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Add an elevator setting to the <cruise> element; otherwise, neutral

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elevator and trim give ridiculously high airspeeds.

Increase the elevator effectiveness slightly.

Increase the vertical stabilizer effectiveness, and give it a 1.5
degree incidence angle, to compensate for asymmetric propeller
effects.

Increase the rudder effectiveness to help with cross-wind takeoffs and
landings.
This commit is contained in:
david 2003-03-26 02:21:06 +00:00
parent 9e76f046e4
commit a2711ac610
1 changed files with 5 additions and 4 deletions
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9
Aircraft-yasim/j3cub.xml
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@ -41,6 +41,7 @@ since it is what the weight-and-balance site above uses.
<cruise speed="64" alt="0"> <cruise speed="64" alt="0">
<control-setting axis="/controls/throttle[0]" value="0.75"/> <control-setting axis="/controls/throttle[0]" value="0.75"/>
<control-setting axis="/controls/mixture[0]" value="0.75"/> <control-setting axis="/controls/mixture[0]" value="0.75"/>
<control-setting axis="/controls/elevator" value="0.1"/>
</cruise> </cruise>
<!-- pilot's eyepoint --> <!-- pilot's eyepoint -->
@ -73,17 +74,17 @@ since it is what the weight-and-balance site above uses.
<hstab x="-4.87" y="0.05" z="-0.42" taper="0.8" effectiveness="1.24" <hstab x="-4.87" y="0.05" z="-0.42" taper="0.8" effectiveness="1.24"
length="1.49" chord="1.13" sweep="0"> length="1.49" chord="1.13" sweep="0">
<stall aoa="16" width="4" peak="1.5"/> <stall aoa="16" width="4" peak="1.5"/>
<flap0 start="0" end="1" lift="1.4" drag="1.2"/> <flap0 start="0" end="1" lift="1.5" drag="1.2"/>
<control-input axis="/controls/elevator" control="FLAP0"/> <control-input axis="/controls/elevator" control="FLAP0"/>
<control-input axis="/controls/elevator-trim" control="FLAP0"/> <control-input axis="/controls/elevator-trim" control="FLAP0"/>
<control-output control="FLAP0" prop="/surface-positions/elevator-pos-norm"/> <control-output control="FLAP0" prop="/surface-positions/elevator-pos-norm"/>
</hstab> </hstab>
<!-- rudder has to be able to counteract aileron drag --> <!-- rudder has to be able to counteract aileron drag -->
<vstab x="-4.87" y="0" z="-0.65" taper="0.38" effectiveness="1.24" <vstab x="-4.87" y="0" z="-0.65" taper="0.38" effectiveness="2.0"
length="1.31" chord="1.37" sweep="0"> length="1.31" chord="1.37" sweep="0" incidence="1.5">
<stall aoa="16" width="4" peak="1.5"/> <stall aoa="16" width="4" peak="1.5"/>
<flap0 start="0" end="1" lift="1.7" drag="1.2" effectiveness="1.5"/> <flap0 start="0" end="1" lift="2.0" drag="1.2"/>
<control-input axis="/controls/rudder" control="FLAP0" invert="true"/> <control-input axis="/controls/rudder" control="FLAP0" invert="true"/>
<control-input axis="/controls/rudder-trim" control="FLAP0" invert="true"/> <control-input axis="/controls/rudder-trim" control="FLAP0" invert="true"/>
<control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm" <control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm"