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CRJ1000.xml
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<?xml version="1.0" encoding="UTF-8" ?>
<!--
Bombardier CRJ1000 YASim FDM
By Ryan Miller
Specifications can be viewed on Boeing's website:
http://www.crj.bombardier.com/CRJ/en/specifications.jsp?langId=en&crjId=900
More can be found on Wikipedia:
http://en.wikipedia.org/wiki/Bombardier_CRJ700_series#Specifications
<weight n="1">
<name>PAX</name>
<max-lb>18600</max-lb>
</weight>
<weight n="2">
<name>Main Cargo</name>
<max-lb>5030</max-lb>
</weight>
<weight n="3">
<name>Aft Cargo</name>
<max-lb>2150</max-lb>
</weight>
-->
<airplane mass="51100" mlw-lbs="81500" mtow-lbs="90000" cg-min="0.11" cg-max="0.32" version="2018.1">
<!-- Approach speed is 125-140 knots http://forums.jetcareers.com/airline-pilots/57253-crj-900-v-speeds.html#post758173 -->
<approach speed="125" aoa="2.0" fuel="0.2">
<control-setting axis="/controls/engines/engine[0]/throttle-lever" value="0.6" />
<control-setting axis="/controls/engines/engine[1]/throttle-lever" value="0.6" />
<control-setting axis="/controls/flight/flaps-cmd" value="1.0" />
<control-setting axis="/controls/flight/slats-cmd" value="1.0" />
<control-setting axis="/fcs/gear-down" value="1.0" />
<solve-weight idx="0" weight="400.0" />
<solve-weight idx="1" weight="5050.0" />
<solve-weight idx="2" weight="550.0" />
<solve-weight idx="3" weight="630.0" />
</approach>
<cruise speed="560" alt="40000" fuel="0.8">
<control-setting axis="/controls/engines/engine[0]/throttle-lever" value="0.95" />
<control-setting axis="/controls/engines/engine[1]/throttle-lever" value="0.95" />
<control-setting axis="/controls/flight/flaps-cmd" value="0.0" />
<control-setting axis="/controls/flight/slats-cmd" value="0.0" />
<control-setting axis="/fcs/gear-down" value="0.0" />
<solve-weight idx="0" weight="400.0" />
<solve-weight idx="1" weight="18000.0" />
<solve-weight idx="2" weight="5000.0" />
<solve-weight idx="3" weight="2100.0" />
</cruise>
<cockpit x="16.395" y="0.528" z="-0.468" />
<!-- Fuselage -->
<fuselage ax="15.472" ay="0.0" az="-1.043" bx="-8.3" by="0.0" bz="-1.043" width="2.78" taper="1.0" midpoint="1.0" />
<fuselage ax="19.543" ay="0.0" az="-1.733" bx="15.472" by="0.0" bz="-1.043" width="2.78" taper="0.1" midpoint="1.0" />
<fuselage ax="-8.3" ay="0.0" az="-1.043" bx="-16.976" by="0.0" bz="-0.696" width="2.78" taper="0.22" midpoint="0.0" />
<!-- Wings -->
<!-- Inner segment -->
<wing x="-0.07" y="1.226" z="-2.034" length="3.7" chord="5.085" sweep="17.5" taper="0.63"
dihedral="1.5" incidence="5.0" twist="-2.0"
camber="0.05"
flow="TRANSONIC">
<stall aoa="10.0" width="5" peak="1.5" />
<flap0 start="0.0" end="1.0" lift="1.39" drag="1.99" />
<slat start="0.22" end="1.0" aoa="3.0" drag="1.1" />
<spoiler start="0.18" end="1.0" lift="0.6" drag="2.5" />
<control-input axis="/controls/flight/flaps-cmd" control="FLAP0" />
<control-input axis="/controls/flight/slats-cmd" control="SLAT" />
<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="16.72" />
<control-speed control="SLAT" transition-time="8.9" />
<control-speed control="SPOILER" transition-time="0.7" />
</wing>
<!-- Outer segment -->
<wing append="1" length="8.3" sweep="24.0" taper="0.4" dihedral="3.0" twist="-2.9"
camber="0.01"
flow="TRANSONIC">
<stall aoa="7.0" width="5" peak="1.2" />
