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Fix from Dave Perry. The wing Z coordinate was inverted in the original

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version.  This is a low wing aircraft. ;)
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aross 2002-08-30 18:28:52 +00:00
parent 408b9f1d0a
commit 6c931cef21
1 changed files with 3 additions and 9 deletions
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12
Aircraft-yasim/dc3.xml
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@ -28,7 +28,7 @@
<fuselage ax="0" ay="0" az="0" bx="-19.75" by="0" bz="0" <fuselage ax="0" ay="0" az="0" bx="-19.75" by="0" bz="0"
width="2" taper="0.5" midpoint="0.25"/> width="2" taper="0.5" midpoint="0.25"/>
<wing x="-7.02" y="1.09" z="0.95" length="11.58" camber="0.1" <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"> chord="4.77" taper=".286" sweep="19" dihedral="4">
<stall aoa="14" width="6" peak="1.5"/> <stall aoa="14" width="6" peak="1.5"/>
<flap0 start="0.04" end="0.38" lift="1.5" drag="1.2"/> <flap0 start="0.04" end="0.38" lift="1.5" drag="1.2"/>
@ -44,7 +44,7 @@
<control-speed control="FLAP0" transition-time="5"/> <control-speed control="FLAP0" transition-time="5"/>
</wing> </wing>
<hstab x="-18.12" y="0.41" z="0.27" length="3.5" effectiveness="2.00" <hstab x="-18.12" y="0.41" z="0.27" length="3.5" effectiveness="2.4"
chord="3" taper=".545" sweep="15"> chord="3" taper=".545" sweep="15">
<stall aoa="18" width="3" peak="1.5"/> <stall aoa="18" width="3" peak="1.5"/>
<flap0 start="0" end="1" lift="1.5" drag="1.2"/> <flap0 start="0" end="1" lift="1.5" drag="1.2"/>
@ -99,13 +99,9 @@
<control-input axis="/controls/tailwheel-castering" control="CASTERING"/> <control-input axis="/controls/tailwheel-castering" control="CASTERING"/>
</gear> </gear>
<!-- Main wheels; note mapping of rudder input to effect differential
braking -->
<gear x="-6.08" y="2.52" z="-3.49" compression="1" retract-time="7"> <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/parking-brake" control="BRAKE"/>
<control-input axis="/controls/brakes[0]" control="BRAKE"/> <control-input axis="/controls/brakes[0]" control="BRAKE"/>
<!-- <control-input axis="/controls/rudder" control="BRAKE" square="1"
src0="-1" src1="1" dst0="0.5" dst1="-0.5"/> -->
<control-input axis="/controls/gear-down" control="EXTEND"/> <control-input axis="/controls/gear-down" control="EXTEND"/>
<control-speed control="EXTEND" transition-time="7"/> <control-speed control="EXTEND" transition-time="7"/>
<control-output control="EXTEND" prop="/gear/gear[0]/position-norm"/> <control-output control="EXTEND" prop="/gear/gear[0]/position-norm"/>
@ -114,8 +110,6 @@
<gear x="-6.08" y="-2.52" z="-3.49" compression="1" retract-time="7"> <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/parking-brake" control="BRAKE"/>
<control-input axis="/controls/brakes[1]" control="BRAKE"/> <control-input axis="/controls/brakes[1]" control="BRAKE"/>
<!-- <control-input axis="/controls/rudder" control="BRAKE" square="1"
src0="-1" src1="1" dst0="-0.5" dst1="0.5"/> -->
<control-input axis="/controls/gear-down" control="EXTEND"/> <control-input axis="/controls/gear-down" control="EXTEND"/>
<control-speed control="EXTEND" transition-time="7"/> <control-speed control="EXTEND" transition-time="7"/>
<control-output control="EXTEND" prop="/gear/gear[1]/position-norm"/> <control-output control="EXTEND" prop="/gear/gear[1]/position-norm"/>
@ -125,6 +119,6 @@
center section wing: 2 main including fuel system 210 gals. each center section wing: 2 main including fuel system 210 gals. each
(+48) and 2 aux. 201 gals. each (+83.5)" --> (+48) and 2 aux. 201 gals. each (+83.5)" -->
<tank x="-7.02" y="0" z="0.95" capacity="4932"/> <tank x="-7.02" y="0" z="0.95" capacity="4932"/>
<ballast x="-18.0" y="0.0" z="0.6" mass="-2800"/> <!-- move CG forward --> <ballast x="-18.0" y="0.0" z="0.6" mass="-2000"/> <!-- move CG forward -->
</airplane> </airplane>