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dhc6F.xml
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<?xml version="1.0" encoding="UTF-8"?>
<!--
DHC6-300 Twin Otter
Jan 2008 by Syd Adams.
SPECS:
Height: 5.9m
Length: 15.77
Wing span: 19.8
MTOW: 12,500 lbs
Service Ceiling = 26700 ft
Cruise at MTOW
5000 ft - 181 TAS
10,000 ft - 182 TAS
Stall :
Full Flaps = 58 kt
O Flaps = 74 kt
-->
<airplane mass="7500" version="YASIM_VERSION_CURRENT">
<approach speed="78" aoa="6.0" fuel="0.5">
<control-setting axis="/controls/engines/engine[0]/internal-throttle-fwd" value="0.30"/>
<control-setting axis="/controls/engines/engine[1]/internal-throttle-fwd" value="0.30"/>
<control-setting axis="/controls/engines/engine[0]/internal-condition" value="1.0"/>
<control-setting axis="/controls/engines/engine[1]/internal-condition" value="1.0"/>
<control-setting axis="/controls/engines/engine[0]/propeller-pitch" value="1.0"/>
<control-setting axis="/controls/engines/engine[1]/propeller-pitch" value="1.0"/>
<control-setting axis="/controls/flight/flaps" value="0.0"/>
<solve-weight idx="0" weight="360"/>
<solve-weight idx="1" weight="3150"/>
</approach>
<cruise speed="172" alt="10000" fuel="0.8">
<control-setting axis="/controls/engines/engine[0]/internal-throttle-fwd" value="1"/>
<control-setting axis="/controls/engines/engine[1]/internal-throttle-fwd" value="1"/>
<control-setting axis="/controls/engines/engine[0]/internal-condition" value="1.0"/>
<control-setting axis="/controls/engines/engine[1]/internal-condition" value="1.0"/>
<control-setting axis="/controls/engines/engine[0]/propeller-pitch" value="0.96"/>
<control-setting axis="/controls/engines/engine[1]/propeller-pitch" value="0.96"/>
<control-setting axis="/controls/flight/flaps" value="0.0"/>
<solve-weight idx="0" weight="360"/>
<solve-weight idx="1" weight="3350"/>
</cruise>
<cockpit x="2.8" y="0.3" z="0.745"/>
<fuselage ax="6.338" ay="0" az="-0.185" bx="3.609" by="0" bz="0.111"
width="1.8" taper="0.2" midpoint="1.0" cy="1.1" cx="1.1"/>
<fuselage ax="3.609" ay="0" az="0.111" bx="-2.470" by="0" bz="0.111"
width="1.8" taper="1.0" midpoint="0.5" cy="1.1" cx="1.1" />
<fuselage ax="-2.470" ay="0" az="0.111" bx="-8.811" by="0" bz="0.30"
width="1.8" taper="0.1" midpoint="0.0" cy="1.1" cx="1.1" />
<fuselage ax="2.497" ay="2.857" az="0.858" bx="-0.410" by="2.857" bz="1.012"
width="0.6" taper="0.2" midpoint="0.2" cy="1.5" cx="1.5" />
<fuselage ax="2.497" ay="-2.857" az="0.858" bx="-0.410" by="-2.857" bz="1.012"
width="0.6" taper="0.2" midpoint="0.2" cy="1.5" cx="1.5" />
<wing x="0.0" y="0.80" z="1.0" length="9.0" chord="2.0"
sweep="0" dihedral="3" taper="1" incidence="2.5" idrag="1.0" camber="0.24">
<stall aoa="10" width="6" peak="1.5"/>
<flap0 start="0" end="0.90" lift="1.6" drag="3.2"/>
<flap1 start="0.6" end="0.90" lift="1.2" drag="1.2"/>
<control-input axis="/controls/flight/flaps" control="FLAP0"/>
<control-speed control="FLAP0" transition-time="20"/>
<control-output control="FLAP0" prop="/surface-positions/flap-pos-norm"/>
<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="-7.47" y="0.08" z="1.186" length="3.15" chord="1.4"
sweep="0" dihedral="0" taper="1" camber="-0.05">
<stall aoa="17" width="6" peak="1.5"/>
<flap0 start="0" end="1" lift="1.7" drag="1.5"/>
