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EF-Typhoon-yasim-test-noG.xml
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<?xml version="1.0"?>
<!--
Eurofighter Typhoon
Testing version without G-limitations: Search #G# for uncomment
(bugs: easy spin)
TODO:
* Strengthen parking brakes
* Adjust coord. of ballast, tanks, weights, slats more effective, thrust vectoring
* Fixed: error on wing degres, fuel consume more moderated, mach 1.2 without afterburners (for mach 1.5 -sea level-, 2 -hight altitude- within & "fuel freeze":
*Missing some message warning over fuel consume on right-bottom cockpit panel).
TESTING:
ballast and tank(1)
Solution results: Iterations: 181
Drag Coefficient: 14.511739
Lift Ratio: 207.134399
Cruise AoA: 0.744704
Tail Incidence: 0.707308
Approach Elevator: 0.005814
CG: x:-9.649, y:-0.000, z:0.095
Inertia tensor : 40838.133, -0.000, 5923.480
[kg*m^2] -0.000, 178467.578, 0.000
Origo at CG 5923.480, 0.000, 209226.156
-->
<airplane mass="24581" version="YASIM_VERSION_ORIGINAL">
<!-- Approach configuration -->
<approach speed="130" aoa="9">
<control-setting axis="/controls/engines/engine[0]/throttle" value="0.4"/>
<control-setting axis="/controls/engines/engine[1]/throttle" value="0.4"/>
<control-setting axis="/controls/flight/flaps" value="0"/>
<control-setting axis="/controls/gear/gear-down" value="1"/>
<control-setting axis="/controls/flight/speedbrake" value="0"/>
<control-setting axis="/controls/flight/slats" value="0"/>
</approach>
<!-- For Maximun perfomance test. Mach 2.0+
<cruise speed="1480" alt="45000">
<control-setting axis="/controls/engines/engine[0]/throttle" value="1"/>
<control-setting axis="/controls/engines/engine[1]/throttle" value="1"/>
<control-setting axis="/controls/engines/engine[0]/afterburner" value="1"/>
<control-setting axis="/controls/engines/engine[1]/afterburner" value="1"/>
<control-setting axis="/controls/flight/flaps" value="0"/>
<control-setting axis="/controls/gear/gear-down" value="0"/>
<control-setting axis="/controls/flight/speedbrake" value="0"/>
<control-setting axis="/controls/flight/slats" value="1"/>
</cruise>
-->
<!--
Cruise configuration. Reaches 1.1/1.3 Mach without afterburne and basic air-to-air load
with 860 seem fine and reaches within 1.5 sea level; stall 80-90 kt!
-->
<cruise speed="860" alt="45000">
<control-setting axis="/controls/engines/engine[0]/throttle" value="0.94"/>
<control-setting axis="/controls/engines/engine[1]/throttle" value="0.94"/>
<control-setting axis="/controls/flight/flaps" value="0"/>
<control-setting axis="/controls/gear/gear-down" value="0"/>
<control-setting axis="/controls/flight/speedbrake" value="0"/>
<control-setting axis="/controls/flight/slats" value="0"/>
</cruise>
<!-- pilot eyepoint -->
<cockpit x="-4" y="0.0" z="1.18"/>
<!--
fuselage : another test
<fuselage ax="0" ay="0" az="0.067"
bx="-3.0" by="0" bz="0.35"
width="1.2" taper= "0.0" midpoint= "1.0"/>
<fuselage ax="-3" ay="0" az="0.35"
bx="-11.08" by="0" bz="0.35"
