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139 lines
5.0 KiB
139 lines
5.0 KiB
<?xml version="1.0" encoding="UTF-8"?>
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<!-- Resolution - blended body flying wing : 2011 Curtis L. Olson -->
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<airplane mass="12">
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<approach speed="25" aoa="7.5" fuel="0.5" >
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<control-setting axis="/controls/engines/engine[0]/throttle" value="0.0"/>
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<control-setting axis="/controls/gear/gear-down" value="1"/>
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</approach>
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<cruise speed="45" alt="1000" fuel="0.5">
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<control-setting axis="/controls/engines/engine[0]/throttle" value="0.75"/>
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<control-setting axis="/controls/gear/gear-down" value="1"/>
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</cruise>
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<cockpit x="0.0" y="0.0" z="0.0"/>
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<fuselage ax="0.0" ay="0.0" az="0.0" bx="-0.622" by="0.0" bz="0.0" width="0.26" taper="0.4" midpoint="0.415"/>
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<wing x="-0.304" y="0.0" z="0.0"
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chord="0.418"
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length="0.921"
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taper="0.614"
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sweep="17.84"
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dihedral="0.0"
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incidence="0.0"
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twist="-3.0"
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camber="0.0">
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<stall aoa="13" width="5" peak="1.5"/>
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<flap0 start="0.29" end="1.0" lift="1.15" drag="1.2"/>
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<control-input axis="/controls/flight/aileron" control="FLAP0"
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split="true"/>
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<control-input axis="/controls/flight/elevator" control="FLAP0"/>
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<control-input axis="/controls/flight/elevator-trim" control="FLAP0"/>
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<control-output control="FLAP0" side="left"
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prop="/surface-positions/left-aileron-pos-norm"/>
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<control-output control="FLAP0" side="right"
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prop="/surface-positions/right-aileron-pos-norm"/>
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</wing>
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<hstab x="-0.586" y="0.876" z="0.0"
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chord="0.257"
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length="0.307"
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taper="0.791"
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sweep="17.84"
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dihedral="0.0"
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incidence="-3.0"
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twist="-1.0"
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camber="0.0"
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effectiveness="1.0">
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<stall aoa="13" width="5" peak="1.5"/>
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<flap0 start="0.0" end="0.826" lift="1.3" drag="1.2"/>
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<control-input axis="/controls/flight/aileron" control="FLAP0"
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split="true"/>
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<control-input axis="/controls/flight/elevator" control="FLAP0"/>
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<control-input axis="/controls/flight/elevator-trim" control="FLAP0"/>
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<control-output control="FLAP0" side="left"
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prop="/surface-positions/left-aileron-pos-norm"/>
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<control-output control="FLAP0" side="right"
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prop="/surface-positions/right-aileron-pos-norm"/>
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</hstab>
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<!-- y=1.17 is at the wingtip, y=0.20 is at the wing root, x=-0.68 -->
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<vstab x="-0.68" y="0.20" z="0.0"
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chord="0.1"
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length="0.2"
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taper="0.75"
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sweep="17.84">
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<stall aoa="14" width="2" peak="1.5"/>
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<flap0 start="0.1" end="0.95" lift="1.25" drag="1.25"/>
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<control-input axis="/controls/flight/rudder" control="FLAP0"
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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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<!-- y=1.17 is at the wingtip, y=0.20 is at the wing root -->
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<vstab x="-0.68" y="-0.20" z="0.0"
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chord="0.1"
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length="0.2"
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taper="0.75"
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sweep="17.84">
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<stall aoa="14" width="2" peak="1.5"/>
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<flap0 start="0.1" end="0.95" lift="1.25" drag="1.25"/>
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<control-input axis="/controls/flight/rudder" control="FLAP0"
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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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<!-- simple thruster for testing -->
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<thruster thrust="2.5"
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x="-0.622" y="0.0" z="0.0"
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vx="1.0" vy="0.0" vz="0.0">
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<control-input axis="/controls/engines/engine[0]/throttle"
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control="THROTTLE"/>
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</thruster>
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<!-- Landing Gear -->
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<!-- front -->
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<gear x="-0.1" y="0.0" z="-0.254"
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compression="0.05">
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<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
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<control-input axis="/controls/flight/rudder" control="STEER"
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square="true"/>
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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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<!-- rear left -->
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<gear x="-0.5" y="0.2" z="-0.244"
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compression="0.1">
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<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
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<control-input axis="/controls/gear/brake-left" control="BRAKE"/>
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<control-input axis="/controls/gear/brake-parking" control="BRAKE"/>
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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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<!-- rear right -->
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<gear x="-0.5" y="-0.2" z="-0.244"
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compression="0.1">
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<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
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<control-input axis="/controls/gear/brake-right" control="BRAKE"/>
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<control-input axis="/controls/gear/brake-parking" control="BRAKE"/>
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<control-speed control="EXTEND" transition-time="7"/>
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<control-output control="EXTEND" prop="/gear/gear[2]/position-norm"/>
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</gear>
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<!-- goal: CG at -0.374 -->
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<ballast x="0.0" y="0.0" z="0.0" mass="1.6"/>
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<hitch name="winch" x="0.0" y="0" z="-0.1">
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<!-- goal is to model a 30m hi-start bungee -->
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<tow length="400" weight-per-meter="0.05" elastic-constant="10000" break-force="10000"/>
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<winch max-tow-length="400" min-tow-length="1" initial-tow-length="400" max-winch-speed="25" power="15" max-force="600" />
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<control-input axis="/controls/winch/place" control="PLACEWINCH"/>
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</hitch>
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</airplane>
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