AC_WINGAREA 174
AC_WINGSPAN 35.8
AC_CHORD 4.9
AC_HTAILAREA 21.9
AC_HTAILARM 15.7
AC_VTAILAREA 16.5
AC_LV 15.7
AC_IXX 948
AC_IYY 1346
AC_IZZ 1967
AC_IXZ 0
AC_EMPTYWT 1500
AC_AERORP 43.2 0.0 59.4
AC_CGLOC 41.0 0.0 36.5
AC_POINTMASS 180.0 36.0 -14.0 24.0
AC_EYEPTLOC 37.0 0.0 48.0
AC_GEAR NOSE -6.8 0.0 -20.0 1800 600 0.5 0.8 0.02 STEERABLE NOSE 20 FIXED
AC_GEAR LEFT_MAIN 58.2 -43.0 -17.9 5400 1600 0.5 0.8 0.02 FIXED LEFT 0 FIXED
AC_GEAR RIGHT_MAIN 58.2 43.0 -17.9 5400 1600 0.5 0.8 0.02 FIXED RIGHT 0 FIXED
AC_GEAR TAIL_SKID 188.0 0.0 8.0 20000 1000 0.2 0.2 0.2 FIXED NONE 0 FIXED
AC_GEAR LEFT_TIP 43.2 -214.8 59.4 10000 2000 0.2 0.2 0.2 FIXED NONE 0 FIXED
AC_GEAR RIGHT_TIP 43.2 214.8 59.4 10000 2000 0.2 0.2 0.2 FIXED NONE 0 FIXED
XLOC -19.7
YLOC 0.0
ZLOC 26.6
PITCH 0.0
YAW 0.0
FEED 0
FEED 1
XLOC -37.7
YLOC 0.0
ZLOC 26.6
PITCH 0.0
YAW 0
P_FACTOR 10.0
SENSE 1.0
XLOC 56.0
YLOC -112.0
ZLOC 59.4
RADIUS 29.4
CAPACITY 185.0
CONTENTS 100.0
XLOC 56.0
YLOC 112.0
ZLOC 59.4
RADIUS 29.4
CAPACITY 185.0
CONTENTS 100.0
ID 0
INPUT FG_ELEVATOR_CMD
INPUT FG_PITCH_TRIM_CMD
CLIPTO -1 1
ID 1
INPUT 0
MIN -28
MAX 23
OUTPUT FG_ELEVATOR_POS
GAIN 0.01745
ID 2
INPUT FG_AILERON_CMD
INPUT FG_ROLL_TRIM_CMD
CLIPTO -1 1
ID 3
INPUT 2
MIN -20
MAX 15
GAIN 0.01745
OUTPUT FG_LEFT_AILERON_POS
ID 4
INPUT 2
MIN -20
MAX 15
INVERT
GAIN 0.01745
OUTPUT FG_RIGHT_AILERON_POS
ID 5
INPUT FG_RUDDER_CMD
INPUT FG_YAW_TRIM_CMD
CLIPTO -1 1
ID 6
INPUT 5
MIN -16
MAX 16
GAIN 0.01745
OUTPUT FG_RUDDER_POS
ID 7
INPUT FG_FLAPS_CMD
DETENTS 4
0 0
10 2
20 1
30 1
OUTPUT FG_FLAPS_POS
AC_ALPHALIMITS -0.087 0.28
AC_HYSTLIMITS 0.09 0.36
Basic_lift
Change_in_lift_due_to_ground_effect
13
FG_HOVERB
FG_NONE
0.0 1.203
0.1 1.127
0.15 1.090
0.2 1.073
0.3 1.046
0.4 1.055
0.5 1.019
0.6 1.013
0.7 1.008
0.8 1.006
0.9 1.003
1.0 1.002
1.1 1.0
Lift_due_to_alpha
17
2
FG_ALPHA
FG_HYSTPARM
FG_QBAR|FG_WINGAREA
0 1
-0.09 -0.22 -0.22
0 0.25 0.25
0.09 0.73 0.73
0.1 0.83 0.78
0.12 0.92 0.79
0.14 1.02 0.81
0.16 1.08 0.82
0.17 1.13 0.83
0.19 1.19 0.85
0.21 1.25 0.86
0.24 1.35 0.88
0.26 1.44 0.9
0.28 1.47 0.92
0.3 1.43 0.95
0.32 1.38 0.99
0.34 1.3 1.05
0.36 1.15 1.15
Delta_lift_due_to_flap_deflection
4
FG_FLAPS_POS
FG_QBAR|FG_WINGAREA
0 0
10 0.20
20 0.30
30 0.35
Lift_due_to_Elevator_Deflection
FG_QBAR|FG_WINGAREA|FG_ELEVATOR_POS
0.347
Lift_due_to_alpha_rate
FG_QBAR|FG_WINGAREA|FG_ALPHADOT|FG_CI2VEL
1.7
Lift_due_to_pitch_rate
FG_QBAR|FG_WINGAREA|FG_AEROQ|FG_CI2VEL
3.9
Drag_at_zero_lift
FG_QBAR|FG_WINGAREA
0.026
Basic_drag
Change_in_drag_due_to_ground_effect
13
FG_HOVERB
FG_NONE
0.0 0.048
0.1 0.515
0.15 0.629
0.2 0.709
0.3 0.815
0.4 0.882
0.5 0.928
0.6 0.962
0.7 0.988
0.8 1.0
0.9 1.0
1.0 1.0
1.1 1.0
Delta_drag_due_to_flap_deflection
4
FG_FLAPS_POS
FG_QBAR|FG_WINGAREA
0 0
10 0.007
20 0.012
30 0.018
Drag_due_to_alpha
26
4
FG_ALPHA
FG_FLAPS_POS
FG_QBAR|FG_WINGAREA
0 10 20 30
-0.0872664 0.00407143 3.8165e-05 0.000512444 0.00137231
-0.0698132 0.0013424 0.000440634 0.00248067 0.00412341
-0.0523599 8.96747e-05 0.00231942 0.0059252 0.00835082
