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A340-600HGW.xml
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<!--A340-600HGW yasim
Liam Gathercole
Specs:
4 - 60,000lb Rolls-Royce Trent 560 Engines
A346 Values Reference:
Typical Cruise = 0.83 Mach / 35000 ft
Max Speed = 0.86 / 35000 ft
Wing span: 63.45m
Length: 75.30m
Tail Height: 17.30m
Diameter : 5.64m
Wing Area: 439.4m2
Max Fuel :51.2493 US gal
Max TO weight: 837,756.6 lbs
TO speed : 145 kt
Landing speed : 131 kt
Mach 1 = 576.6 kt @ 35,000 ft
Leading edge MAC = -3.132V
From the Wikipedia:
The A340-600HGW (High Gross Weight) version first flew on 18 November 2005 and was certified on 14 April 2006. It has an MTOW of 380 tonnes (837,756.6 lb) and a range of up to 7,900 nautical miles (14,630.8 km), made possible by strengthened structure, increased fuel capacity, more powerful engines and new manufacturing techniques like laser beam welding. The A340-600HGW is powered by four 60,000 lbf (266.9 kN) thrust Rolls-Royce Trent 560 turbofans.
-->
<airplane mass="401000" version="YASIM_VERSION_CURRENT">
<approach speed="132" alt="0.0" aoa="5.0" fuel="0.2" glide-angle="0.0">
<control-setting axis="/controls/engines/engine[0]/throttle-fdm" value="0.25"/>
<control-setting axis="/controls/engines/engine[1]/throttle-fdm" value="0.25"/>
<control-setting axis="/controls/engines/engine[2]/throttle-fdm" value="0.25"/>
<control-setting axis="/controls/engines/engine[3]/throttle-fdm" value="0.25"/>
<control-setting axis="/controls/flight/flaps" value="1"/>
<control-setting axis="/surface-positions/slats" value="1"/>
<control-setting axis="/controls/gear/gear-down" value="1"/>
<solve-weight idx="0" weight="360"/>
<solve-weight idx="1" weight="42072"/>
</approach>
<!-- Cruise configuration -->
<cruise speed="500" alt="35000" fuel="0.7">
<control-setting axis="/controls/engines/engine[0]/throttle-fdm" value="0.75"/>
<control-setting axis="/controls/engines/engine[1]/throttle-fdm" value="0.75"/>
<control-setting axis="/controls/engines/engine[2]/throttle-fdm" value="0.75"/>
<control-setting axis="/controls/engines/engine[3]/throttle-fdm" value="0.75"/>
<control-setting axis="/controls/flight/flaps" value="0.0"/>
<control-setting axis="/controls/gear/gear-down" value="0"/>
<solve-weight idx="0" weight="350"/>
<solve-weight idx="1" weight="45000"/>
</cruise>
<cockpit x="30.0" y="0.0" z="0.75"/>
<!--cockpit-->
<fuselage ax="36.36" ay="0" az="-0.64" bx="26.0" by="0.00" bz="0.0"
width="6.2" taper="0.0" midpoint="1.0"/>
<!--central-->
<fuselage ax="26.231" ay="0" az="0" bx="-20.0" by="0.00" bz="0.0"
width="6.2" taper="1.0" midpoint="0.5"/>
<fuselage ax="-20.0" ay="0" az="0" bx="-37.0" by="0.00" bz="1.2"
width="6.2" taper="0.0" midpoint="0.0"/>
<!-- engines in fuselage -->
<fuselage ax="11.0" ay="9.8" az="-3" bx="6.2" by="9.8" bz="-3"
width="2.8" taper="1.0"/>
<fuselage ax="11.0" ay="-9.8" az="-3" bx="6.2" by="-9.8" bz="-3"
width="2.8" taper="1.0"/>
<fuselage ax="4.0" ay="19.8" az="-2" bx="-0.8" by="19.8" bz="-2"
width="2.8" taper="1.0"/>
<fuselage ax="4.0" ay="-19.8" az="-2" bx="-0.8" by="-19.8" bz="-2"
width="2.8" taper="1.0"/>
<wing x="4.0" y="3.0" z="-1.66" length="31.0" chord="11.0" sweep="25"
taper=".13" dihedral="7" camber="0.005" incidence="2.6" twist="-1">
<stall aoa="15" width="8" peak="1.5"/>
<flap0 start="0" end=".56" lift="1.5" drag="1.7"/>
<flap1 start=".64" end=".88" lift="1.5" drag="1.2"/>
<slat start="0" end="1" aoa="2" drag="1.2"/>
