# Mass system setup

# Empty mass
mass {
   name           = fuselage_wings
   mass           = 250.0
   inertia        = [ 2000.0  800.0 2150.0 ]
   position       = [ -0.3  0.0 0.0 ]
}

# Pilot's mass, assume no inertia 
mass {
   name           = pilot
   mass           = 75.0
   position       = [   0.68    0.0    0.0 ]
}

# water ballast
water {
   name           = wing
   position       = [    0.0    0.0   0.0 ]
   capacity       = 120.0
   valve_size     = 0.2
   y_inner        = 2.0
   y_outer        = 6.0

   valve_position = [ 0.0 0.5 0.1 ]
   valve_max_flow = 50.0
}