width="1.3" taper= "0.9" midpoint= "1.0"/>
<fuselage ax="-11.08" ay="0" az="0.261"
bx="-14.96" by="0" bz="0.261"
width="1.8" taper= "0.9" midpoint= "0.1"/>
-->
<fuselage ax="0" ay="0" az="0.067"
bx="-3.0" by="0" bz="0.35"
width="1.2" taper= "0.0" midpoint= "1.0"/>
<fuselage ax="-3" ay="0" az="0.35"
bx="-5.0" by="0" bz="0.35"
width="1.3" taper= "0.9" midpoint= "1.0"/>
<fuselage ax="-5.0" ay="0" az="0.067"
bx="-14.96" by="0" bz="0.05"
width="2.1" taper= "0.6" midpoint= "0.7"/>
<!-- cockpit and upper fuselage -->
<fuselage ax="-2.61" ay="0.0" az="1"
bx="-6" by="0.0" bz="0.8"
width="0.9" taper= "0.45" midpoint= "0.17"/>
<!-- vstab mount cx="1.6" cy="1.2"
<fuselage ax="-11.20" ay="0" az="1.1"
bx="-14.88" by="0" bz="0.6"
width="0.4" taper= "0.9" midpoint= "0.65"/>
-->
<!-- pods -->
<fuselage ax="-10.6964" ay="5.471" az="-0.263"
bx="-13.231" by="5.461" bz="-0.263"
width="0.37" taper= "0.8" midpoint= "0.65"/>
<fuselage ax="-10.6964" ay="-5.471" az="-0.263"
bx="-13.231" by="-5.461" bz="-0.263"
width="0.37" taper= "0.8" midpoint= "0.65"/>
<!-- wing mounts
<fuselage ax="-5.9526" ay="0.99" az="-0.14"
bx="-13.65" by="1.183" bz="-0.35"
width="0.2" taper= "0.9" midpoint= "0.9"/>
<fuselage ax="-5.9526" ay="-0.99" az="-0.14"
bx="-13.65" by="-1.183" bz="-0.35"
width="0.2" taper= "0.9" midpoint= "0.9"/>
-->
<fuselage ax="-5.9526" ay="0.79" az="-0.14"
bx="-13.65" by="0.983" bz="-0.35"
width="0.4" taper= "0.9" midpoint= "0.9"/>
<fuselage ax="-5.9526" ay="-0.79" az="-0.14"
bx="-13.65" by="-0.983" bz="-0.35"
width="0.4" taper= "0.9" midpoint= "0.9"/>
<!-- engine mounts -->
<fuselage ax="-11.08" ay="0.532" az="-0.06"
bx="-14.914" by="0.532" bz="-0.06"
width="1" taper= "1" midpoint= "0.8"/>
<fuselage ax="-11.08" ay="-0.532" az="-0.06"
bx="-14.914" by="-0.532" bz="-0.06"
width="1" taper= "1" midpoint= "0.8"/>
<!--
on testing
flap0 = foreplane, flap1 = variable capture air intake
-->
<hstab x="-2.785" y="0.556" z="0.222"
taper="0.34"
length="1.6"
chord="1.642"
sweep="35"
dihedral="-10">
<stall aoa="35" width="13" peak="1.5"/>
<flap0 start="0.001" end="1" lift="1.9" drag="1.4"/>
<flap1 start="0.001" end="0.15" lift="1.4" drag="1.2"/>
<control-input axis="/controls/flight/elevator" control="FLAP0" invert="true" square="true"/>
<control-input axis="/controls/flight/elevator-trim" control="FLAP0" invert="true"/>
<control-input axis="/controls/flight/flaps" control="FLAP1" invert="false"/>
<control-output control="FLAP0" prop="/surface-positions/elevator-pos-norm"/>
<control-output control="FLAP1" prop="/surface-positions/flap-pos-norm"/>
<!-- #G#
<control-input axis="/accelerations/pilot-g" control="FLAP0" invert="true" src0="5" src1="9.5" dst0="0" dst1="1" />
<control-input axis="/accelerations/pilot-g" control="FLAP0" invert="true" src0="-5" src1="-4" dst0="-1" dst1="0" />
#G#
-->
<control-speed control="FLAP1" transition-time="1.5"/>
</hstab>
<!--
Other test, for fine AFCS work: flap0 = flapleron0, flap1 = flapleron1, slats, spoiler=speedbrake
Problem: spoilers do nothing.
