AC_WINGAREA 174 AC_WINGSPAN 35.8 AC_CHORD 4.9 AC_HTAILAREA 21.9 AC_HTAILARM 15.7 AC_VTAILAREA 16.5 AC_LV 15.7 AC_IXX 948 AC_IYY 1346 AC_IZZ 1967 AC_IXZ 0 AC_EMPTYWT 1500 AC_AERORP 43.2 0.0 59.4 AC_CGLOC 41.0 0.0 36.5 AC_POINTMASS 180.0 36.0 -14.0 24.0 AC_EYEPTLOC 37.0 0.0 48.0 AC_GEAR NOSE -6.8 0.0 -20.0 1800 600 0.5 0.8 0.02 STEERABLE NOSE 20 FIXED AC_GEAR LEFT_MAIN 58.2 -43.0 -17.9 5400 1600 0.5 0.8 0.02 FIXED LEFT 0 FIXED AC_GEAR RIGHT_MAIN 58.2 43.0 -17.9 5400 1600 0.5 0.8 0.02 FIXED RIGHT 0 FIXED AC_GEAR TAIL_SKID 188.0 0.0 8.0 20000 1000 0.2 0.2 0.2 FIXED NONE 0 FIXED AC_GEAR LEFT_TIP 43.2 -214.8 59.4 10000 2000 0.2 0.2 0.2 FIXED NONE 0 FIXED AC_GEAR RIGHT_TIP 43.2 214.8 59.4 10000 2000 0.2 0.2 0.2 FIXED NONE 0 FIXED XLOC -19.7 YLOC 0.0 ZLOC 26.6 PITCH 0.0 YAW 0.0 FEED 0 FEED 1 XLOC -37.7 YLOC 0.0 ZLOC 26.6 PITCH 0.0 YAW 0 P_FACTOR 10.0 SENSE 1.0 XLOC 56.0 YLOC -112.0 ZLOC 59.4 RADIUS 29.4 CAPACITY 185.0 CONTENTS 100.0 XLOC 56.0 YLOC 112.0 ZLOC 59.4 RADIUS 29.4 CAPACITY 185.0 CONTENTS 100.0 INPUT fcs/elevator-cmd-norm INPUT fcs/pitch-trim-cmd-norm CLIPTO -1 1 INPUT fcs/pitch-trim-sum MIN -28 MAX 23 OUTPUT fcs/elevator-pos-rad GAIN 0.01745 INPUT fcs/aileron-cmd-norm INPUT fcs/roll-trim-cmd-norm CLIPTO -1 1 INPUT fcs/roll-trim-sum MIN -20 MAX 15 GAIN 0.01745 OUTPUT fcs/left-aileron-pos-rad INPUT fcs/roll-trim-sum MIN -20 MAX 15 GAIN -0.01745 OUTPUT fcs/right-aileron-pos-rad INPUT fcs/rudder-cmd-norm INPUT fcs/yaw-trim-cmd-norm CLIPTO -1 1 INPUT fcs/yaw-trim-sum MIN -16 MAX 16 GAIN 0.01745 OUTPUT fcs/rudder-pos-rad INPUT fcs/flap-cmd-norm DETENTS 4 0 0 10 2 20 1 30 1 OUTPUT fcs/flap-pos-deg AC_ALPHALIMITS -0.087 0.28 AC_HYSTLIMITS 0.09 0.36 Basic_lift Change_in_lift_due_to_ground_effect 13 aero/h_b-mac-ft none 0.0 1.203 0.1 1.127 0.15 1.090 0.2 1.073 0.3 1.046 0.4 1.055 0.5 1.019 0.6 1.013 0.7 1.008 0.8 1.006 0.9 1.003 1.0 1.002 1.1 1.0 Lift_due_to_alpha 17 2 aero/alpha-rad aero/stall-hyst-norm aero/qbar-psf | metrics/Sw-sqft 0 1 -0.09 -0.22 -0.22 0 0.25 0.25 0.09 0.73 0.73 0.1 0.83 0.78 0.12 0.92 0.79 0.14 1.02 0.81 0.16 1.08 0.82 0.17 1.13 0.83 0.19 1.19 0.85 0.21 1.25 0.86 0.24 1.35 0.88 0.26 1.44 0.9 0.28 1.47 0.92 0.3 1.43 0.95 0.32 1.38 0.99 0.34 1.3 1.05 0.36 1.15 1.15 Delta_lift_due_to_flap_deflection 4 fcs/flap-pos-deg aero/qbar-psf | metrics/Sw-sqft 0 0 10 0.20 20 0.30 30 0.35 Lift_due_to_Elevator_Deflection aero/qbar-psf | metrics/Sw-sqft | fcs/elevator-pos-rad 0.43 Lift_due_to_alpha_rate