Move *-set.xml and Aircraft-yasim/*.xml into their individual aircraft
subdirectories in yet another step towards making aircraft more self contained rather than potentially spread out.
This commit is contained in:
curt
parent
788adc9e6b
commit
98804a6793
30 changed files with 189 additions and 3371 deletions
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@ -1,133 +0,0 @@
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<airplane mass="400000">
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<!-- Approach configuration -->
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<approach speed="136" aoa="7">
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<control-setting axis="/controls/engines/engine[0]/throttle" value="0.2"/>
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<control-setting axis="/controls/engines/engine[1]/throttle" value="0.2"/>
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<control-setting axis="/controls/flight/flaps" value="1.0"/>
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<control-setting axis="/controls/flight/slats" value="1.0"/>
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<control-setting axis="/controls/gear/gear-down" value="1"/>
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</approach>
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<!-- Cruise configuration -->
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<cruise speed="490" alt="36000">
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<control-setting axis="/controls/engines/engine[0]/throttle" value="0.75"/>
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<control-setting axis="/controls/engines/engine[1]/throttle" value="0.75"/>
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<control-setting axis="/controls/flight/flaps" value="0.0"/>
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<control-setting axis="/controls/gear/gear-down" value="0"/>
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</cruise>
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<cockpit x="19.08" y="1.81" z="15.06"/>
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<fuselage ax="24.5" ay="0" az="0" bx="-45.36" by="0.00" bz="2.41"
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width="6" taper="0.3" midpoint="0.2"/>
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<wing x="-2" y="3.01" z="-1.45" length="33.72" chord="13.25" sweep="33"
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taper=".27" dihedral="7" camber="0.15" incidence="-0.7">
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<stall aoa="12" width="2" peak="2"/>
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<flap0 start="0" end=".56" lift="1.8" drag="1.2"/>
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<flap1 start=".64" end=".88" lift="1.3" drag="1.2"/>
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<slat start="0" end="1" aoa="2" drag="1.1"/>
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<spoiler start="0.2" end="0.6" lift="0.3" drag="2.0"/>
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<control-input axis="/controls/flight/flaps" control="FLAP0"/>
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<control-input axis="/controls/flight/aileron" control="FLAP1" split="true"/>
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<control-input axis="/controls/flight/aileron-trim" control="FLAP1" split="true"/>
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<control-input axis="/controls/flight/slats" control="SLAT"/>
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<control-input axis="/controls/flight/spoilers" control="SPOILER"/>
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<control-output control="FLAP0" prop="/surface-positions/flap-pos-norm"/>
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<control-output control="FLAP1" side="left"
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prop="/surface-positions/left-aileron-pos-norm"/>
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<control-output control="FLAP1" side="right"
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prop="/surface-positions/right-aileron-pos-norm"/>
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<control-speed control="FLAP0" transition-time="10"/>
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</wing>
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<hstab x="-38.13" y="1.81" z="1.81" chord="8.43" length="10.84" taper=".29"
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sweep="28" dihedral="7" camber="-0.1" effectiveness="2.3">
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<stall aoa="15" width="2" peak="1.5"/>
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<flap0 start="0" end="1" lift="1.6" drag="1.2"/>
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<control-input axis="/controls/flight/elevator" control="FLAP0"/>
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<control-input axis="/controls/flight/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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<vstab x="-38.13" y="0.00" z="3.61" chord="12.04" length="12.04" taper="0.3"
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sweep="33">
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<stall aoa="15" width="2" peak="1.5"/>
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<flap0 start="0" end="1" lift="1.2" drag="1.3"/>
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<control-input axis="/controls/flight/rudder" control="FLAP0" invert="true"/>
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<control-input axis="/controls/flight/rudder-trim" control="FLAP0" invert="true"/>
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<control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm"
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min="1" max="-1"/>
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</vstab>
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<!-- The CF6 engines are rated at 60000 lbs thrust, flat rated to 33 -->
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<!-- degrees C. Corrected to YASim's standard atmosphere temperature -->
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<!-- of 288.2 kelvins, that gives 63737 lbs of nominal thrust. -->
