Erik Hofman 2010-08-08 $Revision: 1.3 $ Fokker 70 commercial airliner 1006.53 92.13 2.00 12.4671 233.792 47.2440 132.396 37.4015 587.73 0.00 38.00 76.84 -30.00 88.94 101.65 0.0 0.0 200203 455983 672987 49985 605.73 0.00 38.12 230 96.84 -30.0 66.0 230 96.84 30.0 66.0 400 206 30.0 66.0 142.70 0.00 -55.73 0.80 0.50 0.02 7750.51 1600.17 5.00 NONE 1 627.88 -101.65 -63.53 0.80 0.50 0.02 81011.70 16202.34 0 LEFT 1 627.88 101.65 -63.53 0.80 0.50 0.02 81011.70 16202.34 0 RIGHT 1 603.73 -1105.4 0.0 0.80 0.50 81011.70 16202.34 603.73 1105.4 0.0 0.80 0.50 81011.70 16202.34 -139 0 -71 1 0 0 893.52 -101.65 43.53 0.00 0.00 0.00 0 893.52 -101.65 43.53 0.00 0.00 0.00 893.52 101.65 43.53 0.00 0.00 0.00 1 893.52 101.65 43.53 0.00 0.00 0.00 601.73 -190.59 0.0 1174.08 587.04 601.73 190.59 0.0 1174.08 587.04 fcs/elevator-cmd-norm fcs/pitch-trim-cmd-norm -1 1 fcs/pitch-trim-sum -0.35 0.35 fcs/elevator-pos-rad fcs/elevator-pos-rad -0.35 0.35 -1 1 fcs/elevator-pos-norm 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/left-aileron-pos-rad -0.35 0.35 -1 1 fcs/left-aileron-pos-norm fcs/right-aileron-pos-rad -0.35 0.35 -1 1 fcs/right-aileron-pos-norm fcs/rudder-cmd-norm fcs/yaw-trim-cmd-norm -0.35 0.35 velocities/r-aero-rad_sec velocities/ve-kts 30 0.00 60 2.00
aero/beta-rad velocities/ve-kts 30 0.00 60 0.00
fcs/yaw-damper-beta fcs/yaw-damper-rate -0.1 0.1 fcs/yaw-damper-sum velocities/ve-kts 30 0.0 31 1.0
fcs/rudder-command-sum fcs/yaw-damper-final -1 1 fcs/rudder-sum -0.35 0.35 fcs/rudder-pos-rad fcs/rudder-pos-rad -0.35 0.35 -1 1 fcs/rudder-pos-norm fcs/flap-cmd-norm 0 8 15 25 42 fcs/flap-pos-deg fcs/flap-pos-deg 0 42 0 1 fcs/flap-pos-norm gear/gear-cmd-norm 0 1 gear/gear-pos-norm fcs/speedbrake-cmd-norm 0 1 fcs/speedbrake-pos-norm fcs/spoiler-cmd-norm 0 1 fcs/spoiler-pos-norm Change_in_drag_due_to_ground_effect aero/h_b-mac-ft 0.0000 0.0350 0.1000 0.4170 0.1500 0.5390 0.2000 0.6240 0.3000 0.7510 0.4000 0.8000 0.5000 0.8960 0.6000 0.9390 0.7000 0.9740 0.8000 0.9810 0.9000 0.9900 1.0000 0.9940 1.1000 1.0000
Change_in_lift_due_to_ground_effect aero/h_b-mac-ft 0.0000 1.3910 0.1000 1.2350 0.1500 1.1670 0.2000 1.1350 0.3000 1.0850 0.4000 1.1020 0.5000 1.0350 0.6000 1.0240 0.7000 1.0150 0.8000 1.0110 0.9000 1.0060 1.0000 1.0040 1.1000 1.0000
Drag_at_zero_lift aero/qbar-psf metrics/Sw-sqft aero/function/kCDge aero/alpha-rad -1.5700 1.5000 -0.2600 0.0400 0.0000 0.0192 0.2600 0.0400 1.5700 1.5000
Induced_drag aero/qbar-psf metrics/Sw-sqft aero/cl-squared aero/function/kCDge 0.00717 Drag_due_to_flaps aero/qbar-psf metrics/Sw-sqft fcs/flap-pos-norm aero/function/kCDge 0.0830 Drag_due_to_mach aero/qbar-psf metrics/Sw-sqft velocities/mach 0.0000 0.0000 0.6500 0.0000 0.7700 0.0015 0.8600 0.0200 1.1000 0.0390 1.8000 0.0260
Drag_due_to_gear aero/qbar-psf metrics/Sw-sqft gear/gear-pos-norm 0.0120 Drag_due_to_speedbrakes aero/qbar-psf metrics/Sw-sqft fcs/speedbrake-pos-norm 0.1200 Drag_due_to_spoilers aero/qbar-psf metrics/Sw-sqft fcs/spoiler-pos-norm 0.0280 Drag_due_to_reverse aero/qbar-psf metrics/Sw-sqft propulsion/engine[0]/reverser-angle-rad propulsion/engine[1]/reverser-angle-rad 0.0187 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/mag-elevator-pos-rad 0.0590 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/function/kCLge aero/alpha-rad -0.20 -0.680 0.00 0.217 0.23 1.300 0.60 0.600
Delta_Lift_due_to_flaps aero/qbar-psf metrics/Sw-sqft aero/function/kCLge fcs/flap-pos-norm 0.0000 0.0000 0.3570 0.4900 1.0000 1.1800
Delta_Lift_due_to_spoiler aero/qbar-psf metrics/Sw-sqft fcs/spoiler-pos-norm aero/function/kCLge -0.1200 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 Change_in_lift_due_to_ground_effect aero/h_b-mac-ft 0.0000 1.2030 0.1000 1.1270 0.1500 1.0900 0.2000 1.0730 0.3000 1.0460 0.4000 1.0550 0.5000 1.0190 0.6000 1.0130 0.7000 1.0080 0.8000 1.0060 0.9000 1.0030 1.0000 1.0020 1.1000 1.0000
Pitching_moment_at_zero_alpha aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft aero/function/kCmge -0.000737 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 -31.0000 Pitch_moment_due_to_alpha_rate aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft aero/ci2vel aero/alphadot-rad_sec -16.0000 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