<spoiler start="0.2" end="0.6" lift="0.2" drag="3.0"/>
<control-input axis="/controls/flight/flaps" control="FLAP0"/>
<control-input axis="/surface-positions/flap-pos-norm" control="SLAT"/>
<control-output control="FLAP0" prop="/surface-positions/flap-pos-norm"/>
<control-output control="FLAP0" prop="/surface-positions/slats"/>
<control-speed control="FLAP0" transition-time="10"/>
<control-input axis="/controls/flight/speedbrake" control="SPOILER"/>
<control-output control="SPOILER" prop="/surface-positions/speedbrake-norm"/>
<control-speed control="SPOILER" transition-time="5"/>
<control-input axis="/controls/flight/aileron" control="FLAP1" split="true"/>
<control-input axis="/controls/flight/aileron-trim" control="FLAP1" split="true"/>
<control-output control="FLAP1" side="left"
prop="/surface-positions/left-aileron-pos-norm"/>
<control-output control="FLAP1" side="right"
prop="/surface-positions/right-aileron-pos-norm"/>
</wing>
<hstab x="-32.0" y="1.5" z="1.5" chord="6.0" length="10.50" taper=".20"
sweep="28" dihedral="7">
<stall aoa="15" width="2" peak="1.5"/>
<flap0 start="0" end="1" lift="1.4" drag="1.2"/>
<control-input axis="/controls/flight/elevator" control="FLAP0"/>
<control-input axis="/controls/flight/elevator-trim" control="FLAP0"/>
<control-output control="FLAP0" prop="/surface-positions/elevator-pos-norm"/>
</hstab>
<!--hstab x="-31.0" y="1.5" z="1.0" chord="6.0" length="10.84" taper=".20"
sweep="28" dihedral="7">
<stall aoa="15" width="2" peak="1.5"/>
<flap0 start="0" end="1" lift="1.4" drag="1.2"/>
<control-input axis="/controls/flight/elevator" control="FLAP0"/>
<control-input axis="/controls/flight/elevator-trim" control="FLAP0"/>
<control-output control="FLAP0" prop="/surface-positions/elevator-pos-norm"/>
</hstab-->
<vstab x="-30.0" y="0.00" z="2.7" chord="8.0" length="12.2" taper="0.3"
sweep="33">
<stall aoa="15" width="2" peak="1.5"/>
<flap0 start="0" end="1" lift="1.4" drag="1.2"/>
<control-input axis="/controls/flight/rudder" control="FLAP0" invert="true"/>
<control-input axis="/controls/flight/rudder-trim" control="FLAP0" invert="true"/>
<control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm"
min="1" max="-1"/>
</vstab>
<!-- Engines -->
<jet x="2.16" y="19.89" z="-1.995" mass="10660" thrust="60000" spool-time="3"
egt="840" tsfc="0.235" n1-idle="23" n1-max="105" n2-idle="70" n2-max="108">
<control-input axis="/controls/engines/engine[0]/throttle-fdm" control="THROTTLE"/>
<control-input axis="/controls/engines/engine[0]/mixture" control="MIXTURE"/>
<control-input axis="/controls/engines/engine[0]/reverser" control="REVERSE_THRUST"/>
<control-output control="REVERSE_THRUST" prop="/surface-positions/reverser-norm[0]"/>
<control-speed control="REVERSE_THRUST" transition-time="1.5"/>
<actionpt x="-2.7" y="9.89" z="-2.995"/>
</jet>
<jet x="8.16" y="9.89" z="-2.995" mass="10660" thrust="60000" spool-time="3"
egt="840" tsfc="0.235" n1-idle="23" n1-max="105" n2-idle="70" n2-max="108">
<control-input axis="/controls/engines/engine[1]/throttle-fdm" control="THROTTLE"/>
<control-input axis="/controls/engines/engine[1]/mixture" control="MIXTURE"/>
<control-input axis="/controls/engines/engine[1]/reverser" control="REVERSE_THRUST"/>
<control-output control="REVERSE_THRUST" prop="/surface-positions/reverser-norm[1]"/>
<control-speed control="REVERSE_THRUST" transition-time="1.5"/>
<actionpt x="-2.7" y="9.89" z="-2.995"/>
</jet>
<jet x="8.16" y="-9.89" z="-2.995" mass="10660" thrust="60000" spool-time="3"
