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CRJ200.xml
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CRJ200.xml
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<!--CRJ-200 LR yasim
Specs:
2 X GE CF34-3B: 19,220 lb
Range: 1,345 nm
Ceiling: 41,000 ft
Typical Cruise Speed = 0.74 Mach
Max Speed = 0.81 Mach
Length: 26.7 m
Wing span: 21.2 m
Wing Area: 48.35 m2
Height: 6.22m
Fuselage Diameter : 2.69 m
Fuel burn per hour:325 us gal
Max Fuel : 2,110 us gal
Operating empty weight: 30,900 lb
Max zero fuel weight: 44,000 lb
Max TO weight: 53,000 lb
http://www.crj.bombardier.com/CRJ/en/home_crj.jsp?langId=en&crjId=200
Mach 1 = 576.6 kt @ 35,000 ft -->
<airplane mass="30900">
<!-- Approach configuration -->
<approach speed="115" aoa="3" fuel=".2">
<control-setting axis="/controls/engines/engine[0]/throttle-lever" value="0.2"/>
<control-setting axis="/controls/engines/engine[1]/throttle-lever" value="0.2"/>
<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. The CRJ has a service ceiling of 41000 feet. Bad
things have happened when pilots try to join the "40000 club," but those
can't be modeled in FlightGear without extremely complicated scripts.-->
<cruise speed="424" alt="35000" fuel=".78">
<control-setting axis="/controls/engines/engine[0]/throttle-lever" value="0.8"/>
<control-setting axis="/controls/engines/engine[1]/throttle-lever" value="0.8"/>
<control-setting axis="/controls/flight/flaps" value="0.0"/>
<control-setting axis="/controls/gear/gear-down" value="0"/>
<solve-weight idx="0" weight="360"/>
<solve-weight idx="1" weight="7000"/>
<solve-weight idx="2" weight="250"/>
</cruise>
<cockpit x="9.4" y="0.5" z="1.4"/>
<!--The fuselage pieces. A front cone, a main fuselage piece, and then a
rear cone. Plus some pieces to make up the engine nacelles.-->
<!--front cone-->
<fuselage ax="12.4" ay="0" az="-0.1" bx="8.2" by="0.00" bz="0.65" width="3" taper="0.0" midpoint="1.0"/>
<!--main fuselage-->
<fuselage ax="8.2" ay="0" az="0.65" bx="-7.3" by="0.00" bz="0.6" width="3.1" taper=".95" midpoint="1"/>
<!--rear cone-->
<fuselage ax="-7.3" ay="0" az="0.65" bx="-14.0" by="0.00" bz="1.0" width="3.1" taper="0.15" midpoint="0"/>
<!--left engine-->
<fuselage ax="-5.7" ay="2.4" az="1.5" bx="-8.3" by="2.4" bz="1.5" width=".8" taper=".9" midpoint=".5"/>
<!--right engine-->
<fuselage ax="-5.7" ay="-2.4" az="1.5" bx="-8.3" by="-2.4" bz="1.5" width=".8" taper=".9" midpoint=".5"/>
<!--The wing. The real wing has a 2-segment geometry, this is modeled here.-->
<!--inboard segment-->
<wing x="-.75" y="1.5" z="-0.35" length="2.63" chord="4.9" sweep="20.5" taper=".615" dihedral="2.5" camber=".1" incidence="3" twist="-2.0">
<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" />
</wing>
<!--outboard segment-->
<mstab x="-1.67" y="3.96" z="-0.307" length="7.8" chord="3.05" sweep="22.2" taper=".45" dihedral="3.2" camber=".1" incidence="1" twist="-1">
<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="/fcs/aileron-cmd-norm" 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" />
</mstab>
<!--Winglets-->
<mstab x="-4.8" y="11.15" z="0" chord="1" length="1.53" taper=".45" sweep="22.5" dihedral="78" idrag="-.5"/>
<!--The CRJ has a T-tail design-->
<hstab x="-14.95" y="0.15" z="4.7" chord="2.3" length="3.5" taper=".44" sweep="20" dihedral="-1" effectiveness="1">
<stall aoa="16" width="10" peak="1.5"/>
<flap0 start="0" end=".93" lift="1.5" drag="1.2"/>
<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>
<vstab x="-12.2" y="0.00" z="1.7" chord="3.6" length="3.8" taper="0.75" 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="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" min="1" max="-1"/>
</vstab>
<!--2 GE CF34-3B1-->
<jet x="-7" y="2.4" z="1.5" mass="1670" thrust="9220" egt="810" tsfc="0.346" afterburner="0" rotate="-2.5" n1-idle="21.0" n1-max="99.5" n2-idle="60.0" n2-max="99.4" 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" y="2.4" z="1.5"/>
</jet>
<jet x="-7" y="-2.4" z="1.5" mass="1670" thrust="9220" egt="810" tsfc="0.346" afterburner="0" rotate="-2.5" n1-idle="21.0" n1-max="99.5" n2-idle="60.0" n2-max="99.4" 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" y="-2.4" z="1.5"/>
</jet>
<!--user controlled pushback-->
<thruster x="10.1" y="0.00" z="-1.75465" 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="10.09746" y="0.00" z="-1.75465" 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="-2.37" y="1.675" z="-1.87" 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="-2.37" y="-1.675" z="-1.87" 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>
<tank x="-1" y="3" z="-0.5" jet="true" capacity="4760"/>
<tank x="-1" y="-3" z="-0.5" jet="true" capacity="4760"/>
<tank x="0.0" y="0" z="-0.5" jet="true" capacity="4998"/>
<weight x="10" y="0" z="0.4" mass-prop="/sim/weight[0]/weight-lb"/>
<weight x=".331" y="0" z="0.869" mass-prop="/sim/weight[1]/weight-lb"/>
<weight x=".331" y="0" z="-0.4" mass-prop="/sim/weight[2]/weight-lb"/>
<!--weight x="-3.5" y="0" z="0.4" mass-prop="/sim/weight[3]/weight-lb"/-->
<ballast x="8.0" y="0.0" z="0" mass="5000"/>
<ballast x="-4" y="0.0" z="-0.5" mass="2000"/>
<!--ballast x="-10" y="0" z="0" mass="-3500"/-->
</airplane>