101 lines
4 KiB
XML
101 lines
4 KiB
XML
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<airplane mass="3903">
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<approach speed="70" aoa="16">
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<control axis="/controls/throttle[0]" value="0.4"/>
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<control axis="/controls/throttle[1]" value="0.4"/>
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<control axis="/controls/mixture[0]" value="1.0"/>
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<control axis="/controls/mixture[1]" value="1.0"/>
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<control axis="/controls/propellor-pitch[0]" value="0.5"/>
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<control axis="/controls/propellor-pitch[1]" value="0.5"/>
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<control axis="/controls/flaps" value="1.0"/>
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</approach>
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<cruise speed="223" alt="20000">
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<control axis="/controls/throttle[0]" value="1.0"/>
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<control axis="/controls/throttle[1]" value="1.0"/>
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<control axis="/controls/mixture[0]" value="1.0"/>
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<control axis="/controls/mixture[1]" value="1.0"/>
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<control axis="/controls/propellor-pitch[0]" value="1.0"/>
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<control axis="/controls/propellor-pitch[1]" value="1.0"/>
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<control axis="/controls/flaps" value="0.0"/>
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</cruise>
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<cockpit x="-2.78" y="0.26" z="0.95"/>
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<fuselage ax="0.00" ay="0" az="0"
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bx="-9.50" by="0" bz="0" width="0.8"/>
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<wing x="-3.65" y="0.62" z="-0.18" length ="4.68" chord ="1.68"
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sweep="0" dihedral="5" taper="0.8" camber="0.1">
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<stall aoa="16" width="4" peak="1.5"/>
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<flap0 start="0" end=".5" lift="1.5" drag="2.0"/>
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<flap1 start=".55" end=".94" lift="1.3" drag="1.5"/>
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<control axis="/controls/flaps" output="FLAP0"/>
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<control axis="/controls/aileron" output="FLAP1" split="true"/>
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</wing>
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<hstab x="-8.33" y="0.22" z="0.07" length ="2.34" chord ="1.24"
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sweep="0" dihedral="0" taper="0.6" camber="0.1">
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<stall aoa="16" width="4" peak="1.5"/>
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<flap0 start="0" end="1" lift="1.5" drag="1.8"/>
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<control axis="/controls/elevator" output="FLAP0"/>
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<control axis="/controls/elevator-trim" output="FLAP0"/>
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</hstab>
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<vstab x="-8.26" y="0.00" z="0.26" length ="2.16" chord ="1.61"
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sweep="36" taper="0.5">
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<stall aoa="16" width="4" peak="1.5"/>
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<flap0 start="0" end="1" lift="1.3" drag="1.5"/>
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<control axis="/controls/rudder" output="FLAP0" invert="true" square="true"/>
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</vstab>
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<!-- Late model 310's had 50 gallon tip tanks, and 31.5 gallon wing
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tanks. Some also had nacelle tanks, but those aren't modeled
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here -->
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<tank x="-3.62" y="5.30" z="0.44" capacity="300"/>
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<tank x="-3.62" y="1.02" z="-0.15" capacity="189"/>
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<tank x="-3.62" y="-1.02" z="-0.15" capacity="189"/>
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<tank x="-3.62" y="-5.30" z="0.44" capacity="300"/>
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<gear x="0.00" y="0.00" z="-1.35" compression=".5" retract-time="7">
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<control axis="/controls/rudder" output="STEER"/>
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</gear>
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<gear x="-4.02" y="1.32" z="-1.35" compression=".5" retract-time="7">
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<control axis="/controls/brakes[0]" output="BRAKE"/>
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</gear>
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<gear x="-4.02" y="-1.32" z="-1.35" compression=".5" retract-time="7">
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<control axis="/controls/brakes[1]" output="BRAKE"/>
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</gear>
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<propeller x="-2.56" y="1.83" z="0.07"
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mass="800" moment="20" radius="1.0"
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eng-power="285" eng-rpm="2700"
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turbo-mul="2" wastegate-mp="40"
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cruise-power="157" 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="-1.53" y="1.83" z="0.07"/>
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<control axis="/controls/throttle[0]" output="THROTTLE"/>
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<control axis="/controls/mixture[0]" output="MIXTURE"/>
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<control axis="/controls/propellor-pitch[0]" output="ADVANCE"/>
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</propeller>
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<propeller x="-2.56" y="-1.83" z="0.07"
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mass="800" moment="20" radius="1.0"
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eng-power="285" eng-rpm="2700"
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turbo-mul="2" wastegate-mp="40"
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cruise-power="157" cruise-speed="195"
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cruise-rpm="2100" cruise-alt="10000"
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min-rpm="1600" max-rpm="2700">
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<actionpt x="-1.53" y="-1.83" z="0.07"/>
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<control axis="/controls/throttle[1]" output="THROTTLE"/>
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<control axis="/controls/mixture[1]" output="MIXTURE"/>
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<control axis="/controls/propellor-pitch[1]" output="ADVANCE"/>
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</propeller>
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<ballast x="-2.78" y="0.26" z="0.0" mass="180"/> <!-- pilot -->
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<ballast x="-8.5" y="0" z="0" mass="-150"/>
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<ballast x="-7" y="0" z="0" mass="-300"/>
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<weight x="-4.24" y="0" z="0" mass-prop="/yasim/c310/passenger-lbs"/>
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</airplane>
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