Unknown
2003-01-01
Version
Airbus A320
This model was created using publicly available data, publicly available
technical reports, textbooks, and guesses. It contains no proprietary or
restricted data. If this model has been validated at all, it would be
only to the extent that it seems to "fly right", and that it possibly
complies with published, publicly known, performance data (maximum speed,
endurance, etc.). Thus, this model is meant for educational and entertainment
purposes only.
This simulation model is not endorsed by the manufacturer. This model is not
to be sold.
1317
111.3
14.1
333.6
44.4
231.3
0
672
0
20
80
-30
70
661.1
0
-37
942877
2.78892e+06
3.59757e+06
-0
-10000
-0
111000
672
0
-40
196.1
0
-138.2
0.5
0.8
0.02
100000
5000
5
NONE
1
688.7
-144.4
-142
0.5
0.8
0.02
150000
12000
0.0
LEFT
1
688.7
144.4
-142
0.5
0.8
0.02
150000
12000
0.0
RIGHT
1
987
0
-55.7
0.2
0.2
0.02
1.5e+06
60000
0.0
NONE
0
515.4
226.2
-104.3
0.2
0.2
0.02
1.5e+06
60000
0.0
NONE
0
515.4
-226.2
-104.3
0.2
0.2
0.02
1.5e+06
60000
0.0
NONE
0
846.1
-667.6
-37.4
0.2
0.2
0.02
1.5e+06
60000
0.0
NONE
0
846.1
667.6
-37.4
0.2
0.2
0.02
1.5e+06
60000
0.0
NONE
0
0
0
0
0.2
0.2
0.02
1.5e+06
60000
0.0
NONE
0
131.6
0
92.6
0.2
0.2
0.02
1.5e+06
60000
0.0
NONE
0
1382.6
0
340
0.2
0.2
0.02
1.5e+06
60000
0.0
NONE
0
1476.7
0
58.9
0.2
0.2
0.02
1.5e+06
60000
0.0
NONE
0
540
-200
-45
0.0
0
0
0
670
-200
-45
0.0
0.0
0.0
540
200
-45
0.0
0
0
1
670
200
-45
0.0
0.0
0.0
600
-90
-20
23940
15000
600
90
-20
23940
15000
fcs/elevator-cmd-norm
fcs/pitch-trim-cmd-norm
-1
1
fcs/pitch-trim-sum
0.018
-25
35
fcs/elevator-pos-deg
-25
35
-1
1
fcs/aileron-cmd-norm
fcs/roll-trim-cmd-norm
-1
1
fcs/roll-trim-sum
0.02
-20
15
-fcs/roll-trim-sum
0.02
-20
15
fcs/left-aileron-pos-deg
-20
15
-0.75
1
fcs/right-aileron-pos-deg
-20
15
-0.75
1
velocities/r-rad_sec
2
aero/beta-rad
-5
fcs/rudder-cmd-norm
fcs/yaw-trim-cmd-norm
-1
1
fcs/yaw-trim-sum
fcs/yaw-damper-rate
fcs/yaw-damper-beta
-1
1
fcs/rudder-sum
0.01745
-25
25
fcs/rudder-pos-deg
-25
25
-1
1
fcs/flap-cmd-norm
0
1
2
5
10
15
25
30
40
fcs/flap-pos-deg
0
40
0
1
gear/gear-cmd-norm
0
1
fcs/speedbrake-cmd-norm
0
1
Drag_at_zero_lift
aero/qbar-psf
metrics/Sw-sqft
0.016
Drag_due_to_alpha
aero/qbar-psf
metrics/Sw-sqft
aero/alpha-rad
fcs/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/mag-elevator-pos-rad
0.0500
Drag_due_to_sideslip
aero/qbar-psf
metrics/Sw-sqft
aero/mag-beta-rad
0.2000
Drag_due_to_landing_gear
aero/qbar-psf
metrics/Sw-sqft
gear/gear-pos-norm
0.0400
Drag_due_to_speedbrake
aero/qbar-psf
metrics/Sw-sqft
fcs/speedbrake-pos-norm
0.0400
Side_force_due_to_beta
aero/qbar-psf
metrics/Sw-sqft
aero/beta-rad
-0.3500 0.5000
0.0000 0.0000
0.3500 -0.5000
Lift_due_to_alpha
aero/qbar-psf
metrics/Sw-sqft
aero/alpha-rad
fcs/flap-pos-deg
0.0000 1.0000 9.0000 10.0000 40.0000
-0.0900 -0.2200 -0.2200 -0.1200 -0.1200 0.3200
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
Roll_moment_due_to_beta
aero/qbar-psf
metrics/Sw-sqft
metrics/bw-ft
aero/beta-rad
-0.3500 0.0100
0.0000 0.0000
0.3500 -0.0100
Roll_moment_due_to_roll_rate_(roll_damping)
aero/qbar-psf
metrics/Sw-sqft
metrics/bw-ft
aero/bi2vel
velocities/p-aero-rad_sec
-0.5000
Roll_moment_due_to_yaw_rate
aero/qbar-psf
metrics/Sw-sqft
metrics/bw-ft
aero/bi2vel
velocities/r-aero-rad_sec
0.0050
Roll_moment_due_to_aileron
aero/qbar-psf
metrics/Sw-sqft
metrics/bw-ft
fcs/left-aileron-pos-rad
0.2000
Roll_moment_due_to_rudder
aero/qbar-psf
metrics/Sw-sqft
metrics/bw-ft
fcs/rudder-pos-rad
0.0050
Pitching_moment_at_zero_alpha
aero/qbar-psf
metrics/Sw-sqft
metrics/cbarw-ft
fcs/flap-pos-deg
0.0000 0.0400
40.0000 -0.1000
Pitch_moment_due_to_alpha
aero/qbar-psf
metrics/Sw-sqft
metrics/cbarw-ft
aero/alpha-rad
-4.0000
Pitch_moment_due_to_elevator_Deflection
aero/qbar-psf
metrics/Sw-sqft
metrics/cbarw-ft
fcs/elevator-pos-rad
-1.5000
Pitch_moment_due_to_pitch_rate
aero/qbar-psf
metrics/Sw-sqft
metrics/cbarw-ft
aero/ci2vel
velocities/q-aero-rad_sec
-10.0000
Pitch_moment_due_to_alpha_rate
aero/qbar-psf
metrics/Sw-sqft
metrics/cbarw-ft
aero/ci2vel
aero/alphadot-rad_sec
-12.0000
Yaw_moment_due_to_yaw_rate
aero/qbar-psf
metrics/Sw-sqft
metrics/bw-ft
aero/bi2vel
velocities/r-aero-rad_sec
-0.0400
Yaw_moment_due_to_beta
aero/qbar-psf
metrics/Sw-sqft
metrics/bw-ft
aero/beta-rad
0.2000
Yaw_moment_due_to_rudder
aero/qbar-psf
metrics/Sw-sqft
metrics/bw-ft
fcs/rudder-pos-rad
-0.5000