-0.0349066 0.000313268 0.00567451 0.0108461 0.0140545
-0.0174533 0.00201318 0.0105059 0.0172432 0.0212346
0 0.0051894 0.0168137 0.0251167 0.0298909
0.0174533 0.00993967 0.0247521 0.0346492 0.0402205
0.0349066 0.0162201 0.0342207 0.0457119 0.0520802
0.0523599 0.0240308 0.0452195 0.0583047 0.0654701
0.0698132 0.0333717 0.0577485 0.0724278 0.0803902
0.0872664 0.0442427 0.0718077 0.088081 0.0968405
0.10472 0.056644 0.0873971 0.105265 0.114821
0.122173 0.0705754 0.104517 0.123978 0.134332
0.139626 0.086037 0.123166 0.144222 0.155373
0.15708 0.096239 0.135317 0.157346 0.168984
0.174533 0.106859 0.147857 0.170848 0.182966
0.191986 0.118034 0.160954 0.184905 0.197503
0.209439 0.129765 0.174606 0.199517 0.212596
0.226893 0.142366 0.189176 0.215072 0.228643
0.244346 0.156452 0.205363 0.23231 0.246406
0.261799 0.172732 0.223956 0.252059 0.266733
0.279253 0.178209 0.230187 0.258667 0.273529
0.296706 0.171598 0.222665 0.25069 0.265325
0.314159 0.161786 0.211468 0.2388 0.253089
0.331613 0.147493 0.19508 0.221364 0.235129
0.349066 0.109678 0.151171 0.174408 0.186649
Drag_due_to_Elevator_Deflection
FG_QBAR|FG_WINGAREA|FG_AELEVATOR_POS
0.06
Drag_due_to_sideslip
FG_QBAR|FG_WINGAREA|FG_ABETA
0.17
Side_force_due_to_beta
3
FG_BETA
FG_QBAR|FG_WINGAREA
-0.349 0.108
0 0
0.349 -0.108
Side_force_due_to_aileron
FG_QBAR|FG_WINGAREA|FG_AILERON_POS
-0.05
Side_force_due_to_rudder
FG_QBAR|FG_WINGAREA|FG_RUDDER_POS
0.098
Side_force_due_to_roll_rate
FG_QBAR|FG_WINGAREA|FG_BI2VEL|FG_AEROP
-0.037
Side_force_due_to_yaw_rate
FG_QBAR|FG_WINGAREA|FG_BI2VEL|FG_AEROR
0.21
Roll_moment_due_to_beta
3
FG_BETA
FG_QBAR|FG_WINGAREA|FG_WINGSPAN
-0.349 0.0311
0 0
0.349 -0.0311
Roll_moment_due_to_roll_rate_(roll_damping)
FG_QBAR|FG_WINGAREA|FG_WINGSPAN|FG_BI2VEL|FG_AEROP
-0.47
Roll_moment_due_to_yaw_rate
2
FG_ALPHA
FG_QBAR|FG_WINGAREA|FG_WINGSPAN|FG_BI2VEL|FG_AEROR
0.000 0.08
0.094 0.19
Roll_moment_due_to_aileron
FG_QBAR|FG_WINGAREA|FG_WINGSPAN|FG_AILERON_POS
0.23
Roll_moment_due_to_rudder
FG_QBAR|FG_WINGAREA|FG_WINGSPAN|FG_RUDDER_POS
0.0147
Pitch_moment_due_to_alpha
FG_QBAR|FG_WINGAREA|FG_CBAR|FG_ALPHA
-1.8
Delta_pitching_moment_due_to_flap_deflection
4
FG_FLAPS_POS
FG_QBAR|FG_WINGAREA|FG_CBAR
0 0
10 -0.0654
20 -0.0981
30 -0.1140
Pitch_moment_due_to_pitch_rate
FG_QBAR|FG_WINGAREA|FG_CBAR|FG_CI2VEL|FG_AEROQ
-12.4
Pitch_moment_due_to_alpha_rate
FG_QBAR|FG_WINGAREA|FG_CBAR|FG_CI2VEL|FG_ALPHADOT
-5.2
Pitching_moment_at_zero_alpha
FG_QBAR|FG_WINGAREA|FG_CBAR
0.1
Pitch_moment_due_to_elevator_deflection
FG_QBAR|FG_WINGAREA|FG_CBAR|FG_ELEVATOR_POS
-1.28
Yaw_moment_due_to_beta
3
FG_BETA
FG_QBAR|FG_WINGAREA|FG_WINGSPAN
-0.349 -0.0227
0 0
0.349 0.0227
Yaw_moment_due_to_roll_rate
FG_QBAR|FG_WINGAREA|FG_WINGSPAN|FG_BI2VEL|FG_AEROP
-0.03
Yaw_moment_due_to_yaw_rate
FG_QBAR|FG_WINGAREA|FG_WINGSPAN|FG_BI2VEL|FG_AEROR
-0.099
Yaw_moment_due_to_aileron
FG_QBAR|FG_WINGAREA|FG_WINGSPAN|FG_AILERON_POS
0.0053
Yaw_moment_due_to_rudder
FG_QBAR|FG_WINGAREA|FG_WINGSPAN|FG_RUDDER_POS
-0.043