<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="-7.312" y="0.00" z="0.3" length="2.6" chord="2.9"
sweep="20" taper="0.7" >
<stall aoa="16" width="4" 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"/>
</vstab>
<!-- frt doors-->
<vstab x="0" y="0" z="0" length="0.001" chord="0.001">
<stall aoa="16" width="4" peak="1.5"/>
<flap0 start="0" end="0.5" lift="0" drag="0"/>
<control-input axis="/controls/doors/LF-door/open" control="FLAP0"/>
<control-output control="FLAP0" prop="/controls/doors/LF-door/position-norm"/>
<control-speed control="FLAP0" transition-time="2"/>
<control-input axis="/controls/doors/RF-door/open" control="FLAP1"/>
<control-output control="FLAP1" prop="/controls/doors/RF-door/position-norm"/>
<control-speed control="FLAP1" transition-time="2"/>
</vstab>
<!-- rear doors pasenger-->
<vstab x="0" y="0" z="0" length="0.001" chord="0.001">
<stall aoa="16" width="4" peak="1.5"/>
<flap0 start="0" end="0.5" lift="0" drag="0"/>
<control-input axis="/controls/doors/LR-door-F/open" control="FLAP0"/>
<control-output control="FLAP0" prop="/controls/doors/LR-door-F/position-norm"/>
<control-speed control="FLAP0" transition-time="2"/>
<control-input axis="/controls/doors/RR-door/open" control="FLAP1"/>
<control-output control="FLAP1" prop="/controls/doors/RR-door/position-norm"/>
<control-speed control="FLAP1" transition-time="2"/>
</vstab>
<!-- rear door baggage -->
<vstab x="0" y="0" z="0" length="0.001" chord="0.001">
<stall aoa="16" width="4" peak="1.5"/>
<flap0 start="0" end="0.5" lift="0" drag="0"/>
<control-input axis="/controls/doors/LR-door-R/open" control="FLAP0"/>
<control-output control="FLAP0" prop="/controls/doors/LR-door-R/position-norm"/>
<control-speed control="FLAP0" transition-time="2"/>
<control-input axis="/controls/doors/Baggage-door/open" control="FLAP1"/>
<control-output control="FLAP1" prop="/controls/doors/Baggage-door/position-norm"/>
<control-speed control="FLAP1" transition-time="2"/>
</vstab>
<!--
2500 lbs (Jet A)
Fuel burn ... 580 lbs/hr
-->
<tank x="0.66" y="0" z="-0.5" capacity="1000" jet="true"/>
<tank x="-1.32" y="0" z="0.5" capacity="1400" jet="true"/>
<tank x="0" y="0" z="0" capacity="0"/>
<!-- Floats-->
<gear x="3.758" y="1.75" z="-2.2" compression="1.5" spring = "15" sfric = "1.2" dfric = "0.7" ignored-by-solver="1"
on-water="1" on-solid="0" reduce-friction-by-extension="1.5"
speed-planing="15" spring-factor-not-planing="0.3">
</gear>
<gear x="3.758" y="-1.75" z="-2.2" compression="1.5" spring = "15" sfric = "1.2" dfric = "0.7" ignored-by-solver="1"
on-water="1" on-solid="0" reduce-friction-by-extension="1.5"
speed-planing="15" spring-factor-not-planing="0.3">
</gear>
<gear x="-2.2" y="1.75" z="-1.7" compression="1.5" spring = "15" sfric = "1.4" dfric = "0.7" ignored-by-solver="1"
on-water="1" on-solid="0" reduce-friction-by-extension="1.2"
speed-planing="25" spring-factor-not-planing="0.25">
</gear>
<gear x="-2.2" y="-1.75" z="-1.7" compression="1.5" spring = "15" sfric = "1.4" dfric = "0.7" ignored-by-solver="1"
on-water="1" on-solid="0" reduce-friction-by-extension="1.2"
speed-planing="25" spring-factor-not-planing="0.25">
</gear>
<!-- Retractable wheels-->
<gear x="4.9" y="1.75" z="-2.744" compression="0.4" spring = "2" sfric = "0.5" dfric=".45" retract-time="4" initial-load="0" damp="0.6">
