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 642.00 0 0.00 400 200 0 0 600 696 0 0 6600 400.1711 0 0 6600 689.5669 0 0 5940 993.2729 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 0 620.0683 -226.575 -45.567 0.0 2.2 1 3 1 2 640.4820 -226.575 -45.567 0.0 2.2 1 620.00683 226.575 -45.567 0.0 2.2 -1 3 5 4 640.4820 226.575 -45.567 0.0 2.2 -1 783.0709 -574.4148 3.1080 150 0 4 JET-A1 50 739.5669 -457.4259 -8.0898 1520.00 0 21 2 JET-A1 50 652.5591 -236.2992 -33.9470 11982 3000 31 3 JET-A1 50 522.0473 0 -47.0 14281 3000 43 1 JET-A1 50 652.5591 236.2992 -33.9470 11982 3000 31 3 JET-A1 50 739.5669 457.4259 -8.0898 1520 0 21 2 JET-A1 50 783.0709 574.4148 3.1080 150 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 /controls/flight/flaps 0 35 fcs/flap-pos-deg fcs/flap-pos-deg 0 35 0 1 fcs/flap-pos-norm /controls/flight/slats 0 27 fcs/slat-pos-deg fcs/slat-pos-deg 0 27 0 1 fcs/slat-pos-norm gear/gear-cmd-norm 0 1 gear/gear-pos-norm fcs/speedbrake-cmd-norm 0 1 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] Lift due to alpha aero/qbar-psf metrics/Sw-sqft aero/alpha-rad -0.20 -0.780 0.00 0.375 0.23 1.300 0.60 0.700
Delta Lift due to flaps aero/qbar-psf metrics/Sw-sqft fcs/flap-pos-deg 0.02000 Delta Lift due to slats aero/qbar-psf metrics/Sw-sqft fcs/flap-pos-deg 0.01800 Delta Lift due to speedbrake aero/qbar-psf metrics/Sw-sqft fcs/speedbrake-pos-norm -0.1 Lift due to Elevator Deflection aero/qbar-psf metrics/Sw-sqft fcs/elevator-pos-rad 0.15 Drag at zero lift aero/qbar-psf metrics/Sw-sqft aero/alpha-rad -1.57 1.300 -0.26 0.021 0.00 0.012 0.26 0.021 1.57 1.300
Induced drag aero/qbar-psf metrics/Sw-sqft aero/cl-squared 0.041 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
Drag due to flaps aero/qbar-psf metrics/Sw-sqft fcs/flap-pos-deg 0.00150 Drag due to slats aero/qbar-psf metrics/Sw-sqft fcs/flap-pos-deg 0.00150 Drag due to gear aero/qbar-psf metrics/Sw-sqft gear/gear-pos-norm 0.020 Drag due to speedbrakes aero/qbar-psf metrics/Sw-sqft fcs/speedbrake-pos-norm 0.02 Drag due to sideslip aero/qbar-psf metrics/Sw-sqft aero/beta-rad -1.57 1.230 -0.26 0.050 0.00 0.000 0.26 0.050 1.57 1.230
Drag due to Elevator Deflection aero/qbar-psf metrics/Sw-sqft fcs/elevator-pos-norm 0.045 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 0.15 Roll moment due to aileron aero/qbar-psf metrics/Sw-sqft metrics/bw-ft fcs/left-aileron-pos-rad 0.1 Roll moment due to rudder aero/qbar-psf metrics/Sw-sqft metrics/bw-ft fcs/rudder-pos-rad 0.01 Pitch moment due to alpha aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft aero/alpha-rad -0.6 Pitch moment due to elevator 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 -17 Pitch moment due to alpha rate aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft aero/ci2vel aero/alphadot-rad_sec -6 Yaw moment due to beta aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/beta-rad 0.12 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 rudder aero/qbar-psf metrics/Sw-sqft metrics/bw-ft fcs/rudder-pos-rad -0.1 Adverse yaw aero/qbar-psf metrics/Sw-sqft metrics/bw-ft fcs/left-aileron-pos-rad 0 294 0 -149 1 0 0