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<jet x="-10.43" y="16.26" z="-1.20" mass="8000" thrust="63737">
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<control-input axis="/controls/engines/engine[0]/throttle" control="THROTTLE"/>
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</jet>
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<jet x="-2" y="12.65" z="-2.41" mass="8000" thrust="63737">
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<control-input axis="/controls/engines/engine[0]/throttle" control="THROTTLE"/>
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</jet>
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<jet x="-2" y="-12.65" z="-2.41" mass="8000" thrust="63737">
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<control-input axis="/controls/engines/engine[1]/throttle" control="THROTTLE"/>
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</jet>
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<jet x="-10.43" y="-16.26" z="-1.20" mass="8000" thrust="63737">
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<control-input axis="/controls/engines/engine[1]/throttle" control="THROTTLE"/>
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</jet>
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<!-- nose -->
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<gear x="19.08" y="0.00" z="-5.42"
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compression="0.75" spring="0.7" damp="4">
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<control-input axis="/controls/flight/rudder" control="STEER" square="true"/>
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<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
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<control-output control="EXTEND" prop="/gear/gear[0]/position-norm"/>
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<control-speed control="EXTEND" transition-time="7"/>
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</gear>
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<gear x="-4.65" y="5.42" z="-5.42" compression="1.1"> <!-- fwd left main -->
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<control-input axis="/controls/gear/wheel[0]/brake" control="BRAKE"/>
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<control-input axis="/controls/gear/parking-brake" control="BRAKE"/>
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<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
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<control-output control="EXTEND" prop="/gear/gear[1]/position-norm"/>
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<control-speed control="EXTEND" transition-time="7"/>
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</gear>
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<gear x="-6.82" y="1.81" z="-5.42" compression="1.1"> <!-- rear left main -->
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<control-input axis="/controls/gear/wheel[0]/brake" control="BRAKE"/>
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<control-input axis="/controls/gear/parking-brake" control="BRAKE"/>
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<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
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<control-output control="EXTEND" prop="/gear/gear[2]/position-norm"/>
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<control-speed control="EXTEND" transition-time="7"/>
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</gear>
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<gear x="-6.82" y="-1.81" z="-5.42" compression="1.1"> <!-- rear right main -->
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<control-input axis="/controls/gear/wheel[1]/brake" control="BRAKE"/>
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<control-input axis="/controls/gear/parking-brake" control="BRAKE"/>
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<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
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<control-output control="EXTEND" prop="/gear/gear[3]/position-norm"/>
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<control-speed control="EXTEND" transition-time="7"/>
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</gear>
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<gear x="-4.65" y="-5.42" z="-5.42" compression="1.1"> <!-- fwd right main -->
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<control-input axis="/controls/gear/wheel[1]/brake" control="BRAKE"/>
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<control-input axis="/controls/gear/parking-brake" control="BRAKE"/>
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<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
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<control-output control="EXTEND" prop="/gear/gear[4]/position-norm"/>
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<control-speed control="EXTEND" transition-time="7"/>
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</gear>
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<tank x="-2" y="0" z="-1.45" jet="true" capacity="128000"/>
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<tank x="-5.6" y="8" z="-1.45" jet="true" capacity="128000"/>
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<tank x="-5.6" y="-8" z="-1.45" jet="true" capacity="128000"/>
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<ballast x="18.5" y="0" z="2.4" mass="30000"/> <!-- hump -->
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<ballast x="12.5" y="0" z="2.4" mass="40000"/> <!-- hump -->
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<ballast x="6.5" y="0" z="2.4" mass="40000"/> <!-- hump -->
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<ballast x="0.5" y="0" z="2.4" mass="30000"/> <!-- hump -->
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</airplane>
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@ -1,233 +0,0 @@
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PIPER J3 CUB PERFORMANCE DATA
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=============================
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[This information is copied from the 1946 J3C-65 owner's handbook.]
