HCI Lab - University of Udine MB-339PAN 2.1 207.76 35.63 5.83 35.32 21.6 20.78 0 195 0 22 95 0 35 0 0 0 10100 20323 23691 6883 195 0 22 180 90 0 20 47 0 -25 0.8 0.5 0.02 6500 400 60 NOSE 1 210 -44 -25 0.8 0.5 0.02 11000 400 0.0 LEFT 1 210 44 -25 0.8 0.5 0.02 11000 400 0.0 RIGHT 1 30 0 -8 0.2 0.2 0.2 2000 100 0 0 0 0.2 0.2 0.2 2000 100 85 0 50 0.2 0.2 0.2 2000 100 370 0 122 0.2 0.2 0.2 2000 100 419 0 37 0.2 0.2 0.2 2000 100 400 0 5 0.2 0.2 0.2 2000 100 245 -116 -12 0.2 0.2 0.2 2000 100 245 116 -12 0.2 0.2 0.2 2000 100 155 -116 -12 0.2 0.2 0.2 2000 100 155 116 -12 0.2 0.2 0.2 2000 100 218 -210 18 0.2 0.2 0.2 2000 100 218 210 18 0.2 0.2 0.2 2000 100 410 -80 34 0.2 0.2 0.2 2000 100 410 80 34 0.2 0.2 0.2 2000 100 210 0 22 0.0 0 0 0 1 2 210 0 22 0.0 0.0 0.0 145 0 5 1135 1100 204 -116 -5 442 420 204 116 -5 442 420 velocities/q-rad_sec 0.6 fcs/elevator-cmd-norm fcs/pitch-trim-cmd-norm -1 1 fcs/pitch-trim-sum 0.01745 -20 17

fcs/elevator-pos-rad

fcs/elevator-pos-deg -20 17 -1 1

fcs/elevator-pos-norm

velocities/p-rad_sec -0.5 velocities/r-rad_sec -0.6 fcs/aileron-cmd-norm fcs/roll-trim-cmd-norm -1 1 fcs/roll-trim-sum 0.01745 -15 10

fcs/left-aileron-pos-rad

fcs/left-aileron-pos-deg -15 10 -1 1

fcs/left-aileron-pos-norm

-fcs/roll-trim-sum 0.01745 -15 10

fcs/right-aileron-pos-rad

fcs/right-aileron-pos-deg -15 10 -1 1

fcs/right-aileron-pos-norm

velocities/r-rad_sec 0.5 fcs/rudder-cmd-norm fcs/yaw-trim-cmd-norm -1 1 fcs/rudder-command-sum 0.01745 -20 20