<flap0 start="0.0" end="0.51" lift="1.39" drag="1.99" />
<flap1 start="0.51" end="0.8" lift="1.3" drag="1.25" />
<slat start="0.0" end="1.0" aoa="3.0" drag="1.1" />
<spoiler start="0.0" end="0.31" lift="0.6" drag="2.5" />
<control-input axis="/controls/flight/flaps-cmd" control="FLAP0" />
<control-input axis="/fcs/aileron-hydraulic-cmd-norm" control="FLAP1" split="true" />
<control-input axis="/controls/flight/aileron-trim" control="FLAP1" split="true" />
<control-input axis="/controls/flight/slats-cmd" control="SLAT" />
<control-input axis="/surface-positions/left-ob-mfs-pos-norm" src0="0" src1="1" dst0="0" dst1="0.25" side="left" control="SPOILER" />
<control-input axis="/surface-positions/left-ib-mfs-pos-norm" src0="0" src1="1" dst0="0" dst1="0.25" side="left" control="SPOILER" />
<control-input axis="/surface-positions/right-ob-mfs-pos-norm" src0="0" src1="1" dst0="0" dst1="0.25" side="right" control="SPOILER" />
<control-input axis="/surface-positions/right-ib-mfs-pos-norm" src0="0" src1="1" dst0="0" dst1="0.25" side="right" 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" min="-1.0" max="1.0" />
<control-output control="FLAP1" side="right" prop="/surface-positions/right-aileron-pos-norm" min="-1.0" max="1.0" />
<control-output control="SLAT" prop="/surface-positions/slat-pos-norm" />
<control-output control="SPOILER" side="left" prop="/surface-positions/fdm-spoiler-outer-pos-norm" />
<control-speed control="FLAP0" transition-time="16.72" />
<control-speed control="FLAP1" transition-time="2.0" />
<control-speed control="SLAT" transition-time="8.9" />
<control-speed control="SPOILER" transition-time="0.7" />
</wing>
<!-- Horizontal stabilizers -->
<hstab x="-16.97" y="0.149" z="2.851" length="4.6" chord="2.574" sweep="26.0" taper="0.4" dihedral="-5.2"
camber="0"
twist="-1.0"
incidence-min-deg="-13"
incidence-max-deg="2"
incidence="5.0">
<stall aoa="15.0" width="7" peak="1.5" />
<flap0 start="0.0" end="0.82" lift="1.5" drag="1.4" />
<control-input axis="/fcs/elevator-cmd-norm" 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="1.5" />
<control-input axis="/controls/flight/hstab-trim" control="INCIDENCE" />
<control-speed control="INCIDENCE" transition-time="20" />
<control-output control="INCIDENCE" prop="/surface-positions/hstab-yasim-rad" />
</hstab>
<!-- Vertical stabilizers -->
<vstab x="-14.655" y="0.0" z="-0.158" length="4.2" chord="3.498" taper="0.7" sweep="36.0" idrag="1.0">
<stall aoa="15" width="2" peak="1.5" />
<flap0 start="0.0" end="0.72" lift="1.5" drag="1.4" />
<control-input axis="/fcs/rudder-cmd-norm" 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="1.5" />
</vstab>
<!-- Engines -->
<!-- Fuselage objects for nacelles -->
<fuselage ax="-9.017" ay="2.27" az="-0.264" bx="-11.166" by="2.27" bz="-0.358" width="1.53" taper="0.9" midpoint="0.5" />
<fuselage ax="-9.017" ay="-2.27" az="-0.264" bx="-11.166" by="-2.27" bz="-0.358" width="1.53" taper="0.9" midpoint="0.5" />
<!-- Actual engines -->
<!-- GE CF34-8C5 -->
<jet x="-9.075" y="2.27" z="-0.319" mass="2450.0" afterburner="0" rotate="-2.5"
thrust="14510.0"
n1-idle="21.0" n1-max="99.5" n2-idle="59.0" n2-max="99.4"
tsfc="0.68" egt="1000.0" epr="28.0" exhaust-speed="1555.0" spool-time="3.0">
<control-input axis="/controls/engines/engine[0]/throttle-lever" control="THROTTLE" src0="0" src1="1" dst0="0.0391" dst1="1" />
