Bicyus (Jon Ortuondo) bicyus@gmail.com 2012-02-15 0.99 Airbus A319-133 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 57.33 700.00 0 0.00 80 -30 70 661.1 0 -37 611903 1735389 2301293 0 0 0 80431 652.00 0 0.00 400 200 0 0 600 696 0 0 6600 470.1711 0 0 6600 809.5669 0 0 5940 1163.2729 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 2 655.4820 -226.575 0.000 0.0 2.2 1 620.0683 226.575 -45.567 0.0 2.2 -1 3 5 4 655.4820 226.575 0.000 0.0 2.2 -1 783.0709 -574.4148 3.1080 412 0 4 JET-A1 50 739.5669 -457.4259 -8.0898 1520.00 1520 21 2 JET-A1 50 652.5591 -236.2992 -33.9470 11982 6000 31 3 JET-A1 50 522.0473 0 -47.0 14281 0 43 1 JET-A1 50 652.5591 236.2992 -33.9470 11982 6000 31 3 JET-A1 50 739.5669 457.4259 -8.0898 1520 1520 21 2 JET-A1 50 783.0709 574.4148 3.1080 412 0 4 JET-A1 50 /controls/flight/elevator-sum /controls/flight/elevator-trim -1 1 fcs/pitch-trim-sum 0.015 -20 20

fcs/elevator-pos-rad

fcs/pitch-trim-sum -1 1

fcs/elevator-pos-norm

/controls/flight/aileron-sum /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]

/controls/flight/rudder-fdm -1

fcs/rudder-cmd-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

/controls/flight/flaps 0 0 35 40

fcs/flap-pos-deg

fcs/flap-pos-deg 0 35 0 1

fcs/flap-pos-norm

/controls/flight/slats 0 0 27 30

fcs/slat-pos-deg

fcs/slat-pos-deg 0 27 0 1

fcs/slat-pos-norm

gear/gear-cmd-norm 0 0 1 10

gear/gear-pos-norm

fcs/speedbrake-cmd-norm 0 0 1 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 -0.520 0.00 0.505 0.23 1.800 0.60 1.000 Delta Lift due to flaps aero/qbar-psf metrics/Sw-sqft fcs/flap-pos-norm 0.000 0.00000 0.290 0.00350 0.596 0.00700 0.645 0.01300 1.000 0.01700 Delta Lift due to slats aero/qbar-psf metrics/Sw-sqft fcs/slat-pos-deg 0.01000 Delta Lift due to speedbrake aero/qbar-psf metrics/Sw-sqft fcs/speedbrake-pos-norm -0.15 Lift due to Elevator Deflection aero/qbar-psf metrics/Sw-sqft fcs/elevator-pos-rad 0.04 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 0.028 1.57 1.350 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 0.00120 Drag due to slats aero/qbar-psf metrics/Sw-sqft fcs/flap-pos-deg 0.00200 Drag due to gear aero/qbar-psf metrics/Sw-sqft gear/gear-pos-norm 0.030 Drag due to speedbrakes aero/qbar-psf metrics/Sw-sqft fcs/speedbrake-pos-norm 0.03 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 -0.95 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 0.20 Roll moment due to rudder aero/qbar-psf metrics/Sw-sqft metrics/bw-ft fcs/rudder-pos-rad 0.003 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 -1.900 2.0 -0.900 Pitch moment due to pitch rate aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft aero/ci2vel velocities/q-aero-rad_sec -140 Pitch moment due to alpha rate aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft aero/ci2vel aero/alphadot-rad_sec -1 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 -0.2 Yaw moment due to rudder aero/qbar-psf metrics/Sw-sqft metrics/bw-ft fcs/rudder-pos-rad -0.2 Adverse yaw aero/qbar-psf metrics/Sw-sqft metrics/bw-ft fcs/left-aileron-pos-rad 0 294 0 -149 1 0 0