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FLYING HINTS
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The Piper Cub Special represents more than 15 years of diligent
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aircraft engineering and manufacturing experience. Its simplicity of
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design and construction, its low operating and maintenance costs, its
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inherent stability, ruggedness, and its outstanding safety and ease of
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flying, have made it the most popular airplane in aviation history.
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The Piper Cub Special is the time-tested product of millions of hours
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of flying under all conceivable conditions both in the military and in
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peace time.
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There are hints on starting, flying, stopping, and other related
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topics that are important to the owner who wants to conserve his
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airplane -- keep it in maximum airworthy condition -- and enjoy a full
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measure of flying satisfaction.
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First, each pilot should become familiar enough with his Piper Cub
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Special that he can accomplish a satisfactory pre-flight inspection.
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This check is simple and requires only a few minutes. See Section IX
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for check list. Daily check of airplane prior to flight should be the
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first in a number of safe flying habits the pilot should acquire.
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A. BEFORE STARTING ENGINE
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(1) Make routine check of gasoline supply. Visible fuel gauge is
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integral part of gas tank cap; it will not show number of gallons but
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will show proportion of fuel in tank by length of rod which extends
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upward from cap. A full tank of 12 U.S. gallons will be indicated by
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11 inches of rod extending beyond cap. Keep gas gauge rod clean and
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smooth with crocus cloth for accuracy and freedom of movement.
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(2) Check oil level in engine sump by removing oil cap and gauge. Oil
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stick should indicate oil level up to index mark of 4 quarts.
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(3) Check freedom of movement of flight and engine controls.
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B. STARTING ENGINE
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(1) Chock wheels, or have occupant who is familiar with controls set
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brakes in cabin.
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(2) Ignition switch OFF. Verify.
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(3) Set throttle approximately 1/10 open.
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(4) Push fuel shut-off ON.
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(5) Turn propeller through several times.
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(6) Turn ignition switch ON.
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(7) Start engine by pulling propeller through with a snap.
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CAUTION -- Always handle propeller as if switch were "ON." Stand as
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far in front of propeller as possible. Use both hands and grasp one
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blad approximately midway from tip. Do not overgrasp blade. Do not
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wear long, loose clothing. Make sure footing is sure to preclude
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possibility of feet slipping.
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(8) If engine does not start, turn switch OFF. Turn primer knob to
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unlock, pull out, pump three or four times, then reseat primer and
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lock by turning in opposite direction. In extremely cold weather a
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few strokes of the primer as the engine starts will enable it to keep
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running. NOTE -- Avoid excessive priming as it causes raw gasoline to
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wash lubricating oil from engine cylinder walls. Do not prime warm
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engine.
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(9) Repeat starting procedures 6, 7.
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(10) If engine loads up and refuses to start, turn ignition switch
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"OFF,", open throttle wide and turn propeller through backwards
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several times to unload excessive gas mixture in cylinders. Then
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close throttle and repeat starting procedure.
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C. ENGINE WARM-UP
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(1) As soon as engine starts, advance throttle slightly to idle at 700
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R.P.M. Check engine instruments. If oil pressure gauge does not
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indicate pressure within 30 seconds, stop engine immediately, check
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and correct trouble before any further operation. Oil temperature
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during operating should not rise above 200° F. and oil pressure should
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not fall below 30 pounds. With engine warm, idling speed should be
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550-600 R.P.M.
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(2) Rev engine up to 2100 R.P.M. on both magnetos. Switch to LEFT and
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RIGHT magnetos. R.P.M. drop should not be over 75 R.P.M. CAUTION
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--Do not operate engine on either single magneto for more than 30
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seconds at a time, as this tends to foul the non-operating spark plugs
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in the ignition circuit of the magneto that is switched off.
