Erik Hofman 2004-01-01 $Revision: 1.1 $ Models an F-22 Raptor GPL (General Public License) http://www.gnu.org/licenses/gpl.html This model was created using data that is, or has been, publically available by means of technical reports, textbooks, image graphs or published code. This aircraft description file is in no way related to the manufacturer of the real aircraft. Neither the name of (any of) the authors nor the names of (any of) the manufacturers may be used to endorse or promote products derived from this file. The data is provided ''as is'' and any express or implied warranties, including, but not limitted to the implied warranties of merchantability and fitness for a particular purpose are disclaimed. 840.0 44.49 23.06 238.9 18.66 158.2 0 446.5 0 0 148.8 0 38 100 0 0 40843 204751 258201 520 43430 446.5 0 -18.6 230 148.8 0 20 96.7 0 -89.3 0.8 0.5 0.02 18603.4 6201.1 5 NONE 1 468.8 -48 -89.3 0.8 0.5 0.02 62011.2 12402.2 0.0 LEFT 1 468.8 48 -89.3 0.8 0.5 0.02 62011.2 12402.2 0.0 RIGHT 1 684.131 -20 0 0.0 0 0 0 684.131 -20 0 0.0 0.0 0.0 684.131 20 0 0.0 0 0 1 684.131 20 0 0.0 0.0 0.0 446.478 0 -18.6033 7000 3500 446.478 0 -18.6033 7000 3500 fcs/throttle-cmd-norm 2 fcs/throttle-pos-norm 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 0.0 3.00 1.0
fcs/rudder-command-sum fcs/yaw-damper-final -1 1 fcs/rudder-sum -0.35 0.35 fcs/rudder-pos-rad velocities/vc-kts lt 250 fcs/flap-command 0 15 30 fcs/flap-pos-deg fcs/flap-pos-deg 0 30 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 Change_in_lift_due_to_ground_effect aero/h_b-mac-ft 0.0000 1.3893 0.1000 1.2108 0.1500 1.1972 0.2000 1.2108 0.3000 1.1785 0.4000 1.0697 0.5000 1.0578 0.6000 1.0323 0.7000 1.0136 0.8000 1.0051 0.9000 1.0017 1.0000 1.0000 1.1000 1.0000
Change_in_drag_due_to_ground_effect aero/h_b-mac-ft 0.0000 0.5235 0.1000 0.4759 0.1500 0.5250 0.2000 0.5388 0.3000 0.5924 0.4000 0.6471 0.5000 0.6941 0.6000 0.7624 0.7000 0.8253 0.8000 0.8812 0.9000 0.9412 1.0000 1.0000 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 0.0480 0.0000 0.0240 0.2600 0.0480 1.5700 1.5000
Induced_drag aero/qbar-psf metrics/Sw-sqft aero/cl-squared aero/function/kCDge 0.0900 Drag_due_to_mach aero/qbar-psf metrics/Sw-sqft velocities/mach 0.0000 0.0000 0.8100 0.0000 1.1000 0.0230 1.8000 0.0150
Drag_due_to_flaps aero/qbar-psf metrics/Sw-sqft fcs/flap-pos-norm aero/function/kCDge 0.0750 Drag_due_to_gear aero/qbar-psf metrics/Sw-sqft gear/gear-pos-norm 0.0200 Drag_due_to_speedbrakes aero/qbar-psf metrics/Sw-sqft fcs/speedbrake-pos-norm 0.0240 Drag_due_to_sideslip aero/qbar-psf metrics/Sw-sqft aero/function/kCDge 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 aero/function/kCDge 0.0750 Side_force_due_to_beta aero/qbar-psf metrics/Sw-sqft aero/beta-rad -0.2875 Side_force_due_to_beta_rate aero/qbar-psf metrics/Sw-sqft aero/betadot-rad_sec -0.0458 Side_force_due_to_rudder aero/qbar-psf metrics/Sw-sqft fcs/rudder-pos-rad 0.0619 Side_force_due_to_roll_rate aero/qbar-psf metrics/Sw-sqft aero/bi2vel velocities/p-aero-rad_sec 0.0399 Side_force_due_to_yaw_rate aero/qbar-psf metrics/Sw-sqft aero/bi2vel velocities/r-aero-rad_sec 0.1218 Lift_due_to_alpha aero/qbar-psf metrics/Sw-sqft aero/alpha-rad -0.1745 -0.4279 0.7854 2.0000 1.3963 1.0726