<control-input control="STEER" axis="/controls/gear/tiller" square="true"/>
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
<control-output control="EXTEND" prop="/gear/gear[4]/position-norm"/>
<control-speed control="EXTEND" transition-time="4"/>
</gear>
<gear x="4.9" y="-1.75" z="-2.744" compression="0.4" spring = "2" sfric = "0.5" dfric=".45" retract-time="4" initial-load="0" damp="0.6">
<control-input control="STEER" axis="/controls/gear/tiller" square="true"/>
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
<control-output control="EXTEND" prop="/gear/gear[5]/position-norm"/>
<control-speed control="EXTEND" transition-time="4"/>
</gear>
<gear x="-1.26" y="1.75" z="-2.68" compression="0.4" spring = "3.5" sfric = "0.5" dfric=".45" retract-time="4" initial-load="1" damp="10.1">
<control-input control="BRAKE" axis="/controls/gear/brake-parking" />
<control-input control="BRAKE" axis="/controls/gear/brake-left" />
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
<control-output control="EXTEND" prop="/gear/gear[6]/position-norm"/>
<control-speed control="EXTEND" transition-time="4"/>
</gear>
<gear x="-1.26" y="-1.75" z="-2.68" compression="0.4" spring = "3.5" sfric = "0.5" dfric=".45" retract-time="4" initial-load="1" damp="10.1">
<control-input control="BRAKE" axis="/controls/gear/brake-parking" />
<control-input control="BRAKE" axis="/controls/gear/brake-right" />
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
<control-output control="EXTEND" prop="/gear/gear[7]/position-norm"/>
<control-speed control="EXTEND" transition-time="4"/>
</gear>
<!-- 2 more Floats, need to be at this position in the file to do not brake the animation
"reduce-friction-by-extension" is reduced to get steering control-->
<gear x="-4.2" y="1.75" z="-1.7" compression="1.8" spring = "8" sfric = "0.9" dfric = "0.8" ignored-by-solver="1"
on-water="1" on-solid="0" reduce-friction-by-extension="0.7"
speed-planing="25" spring-factor-not-planing="3">
<control-input axis="/controls/gear/tiller" control="STEER"
invert ="true" square="true"/>
</gear>
<gear x="-4.2" y="-1.75" z="-1.7" compression="1.8" spring = "8" sfric = "0.9" dfric = "0.8" ignored-by-solver="1"
on-water="1" on-solid="0" reduce-friction-by-extension="0.7"
speed-planing="25" spring-factor-not-planing="3">
<control-input axis="/controls/gear/tiller" control="STEER"
invert="true" square="true"/>
</gear>
<!-- The Floats on solid ground-->
<gear x="3.75" y="1.75" z="-2.2" compression="0.4" spring = "10" sfric = "1.5" dfric = "1.3" skid="1" ignored-by-solver="1">
</gear>
<gear x="3.75" y="-1.75" z="-2.2" compression="0.4" spring = "10" sfric = "1.5" dfric = "1.3" skid="1" ignored-by-solver="1">
</gear>
<gear x="-4.2" y="1.75" z="-1.70" compression="0.2" spring = "10" sfric = "1.5" dfric = "1.3" skid="1" ignored-by-solver="1">
</gear>
<gear x="-4.2" y="-1.75" z="-1.7" compression="0.2" spring = "10" sfric = "1.5" dfric = "1.3" skid="1" ignored-by-solver="1">
</gear>
<!-- Retractable wheels on water-->
<gear x="0" y="1.75" z="-2.2" compression="0.2" spring = "0.1" sfric = "1" dfric="1" retract-time="4" on-water="1" on-solid="0"
ignored-by-solver="1" reduce-friction-by-extension="0.5">
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
