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CRJ900ER.xml
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CRJ900ER.xml
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<?xml version="1.0" encoding="UTF-8" ?>
<!--
Bombardier CRJ900ER 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
-->
<airplane mass="47250">
<!-- Approach speed is 125-140 knots http://forums.jetcareers.com/airline-pilots/57253-crj-900-v-speeds.html#post758173 -->
<approach speed="115" aoa="4.0" fuel="0.6">
<control-setting axis="/controls/engines/engine[0]/throttle-lever" value="0.7" />
<control-setting axis="/controls/engines/engine[1]/throttle-lever" value="0.7" />
<control-setting axis="/controls/flight/flaps" value="1.0" />
<control-setting axis="/fcs/gear-down" value="1.0" />
<solve-weight idx="0" weight="600.0" />
<solve-weight idx="1" weight="10.0" />
</approach>
<cruise speed="560" alt="35000" 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" value="0.0" />
<control-setting axis="/fcs/gear-down" value="0.0" />
<solve-weight idx="0" weight="600.0" />
<solve-weight idx="1" weight="22150.0" />
</cruise>
<cockpit x="15.045" y="0.528" z="-0.468" />
<!-- Fuselage -->
<fuselage ax="14.122" ay="0.0" az="-1.043" bx="-7.01" by="0.0" bz="-1.043" width="2.78" taper="1.0" midpoint="1.0" />
<fuselage ax="18.193" ay="0.0" az="-1.733" bx="14.122" by="0.0" bz="-1.043" width="2.78" taper="0.1" midpoint="1.0" />
<fuselage ax="-7.01" ay="0.0" az="-1.043" bx="-15.608" by="0.0" bz="-0.696" width="2.78" taper="0.22" midpoint="0.0" />
<!-- Wings -->
<!-- Inner segment -->
<mstab x="0.08" y="1.226" z="-2.034" length="3.7" chord="5.085" sweep="17.5" taper="0.63" camber="-0.1" dihedral="1.5" incidence="5.0" 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" />
<slat start="0.22" end="1.0" aoa="3.0" drag="1.1" />
<spoiler start="0.18" end="0.94" lift="0.0" drag="6.123" />
<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" />
</mstab>
<!-- Outer segment -->
<wing x="-1.036" y="4.754" z="-2.039" length="7.2" chord="3.204" sweep="24.0" taper="0.4" camber="0.01" dihedral="3.0" incidence="3.0" twist="-2.9" 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" />
<slat start="0.0" end="0.94" aoa="3.0" drag="1.1" />
<spoiler start="0.06" end="0.31" lift="0.0" drag="10.0" />
<control-input axis="/controls/flight/flaps-cmd" control="FLAP0" />
<control-input axis="/fcs/aileron-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="/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="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>
<!-- Winglets -->
<vstab x="-4.012" y="11.332" z="-1.844" length="1.49" chord="1.12" taper="0.25" dihedral="75.6" sweep="34.9" idrag="-0.5" />
<vstab x="-4.012" y="-11.332" z="-1.844" length="1.49" chord="1.12" taper="0.25" dihedral="104.4" sweep="34.9" idrag="-0.5" />
<!-- Horizontal stabilizers -->
<hstab x="-15.62" y="0.149" z="2.851" length="4.6" chord="2.574" sweep="26.0" taper="0.4" dihedral="-5.2" camber="-0.12" twist="-1.0" idrag="1.0">
<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" />
</hstab>
<!-- Vertical stabilizers -->
<vstab x="-13.305" 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="-7.667" ay="2.27" az="-0.264" bx="-9.816" by="2.27" bz="-0.358" width="1.53" taper="0.9" midpoint="0.5" />
<fuselage ax="-7.667" ay="-2.27" az="-0.264" bx="-9.816" by="-2.27" bz="-0.358" width="1.53" taper="0.9" midpoint="0.5" />
<!-- Actual engines -->
<jet x="-8.925" y="2.27" z="-0.319" mass="9047.0" thrust="13360.0" afterburner="0" rotate="-2.5" n1-idle="21.0" n1-max="99.5" n2-idle="60.0" n2-max="99.4" tsfc="0.39" egt="1050.0" epr="3.0" exhaust-speed="1555.0" spool-time="3.0">
<control-input axis="/controls/engines/engine[0]/throttle-lever" 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="-10.983" y="2.27" z="-0.409" />
</jet>
<jet x="-8.925" y="-2.27" z="-0.319" mass="9047.0" thrust="13360.0" afterburner="0" rotate="-2.5" n1-idle="21.0" n1-max="99.5" n2-idle="60.0" n2-max="99.4" tsfc="0.39" egt="1050.0" epr="3.0" exhaust-speed="1555.0" spool-time="3.0">
<control-input axis="/controls/engines/engine[1]/throttle-lever" control="THROTTLE" />
<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="-10.983" y="-2.27" z="-0.409" />
</jet>
<!-- Landing gear -->
<!-- Pushback -->
<thruster x="16.172" 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="16.172" 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="-1.356" 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="-1.356" 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="-0.8" y="4.8" z="-1.9" jet="true" capacity="8914" />
<!-- Right wing tank -->
<tank x="-0.8" y="-4.8" z="-1.9" jet="true" capacity="8914" />
<!-- Center tank -->
<tank x="1.5" y="0.0" z="-2.2" jet="true" capacity="5478" />
<!-- Ballast to adjust center of gravity -->
<!-- Redistribute the mass toward the nose -->
<ballast x="15.3" y="0.0" z="-1.9" mass="10000.0" />
<!-- Weight of the main landing gear assemblies (approx.) -->
<ballast x="-1.0" y="0.0" z="-2.6" mass="5000.0" />
<!-- Crew -->
<weight x="14.94" y="0.0" z="-1.0" mass-prop="/sim/weight[0]/weight-lb" solve-weight="1" idx="0" />
<!-- PAX/Cargo -->
<weight x="3.5" y="0.0" z="-1.0" mass-prop="/sim/weight[1]/weight-lb" solve-weight="1" idx="1" />
</airplane>