fcs/rudder-pos-rad

fcs/rudder-pos-rad -0.35 0.35 -1 1

fcs/rudder-pos-norm

fcs/flap-cmd-norm 0 0 .33 3 .66 1 1 1

fcs/flap-pos-norm

gear/gear-cmd-norm 0 0 1 4

gear/gear-pos-norm

fcs/speedbrake-cmd-norm 0 0 1 3

fcs/speedbrake-pos-norm

Change_in_lift_due_to_ground_effect aero/h_b-mac-ft 0.0000 1.4000 0.1000 1.3500 0.1500 1.2950 0.2000 1.2400 0.3000 1.1730 0.4000 1.1030 0.5000 1.0340 0.6000 1.0460 0.7000 1.0190 0.8000 1.0100 0.9000 1.0050 1.0000 1.0000 1.1000 1.0000 Drag_due_to_alpha aero/qbar-psf metrics/Sw-sqft aero/alpha-rad -1.5700 1.5000 -0.2600 0.0490 0.0000 0.0270 0.2600 0.0490 1.5700 1.5000 Induced_drag aero/qbar-psf metrics/Sw-sqft aero/cl-squared 0.0470 Drag_due_to_flaps aero/qbar-psf metrics/Sw-sqft fcs/flap-pos-deg 0.0000 0.0000 30.0000 0.0260 60.0000 0.0600 Drag_due_to_gear aero/qbar-psf metrics/Sw-sqft gear/gear-pos-norm 0.0000 0.0000 1.0000 0.0340 Drag_due_to_speedbrakes aero/qbar-psf metrics/Sw-sqft fcs/speedbrake-pos-norm 0.0000 0.0000 1.0000 0.1100 Drag_due_to_sideslip aero/qbar-psf metrics/Sw-sqft aero/beta-rad -1.5700 1.2300 -0.2600 0.0470 0.0000 0.0000 0.2600 0.0470 1.5700 1.2300 Drag_due_to_Elevator_Deflection aero/qbar-psf metrics/Sw-sqft fcs/elevator-pos-norm -1.0000 0.0380 -0.7500 0.0260 -0.5000 0.0160 -0.2500 0.0080 0.0000 0.0040 0.2500 0.0120 0.5000 0.0190 0.7500 0.0280 1.0000 0.0400 Side_force_due_to_beta aero/qbar-psf metrics/Sw-sqft aero/beta-rad -0.7000 Lift_due_to_alpha aero/qbar-psf metrics/Sw-sqft aero/function/kCLge aero/alpha-rad -1.5700 -1.5000 -0.2000 -0.6500 0.0000 0.2900 0.2300 1.3600 0.6000 0.6500 1.5700 0.0500 Delta_Lift_due_to_flaps aero/qbar-psf metrics/Sw-sqft aero/function/kCLge fcs/flap-pos-deg 0.0000 0.0000 30.0000 0.3600 60.0000 0.4100 Lift_due_to_Elevator_Deflection aero/qbar-psf metrics/Sw-sqft aero/function/kCLge fcs/elevator-pos-rad -0.3490 -0.0664 -0.1750 -0.0338 0.0000 0.0000 0.1750 0.0327 0.2970 0.0614 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_(roll_damping) aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/bi2vel velocities/p-aero-rad_sec aero/alpha-rad -1.5700 -0.3400 -0.2600 -0.3700 0.0000 -0.4000 0.2600 -0.3700 1.5700 -0.3400 Roll_moment_due_to_yaw_rate aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/bi2vel velocities/r-aero-rad_sec 0.0025 Roll_moment_due_to_aileron_left aero/qbar-psf metrics/Sw-sqft metrics/bw-ft fcs/left-aileron-pos-radvelocities/mach 0.0000 0.9000 -0.2617 -0.0180 -0.0150 -0.1745 -0.0120 -0.0105 -0.0872 -0.0068 -0.0057 0.0000 0.0000 0.0000 0.0872 0.0040 0.0026 0.1745 0.0087 0.0059 Roll_moment_due_to_aileron_right aero/qbar-psf metrics/Sw-sqft metrics/bw-ft fcs/right-aileron-pos-radvelocities/mach 0.0000 0.9000 -0.2617 0.0180 0.0150 -0.1745 0.0120 0.0105 -0.0872 0.0068 0.0057 0.0000 0.0000 0.0000 0.0872 -0.0040 -0.0026 0.1745 -0.0087 -0.0059 Pitch_moment_due_to_alpha aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft aero/alpha-rad -0.5000 Pitch_moment_due_to_flaps aero/qbar-psf metrics/Sw-sqft fcs/flap-pos-deg 0.0000 0.0000 30.0000 -0.0200 60.0000 -0.0300 Pitch_moment_due_to_elevator aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft fcs/elevator-pos-radvelocities/mach 0.0000 0.9000 -0.3490 0.3400 0.3190 -0.1750 0.1810 0.1510 0.0000 0.0140 0.0100 0.1750 -0.1680 -0.1430 0.2970 -0.2770 -0.2530 Pitch_moment_due_to_pitch_rate_(pitch_damping) aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft aero/ci2vel velocities/q-aero-rad_sec -15.0000 Pitch_moment_due_to_alpha_rate aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft aero/ci2vel aero/alphadot-rad_sec velocities/mach 0.0000 -10.5000 0.3000 -9.0000 0.6000 -7.9000 0.9000 -7.0000 Yaw_moment_due_to_beta aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/beta-rad 0.1000 Yaw_moment_due_to_yaw_rate_(yaw_damping) aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/bi2vel velocities/r-aero-rad_sec -0.2400 Yaw_moment_due_to_roll_rate aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/bi2vel velocities/p-aero-rad_sec -0.0300 Yaw_moment_due_to_rudder aero/qbar-psf metrics/Sw-sqft metrics/bw-ft fcs/rudder-pos-rad -0.3490 0.0360 -0.2620 0.0250 -0.1750 0.0160 -0.0870 0.0070 0.0000 0.0000 0.0870 -0.0070 0.1750 -0.0160 0.2620 -0.0250 0.3490 -0.0360 Adverse_yaw_left_aileron aero/qbar-psf metrics/Sw-sqft metrics/bw-ft fcs/left-aileron-pos-rad -0.2620 0.0002 -0.1750 0.0001 -0.0870 0.0000 0.0000 0.0000 0.0870 -0.0000 0.1750 -0.0001 Adverse_yaw_right_aileron aero/qbar-psf metrics/Sw-sqft metrics/bw-ft fcs/right-aileron-pos-rad -0.2620 -0.0002 -0.1750 -0.0001 -0.0870 -0.0000 0.0000 0.0000 0.0870 0.0000 0.1750 0.0001