[CONFIG]
MESHNAME="A380"
SIZE=37
CAMERA=(0,1.467,6.782)
EMPTY_MASS=12000
FUEL_MASS=10000
MAIN_THRUST=2.16e5
RETRO_THRUST=5.4e4
HOVER_THRUST=2.16e5
ATTITUDE_THRUST=30000
ISP=50000
TRIM=0.05
PMI=(15.5,22.1,7.7)
CW_Z_POS=0.09
CW_Z_NEG=0.09
CW_X=2.
CW_Y=1.4
CROSS_SECTION=(53.0,186.9,25.9)
COG=9.8
PITCH_MOMENT_SCALE=0.00005
BANK_MOMENT_SCALE=0.00005
ROT_DRAG=(0.10,0.13,0.04)
[AERODYNAMICS]
; lift/drag attack point of the vertical airfoil
VAIRFOIL_ATTACK=(0,0,-0.2)
; wing chord length of the vertical airfoil
VAIRFOIL_CHORD=5
; wing area of the vertical airfoil
VAIRFOIL_AREA=90
; wing aspect ratio of the vertical airfoil
VAIRFOIL_ASPECT=1.5
; lift/drag attack point of the horizontal airfoil
HAIRFOIL_ATTACK=(0,0,-4)
; wing chord length of the horizontal airfoil
HAIRFOIL_CHORD=5
; wing area of the horizontal airfoil
HAIRFOIL_AREA=15
; wing aspect ratio of the horizontal airfoil
HAIRFOIL_ASPECT=1.5
; surface area of aileron
AILERON_AREA=0.1
; lift change of aileron
AILERON_LIFT=1.5
; lift/drag attack point of left aileron (right aileron deduced by x -> -x
AILERON_ATTACK=(7.5,0,-7.2)
ELEVATOR_AREA=1.2
; lift change of elevator
ELEVATOR_LIFT=1.5
; lift/drag attack point of elevator
ELEVATOR_ATTACK=(0,0,-7.2)
RUDDER_AREA=0.3
; lift change of rudder
RUDDER_LIFT=1.5
; lift/drag attack point of rudder
RUDDER_ATTACK=(0,0,-7.2)
[EX_MAIN_0]
OFF=(-15,-2.7.7)
DIR=(0,0,-1)
LENGTH=12
WIDTH=1
[EX_MAIN_1]
OFF=(15,-2.7.7)
DIR=(0,0,-1)
LENGTH=12
WIDTH=1
[ANIM_SEQ_0]
; Airbrake
NAME="Airbrake"
KEY=K
DURATION=1
REPEAT=0
[ANIM_SEQ_1]
; Flaps
NAME="Flaps"
KEY=F
DURATION=1.0
DIRECTION=(0,1,-0.2)
QFACTOR=2
INITIAL=0
REPEAT=0
[ANIM_SEQ_2]
; landing gear
KEY=G
DURATION=3
[ANIM_COMP_0]
; left wheel door
SEQ=2
GROUPS=53
RANGE=(0.2,0.7)
ROT_PNT=(-2.1,-8.1611,-11.417)
ROT_AXIS=(0,0,1)
ANGLE=-90
[ANIM_COMP_1]
; left wheel
SEQ=2
GROUPS=51
RANGE=(0.0,0.3)
ROT_PNT=(-6.5352,-1.8413,-0.982)
ROT_AXIS=(0,0,1)
ANGLE=90
[SOUND]
COCKPIT_AMBIENCE_1=ambience1
COCKPIT_AMBIENCE_2=BG typing