<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="-12.333" y="2.27" z="-0.409" />
</jet>
<jet x="-9.075" y="-2.27" z="-0.319" mass="2450.0" afterburner="0" rotate="-2.5"
thrust="14510.0"
n1-idle="21.0" n1-max="99.5" n2-idle="59.0" n2-max="99.4"
tsfc="0.68" egt="1000.0" epr="28.0" exhaust-speed="1555.0" spool-time="3.0">
<control-input axis="/controls/engines/engine[1]/throttle-lever" control="THROTTLE" src0="0" src1="1" dst0="0.0391" dst1="1" />
<control-input axis="/controls/engines/engine[1]/reverser" control="REVERSE_THRUST" />
<control-output control="REVERSE_THRUST" prop="/engines/engine[1]/reverser-pos-norm" />
<control-speed control="REVERSE_THRUST" transition-time="1.0" />
<actionpt x="-12.333" y="-2.27" z="-0.409" />
</jet>
<!-- Landing gear -->
<!-- Pushback -->
<thruster x="17.522" y="0.0" z="-3.459" vx="1" vy="0" vz="0" thrust="10000">
<control-input axis="/sim/model/pushback/force" control="THROTTLE" src0="-1" dst0="-1" src1="1" dst1="1" />
</thruster>
<!-- Nosegear -->
<gear x="17.522" y="0.0" z="-3.459" compression="0.4" spring="0.7" damp="4.0">
<control-input axis="/fcs/nose-gear-steer-deg" control="STEER" src0="-80" dst0="-1" src1="80" dst1="1" />
<control-input axis="/fcs/gear-down" control="EXTEND" />
<control-output control="EXTEND" prop="/gear/gear[0]/position-norm" />
<control-output control="STEER" prop="/gear/gear[0]/steering-norm" />
<control-speed control="EXTEND" transition-time="9.2" />
</gear>
<!-- Left main gear -->
<gear x="-1.506" y="2.054" z="-3.81" compression="0.35" spring="0.6" damp="1.0">
<control-input axis="/fcs/brake-left-cmd-norm" control="BRAKE" />
<control-input axis="/controls/gear/brake-parking" control="BRAKE" />
<control-input axis="/fcs/gear-down" control="EXTEND" />
<control-output control="EXTEND" prop="/gear/gear[1]/position-norm" />
<control-speed control="EXTEND" transition-time="9.2" />
</gear>
<!-- Right main gear -->
<gear x="-1.506" y="-2.054" z="-3.81" compression="0.35" spring="0.6" damp="1.0">
<control-input axis="/fcs/brake-right-cmd-norm" control="BRAKE" />
<control-input axis="/controls/gear/brake-parking" control="BRAKE" />
<control-input axis="/fcs/gear-down" control="EXTEND" />
<control-output control="EXTEND" prop="/gear/gear[2]/position-norm" />
<control-speed control="EXTEND" transition-time="9.2" />
</gear>
<!-- Fuel and payload -->
<!-- Left wing tank -->
<tank x="-1.69" y="5.62" z="-1.99" jet="true" capacity="7554" />
<!-- Right wing tank -->
<tank x="-1.69" y="-5.62" z="-1.99" jet="true" capacity="7554" />
<!-- Center tank -->
<tank x="0.0" y="0.0" z="-2.2" jet="true" capacity="4642" />
<!-- Ballast to adjust center of gravity -->
<!-- Redistribute the mass toward the nose -->
<ballast x="17.26" y="0.0" z="-1.9" mass="2100.0" />
<!-- Weight of the main landing gear assemblies (approx.) -->
<ballast x="-1.0" y="0.0" z="-2.6" mass="5000.0" />
<!-- Crew -->
<weight x="16.5" y="0.0" z="-1.0" mass-prop="/sim/weight[0]/weight-lb" solve-weight="1" idx="0" />
<!-- PAX -->
<weight x="0.0" y="0.0" z="-1.0" mass-prop="/sim/weight[1]/weight-lb" solve-weight="1" idx="1" />
<!-- Main Cargo -->
<weight x="6.3" y="0.0" z="-2.1" mass-prop="/sim/weight[2]/weight-lb" solve-weight="1" idx="2" />
<!-- Aft Cargo -->
<weight x="-10.0" y="0.0" z="-1.5" mass-prop="/sim/weight[3]/weight-lb" solve-weight="1" idx="3" />
</airplane>