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fgdata/Aircraft-yasim/pa28-161.xml
2002-12-18 02:03:46 +00:00

93 lines
3.8 KiB
XML

<airplane mass="1480">
<!-- Approach configuration -->
<approach speed="43" aoa="17">
<control-setting axis="/controls/throttle[0]" value="0.3"/>
<control-setting axis="/controls/mixture[0]" value="1.0"/>
<control-setting axis="/controls/flaps" value="1.0"/>
</approach>
<!-- Cruise configuration -->
<cruise speed="122" alt="0">
<control-setting axis="/controls/throttle[0]" value="1.0"/>
<control-setting axis="/controls/mixture[0]" value="1.0"/>
<control-setting axis="/controls/flaps" value="0.0"/>
</cruise>
<cockpit x="-2.5" y=".33" z="0.6"/>
<fuselage ax="0.5" ay="0" az="0" bx="-7.75" by="0" bz="0"
width="1.5" taper="0.2" midpoint="0.3"/>
<wing x="-2.75" y="0.6" z="-0.75" taper="0.65"
length="4.5" chord="1.65" sweep="0" dihedral="5" camber="0.1">
<stall aoa="16" width="6" peak="1.5"/>
<flap0 start="0" end="0.5" lift="1.3" drag="1.5"/>
<flap1 start="0.5" end="1.0" 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"/>
</wing>
<hstab x="-6.5" y="0.00" z=".15" taper="1.0" effectiveness="2"
length="1.9" chord="0.9" sweep="0">
<stall aoa="18" width="4" peak="1.5"/>
<flap0 start="0" end="1" lift="2.0" drag="1.2"/>
<control-input axis="/controls/elevator" control="FLAP0"/>
<control-input axis="/controls/elevator-trim" control="FLAP0"/>
<control-output control="FLAP0" prop="/surface-positions/elevator-pos-norm"/>
</hstab>
<vstab x="-6.25" y="0" z=".3" taper=".5"
length="1.2" chord="1.2" sweep="10">
<stall aoa="16" width="4" peak="1.5"/>
<flap0 start="0" end="1" lift="1.3" drag="1.1"/>
<control-input axis="/controls/rudder" control="FLAP0" invert="true"/>
<control-input axis="/controls/rudder-trim" control="FLAP0" invert="true"/>
<control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm"
min="1" max="-1"/>
</vstab>
<propeller radius="1.0"
cruise-speed="125" cruise-rpm="2665"
cruise-alt="8000" cruise-power="120"
takeoff-power="140.8" takeoff-rpm="2200"
eng-power="160" eng-rpm="2800"
x="-1" y="0" z="0" mass="400" moment="8">
<actionpt x="0" y="0" z="0"/>
<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"/>
</propeller>
<gear x="-1" y="0" z="-1.3" compression=".05"> <!-- nose -->
<control-input axis="/controls/rudder" control="STEER"
src0="-1.0" src1="1.0"
dst0="-0.1" dst1="0.1"/>
</gear>
<gear x="-2.8" y="1.5" z="-1.3" compression=".05"> <!-- left main -->
<control-input axis="/controls/brakes[0]" control="BRAKE" split="true"/>
<control-input axis="/controls/parking-brake" control="BRAKE" split="true"/>
</gear>
<gear x="-2.8" y="-1.5" z="-1.3" compression=".05"> <!-- left main -->
<control-input axis="/controls/brakes[1]" control="BRAKE" split="true"/>
<control-input axis="/controls/parking-brake" control="BRAKE" split="true"/>
</gear>
<tank x="-2.5" y="1.5" z="-0.25" capacity="144"/>
<tank x="-2.5" y="-1.5" z="-0.25" capacity="144"/>
<ballast x="-2.0" y="0" z="0" mass="400"/> <!-- cockpit -->
<weight x="-2.5" y=".33" z="0" mass-prop="/yasim/pa28/pilot-lb"/>
<weight x="-2.5" y="-.33" z="0" mass-prop="/yasim/pa28/copilot-lb"/>
</airplane>