# Mass system setup
mtow = 580

# Mass of aircraft minus pilot and motor
mass {
   name           = fuselage_wings
   mass           = 368.0
   inertia        = [ 3300.0  1200.0 5000.0 ]
   position       = [ 0.0  0.0 0.0 ]
}

# Pilot's mass, assume no inertia 
seat {
   name           = pilot
   mass           = 75.0
   min            = 70
   max            = 110
   position       = [   1.2    0.0    0.0 ]
}

# Rear pilot's mass, assume no inertia 
seat {
   name           = copilot
   mass           = 0.1
   min            = 0
   max            = 110
   position       = [   0.1    0.0    0.0 ]
}


