124 lines
5.8 KiB
XML
124 lines
5.8 KiB
XML
<airplane mass="16865">
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<approach speed="58" aoa="13">
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<control-setting axis="/controls/throttle[0]" value="0.4"/>
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<control-setting axis="/controls/throttle[1]" value="0.4"/>
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<control-setting axis="/controls/mixture[0]" value="1.0"/>
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<control-setting axis="/controls/mixture[1]" value="1.0"/>
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<control-setting axis="/controls/propeller-pitch[0]" value="0.5"/>
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<control-setting axis="/controls/propeller-pitch[1]" value="0.5"/>
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<control-setting axis="/controls/flaps" value="1.0"/>
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<control-setting axis="/controls/gear-down" value="1"/>
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</approach>
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<cruise speed="180" alt="23200">
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<control-setting axis="/controls/throttle[0]" value="1.0"/>
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<control-setting axis="/controls/throttle[1]" value="1.0"/>
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<control-setting axis="/controls/mixture[0]" value="1.0"/>
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<control-setting axis="/controls/mixture[1]" value="1.0"/>
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<control-setting axis="/controls/propeller-pitch[0]" value="1.0"/>
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<control-setting axis="/controls/propeller-pitch[1]" value="1.0"/>
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<control-setting axis="/controls/boost[0]" value="1.0"/>
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<control-setting axis="/controls/boost[1]" value="1.0"/>
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<control-setting axis="/controls/flaps" value="0.0"/>
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<control-setting axis="/controls/gear-down" value="0"/>
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</cruise>
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<cockpit x="-1.63" y="0.41" z="0.76"/>
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<fuselage ax="0" ay="0" az="0" bx="-19.75" by="0" bz="0"
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width="2" taper="0.5" midpoint="0.25"/>
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<wing x="-7.02" y="1.09" z="-0.95" length="11.58" camber="0.1"
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chord="4.77" taper=".286" sweep="19" dihedral="4">
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<stall aoa="14" width="6" peak="1.5"/>
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<flap0 start="0.04" end="0.38" lift="1.5" drag="1.2"/>
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<flap1 start="0.38" end="0.97" lift="1.2" drag="1.2"/>
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<control-input axis="/controls/flaps" control="FLAP0"/>
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<control-input axis="/controls/aileron" control="FLAP1" split="true"/>
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<control-input axis="/controls/aileron-trim" control="FLAP1" split="true"/>
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<control-output control="FLAP0" prop="/surface-positions/flap-pos-norm"/>
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<control-output control="FLAP1" side="left"
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prop="/surface-positions/left-aileron-pos-norm"/>
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<control-output control="FLAP1" side="right"
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prop="/surface-positions/right-aileron-pos-norm"/>
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<control-speed control="FLAP0" transition-time="5"/>
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</wing>
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<hstab x="-18.12" y="0.41" z="0.27" length="3.5" effectiveness="2.4"
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chord="3" taper=".545" sweep="15">
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<stall aoa="18" width="3" peak="1.5"/>
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<flap0 start="0" end="1" lift="1.5" drag="1.2"/>
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<control-input axis="/controls/elevator" control="FLAP0" effectiveness="1.25"/>
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<control-input axis="/controls/elevator-trim" control="FLAP0"/>
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<control-output control="FLAP0" prop="/surface-positions/elevator-pos-norm"/>
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</hstab>
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<vstab x="-18.12" y="0" z="0.95" length="2.72" effectiveness="1.25"
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chord="3.95" taper=".462" sweep="2">
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<stall aoa="14" width="3" peak="1.5"/>
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<flap0 start="0" end="1" lift="1.5" drag="1.2"/>
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<control-input axis="/controls/rudder" control="FLAP0" effectiveness="1.25" invert="true"/>
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<control-input axis="/controls/rudder-trim" control="FLAP0" invert="true"/>
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<control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm"/>
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</vstab>
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<propeller x="-4.09" y="2.52" z="-0.95"
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mass="2000" moment="35" radius="1.4"
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eng-power="1200" eng-rpm="2700"
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turbo-mul="1.5"
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cruise-power="660" cruise-speed="195"
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cruise-rpm="2100" cruise-alt="20000"
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min-rpm="1600" max-rpm="2700">
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<actionpt x="-2.45" y="2.52" z="-0.95"/>
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<control-input axis="/controls/throttle[0]" control="THROTTLE"/>
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<control-input axis="/controls/starter[0]" control="STARTER"/>
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<control-input axis="/controls/magnetos[0]" control="MAGNETOS"/>
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<control-input axis="/controls/mixture[0]" control="MIXTURE"/>
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<control-input axis="/controls/propeller-pitch[0]" control="ADVANCE"/>
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<control-input axis="/controls/boost[0]" control="BOOST"/>
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</propeller>
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<propeller x="-4.09" y="-2.52" z="-0.95"
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mass="2000" moment="-35" radius="1.4"
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eng-power="1200" eng-rpm="2700"
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turbo-mul="1.5"
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cruise-power="660" cruise-speed="195"
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cruise-rpm="2100" cruise-alt="20000"
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min-rpm="1600" max-rpm="2700">
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<actionpt x="-2.45" y="-2.52" z="-0.95"/>
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<control-input axis="/controls/throttle[1]" control="THROTTLE"/>
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<control-input axis="/controls/starter[1]" control="STARTER"/>
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<control-input axis="/controls/magnetos[1]" control="MAGNETOS"/>
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<control-input axis="/controls/mixture[1]" control="MIXTURE"/>
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<control-input axis="/controls/propeller-pitch[1]" control="ADVANCE"/>
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<control-input axis="/controls/boost[1]" control="BOOST"/>
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</propeller>
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<!-- Tail wheel; has castering selectable by a wheel lock -->
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<gear x="-17.3" y="0" z="-1.5" compression="0.2">
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<control-input axis="/controls/tailwheel-castering" control="CASTERING"/>
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</gear>
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<gear x="-6.08" y="2.52" z="-3.49" compression="1" retract-time="7">
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<control-input axis="/controls/parking-brake" control="BRAKE"/>
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<control-input axis="/controls/brakes[0]" control="BRAKE"/>
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<control-input axis="/controls/gear-down" control="EXTEND"/>
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<control-speed control="EXTEND" transition-time="7"/>
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<control-output control="EXTEND" prop="/gear/gear[0]/position-norm"/>
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</gear>
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<gear x="-6.08" y="-2.52" z="-3.49" compression="1" retract-time="7">
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<control-input axis="/controls/parking-brake" control="BRAKE"/>
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<control-input axis="/controls/brakes[1]" control="BRAKE"/>
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<control-input axis="/controls/gear-down" control="EXTEND"/>
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<control-speed control="EXTEND" transition-time="7"/>
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<control-output control="EXTEND" prop="/gear/gear[1]/position-norm"/>
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</gear>
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<!-- From the type certificate: "Fuel capacity: 822 gals. (4 tanks in
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center section wing: 2 main including fuel system 210 gals. each
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(+48) and 2 aux. 201 gals. each (+83.5)" -->
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<tank x="-7.02" y="0" z="0.95" capacity="4932"/>
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<ballast x="-18.0" y="0.0" z="0.6" mass="-2000"/> <!-- move CG forward -->
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</airplane>
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