<control-speed control="EXTEND" transition-time="4"/>
</gear>
<gear x="0" y="-1.75" z="-2.2" compression="0.2" spring = "0.1" sfric = "1" dfric ="1" retract-time="4" on-water="1" on-solid="0"
ignored-by-solver="1" reduce-friction-by-extension="0.5">
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
<control-speed control="EXTEND" transition-time="4"/>
</gear>
<!--
Engines:
2 PT6A-34
750 shp
Prop diam: 2.59 m
-->
<propeller x="1.3" y="2.65" z="1.0"
mass="500" moment="40" radius="1.1"
cruise-speed="146" cruise-rpm="1650"
cruise-power="375" cruise-alt="10000"
min-rpm="1650" max-rpm="2110"
fine-stop="0.2" coarse-stop="4.0">
<turbine-engine
eng-power="750" eng-rpm="2110" alt="0"
flat-rating="750" n2-low-idle="50" n2-high-idle="50" n2-max="101.5" bsfc="0.6"/>
<actionpt x="2.2" y="2.65" z="1.0"/>
<control-input axis="/controls/engines/engine[0]/internal-throttle-fwd"
src0="0" dst0="0.05" src1="1" dst1="1" control="THROTTLE"/>
<control-input axis="/controls/engines/engine[0]/internal-condition"
control="CONDLEVER"/>
<control-input axis="/controls/engines/engine[0]/starter"
control="STARTER"/>
<control-input axis="/controls/engines/engine[0]/propeller-pitch"
control="ADVANCE"/>
<control-input axis="/controls/engines/engine[0]/propeller-feather"
control="PROPFEATHER"/>
</propeller>
<propeller x="1.3" y="-2.65" z="1.1"
mass="500" moment="40" radius="1.0"
cruise-speed="146" cruise-rpm="1650"
cruise-power="375" cruise-alt="10000"
min-rpm="1650" max-rpm="2110"
fine-stop="0.2" coarse-stop="4.0">
<turbine-engine
eng-power="750" eng-rpm="2110" alt="0"
flat-rating="750" n2-low-idle="50" n2-high-idle="50" n2-max="101.5" bsfc="0.6"/>
<actionpt x="2.2" y="-2.65" z="1.0"/>
<control-input axis="/controls/engines/engine[1]/internal-throttle-fwd"
src0="0" dst0="0.05" src1="1" dst1="1" control="THROTTLE"/>
<control-input axis="/controls/engines/engine[1]/internal-condition"
control="CONDLEVER"/>
<control-input axis="/controls/engines/engine[1]/starter"
control="STARTER"/>
<control-input axis="/controls/engines/engine[1]/propeller-pitch"
control="ADVANCE"/>
<control-input axis="/controls/engines/engine[1]/propeller-feather"
control="PROPFEATHER"/>
</propeller>
<thruster x="2.2" y="2.65" z="1.0" vx="-1" vy="0" vz="0" thrust="1600">
<control-input axis="/controls/engines/engine[0]/internal-throttle-rvrs" control="THROTTLE"/>
<control-output control="THROTTLE" prop="engines/engine[0]/reverse"/>
<control-speed control="THROTTLE" transition-time="2"/>
</thruster>
<thruster x="2.2" y="-2.65" z="1.0" vx="-1" vy="0" vz="0" thrust="1600">
<control-input axis="/controls/engines/engine[1]/internal-throttle-rvrs" control="THROTTLE"/>
<control-output control="THROTTLE" prop="engines/engine[1]/reverse"/>
<control-speed control="THROTTLE" transition-time="2"/>
</thruster>
<weight x="2.5" y="0" z="0" mass-prop="/sim/weight[0]/weight-lb"/>
<weight x="0.0" y="0" z="0" mass-prop="/sim/weight[1]/weight-lb"/>
<ballast x="5" y="0" z="-2.5" mass="2078"/>
<hitch name="aerotow" x="-2.5" y="0" z="-0.85" force-is-calculated-by-other="1">
<tow length="60" weight-per-meter="0.035" elastic-constant="9000" break-force="10000" mp-auto-connect-period="1.0"/>
<winch max-tow-length="1000" min-tow-length="60" initial-tow-length="60"/>
</hitch>
</airplane>