Bicyus (Jon Ortuondo) bicyus@gmail.com 2012-03-09 0.01 Airbus A350XWB - 900 460 64.8 2 7.38 70.92 19.29 49.64 9.42 0 0 0 1725000 2550000 3950000 0 0 0 229100 0 0 0 400 -1165.35 0 0 40000 -300 0 0 7000 -800 0 0 0 638 0 0 0 874 0 0 13000 -307 -404 54 13000 -307 404 54 -1109.03 0 -157.33 0.8 0.5 0.02 20000 20000 70 NONE 1 -11.42 -210.04 -157.87 0.8 0.5 0.02 100000 100000 0.0 LEFT 1 -11.42 210.04 -157.87 0.8 0.5 0.02 100000 100000 0.0 RIGHT 1 -1291.33 0 0 1.0 0.4 0.4 100000 50000 0.0 NONE 0 -1138.98 0 -56.69 1.0 0.4 0.4 100000 50000 0.0 NONE 0 -986.61 0 176.77 1.0 0.4 0.4 100000 50000 0.0 NONE 0 0 0 -81.10 1.0 0.4 0.4 100000 50000 0.0 NONE 0 -79.53 0 179.92 1.0 0.4 0.4 100000 50000 0.0 NONE 0 -320.08 409.84 -128.74 1.0 0.4 0.4 100000 50000 0.0 NONE 0 -320.08 -409.84 -128.74 1.0 0.4 0.4 100000 50000 0.0 NONE 0 740.55 0 -31.21 1.0 0.4 0.4 100000 50000 0.0 NONE 0 1233.07 0 514.57 1.0 0.4 0.4 100000 50000 0.0 NONE 0 1327.95 -371.65 137.79 1.0 0.4 0.4 100000 50000 0.0 NONE 0 1327.95 371.65 137.79 1.0 0.4 0.4 100000 50000 0.0 NONE 0 394.09 -1153.94 116.54 1.0 0.4 0.4 100000 50000 0.0 NONE 0 534.25 -1274.41 207.87 1.0 0.4 0.4 100000 50000 0.0 NONE 0 394.09 1153.94 116.54 1.0 0.4 0.4 100000 50000 0.0 NONE 0 534.25 1274.41 207.87 1.0 0.4 0.4 100000 50000 0.0 NONE 0 -307 -404 54 0.0 2.2 1 5 -307 -404 54 0.0 2.2 1 -307 404 54 0.0 2.2 -1 6 -307 404 54 0.0 2.2 -1 100 0 0 0.0 0 0 0 100 0 0 0.0 0.0 0.0 534 -1274 207 300 0 0 JET-A1 50 -41 -333 51 52238 30000 31 3 JET-A1 50 -183.46 0 -59.05 145366 64000 43 1 JET-A1 50 -41 333 51 52238 30000 31 3 JET-A1 50 534 1274 207 300 0 0 JET-A1 50 -320 -409 -128 100 100 1 JET-A1 -320 409 -128 100 100 1 JET-A1 fcs/elevator-cmd-norm fcs/pitch-trim-cmd-norm -1 1 fcs/pitch-trim-sum 0.018 -30 15 fcs/elevator-pos-rad fcs/elevator-pos-deg -30 15 -1 1 fcs/elevator-pos-norm fcs/aileron-cmd-norm fcs/roll-trim-cmd-norm -1 1 fcs/roll-trim-sum 0.02 -25 25 fcs/left-aileron-pos-rad -fcs/roll-trim-sum 0.02 -25 25 fcs/right-aileron-pos-rad fcs/left-aileron-pos-deg -25 25 -0.75 1 fcs/left-aileron-pos-norm fcs/right-aileron-pos-deg -25 25 -0.75 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 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 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 0.250 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 -980.19 0.00 -65.00 1 0 0