text: import unittest
  import numpy as np
  from plain_fdm.physikFDM.aircraft_beaver import AircraftBaever
  from plain_fdm.physikFDM.dynamic_system6DoF import DynamicSystem6DoF
  
  class DynamicSystem6DoFTest(unittest.TestCase):
      def test_something(self):
          aircraft = AircraftBaever()
          dynamic_system = DynamicSystem6DoF()
          step_length = 0.02
  
          solver = dynamic_system.integrate(
              state=aircraft.getState(),
              forces=aircraft.getForces(),
              moments=aircraft.getMoments(),
              mass=aircraft.mass,
              inertia=aircraft.inertia,
              stepweite=step_length
          )
  
          ## TODO: Check if integrated values are correct
          self.u, self.v, self.w, self.x, self.y, self.z, self.p, self.q, self.r, self.phi, self.theta, self.psi = solver.y.flatten()
  
          self.assertEqual(True, False)
  
  
  if __name__ == '__main__':
      unittest.main()
  