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fgdata/Aircraft-yasim/dc3.xml
aross c70491368a More updates from Dave Perry. Fix the tank location to be in the wing (this
is the same "wrong sign" issue that affected the wing location).  Adjust
the ballast accordingly.  Tune the surfaces a little bit.  Also adjust the
location of the tail wheel, presumably to get the on-ground orientation right.
2002-09-03 17:12:33 +00:00

124 lines
5.8 KiB
XML

<airplane mass="16865">
<approach speed="58" aoa="13">
<control-setting axis="/controls/throttle[0]" value="0.4"/>
<control-setting axis="/controls/throttle[1]" value="0.4"/>
<control-setting axis="/controls/mixture[0]" value="1.0"/>
<control-setting axis="/controls/mixture[1]" value="1.0"/>
<control-setting axis="/controls/propeller-pitch[0]" value="0.5"/>
<control-setting axis="/controls/propeller-pitch[1]" value="0.5"/>
<control-setting axis="/controls/flaps" value="1.0"/>
<control-setting axis="/controls/gear-down" value="1"/>
</approach>
<cruise speed="180" alt="23200">
<control-setting axis="/controls/throttle[0]" value="1.0"/>
<control-setting axis="/controls/throttle[1]" value="1.0"/>
<control-setting axis="/controls/mixture[0]" value="1.0"/>
<control-setting axis="/controls/mixture[1]" value="1.0"/>
<control-setting axis="/controls/propeller-pitch[0]" value="1.0"/>
<control-setting axis="/controls/propeller-pitch[1]" value="1.0"/>
<control-setting axis="/controls/boost[0]" value="1.0"/>
<control-setting axis="/controls/boost[1]" value="1.0"/>
<control-setting axis="/controls/flaps" value="0.0"/>
<control-setting axis="/controls/gear-down" value="0"/>
</cruise>
<cockpit x="-1.63" y="0.41" z="0.76"/>
<fuselage ax="0" ay="0" az="0" bx="-19.75" by="0" bz="0"
width="2" taper="0.5" midpoint="0.25"/>
<wing x="-7.02" y="1.09" z="-0.95" length="11.58" camber="0.1"
chord="4.77" taper=".286" sweep="19" dihedral="4">
<stall aoa="14" width="6" peak="1.5"/>
<flap0 start="0.04" end="0.38" lift="1.5" drag="1.2"/>
<flap1 start="0.38" end="0.97" lift="1.2" drag="1.2"/>
<control-input axis="/controls/flaps" control="FLAP0"/>
<control-input axis="/controls/aileron" control="FLAP1" split="true"/>
<control-input axis="/controls/aileron-trim" control="FLAP1" split="true"/>
<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-speed control="FLAP0" transition-time="5"/>
</wing>
<hstab x="-18.12" y="0.41" z="0.27" length="3.5" effectiveness="3.0"
chord="3" taper=".545" sweep="15">
<stall aoa="18" width="3" peak="1.5"/>
<flap0 start="0" end="1" lift="1.5" drag="1.2"/>
<control-input axis="/controls/elevator" control="FLAP0" effectiveness="1.25"/>
<control-input axis="/controls/elevator-trim" control="FLAP0"/>
<control-output control="FLAP0" prop="/surface-positions/elevator-pos-norm"/>
</hstab>
<vstab x="-18.12" y="0" z="0.95" length="2.72" effectiveness="1.25"
chord="3.95" taper=".462" sweep="2">
<stall aoa="14" width="3" peak="1.5"/>
<flap0 start="0" end="1" lift="1.5" drag="1.2"/>
<control-input axis="/controls/rudder" control="FLAP0" effectiveness="1.25" invert="true"/>
<control-input axis="/controls/rudder-trim" control="FLAP0" invert="true"/>
<control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm"/>
</vstab>
<propeller x="-4.09" y="2.52" z="-0.95"
mass="2000" moment="35" radius="1.4"
eng-power="1200" eng-rpm="2700"
turbo-mul="1.5"
cruise-power="660" cruise-speed="195"
cruise-rpm="2100" cruise-alt="20000"
min-rpm="1600" max-rpm="2700">
<actionpt x="-2.45" y="2.52" z="-0.95"/>
<control-input axis="/controls/throttle[0]" control="THROTTLE"/>
<control-input axis="/controls/starter[0]" control="STARTER"/>
<control-input axis="/controls/magnetos[0]" control="MAGNETOS"/>
<control-input axis="/controls/mixture[0]" control="MIXTURE"/>
<control-input axis="/controls/propeller-pitch[0]" control="ADVANCE"/>
<control-input axis="/controls/boost[0]" control="BOOST"/>
</propeller>
<propeller x="-4.09" y="-2.52" z="-0.95"
mass="2000" moment="-35" radius="1.4"
eng-power="1200" eng-rpm="2700"
turbo-mul="1.5"
cruise-power="660" cruise-speed="195"
cruise-rpm="2100" cruise-alt="20000"
min-rpm="1600" max-rpm="2700">
<actionpt x="-2.45" y="-2.52" z="-0.95"/>
<control-input axis="/controls/throttle[1]" control="THROTTLE"/>
<control-input axis="/controls/starter[1]" control="STARTER"/>
<control-input axis="/controls/magnetos[1]" control="MAGNETOS"/>
<control-input axis="/controls/mixture[1]" control="MIXTURE"/>
<control-input axis="/controls/propeller-pitch[1]" control="ADVANCE"/>
<control-input axis="/controls/boost[1]" control="BOOST"/>
</propeller>
<!-- Tail wheel; has castering selectable by a wheel lock -->
<gear x="-17.3" y="0" z="-0.9" compression="0.2">
<control-input axis="/controls/tailwheel-castering" control="CASTERING"/>
</gear>
<gear x="-6.08" y="2.52" z="-3.49" compression="1" retract-time="7">
<control-input axis="/controls/parking-brake" control="BRAKE"/>
<control-input axis="/controls/brakes[0]" control="BRAKE"/>
<control-input axis="/controls/gear-down" control="EXTEND"/>
<control-speed control="EXTEND" transition-time="7"/>
<control-output control="EXTEND" prop="/gear/gear[0]/position-norm"/>
</gear>
<gear x="-6.08" y="-2.52" z="-3.49" compression="1" retract-time="7">
<control-input axis="/controls/parking-brake" control="BRAKE"/>
<control-input axis="/controls/brakes[1]" control="BRAKE"/>
<control-input axis="/controls/gear-down" control="EXTEND"/>
<control-speed control="EXTEND" transition-time="7"/>
<control-output control="EXTEND" prop="/gear/gear[1]/position-norm"/>
</gear>
<!-- From the type certificate: "Fuel capacity: 822 gals. (4 tanks in
center section wing: 2 main including fuel system 210 gals. each
(+48) and 2 aux. 201 gals. each (+83.5)" -->
<tank x="-7.02" y="0" z="-0.95" capacity="4932"/>
<ballast x="-18.0" y="0.0" z="0.6" mass="-2400"/> <!-- move CG forward -->
</airplane>