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D. STOPPING ENGINE
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(1) Never cut switch immediately after landing as this causes engine
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to cool too rapidly.
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(2) Idle engine, especially in high temperature operating conditions,
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for several minutes. It is advisable to switch to each magneto for 30
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second intervals to allow gradual cooling of engine. This helps to
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prevent overheating of spark plug insulators and will lessen tendency
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for "after-firing."
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(3) Check for carburetor heat OFF during idling.
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E. TAXIING
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(1) Open throttle to start airplane in motion; then close throttle to
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a setting sufficient to keep airplane rolling. Do not keep throttle
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advanced so that it is necessary to control taxi speed of airplane
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with brakes. This causes unnecessary wear and tear on brakes and
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tires.
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(2) Taxi slowly (speed of a fast walk) controlling direction with
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rudder which is connected to a steerable tail wheel. Use brakes only
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for positive, precision ground control when necessary.
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(3) Taxi upwind with stick back; downwind with stick foreward. When
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ground winds are in excess of 15 M.P.H., turn into wind using ailerons
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in direction of turn; apply ailerons away from the turn when turning
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downwind. This procedure helps to prevent the wind "picking up" a
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wing during windy, gusty conditions. Always make ground turns slowly.
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F. GENERAL FLYING
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(1) For takeoff use full throttle, heading into wind. Airplane loaded
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will become airborne at approximately 39 M.P.H. Best climb speed is
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an indicated 55 M.P.H.
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(2) Indicated R.P.M. for cruising speed of 73 M.P.H. is 2150.
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Take-off R.P.M. is 2300. Do not fly at full throttle over 3 minutes.
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(3) Use CARBURETOR AIR HEAT when engine runs "rough" and tachometer
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shows drop in R.P.M. which may be due to ice forming in carburetor.
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Tachometer should recover to within 50 R.P.M. below normal when using
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carburetor heat. Push heater to "OFF" position, and if icing
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condition has been cleared, R.P.M. should return to normal. Continued
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use of carburetor heat will only cause increased fuel consumption and
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loss of power.
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(4) Maximum permissible diving speed is 122 M.P.H.
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G. APPROACH AND LANDING
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(1) Push carburetor heat ON prior to throttling back for glide, or for
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any other flight maneuver.
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(2) Glide between 50-60 M.P.H. depending upon loading of airplane and
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gust conditions.
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NOTE -- "Clear" engine by opening throttle gently, every 200-250 feet
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of descent during a long glide so that engine temperature will be
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maintained.
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Throttle action on the part of the pilot should be smooth and gentle
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at all times.
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H. PARKING AND MOORING
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(1) After termination of flight, enter flying time in aircraft and
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engine log books.
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(2) Turn ignition and fuel OFF.
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(3) Chcok the wheels of airplane.
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(4) If airplane is not to be flown for some time, it should be
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hangared or tied down. Use good quality 1/2" - 5/8" diameter rope.
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Secure to lift assist handle at aft end of fuselage; also at upper end
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of both front wing lift struts where they attach to wing. Make sure
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that rope passes between aileron cable and lift strut. Mooring ropes,
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when airplane is tied down, should have no slack.
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(5) Lock aileron and elevator controls by wrapping front seat belt
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completely around rear control stick, tighten and buckle.
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(6) Under excessively wind conditions, airplane should be tailed into
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wind for mooring.
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[Here is my older information.]
