Bicyus (Jon Ortuondo) bicyus@gmail.com 2012-02-22 0.99 Airbus A320-200 with IAE V2500 Engines Revised and fixed by Peter Brendt (jwocky) and Joshua Davidson (it0uchpods). Fork from the A320-Family aircraft project (Thanks to all authors) 1319.79 111.26 1.03 13.76 334.24 57.88 248.79 57.33 642.122 0 -25.2091 80 -30 70 661.1 0 -37 1725000 2550000 3950000 0 0 0 42095.1863 650.122 0 -41.7398 400 200 0 0 19750 705 0 0 3750 383.01 0 -59.05 0 857.55 0 -59.05 0 1094 0 -39.37 5248 589.735 -226.575 -45.567 5248 589.735 226.575 -45.567 197.6772 0 -137.9617 0.8 0.5 0.02 30935.5 16978.5 70 NONE 1 695.3149 -149.4094 -150.4824 0.8 0.5 0.02 59785 23957 0.0 LEFT 1 695.3149 149.4094 -150.4824 0.8 0.5 0.02 59785 23957 0.0 RIGHT 1 37.7953 0 -38.1374 1.0 0.4 0.4 50000 50000 0.0 NONE 0 128.1102 0 -55.0271 1.0 0.4 0.4 50000 50000 0.0 NONE 0 274.0157 0 -60.0665 1.0 0.4 0.4 50000 50000 0.0 NONE 0 930 0 -60.0665 1.0 0.4 0.4 50000 50000 0.0 NONE 0 589.735 -226.575 -95.567 1.0 0.5 0.4 50000 50000 0.0 NONE 0 589.735 226.575 -95.567 1.0 0.4 0.4 50000 50000 0.0 NONE 0 1097.9921 0 -44.7722 1.0 0.4 0.4 50000 50000 0.0 NONE 0 1225 0 -18.8067 1.0 0.4 0.4 50000 50000 0.0 NONE 0 1341.6142 0 -10.2599 1.0 0.4 0.4 50000 50000 0.0 NONE 0 1469.0945 0 47.4138 1.0 0.4 0.4 50000 50000 0.0 NONE 0 838.8898 -667.5197 35.7926 1.0 1 1 50000 50000 0.0 NONE 0 838.8898 667.5197 35.7926 1.0 1 1 50000 50000 0.0 NONE 0 589.735 -226.575 -45.567 0.0 2.2 1 3 1 2 589.735 -226.575 -45.567 0.0 2.2 1 589.735 226.575 -45.567 0.0 2.2 -1 3 5 4 589.735 226.575 -45.567 0.0 2.2 -1 788.4322 -574.4148 3.1080 328.13 0 4 JET-A1 50 737.4190 -457.4259 -8.0898 1548.8 154.88 21 2 JET-A1 50 630.6588 -236.2992 -33.9470 12186.9 2437.38 31 3 JET-A1 50 580.9955 0 -47.0 14520 0 43 1 JET-A1 50 630.6588 236.2992 -33.9470 12186.9 2437.38 31 3 JET-A1 50 737.4190 457.4259 -8.0898 1548.8 154.88 21 2 JET-A1 50 788.4322 574.4148 3.1080 328.13 0 4 JET-A1 50 /controls/flight/elevator /controls/flight/elevator-trim -1 1 fcs/pitch-trim-sum 0.025 -10 10 fcs/elevator-pos-rad fcs/elevator-pos-deg -10 10 -1 1 fcs/elevator-pos-norm /controls/flight/aileron /controls/flight/aileron-trim -1 1 fcs/roll-trim-sum 0.02 -15 15 fcs/left-aileron-pos-rad -fcs/roll-trim-sum 0.02 -15 15 fcs/right-aileron-pos-rad fcs/left-aileron-pos-deg -15 15 -1 1 fcs/left-aileron-pos-norm fcs/right-aileron-pos-deg -15 15 -1 1 fcs/right-aileron-pos-norm /controls/engines/engine[0]/throttle-fdm 1 fcs/throttle-cmd-norm fcs/throttle-pos-norm /controls/engines/engine[1]/throttle-fdm 1 fcs/throttle-cmd-norm[1] fcs/throttle-pos-norm[1] 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 0 40 40 fcs/flap-pos-deg fcs/flap-pos-deg 0 40 0 1 fcs/flap-pos-norm gear/gear-cmd-norm 0 0 1 10 gear/gear-pos-norm fcs/speedbrake-cmd-norm 0 0 1 2 fcs/speedbrake-pos-norm /controls/gear/tiller-enabled == 0 Steering command for nose gear /controls/gear/tiller-cmd-norm/controls/flight/rudder -1 0 1 -1 -70 -70 -70 0 -7 0 7 1 70 70 70

/controls/gear/tiller-enabled /controls/flight/rudder 70 /controls/gear/tiller-disabled fcs/steer-nose-deg[0] 70 fcs/steer-pos-deg[0] Change_in_drag_due_to_ground_effect aero/h_b-mac-ft 0.0000 0.4800 0.1000 0.5150 0.1500 0.6290 0.2000 0.7090 0.3000 0.8150 0.4000 0.8820 0.5000 0.9280 0.6000 0.9620 0.7000 0.9880 0.8000 1.0000 0.9000 1.0000 1.0000 1.0000 1.1000 1.0000

