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CS300.xml
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<!--Bombardier C-series-->
<!--CS300-->
<!--Data, source: https://en.wikipedia.org/wiki/Bombardier_CSeries#Specifications
http://commercialaircraft.bombardier.com/content/dam/Websites/bca/literature/cseries/Bombardier-Commercial-Aircraft-CSeries-Brochure-en.pdf.pdf
Dimensions: length: 35 m heigth: 11.5 wingspan:35.1m Fuselage diameter: 3.7m
mass: empty: 131000lbs?; MTOW: 134000lbs max payload= 33 350lbs
ceiling: 41000ft
range: 5741km
engine:
type=Pratt&Whitney PW1500G
diameter=1.85m
thrust= 18900lbs/84.1kN
flat rating
ISA+15°C
speed:
stall:
cruise:447kts
max cruise:470kts
-->
<!--THE COORDINATES NEED TO BE ADJUSTED!!-->
<airplane mass="141000">
<!-- Approach configuration -->
<approach speed="110" aoa="4.0" fuel="0.6"> <!--no data avail?-->
<control-setting axis="/controls/engines/engine[0]/throttle" value="0.7" />
<control-setting axis="/controls/engines/engine[1]/throttle" value="0.7" />
<control-setting axis="/controls/flight/flaps" value="1.0"/>
<control-setting axis="/controls/gear/gear-down" value="1"/>
<solve-weight idx="0" weight="360"/>
<solve-weight idx="1" weight="7000"/>
<solve-weight idx="2" weight="2500"/>
</approach>
<!-- Cruise configuration-->
<cruise speed="447" alt="35000" fuel=".78">
<control-setting axis="/controls/engines/engine[0]/throttle" value="0.8"/>
<control-setting axis="/controls/engines/engine[1]/throttle" value="0.8"/>
<control-setting axis="/controls/flight/flaps" value="0.0"/>
<control-setting axis="/controls/gear/gear-down" value="0"/>
</cruise>
<cockpit x="16.51701" y="0.5" z="-1.55091"/>
<!--The fuselage pieces. A front cone, a main fuselage piece, and then a
rear cone. Plus some pieces to make up the engine nacelles.-->
<!--Fuselage diameter: 3.7m-->
<!--front cone-->
<fuselage ax="19" ay="0" az="-2.9434" bx="13.7" by="0.00" bz="-2.1126" width="3.7" taper="0.0" midpoint="1.0"/>
<!--main fuselage-->
<fuselage ax="13.7" ay="0" az="-2.1126" bx="-7.11" by="0.00" bz="-2.3568" width="3.7" taper=".95" midpoint="1"/>
<!--rear cone-->
<fuselage ax="-7.11" ay="0" az="-2.3568" bx="-19" by="0.00" bz="-1.0617" width="3.7" taper="0.15" midpoint="0"/>
<!--left engine-->
<fuselage ax="7.17578" ay="5.42259" az="-4.01043" bx="3.65778" by="5.42259" bz="-4.01043" width="2.5" taper=".95" midpoint=".5"/>
<!--right engine-->
<fuselage ax="7.17578" ay="-5.42259" az="-4.01043" bx="3.65778" by="-5.42259" bz="-4.01043" width="2.5" taper=".95" midpoint=".5"/>
<!--The wing has two parts-->
<!-- Inner segment -->
<mstab x="2.7662" y="1.5" z="-3.2325" length="5" chord="5.4" sweep="14" taper=".615" dihedral="9" camber=".1" incidence="3" twist="-2.0" idrag="1.0">
<stall aoa="10.0" width="7" peak="1.5" />
<flap0 start="0.05" end="0.99" lift="1.4" drag="2.0" />
<spoiler start="0.18" end="0.94" lift="0.0" drag="2.0" />
<control-input axis="/controls/flight/flaps" control="FLAP0" />
<control-input axis="/surface-positions/spoiler-ground-pos-norm" control="SPOILER" />
<control-output control="FLAP0" prop="/surface-positions/flap-pos-norm" />
<control-output control="SLAT" prop="/surface-positions/slat-pos-norm" />
<control-output control="SPOILER" side="left" prop="/surface-positions/fdm-spoiler-inner-pos-norm" />
<control-speed control="FLAP0" transition-time="40.0" />
<control-speed control="SPOILER" transition-time="0.7" />
</mstab>
<!-- Outer segment -->
<wing x="1.51605" y="6.28899" z="-2.5" length="11.5" chord="3.321" sweep="25" taper=".50" dihedral="11" camber=".1" incidence="3" twist="-2.0" idrag="1.0">
<stall aoa="8.0" width="5" peak="0.8" />
<flap0 start="0.0" end="0.51" lift="1.4" drag="2.0" />
<flap1 start="0.51" end="0.8" lift="1.35" drag="1.3" />
<spoiler start="0.06" end="0.31" lift="0.0" drag="2.0" />
<control-input axis="/controls/flight/flaps" control="FLAP0" />
<control-input axis="/controls/flight/aileron" control="FLAP1" split="true" />
<control-input axis="/controls/flight/aileron-trim" control="FLAP1" split="true" />
<control-input axis="/controls/flight/flaps" control="SLAT" />
<control-input axis="/controls/flight/speedbrake" control="SPOILER" />
<control-output control="FLAP0" prop="/surface-positions/flap-pos-norm" />
<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" />
<control-output control="SPOILER" side="left" prop="/surface-positions/fdm-spoiler-outer-pos-norm" />
