ribs", "Ribs")
#obj.addProperty("App::PropertyLinkList", "RibTip", "Ribs", "Tip Ribs")
_ribs = []
#_ribsRoot=[]
_panel = []
_position = 0
_PanelLength = []
profil = []
#for i in range(0,obj.NberOfPanel) :
for i in range(0, obj.NberOfPanel):
_row = _panelInput[i]
profil.append(_row[2])
#_wingRibProfilDir+u"/e207.dat"
_PanelLength.append(float(_row[4]))
#obj.addProperty("App::PropertyFloatList","PanelDelta","WingPanel","Delta").PanelDelta=[0.0,70.0]
#obj.addProperty("App::PropertyLinkList", "RibRoot", "Ribs", "Root Ribs")
#obj.addProperty("App::PropertyLinkList", "RibTip", "Ribs", "Tip Ribs")
FreeCAD.Console.PrintMessage("Panel creation : " + str(i))
#FreeCAD.Console.PrintMessage(i)
FreeCAD.Console.PrintMessage("\n")
# Add Rib Root
FreeCAD.Console.PrintMessage("Add Rib Root")
_ribs.append(
FreeCAD.ActiveDocument.addObject("Part::FeaturePython",
"RibRoot_" + str(i)))
#WingRib(_ribs[i*2],obj.PanelProfil,100,0,_position,0)
#obj.RibRoot.append(
WingRib(_ribs[i * 2], _row[2], False, 0, _row[3], _row[6],
_position, _row[8], 0, 0, 0)
ViewProviderWingRib(_ribs[i * 2].ViewObject)
# Add Rib tip
FreeCAD.Console.PrintMessage("Add Rib tip")
FreeCAD.Console.PrintMessage(i + 1)
#_position=_position+obj.PanelLength[i]
_position = _position + float(_row[5])
_ribs.append(
FreeCAD.ActiveDocument.addObject("Part::FeaturePython",
"RibTip_" + str(i)))
#WingRib(_ribs[i*2+1],obj.PanelProfil,100,0,_position,0)
WingRib(_ribs[i * 2 + 1], _row[2], False, 0, _row[4], _row[7],
_position, _row[9], 0, 0, 0)
ViewProviderWingRib(_ribs[i * 2 + 1].ViewObject)
#obj.RibTip.append(_ribs[i*2+1])
FreeCAD.Console.PrintMessage("create the panel")
if obj.NberOfPanel > 1:
_panel.append(
FreeCAD.ActiveDocument.addObject('Part::Loft', 'panel'))
_panel[i].Sections = [_ribs[i * 2], _ribs[i * 2 + 1]]
_panel[i].Solid = True
_panel[i].Ruled = False
else:
a = FreeCAD.ActiveDocument.addObject('Part::Loft', 'Wing')
_panel.append(a)
_panel[i].Sections = [_ribs[i * 2], _ribs[i * 2 + 1]]
_panel[i].Solid = True
_panel[i].Ruled = False
obj.Group = a
FreeCAD.ActiveDocument.recompute()
obj.Rib = _ribs
if obj.NberOfPanel > 1:
obj.addProperty("App::PropertyFloatList", "PanelLength",
"WingPanel",
"Length of the Wing").PanelLength = _PanelLength
obj.addProperty("App::PropertyStringList", "PanelProfil",
"WingPanel", "Profil type").PanelProfil = profil
a = FreeCAD.activeDocument().addObject("Part::MultiFuse", "Wing")
a.Shapes = _panel
obj.Group = a