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

Drag_at_zero_lift aero/qbar-psf metrics/Sw-sqft 0.30 Lift_due_to_alpha aero/qbar-psf metrics/Sw-sqft aero/function/kCLge aero/alpha-radfcs/flap-pos-deg 0.0000 1.0000 9.0000 10.0000 40.0000 -0.0900 -0.2200 -0.2200 -0.1200 -0.1200 0.2500 0.0000 0.2500 0.2500 0.3500 0.3500 0.7500 0.0900 0.7300 0.7300 0.8300 0.8300 1.2300 0.1000 0.8300 0.8300 0.9300 0.9300 1.3300 0.1200 0.9200 0.9200 1.0200 1.0200 1.4200 0.1400 1.0200 1.0200 1.1200 1.1200 1.5200 0.1600 1.0800 1.0800 1.1800 1.1800 1.5800 0.1700 1.1300 1.1300 1.2300 1.2300 1.6300 0.1900 1.1900 1.1900 1.2900 1.2900 1.6900 0.2100 1.2500 1.2500 1.3500 1.3500 1.7700 0.2400 1.3500 1.3700 1.4700 1.4800 1.9300 0.2600 1.4400 1.4700 1.5700 1.6200 2.1200 0.2800 1.4700 1.5100 1.6100 1.7800 2.4000 0.3000 1.5000 1.5600 1.6600 1.9000 2.3000 0.3200 1.4700 1.6100 1.6000 1.7000 2.0300 0.3400 1.3500 1.5000 1.4100 1.5000 1.5300 0.3600 1.1500 1.2000 1.2000 1.2000 1.2000

Lift due to Elevator Deflection aero/qbar-psf metrics/Sw-sqft fcs/elevator-pos-rad 0.1930 Delta Lift due to speedbrake aero/qbar-psf metrics/Sw-sqft fcs/speedbrake-pos-norm -0.15 Drag_at_zero_lift aero/qbar-psf metrics/Sw-sqft 0.016 Drag_due_to_alpha aero/qbar-psf metrics/Sw-sqft aero/alpha-radfcs/flap-pos-deg 0.0000 1.0000 25.0000 40.0000 -0.0873 0.0041 0.0000 0.0005 0.0014 -0.0698 0.0013 0.0004 0.0025 0.0041 -0.0524 0.0001 0.0023 0.0059 0.0084 -0.0349 0.0003 0.0057 0.0108 0.0141 -0.0175 0.0020 0.0105 0.0172 0.0212 0.0000 0.0052 0.0168 0.0251 0.0399 0.0175 0.0099 0.0248 0.0346 0.0502 0.0349 0.0162 0.0342 0.0457 0.0621 0.0524 0.0240 0.0452 0.0583 0.0755 0.0698 0.0334 0.0577 0.0724 0.0904 0.0873 0.0442 0.0718 0.0881 0.1068 0.1047 0.0566 0.0874 0.1053 0.1248 0.1222 0.0706 0.1045 0.1240 0.1443 0.1396 0.0860 0.1232 0.1442 0.1654 0.1571 0.0962 0.1353 0.1573 0.1790 0.1745 0.1069 0.1479 0.1708 0.1930 0.1920 0.1180 0.1610 0.1849 0.2075 0.2094 0.1298 0.1746 0.1995 0.2226 0.2269 0.1424 0.1892 0.2151 0.2386 0.2443 0.1565 0.2054 0.2323 0.2564 0.2618 0.1727 0.2240 0.2521 0.2767 0.2793 0.1782 0.2302 0.2587 0.2835 0.2967 0.1716 0.2227 0.2507 0.2753 0.3142 0.1618 0.2115 0.2388 0.2631 0.3316 0.1475 0.1951 0.2214 0.2451 0.3491 0.1097 0.1512 0.1744 0.1966

Drag due to Elevator Deflection aero/qbar-psf metrics/Sw-sqft fcs/elevator-pos-norm 0.055 Drag_due_to_sideslip aero/qbar-psf metrics/Sw-sqft aero/mag-beta-rad 0.2000 Drag due to gear aero/qbar-psf metrics/Sw-sqft gear/gear-pos-norm 0.04 Drag due to speedbrakes aero/qbar-psf metrics/Sw-sqft fcs/speedbrake-pos-norm 0.04 Drag due to mach aero/qbar-psf metrics/Sw-sqft velocities/mach 0.00 0.000 0.79 0.000 1.10 0.023 1.80 0.015

Side force due to beta aero/qbar-psf metrics/Sw-sqft aero/beta-rad -1 Roll moment due to beta aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/beta-rad -0.1 Roll moment due to roll rate aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/bi2vel velocities/p-aero-rad_sec -0.4 Roll moment due to yaw rate aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/bi2vel velocities/r-aero-rad_sec 0.005 Roll moment due to aileron aero/qbar-psf metrics/Sw-sqft metrics/bw-ft fcs/left-aileron-pos-rad velocities/mach 0.0 0.100 2.0 0.033

Roll moment due to rudder aero/qbar-psf metrics/Sw-sqft metrics/bw-ft fcs/rudder-pos-rad 0.005 Pitching_moment_at_zero_alpha aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft fcs/flap-pos-deg 0.0000 0.0000 40.0000 -0.1000

Pitch_moment_due_to_alpha aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft aero/alpha-rad -0.6 Pitch_moment_due_to_elevator_Deflection aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft fcs/elevator-pos-rad velocities/mach 0.0 -1.200 2.0 -0.300

Pitch_moment_due_to_pitch_rate aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft aero/ci2vel velocities/q-aero-rad_sec -10 Pitch_moment_due_to_alpha_rate aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft aero/ci2vel aero/alphadot-rad_sec -12 Yaw moment due to yaw rate aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/bi2vel velocities/r-aero-rad_sec -0.15 Yaw moment due to beta aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/beta-rad 0.12 Yaw moment due to rudder aero/qbar-psf metrics/Sw-sqft metrics/bw-ft fcs/rudder-pos-rad -0.2 294 0 -149 1 0 0