Bicyus (Jon Ortuondo) bicyus@gmail.com 2012-02-15 0.99 Airbus A320-200 with IAE V2500 Engines 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 57.33 680.00 0 0.00 80 -30 70 661.1 0 -37 611903 1735389 2301293 0 0 0 80431 655.00 0 0.00 400 200 0 0 600 696 0 0 6600 450.1711 0 0 6600 739.5669 0 0 5940 1093.2729 0 0 2000 383.4792 0 -29.5 2000 849.1324 0 -29.5 1500 931.0653 0 -29.5 2000 1068.2634 0 0 197.6772 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 0.4 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 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 1 1 50000 50000 0.0 NONE 0 838.8898 -667.5197 35.7926 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 0 589.735 -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 -1 783.0709 -574.4148 3.1080 328.13 0 4 JET-A1 50 739.5669 -457.4259 -8.0898 1520.00 154.88 21 2 JET-A1 50 652.5591 -236.2992 -33.9470 11982 11982 31 3 JET-A1 50 522.0473 0 -47.0 14281 7260 43 1 JET-A1 50 652.5591 236.2992 -33.9470 11982 11982 31 3 JET-A1 50 739.5669 457.4259 -8.0898 1520 154.88 21 2 JET-A1 50 783.0709 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 0.080 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 -0.8 Pitch_moment_due_to_elevator_Deflection aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft fcs/elevator-pos-rad velocities/mach 0.0 -1.000 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 -0.15 294 0 -149 1 0 0