aero/qbar-psf | metrics/Sw-sqft | aero/alphadot-rad_sec | aero/ci2vel 1.7 Lift_due_to_pitch_rate aero/qbar-psf | metrics/Sw-sqft | velocities/q-aero-rad_sec | aero/ci2vel 3.9 Drag_at_zero_lift aero/qbar-psf | metrics/Sw-sqft 0.0270 Basic_drag Change_in_drag_due_to_ground_effect 13 aero/h_b-mac-ft none 0.0 0.048 0.1 0.515 0.15 0.629 0.2 0.709 0.3 0.815 0.4 0.882 0.5 0.928 0.6 0.962 0.7 0.988 0.8 1.0 0.9 1.0 1.0 1.0 1.1 1.0 Delta_drag_due_to_flap_deflection 4 fcs/flap-pos-deg aero/qbar-psf | metrics/Sw-sqft 0 0 10 0.007 20 0.012 30 0.018 Drag_due_to_alpha 26 4 aero/alpha-rad fcs/flap-pos-deg aero/qbar-psf | metrics/Sw-sqft 0 10 20 30 -0.0872664 0.00407143 3.8165e-05 0.000512444 0.00137231 -0.0698132 0.0013424 0.000440634 0.00248067 0.00412341 -0.0523599 8.96747e-05 0.00231942 0.0059252 0.00835082 -0.0349066 0.000313268 0.00567451 0.0108461 0.0140545 -0.0174533 0.00201318 0.0105059 0.0172432 0.0212346 0 0.0051894 0.0168137 0.0251167 0.0298909 0.0174533 0.00993967 0.0247521 0.0346492 0.0402205 0.0349066 0.0162201 0.0342207 0.0457119 0.0520802 0.0523599 0.0240308 0.0452195 0.0583047 0.0654701 0.0698132 0.0333717 0.0577485 0.0724278 0.0803902 0.0872664 0.0442427 0.0718077 0.088081 0.0968405 0.10472 0.056644 0.0873971 0.105265 0.114821 0.122173 0.0705754 0.104517 0.123978 0.134332 0.139626 0.086037 0.123166 0.144222 0.155373 0.15708 0.096239 0.135317 0.157346 0.168984 0.174533 0.106859 0.147857 0.170848 0.182966 0.191986 0.118034 0.160954 0.184905 0.197503 0.209439 0.129765 0.174606 0.199517 0.212596 0.226893 0.142366 0.189176 0.215072 0.228643 0.244346 0.156452 0.205363 0.23231 0.246406 0.261799 0.172732 0.223956 0.252059 0.266733 0.279253 0.178209 0.230187 0.258667 0.273529 0.296706 0.171598 0.222665 0.25069 0.265325 0.314159 0.161786 0.211468 0.2388 0.253089 0.331613 0.147493 0.19508 0.221364 0.235129 0.349066 0.109678 0.151171 0.174408 0.186649 Drag_due_to_Elevator_Deflection aero/qbar-psf | metrics/Sw-sqft | fcs/mag-elevator-pos-rad 0 Drag_due_to_sideslip aero/qbar-psf | metrics/Sw-sqft | aero/mag-beta-rad 0.17 Side_force_due_to_beta 3 2 aero/beta-rad fcs/flap-pos-deg aero/qbar-psf | metrics/Sw-sqft 0 30 -0.349 0.137 0.106 0 0 0 0.349 -0.137 -0.106 Side_force_due_to_aileron aero/qbar-psf | metrics/Sw-sqft | fcs/left-aileron-pos-rad 0 Side_force_due_to_rudder aero/qbar-psf | metrics/Sw-sqft | fcs/rudder-pos-rad 0.187 Side_force_due_to_roll_rate 2 2 aero/alpha-rad fcs/flap-pos-deg aero/qbar-psf | metrics/Sw-sqft | aero/bi2vel | velocities/p-aero-rad_sec 0 30 0.000 -0.075 -0.161 0.094 -0.145 -0.231 Side_force_due_to_yaw_rate 2 2 aero/alpha-rad fcs/flap-pos-deg aero/qbar-psf | metrics/Sw-sqft | aero/bi2vel | velocities/r-aero-rad_sec 0 30 0.000 0.214 0.162 0.094 0.267 0.215 Roll_moment_due_to_beta 3 aero/beta-rad aero/qbar-psf | metrics/Sw-sqft | metrics/bw-ft -0.349 0.0322 0 0 0.349 -0.0322 Roll_moment_due_to_roll_rate_(roll_damping) aero/qbar-psf | metrics/Sw-sqft | metrics/bw-ft | aero/bi2vel | velocities/p-aero-rad_sec -0.484 Roll_moment_due_to_yaw_rate 2 2 aero/alpha-rad fcs/flap-pos-deg aero/qbar-psf | metrics/Sw-sqft | metrics/bw-ft | aero/bi2vel | velocities/r-aero-rad_sec 0 30 0.000 0.0798 0.1246 0.094 0.1869 0.2317 Roll_moment_due_to_aileron aero/qbar-psf | metrics/Sw-sqft | metrics/bw-ft | fcs/left-aileron-pos-rad 0.229 Roll_moment_due_to_rudder aero/qbar-psf | metrics/Sw-sqft | metrics/bw-ft | fcs/rudder-pos-rad 0.0147 Pitching_moment_at_zero_alpha aero/qbar-psf | metrics/Sw-sqft | metrics/cbarw-ft 0.1 Pitch_moment_due_to_alpha aero/qbar-psf | metrics/Sw-sqft | metrics/cbarw-ft | aero/alpha-rad -1.8 Pitch_moment_due_to_pitch_rate aero/qbar-psf | metrics/Sw-sqft | metrics/cbarw-ft | aero/ci2vel | velocities/q-aero-rad_sec -12.4 Pitch_moment_due_to_alpha_rate aero/qbar-psf | metrics/Sw-sqft | metrics/cbarw-ft | aero/ci2vel | aero/alphadot-rad_sec -7.27 Pitch_moment_due_to_elevator_deflection aero/qbar-psf | metrics/Sw-sqft | metrics/cbarw-ft | fcs/elevator-pos-rad -1.122 Delta_pitching_moment_due_to_flap_deflection 4 fcs/flap-pos-deg aero/qbar-psf | metrics/Sw-sqft | metrics/cbarw-ft 0 0 10 -0.0654 20 -0.0981 30 -0.1140 Yaw_moment_due_to_beta 3 aero/beta-rad aero/qbar-psf | metrics/Sw-sqft | metrics/bw-ft -0.349 -0.0205 0 0 0.349 0.0205 Yaw_moment_due_to_roll_rate aero/qbar-psf | metrics/Sw-sqft | metrics/bw-ft | aero/bi2vel | velocities/p-aero-rad_sec -0.0278 Yaw_moment_due_to_yaw_rate aero/qbar-psf | metrics/Sw-sqft | metrics/bw-ft | aero/bi2vel | velocities/r-aero-rad_sec -0.0937 Yaw_moment_due_to_aileron aero/qbar-psf | metrics/Sw-sqft | metrics/bw-ft | fcs/left-aileron-pos-rad -0.0053 Yaw_moment_due_to_rudder aero/qbar-psf | metrics/Sw-sqft | metrics/bw-ft | fcs/rudder-pos-rad -0.043

RATE_IN_HZ 20 SIMULATION OFF ATMOSPHERE ON MASSPROPS ON AEROSURFACES ON RATES ON VELOCITIES ON FORCES ON MOMENTS ON POSITION ON COEFFICIENTS ON GROUND_REACTIONS ON FCS ON PROPULSION ON