-->
<!--
On test fine: flap0 = flaplerons, slat = slats, flap1 = speedbrake (from wing)
-->
<wing x="-9.525" y="1.016" z="-0.199"
taper="0.18"
incidence="1.5"
twist="-2"
length="4.95"
chord="7"
sweep="30"
dihedral="0">
<stall aoa="21" width="8" peak="1.3"/>
<slat start="0.2" end="0.95" aoa="6" lift="1.2" drag="1.2"/>
<flap0 start="0.02" end="0.95" lift="1.2" drag="1.0"/>
<flap1 start="0.001" end="0.091" lift="0.001" drag="1.9"/>
<control-input axis="/controls/flight/aileron" control="FLAP0" split="true"/>
<control-input axis="/controls/flight/aileron-trim" control="FLAP0" split="true"/>
<control-input axis="/controls/flight/speedbrake" control="FLAP1" invert="true"/>
<!--control-input axis="/controls/flight/speedbrake" control="SPOILER" invert="true"/-->
<control-input axis="/controls/flight/slats" control="SLAT"/>
<control-output control="SLAT" prop="/surface-positions/slats-pos-norm"/>
<control-output control="FLAP0" side="left" prop="/surface-positions/left-aileron-pos-norm"/>
<control-output control="FLAP0" side="right" prop="/surface-positions/right-aileron-pos-norm"/>
<!--control-output control="FLAP0" prop="/surface-positions/aileron-pos-norm"/-->
<control-output control="FLAP1" prop="/surface-positions/speedbrake-pos-norm"/>
<control-speed control="SLAT" transition-time="2"/>
<control-speed control="FLAP0" transition-time="1.05"/>
<control-speed control="FLAP1" transition-time="3.0"/>
</wing>
<vstab x="-13.198" y="0.0" z="0.817"
taper="0.38"
length="3.9"
chord="2.952"
sweep="40" >
<stall aoa="27" width="10" peak="1.5"/>
<flap0 start="0.001" end="0.8" lift="1.3" drag="1.3"/>
<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"/>
<control-speed control="FLAP0" transition-time="1"/>
</vstab>
<!-- tsfc 0.7 seens excessive; n2-max="105"; 21000
reverse on test -->
<jet x="-12.8" y="0.532" z="-0.028"
mass="2204"
thrust="13490"
afterburner="20230"
tsfc="0.4"
n1-idle="25" n1-max="100" n2-idle="30" n2-max="100"
exhaust-speed="1850"
rotation="0">
<actionpt x="-14.914" y="0.532" z="-0.028"/>
<!--thrust vectoring here -->
<control-input axis="/controls/engines/engine[0]/throttle" control="THROTTLE"/>
<control-input axis="/controls/engines/engine[0]/reheat" control="REHEAT"/>
<control-input axis="/controls/engines/engine[0]/reverser" control="REVERSE_THRUST"/>
<control-output control="REHEAT" prop="engines/engine[0]/afterburner" />
</jet>
<jet x="-12.8" y="-0.532" z="-0.028"
mass="2204"
thrust="13490"
afterburner="20230"
tsfc="0.4"
n1-idle="25" n1-max="100" n2-idle="30" n2-max="100"
exhaust-speed="1850"
rotation="0">
<actionpt x="-14.914" y="-0.532" z="-0.028"/>
<!--thrust vectoring here -->
<control-input axis="/controls/engines/engine[1]/throttle" control="THROTTLE"/>
<control-input axis="/controls/engines/engine[1]/reheat" control="REHEAT"/>
<control-input axis="/controls/engines/engine[1]/reverser" control="REVERSE_THRUST"/>
<control-output control="REHEAT" prop="engines/engine[1]/afterburner" />
</jet>
<!--
Gear:
Parking brakes on until 80% of throttle, real model parking brakes with 100% throttle and reheat.
with brake-parking on noseger, for use only on taxi-ground -->
<gear x="-5.375" y="0" z="-2.05"
retract-time="1" initial-load="10"
compression="0.4" upx="0" upy="0" upz="0.3" spring="5" damp="4"> <!-- testing -->
<control-input axis="/controls/flight/rudder" control="STEER" square="true"
src0="-1" src1="1" dst0="-0.9" dst1="0.9"/>
<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[0]/position-norm"/>
<control-speed control="EXTEND" transition-time="7"/>
</gear>
<!-- left main -->
<gear x="-9.8" y="2.093" z="-2.03"
retract-time="1"
compression="0.4" upx="-0.02" upy="0.01" upz="0.19"
spring="0.8" damp="2">
<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="8"/>
<control-speed control="BRAKE" transition-time="1"/>
</gear>
<!-- right main -->
<gear x="-9.8" y="-2.093" z="-2.03"
