Unknown 2003-01-01 $Revision: 1.10 $ McDonnell Douglas MD-11 This model was created using publicly available data, publicly available technical reports, textbooks, and guesses. It contains no proprietary or restricted data. If this model has been validated at all, it would be only to the extent that it seems to "fly right", and that it possibly complies with published, publicly known, performance data (maximum speed, endurance, etc.). Thus, this model is meant for educational and entertainment purposes only. This simulation model is not endorsed by the manufacturer. This model is not to be sold. 3648 169.5 21.52 912 90.37 729.6 0 1325.5 0 0 168.7 -30 75 0 0 0 1.3185e+07 3.83816e+07 5.56127e+07 378300 1325.5 0 -60.2 313.3 0 -289.2 0.8 0.5 0.02 189150 63050 60 NONE 1 1378.5 -183.1 -289.2 0.8 0.5 0.02 630500 126100 0.0 LEFT 1 1378.5 183.1 -289.2 0.8 0.5 0.02 630500 126100 0.0 RIGHT 1 1325.48 -339 -40 0.0 0 0 0 1325.48 -339 -40 0.0 0.0 0.0 140.83 0 60 0.0 0 0 1 140.83 0 60 0.0 0.0 0.0 1325.48 339 -40 0.0 0 0 2 1325.48 339 -40 0.0 0.0 0.0 1325.48 0 -60.249 9851.6 4925.8 1325.48 0 -60.249 9851.6 4925.8 1325.48 0 -60.249 9851.6 4925.8 1325.48 0 -60.249 9851.6 4925.8 fcs/elevator-cmd-norm fcs/pitch-trim-cmd-norm -1 1 fcs/pitch-trim-sum -0.35 0.3

fcs/elevator-pos-rad

fcs/aileron-cmd-norm fcs/roll-trim-cmd-norm -1 1 fcs/roll-trim-sum -0.35 0.35

fcs/left-aileron-pos-rad

-fcs/roll-trim-sum -0.35 0.35

fcs/right-aileron-pos-rad

fcs/rudder-cmd-norm fcs/yaw-trim-cmd-norm -1 1 velocities/r-aero-rad_sec aero/qbar-psf 3.00 0.00 11.00 2.00 aero/beta-rad aero/qbar-psf 3.00 0.00 11.00 0.00 fcs/yaw-damper-beta fcs/yaw-damper-rate -0.2 0.2 fcs/yaw-damper-sum aero/qbar-psf 2.99 0.00 3.00 1.00 fcs/rudder-command-sum fcs/yaw-damper-final -1 1 fcs/rudder-sum -0.35 0.35

fcs/rudder-pos-rad

fcs/flap-cmd-norm 0 0 15 4 30 3

fcs/flap-pos-deg

fcs/flap-pos-deg 0 30 0 1

fcs/flap-pos-norm

gear/gear-cmd-norm 0 0 1 5

gear/gear-pos-norm

fcs/speedbrake-cmd-norm 0 0 1 1

fcs/speedbrake-pos-norm

Drag_at_zero_lift aero/qbar-psf metrics/Sw-sqft aero/alpha-rad -1.5700 1.5000 -0.2600 0.0380 0.0000 0.0190 0.2600 0.0380 1.5700 1.5000 Induced_drag aero/qbar-psf metrics/Sw-sqft aero/cl-squared 0.0420 Drag_due_to_mach aero/qbar-psf metrics/Sw-sqft velocities/mach 0.0000 0.0000 0.7900 0.0000 1.1000 0.0230 1.8000 0.0150 Drag_due_to_flaps aero/qbar-psf metrics/Sw-sqft fcs/flap-pos-norm 0.0570 Drag_due_to_gear aero/qbar-psf metrics/Sw-sqft gear/gear-pos-norm 0.0130 Drag_due_to_speedbrakes aero/qbar-psf metrics/Sw-sqft fcs/speedbrake-pos-norm 0.0190 Drag_due_to_sideslip aero/qbar-psf metrics/Sw-sqft aero/beta-rad -1.5700 1.2300 -0.2600 0.0500 0.0000 0.0000 0.2600 0.0500 1.5700 1.2300 Drag_due_to_Elevator_Deflection aero/qbar-psf metrics/Sw-sqft fcs/elevator-pos-norm 0.0570 Side_force_due_to_beta aero/qbar-psf metrics/Sw-sqft aero/beta-rad -1.0000 Lift_due_to_alpha aero/qbar-psf metrics/Sw-sqft aero/alpha-rad -0.2000 -0.6800 0.0000 0.2000 0.2300 1.2000 0.6000 0.6000 Delta_Lift_due_to_flaps aero/qbar-psf metrics/Sw-sqft fcs/flap-pos-norm 1.5000 Delta_Lift_due_to_speedbrake aero/qbar-psf metrics/Sw-sqft fcs/speedbrake-pos-norm -0.0900 Lift_due_to_Elevator_Deflection aero/qbar-psf metrics/Sw-sqft fcs/elevator-pos-rad 0.2000 Roll_moment_due_to_beta aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/beta-rad -0.1000 Roll_moment_due_to_roll_rate aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/bi2vel velocities/p-aero-rad_sec -0.4000 Roll_moment_due_to_yaw_rate aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/bi2vel velocities/r-aero-rad_sec 0.1500 Roll_moment_due_to_aileron aero/qbar-psf metrics/Sw-sqft metrics/bw-ft fcs/left-aileron-pos-rad velocities/mach 0.0000 0.1000 2.0000 0.0330 Roll_moment_due_to_rudder aero/qbar-psf metrics/Sw-sqft metrics/bw-ft fcs/rudder-pos-rad 0.0100 Pitch_moment_due_to_alpha aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft aero/alpha-rad -0.6000 Pitch_moment_due_to_elevator aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft fcs/elevator-pos-rad velocities/mach 0.0000 -1.2000 2.0000 -0.3000 Pitch_moment_due_to_pitch_rate aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft aero/ci2vel velocities/q-aero-rad_sec -17.0000 Pitch_moment_due_to_alpha_rate aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft aero/ci2vel aero/alphadot-rad_sec -6.0000 Yaw_moment_due_to_beta aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/beta-rad 0.1200 Yaw_moment_due_to_yaw_rate aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/bi2vel velocities/r-aero-rad_sec -0.1500 Yaw_moment_due_to_rudder aero/qbar-psf metrics/Sw-sqft metrics/bw-ft fcs/rudder-pos-rad -0.1000 Adverse_yaw aero/qbar-psf metrics/Sw-sqft metrics/bw-ft fcs/left-aileron-pos-rad 0.0000