Cas 1
Conditions initiales
  Position drone (m) = (    0.00000,     0.00000,     0.00000 )
  Rotation drone (r) =    0.00000
  Vitesse angulaire drone (r/s) = (    0.00000,     0.00000,     0.00000 )
  Forces (N) = (    1.00000,     1.00000,     1.00000,     1.00000 )
Resultats avion sur la piste
  Centre de masse (m) = (    0.00000,     0.02353,     0.02328 )
  Moment inertie (kg/m^2) =
      0.80749 &    0.00000 &    0.00846
      0.00000 &    0.83978 &    0.01779
      0.00000 &    0.01779 &    1.54509
  acc angulaire (r/s^2) = (   -2.91388,     0.00000,     0.00000 )


Cas 2
Conditions initiales
  Position drone = (    2.50000,     0.00000,    30.50000 )
  Rotation drone (r) =    0.05000
  Vitesse angulaire drone (r/s)= (    0.00000,     0.05000,     0.00100 )
  Forces/Fmax (N) = (    0.40000,     0.50000,     0.60000,     0.50000 )

Resultats avion en vol
  Centre de masse (m) = (    2.50116,     0.02353,    30.52326 )
  Moment inertie  (kg/m^2) =
      0.80914 &    0.00089 &    0.04138 \\
      0.00089 &    0.83978 &    0.01777 \\
      0.03292 &    0.01777 &    1.54345 \\
  acc angulaire (r/s^2) = (   -1.45428,     4.82967,    -0.06426 )