Esempio n. 1
0
    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()
Esempio n. 2
0
    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()
Esempio n. 3
0
    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()
Esempio n. 4
0
    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()