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These are the only numbers I could find. They are for a J3 Cub with
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an 85HP engine rather than 65 hp, so some adjustments may be
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necessary. The source is
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http://www.evergreenfs.com/planedata.htm
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Speeds
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------
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Best rate of climb (Vy): 65 mph (57 kt)
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Best angle of climb (Vx): 55 mph (48 kt)
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Cruise: 70 mph (61 kt)
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Never-exceed (Vne): 122 mph (106 kt)
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Best Glide (Vglide): 60 mph (52 kt)
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Stall (Vs): 38 mph (33 kt)
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Maneuvering (Va): 70 mph (61 kt)
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Approach: 50-60 mph (44-52 kt)
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Power
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-----
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Take off: full
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Climb: 50 rpm below full
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Cruise: 2300 rpm
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Approach: 1200 rpm
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Practice stalls: 1200 rpm
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Distances
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---------
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Take-off: 450-800 ft
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Landing: 200-800 ft
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Fuel
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----
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Total fuel: 12 gal US
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Usable fuel: 12 gal US
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Grade: 80/87
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GPH: 5 gal US/hr
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@ -1,60 +0,0 @@
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P-51D Information
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=============
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FLYING HINTS
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NOTE: the yasim config file for this aircraft currently starts up with
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the booster in 1st stage.
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TAKE OFF:
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Set prop pitch to full increased rpm.
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Start engine with throttle at idle.
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Set BOOST stage one (CTRL-b keybinding cycles through stage 0 (off), 1,
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and 2). Default startup for p51-d should have stage one already on.
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Set throttle to 40 inHG Manifold Pressure (MP).
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Be ready to actuate rudder. When the tail first lifts, the torque will
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pull the nose to the left.
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After tail lifts off slowing move throttle to full open which with
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stage 1 booster engaged should be about 61 inHG Manifold Pressure.
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Hang on. Stay on top of rudder control with small adjustments or you'll
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do a ground loop.
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Rotate at 150 mph or so.
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CLIMB:
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Back off MP to 46 inHG.
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Adjust propeller pitch to 2700 rpm.
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Keep adding throttle as you climb to maintain 46 inHG until you hit full throttle.
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At 18,000 feet turn on second stage (hit CTRL-b) and back off throttle to 46 inHG.
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FLYING:
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Trim and Cruise at about 2400 rpm.
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Do not exceed 2700 rpm sustained.
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Do not exceed 3000 rpm military power (aerobatics)
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Do not exceed 3500 rpm in dives.
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Do not exceed 61 inHG Mainfold Pressure (military power), except 71 inHG for
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maximum of 7 minutes (war emergency power). Note that war emergency
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power is not for flying fast, rather it is for dogfighting at < 200mph.
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LANDING:
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A single long sweeping turn from the downwind leg into a short approach
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seems to work best. Make sure you are below 250mph before starting the
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turn. Use forward slip as necessary to bleed off speed and altitude at the
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same time.
|
||||
Start applying flaps at 250mph, gear at 175mph, and full flaps
|
||||
at 165mph or less.
|
||||
|
||||
Excessive braking can cause you to nose over. Some recommend raising
|
||||
flaps immediately after touchdown.
|
||||
|
||||
|
||||
PERFORMANCE:
|
||||
|
||||
This information is gleaned from various sources:
|
||||
|
||||
Maximum Speed: 437 mph
|
||||
Cruise Speed: 363 mph
|
||||
Landing Speed: 100 mph
|
||||
Initial Climb Rate: 3475 feet per minute
|
||||
Sustained Climb Speed: 175 mph
|
||||
Service Ceiling: 41,900 (with 2nd Stage booster).
|
||||
Stall Speed (9000lbs) Gear/Flaps Up: 102mph Gear/Flaps Down: 95mph
|
||||
|
|
@ -1,43 +0,0 @@
|
|||
PIPER WARRIOR II PERFORMANCE DATA
|
||||
=================================
|
||||
|
||||
These numbers apply to the 160 hp variant of the Warrior II; they come
|
||||
from the Piper POH.
