def __init__(self, aircraft):
'''
@Method: Component Constructor
'''
component.__init__(self)
self.id = 'landingGear'
self.aircraft = aircraft
self.level = 2
#Parameters
self.mLandingGear = mLandingGear(
cpacsPath='/cpacs/vehicles/aircraft/model/analyses/massBreakdown/mOEM/mEM/mStructure/mLandingGears/massDescription/mass')
self.eta = eta()
self.xsi = xsi()
self.xLandingGear = xLandingGear()
self.yLandingGear = yLandingGear()
self.zLandingGear = zLandingGear()
self.xNoseGear = xNoseGear()
#Aerodynamic
self.dCDextendedLG = dCDextendedLG()
def __init__(self, aircraft):
'''
@Method: Component Constructor
'''
component.__init__(self)
self.id = 'landingGear'
self.aircraft = aircraft
self.level = 2
#Parameters
self.mLandingGear = mLandingGear()
self.mNoseGear = mNoseGear()
self.eta = eta()
self.xsi = xsi()
self.xLandingGear = xLandingGear(cpacsPath='/cpacs/vehicles/aircraft/model/landingGear/mainGears/mainGear/fuselageAttachment/translation/x')
self.yLandingGear = yLandingGear(cpacsPath='/cpacs/vehicles/aircraft/model/landingGear/mainGears/mainGear/fuselageAttachment/translation/y')
self.zLandingGear = zLandingGear(cpacsPath='/cpacs/vehicles/aircraft/model/landingGear/mainGears/mainGear/fuselageAttachment/translation/z')
self.xNoseGear = xNoseGear(cpacsPath='/cpacs/vehicles/aircraft/model/landingGear/noseGears/noseGear/fuselageAttachment/translation/x')
self.yNoseGear = yNoseGear(cpacsPath='/cpacs/vehicles/aircraft/model/landingGear/noseGears/noseGear/fuselageAttachment/translation/y')
self.zNoseGear = zNoseGear(cpacsPath='/cpacs/vehicles/aircraft/model/landingGear/noseGears/noseGear/fuselageAttachment/translation/z')
#Aerodynamic
self.dCDextendedLG = dCDextendedLG()