retract-time="1"
compression="0.4" upx="-0.02" upy="-0.01" upz="0.19"
spring="0.8" damp="2">
<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="8"/>
<control-speed control="BRAKE" transition-time="1"/>
</gear>
<!-- Carrier ops -->
<!-- Hook f14b ; true length seem +/- max "2.2246" min "2.06" -->
<hook x="-12.20" y="-0.0192" z="-0.5483" length="2.25" down-angle="60" up-angle="-3">
<control-input axis="/controls/gear/tailhook" control="HEXTEND"/>
<control-speed control="HEXTEND" transition-time="4"/>
</hook>
<!-- Launch-bar f14b ; over nosegear tail: x="-5.406" y="0.0" z="-0.7945" length="1.463"
over nosewheel : x="-5.44" y="0.0" z="-1.175" -->
<launchbar x="-5.44" y="0.0" z="-1.175" length="1.463">
<control-input axis="/controls/gear/launchbar" control="LEXTEND"/>
<control-speed control="LEXTEND" transition-time="1"/>
</launchbar>
<!-- tanks ahead gear 9.2, best that 9.8 (otherwise crash on parking!) -->
<!-- front, 7.3 ? -->
<tank x="-6.5" y="0.0" z="-0.25" jet="true" capacity="3990"/>
<!-- rear, 9.2 ! -->
<tank x="-9.2" y="-0.0" z="-0.25" jet="true" capacity="1873"/>
<!-- left wing tanks -->
<tank x="-9.3" y="2.2" z="-0.18" jet="true" capacity="420"/>
<tank x="-10.1" y="2.7" z="-0.18" jet="true" capacity="882"/>
<!-- right wing tanks -->
<tank x="-9.3" y="-2.2" z="-0.18" jet="true" capacity="420"/>
<tank x="-10.1" y="-2.7" z="-0.18" jet="true" capacity="882"/>
<!-- drop tanks -->
<tank x="-9.2" y="2.824" z="-0.6" jet="true" capacity="2645"/>
<tank x="-9.2" y="-2.824" z="-0.6" jet="true" capacity="2645"/>
<tank x="-9.2" y="0.0" z="-0.8" jet="true" capacity="2204"/>
<tank x="-9.2" y="0.0" z="-0.8" jet="true" capacity="0"/>
<!-- ballast
<ballast x="-3.05" y="0" z="-0.1" mass="1000"/>
<ballast x="-2.74" y="0" z="-0.35" mass="1200"/>
ballast compensation by brute force
<ballast x="-2.7" y="0" z="-1.2" mass="3270"/>
-->
<!-- trim - compensación hasta 3200 -->
<ballast x="-0.7" y="0" z="0.1" mass="1100"/>
<!-- radar, cockpit-->
<ballast x="-2" y="0" z="0.22" mass="400"/>
<ballast x="-3" y="0" z="0.22" mass="500"/>
<!-- piloto -->
<ballast x="-4.09" y="0" z="0.5" mass="400"/>
<!-- mauser (-6.12). APU -->
<ballast x="-5" y="0" z="0.22" mass="300"/>
<ballast x="-5.5" y="0" z="0" mass="700"/>
<!-- <ballast x="-0.9" y="0" z="-0.75" mass ="500"/> -->
<weight x="-4.5" y="0" z="0.6" mass-prop="/yasim/weights/pilot-lb"/>
<!--
<weight x="-0.39" y="0" z="-1.33" size="1.5" mass-prop="/yasim/hunter/weights/right-inboard-lbs"/>
<weight x="-0.79" y="2" z="-1.33" size="1" mass-prop="/yasim/hunter/weights/left-inboard-lbs"/>
-->
<!-- external loads -->
<weight x="-10.36"
y="4.7"
z="-0.65"
size="0.25"
mass-prop="sim/weight[0]/weight-lb"
/>
<weight x="-9.536"
y="3.802"
z="-0.775"
size="0.45"
mass-prop="sim/weight[1]/weight-lb"
/>
<!-- left droptank -->
<weight x="-9.4"
y="2.824"
z="-0.6"
size="0.7"
mass-prop="sim/weight[2]/weight-lb"
/>
<weight x="-7.376"
y="1.739"
z="-0.817"
size="0.45"
mass-prop="sim/weight[3]/weight-lb"
/>
<!-- center -->
<weight x="-9.4"
y="0.0"
z="-0.32"
size="0.6"
mass-prop="sim/weight[4]/weight-lb"
/>
<weight x="-7.376"
y="-1.739"
z="-0.817"
size="0.45"
mass-prop="sim/weight[5]/weight-lb"
/>
<!-- right droptank -->
<weight x="-9.4"
y="-2.824"
z="-0.6"
size="0.7"
mass-prop="sim/weight[6]/weight-lb"
/>
<weight x="-9.536"
y="-3.802"
z="-0.775"
size="0.45"
mass-prop="sim/weight[7]/weight-lb"
/>
<weight x="-10.36"
y="-4.7"
z="-0.65"
size="0.25"
mass-prop="sim/weight[8]/weight-lb"
/>
<!-- fuselage AMRAAMs -->
<weight x="-6.793"
y="0.882"
z="-0.616"
size="0.3"
mass-prop="sim/weight[9]/weight-lb"
/>
<weight x="-11.627"
y="0.979"
z="-0.616"
size="0.3"
mass-prop="sim/weight[10]/weight-lb"
/>
<weight x="-6.793"
y="-0.882"
z="-0.616"
size="0.3"
mass-prop="sim/weight[11]/weight-lb"
/>
<weight x="-11.627"
y="-0.979"
z="-0.616"
size="0.3"
mass-prop="sim/weight[12]/weight-lb"
/>
</airplane>