f69f6321fa
I just checked in YASim changes that allow for more cleaner export of control output to the property tree (and flaps now extend slowly now, to boot). But this breaks the XML syntax in an incompatible way, so you'll need to update your planes in order to run the code in CVS.
121 lines
No EOL
5.5 KiB
XML
121 lines
No EOL
5.5 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="3" peak="1.5"/>
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<flap0 start="0.04" end="0.38" lift="1.5" drag="2.0"/>
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<flap1 start="0.38" end="0.97" lift="1.2" drag="1.5"/>
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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"
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chord="3" taper=".545" sweep="15">
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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="2.0"/>
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<control-input axis="/controls/elevator" control="FLAP0"/>
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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"
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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="2.0"/>
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<control-input axis="/controls/rudder" control="FLAP0" 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; freely castering and uncontrollable -->
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<gear x="-17.3" y="0" z="-1.5" compression="0.2" castering="true"/>
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<!-- Main wheels; note mapping of rudder input to effect differential
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braking -->
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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/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/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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</airplane> |