Add an elevator setting to the <cruise> element; otherwise, neutral
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.
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@ -41,6 +41,7 @@ since it is what the weight-and-balance site above uses.
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<cruise speed="64" alt="0">
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<control-setting axis="/controls/throttle[0]" value="0.75"/>
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<control-setting axis="/controls/mixture[0]" value="0.75"/>
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<control-setting axis="/controls/elevator" value="0.1"/>
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</cruise>
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<!-- pilot's eyepoint -->
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@ -73,17 +74,17 @@ since it is what the weight-and-balance site above uses.
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<hstab x="-4.87" y="0.05" z="-0.42" taper="0.8" effectiveness="1.24"
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length="1.49" chord="1.13" sweep="0">
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<stall aoa="16" width="4" peak="1.5"/>
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<flap0 start="0" end="1" lift="1.4" drag="1.2"/>
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<flap0 start="0" end="1" lift="1.5" drag="1.2"/>
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<control-input axis="/controls/elevator" control="FLAP0"/>
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<control-input axis="/controls/elevator-trim" control="FLAP0"/>
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<control-output control="FLAP0" prop="/surface-positions/elevator-pos-norm"/>
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</hstab>
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<!-- rudder has to be able to counteract aileron drag -->
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<vstab x="-4.87" y="0" z="-0.65" taper="0.38" effectiveness="1.24"
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length="1.31" chord="1.37" sweep="0">
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<vstab x="-4.87" y="0" z="-0.65" taper="0.38" effectiveness="2.0"
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length="1.31" chord="1.37" sweep="0" incidence="1.5">
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<stall aoa="16" width="4" peak="1.5"/>
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<flap0 start="0" end="1" lift="1.7" drag="1.2" effectiveness="1.5"/>
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<flap0 start="0" end="1" lift="2.0" drag="1.2"/>
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<control-input axis="/controls/rudder" control="FLAP0" invert="true"/>
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<control-input axis="/controls/rudder-trim" control="FLAP0" invert="true"/>
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<control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm"
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