egt="840" tsfc="0.235" n1-idle="23" n1-max="105" n2-idle="70" n2-max="108">
<control-input axis="/controls/engines/engine[2]/throttle-fdm" control="THROTTLE"/>
<control-input axis="/controls/engines/engine[2]/mixture" control="MIXTURE"/>
<control-input axis="/controls/engines/engine[2]/reverser" control="REVERSE_THRUST"/>
<control-output control="REVERSE_THRUST" prop="/surface-positions/reverser-norm[2]"/>
<control-speed control="REVERSE_THRUST" transition-time="1.5"/>
<actionpt x="-2.7" y="-9.89" z="-2.995"/>
</jet>
<jet x="2.16" y="-19.89" z="-1.995" mass="10660" thrust="60000" spool-time="3"
egt="840" tsfc="0.235" n1-idle="23" n1-max="105" n2-idle="70" n2-max="108">
<control-input axis="/controls/engines/engine[3]/throttle-fdm" control="THROTTLE"/>
<control-input axis="/controls/engines/engine[3]/mixture" control="MIXTURE"/>
<control-input axis="/controls/engines/engine[3]/reverser" control="REVERSE_THRUST"/>
<control-output control="REVERSE_THRUST" prop="/surface-positions/reverser-norm[3]"/>
<control-speed control="REVERSE_THRUST" transition-time="1.5"/>
<actionpt x="-2.7" y="-9.89" z="-2.995"/>
</jet>
<thruster x="19.28" y="0.00" z="-5.55" vx="1" vy="0" vz="0" thrust="20000">
<control-input axis="/sim/model/pushback/target-speed-fps" control="THROTTLE" src0="-1" src1="1" dst0="-1" dst1="1"/>
</thruster>
<!-- nose -->
<gear x="29.28" y="0.00" z="-5.55"
compression="0.6" spring="0.9" damp="1">
<!--control-input axis="/controls/flight/rudder" control="STEER" square="true"/-->
<control-input control="STEER" axis="/controls/gear/nosegear-steering-cmd-norm" src0="-1.0" dst0="-1.2217304764" src1="1.0" dst1="1.2217304764" />
<control-output control="STEER" prop="/controls/gear/nosegear-steering-angle-rad" />
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
<control-output control="EXTEND" prop="/gear/gear[0]/position-norm"/>
<control-speed control="EXTEND" transition-time="7"/>
</gear>
<gear x="-2.39" y="5.6" z="-5.7" compression="0.8" spring="0.6" >
<control-input axis="/controls/gear/brake-left" control="BRAKE"/>
<control-input axis="/controls/gear/brake-parking" control="BRAKE"/>
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
<control-output control="EXTEND" prop="/gear/gear[1]/position-norm"/>
<control-speed control="EXTEND" transition-time="7"/>
</gear>
<gear x="-2.39" y="-5.6" z="-5.7" compression="0.8" spring="0.6">
<control-input axis="/controls/gear/brake-right" control="BRAKE"/>
<control-input axis="/controls/gear/brake-parking" control="BRAKE"/>
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
<control-output control="EXTEND" prop="/gear/gear[2]/position-norm"/>
<control-speed control="EXTEND" transition-time="7"/>
</gear>
<gear x="-3.8" y="0" z="-5.6" compression="3.0" spring="0.6" >
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
<control-output control="EXTEND" prop="/gear/gear[3]/position-norm"/>
<control-speed control="EXTEND" transition-time="7"/>
</gear>
<tank x="0" y="5" z="-1.5" jet="true" capacity="85500"/>
<tank x="1.0" y="0" z="-2.5" jet="true" capacity="152100"/>
<tank x="0" y="-5" z="-1.5" jet="true" capacity="85500"/>
<weight x="25.0" y="0" z="0" mass-prop="/sim/weight[0]/weight-lb"/>
<weight x="0.5" y="0" z="0" mass-prop="/sim/weight[1]/weight-lb"/>
<weight x="0.5" y="0" z="0" mass-prop="/sim/weight[2]/weight-lb"/>
<ballast x="25" y="0" z="0" mass="42000"/>
<ballast x="0" y="0" z="0" mass="40000"/>
</airplane>