Lift_due_to_alpha_rate aero/qbar-psf metrics/Sw-sqft aero/alphadot-rad_sec aero/ci2vel 2.5602 Lift_due_to_pitch_rate aero/qbar-psf metrics/Sw-sqft velocities/q-aero-rad_sec aero/function/kCLge aero/ci2vel 2.7711 Delta_Lift_due_to_flaps aero/qbar-psf metrics/Sw-sqft fcs/flap-pos-norm 0.3500 Delta_Lift_due_to_speedbrake aero/qbar-psf metrics/Sw-sqft fcs/speedbrake-pos-norm 0.0000 Lift_due_to_Elevator_Deflection aero/qbar-psf metrics/Sw-sqft aero/function/kCLge fcs/elevator-pos-rad 0.2000 Roll_moment_due_to_beta aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/beta-rad aero/alpha-rad -0.0873 0.0189 0.0000 0.0176 0.0873 0.0119 0.1745 0.0050 0.2618 0.0049 0.3491 0.0028 0.4363 0.0084 0.5236 0.0171 0.6109 0.0044
Roll_moment_due_to_beta_rate aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/ci2vel aero/betadot-rad_sec -0.0037 Roll_moment_due_to_roll_rate aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/bi2vel velocities/p-aero-rad_sec aero/alpha-rad 0.0000 -0.4000 0.3490 -0.3100
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 0.0489 2.0000 0.0400
Roll_moment_due_to_rudder aero/qbar-psf metrics/Sw-sqft metrics/bw-ft fcs/rudder-pos-rad aero/alpha-rad -0.1745 0.0078 -0.0873 0.0070 0.0000 0.0059 0.0873 0.0043 0.1745 0.0023 0.2618 0.0007 0.3491 -0.0008 0.4363 0.0004 0.5236 0.0019 0.6109 0.0019 0.6981 0.0017 0.7854 0.0009 0.8727 0.0003 1.0472 0.0000 1.2217 0.0000 1.3963 0.0000
Pitch_moment_due_to_horizontal_tail_deflection aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft aero/alpha-radfcs/elevator-pos-rad -0.5236 0.0 0.4363 -0.0873 0.3222 -0.0546 -0.4911 0.0000 0.3482 0.0000 -0.4729 0.0873 0.3897 0.0286 -0.4782 0.1745 0.3689 0.0156 -0.4988 0.2618 0.3975 0.0546 -0.4287 0.3491 0.3819 0.0442 -0.2722 0.4363 0.4131 0.0831 -0.1637 0.5236 0.4599 0.1377 -0.0546 0.6109 0.4443 0.1325 -0.0530 0.6981 0.3819 0.1013 -0.0650 0.7854 0.3585 0.0909 -0.0624 0.8727 0.3430 0.1299 -0.0364 1.0472 0.0208 -0.1117 -0.1975 1.2217 0.3248 -0.4521 -0.5144
Pitch_moment_due_to_pitch_rate aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft aero/ci2vel velocities/q-aero-rad_sec -17.830 Pitch_moment_due_to_alpha_rate aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft aero/ci2vel aero/alphadot-rad_sec velocities/mach 0.2570 -1.5611 1.8000 -2.0500
Pitch_moment_due_to_horizontal_tail_deflection aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft aero/ci2vel aero/alphadot-rad_sec fcs/elevator-pos-rad -1.5611 Pitch_moment_due_to_pitch_rate_and_horizontal_tail_deflection aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft aero/ci2vel velocities/q-aero-rad_sec fcs/elevator-pos-rad -1.1726 Yaw_moment_due_to_beta aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/beta-rad 0.1200 Yaw_moment_due_to_beta aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/beta-rad aero/alpha-rad -0.0873 0.0016 0.0000 0.0016 0.0873 0.0018 0.1745 0.0026 0.2618 0.0028 0.3491 0.0026 0.4363 0.0021 0.5236 0.0033 0.6109 0.0015
Yaw_moment_due_to_beta_rate aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/ci2vel aero/betadot-rad_sec -0.0115 Yaw_moment_due_to_roll_rate aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/bi2vel velocities/p-aero-rad_sec -0.0035 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 aero/alpha-rad -0.1745 -0.0082 -0.0873 -0.0128 0.0000 -0.0131 0.0873 -0.0140 0.1745 -0.0154 0.2618 -0.0128 0.3491 -0.0100 0.4363 -0.0077 0.5236 -0.0065 0.6109 -0.0051 0.6981 -0.0041 0.7854 -0.0025 0.8727 0.0000 1.0472 0.0000 1.2217 0.0000 1.3963 0.0000
Adverse_yaw aero/qbar-psf metrics/Sw-sqft metrics/bw-ft fcs/left-aileron-pos-rad 0.0000