<control-speed control="FLAP0" transition-time="40.0" />
<control-speed control="FLAP1" transition-time="2.0" />
<control-speed control="SPOILER" transition-time="0.7" />
</wing>
<!--Winglets-->
<mstab x="-3.44543" y="16.51502" z="-0.77451" chord="1.85" length="3.2" taper=".35" sweep="39" dihedral="55" idrag="-.5"/>
<hstab x="-14.5" y="0.90079" z="-1.5419" chord="2.7" length="5.9" taper=".44" sweep="27" dihedral="10">
<stall aoa="16" width="10" peak="1.5"/>
<flap0 start="0" end=".93" lift="1.7" drag="1.55"/>
<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"/>
<control-speed control="FLAP0" transition-time="0.3"/>
</hstab>
<vstab x="-13.6926" y="0.00" z="-0.7834" chord="5" length="7.9" taper="0.4" sweep="35" effectiveness="1.5">
<stall aoa="15" width="2" peak="1.5"/>
<flap0 start="0" end="1" 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" min="1" max="-1"/>
<control-speed control="FLAP0" transition-time="0.3"/>
</vstab>
<!--2 PW1500G
Source: https://en.wikipedia.org/wiki/Pratt_%26_Whitney_PW1000G#Specifications
Dry weight: 6300 lb
Thrust: 23300lbf-->
<jet x="4.5" y="-5.5324" z="-4.1365" mass="6300" thrust="18900.0" afterburner="0" rotate="-2.5" n1-idle="21.0" n1-max="99.5" n2-idle="66.0" n2-max="102.4" tsfc="0.394" egt="750.0" epr="2.0" exhaust-speed="1555.0" spool-time="3.0">
<control-input axis="/controls/engines/engine[0]/throttle" control="THROTTLE" />
<control-input axis="/controls/engines/engine[0]/reverser" control="REVERSE_THRUST" />
<control-output control="REVERSE_THRUST" prop="/engines/engine[0]/reverser-pos-norm" />
<control-speed control="REVERSE_THRUST" transition-time="1.0" />
<actionpt x="6" y="5.5324" z="-4.1365"/>
</jet>
<jet x="4.5" y="-5.5324" z="-4.1365" mass="6300" thrust="18900.0" afterburner="0" rotate="-2.5" n1-idle="21.0" n1-max="99.5" n2-idle="66.0" n2-max="102.4" tsfc="0.394" egt="750.0" epr="2.0" exhaust-speed="1555.0" spool-time="3.0">
<control-input axis="/controls/engines/engine[1]/throttle" control="THROTTLE" />
<control-input axis="/controls/engines/engine[1]/reverser" control="REVERSE_THRUST" />
<control-output control="REVERSE_THRUST" prop="/engines/engine[0]/reverser-pos-norm" />
<control-speed control="REVERSE_THRUST" transition-time="1.0" />
<actionpt x="6" y="-5.5324" z="-4.1365"/>
</jet>
<!--user controlled pushback-->
<thruster x="10.1" y="0.00" z="-1.75" vx="1" vy="0" vz="0" thrust="1500">
<control-input axis="/sim/model/pushback/target-speed-fps" control="THROTTLE" src0="-1" src1="1" dst0="-1" dst1="1"/>
</thruster>
<gear x="15.74587" y="0.00" z="-5.59563" compression="0.15" spring="0.2" damp="2">
<control-input axis="/controls/flight/rudder" control="STEER" square="true"/>
<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"/>
<control-output control="STEER" prop="gear/gear[0]/steering-norm"/>
</gear>
<gear x="0.56" y="2.3337" z="-5.7541" spring=".3" compression="0.3" >
<control-input axis="/controls/gear/brake-left" control="BRAKE"/>
<control-input axis="/controls/gear/brake-parking" control="BRAKE"/>
<control-input axis="/controls/gear/autobrake" 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="0.56" y="-2.3337" z="-5.7541" spring=".3" compression="0.3" >
<control-input axis="/controls/gear/brake-right" control="BRAKE"/>
<control-input axis="/controls/gear/brake-parking" control="BRAKE"/>
<control-input axis="/controls/gear/autobrake" 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>
<!--Engines--><!--CAUSING SEVERE BANKING ON TAKEOFF-->
<!--<gear x="5.51453" y="5.86412" z="-5.24404" skid="true" >
</gear>
<gear x="5.51453" y="-5.86412" z="-5.24404" skid="true" >
</gear>-->
<!--No tank data available-->
<tank x="2.5" y="3" z="-3.1259" jet="true" capacity="5000"/>
<tank x="2.5" y="-3" z="-3.1259" jet="true" capacity="5000"/>
<tank x="2.7" y="0" z="-0.5" jet="true" capacity="4305"/>
<weight x="16.51701" y="0.0" z="-1.55091" mass-prop="/sim/weight[0]/weight-lb"/><!--Crew mass-->
<weight x="5.3" y="0" z="-1.5" mass-prop="/sim/weight[1]/weight-lb"/><!--Passengers front mass-->
<weight x="-5.3" y="0" z="-1.5" mass-prop="/sim/weight[2]/weight-lb"/><!--Passengers rear mass-->
<weight x="9.97759" y="0" z="-3.05628" mass-prop="/sim/weight[3]/weight-lb"/><!--Cargo mass front-->
<weight x="-4.68367" y="0" z="-3.05628" mass-prop="/sim/weight[3]/weight-lb"/><!--Cargo mass rear-->
<ballast x="16" y="0.0" z="-2" mass="36500"/>
<!--ballast x="-10" y="0" z="0" mass="-3500"/-->
</airplane>