|
||||
|
||||
Speeds
|
||||
------
|
||||
Vne (never exceed): 160 KIAS
|
||||
Vno (max. cruise): 126 KIAS
|
||||
Vfe (max. flaps): 103 KIAS
|
||||
Va (maneuvering): 111 KIAS (2440 lb) - 88 KIAS (1531 lb)
|
||||
Vs (clean stall): 50 KIAS
|
||||
Vso (flaps stall): 44 KIAS
|
||||
Vglide (best glide): 73 KIAS
|
||||
Vx (best climb angle): 63 KIAS
|
||||
Vy (best climb rate): 79 KIAS
|
||||
Enroute climb: 87 KIAS
|
||||
Approach (no flaps): 70 KIAS
|
||||
Approach (full flaps): 63 KIAS
|
||||
|
||||
Cruise (75%, 8000 ft): 124 KTAS (107 KIAS)
|
||||
Cruise (55%, 8000 ft): 103 KTAS (89 KIAS)
|
||||
|
||||
Power
|
||||
-----
|
||||
Take off: full
|
||||
Climb: full
|
||||
75% power at 8,000 ft: 2665 rpm
|
||||
75% power at 4,000 ft: 2570 rpm
|
||||
75% power at sea level: 2480 rpm
|
||||
55% power at 12,000 ft: 2470 rpm
|
||||
55% power at 8,000 ft: 2375 rpm
|
||||
55% power at 4,000 ft: 2285 rpm
|
||||
55% power at sea level: 2195 rpm
|
||||
|
||||
Fuel
|
||||
----
|
||||
Total fuel: 50 gal US
|
||||
Usable fuel: 48 gal US
|
||||
Grade: 100LL/100 (Avgas)
|
||||
GPH (75%, 8000 ft): 10.0 gph
|
||||
GPH (55%, 8000 ft): 7.0 gph
|
||||
|
|
@ -1,146 +0,0 @@
|
|||
<!-- A10 yasim config. This is a hack and not an authentic
|
||||
representation of the aircraft. Having said that, the
|
||||
numbers, where I could find them, roughly match those of
|
||||
the original aircraft.
|
||||
Lee Elliott. leee-fgfs@spatial.freeserve.co.uk
|
||||
-->
|
||||
|
||||
<airplane mass="37700">
|
||||
|
||||
<!-- Approach configuration -->
|
||||
<approach speed="110" aoa="7">
|
||||
<control-setting axis="/controls/engines/engine[0]/throttle" value="0.5"/>
|
||||
<control-setting axis="/controls/engines/engine[1]/throttle" value="0.5"/>
|
||||
<control-setting axis="/controls/flight/flaps" value="1.0"/>
|
||||
<control-setting axis="/controls/gear/gear-down" value="1"/>
|
||||
</approach>
|
||||
|
||||
<!-- Cruise configuration -->
|
||||
<cruise speed="380" alt="0">
|
||||
<control-setting axis="/controls/engines/engine[0]/throttle" value="1.0"/>
|
||||
<control-setting axis="/controls/engines/engine[1]/throttle" value="1.0"/>
|
||||
<control-setting axis="/controls/flight/flaps" value="0.0"/>
|
||||
<control-setting axis="/controls/gear/gear-down" value="0"/>
|
||||
</cruise>
|
||||
|
||||
<cockpit x="-3.5" y="0.0" z="1.2"/>
|
||||
|
||||
<fuselage ax="0" ay="0" az="0" bx="-16.26" by="0" bz="0"
|
||||
width="1.4"/>
|
||||
|
||||
<!-- Left Engine -->
|
||||
<fuselage ax="-10" ay="1.50" az="1" bx="-13.5" by="1.50" bz="0.8"
|
||||
width="1.5"/>
|
||||
|
||||
<!-- Right Engine -->
|
||||
<fuselage ax="-10" ay="-1.50" az="1" bx="-13.5" by="-1.50" bz="0.8"
|
||||
width="1.5"/>
|
||||
|
||||
<wing x="-8.8" y="0.5" z="-0.5" taper="0.6" incidence="-1"
|
||||
length="8.3" chord="3.1" sweep="0.0" dihedral="3.0" camber="0">
|
||||
<stall aoa="14" width="6" peak="1.3"/>
|
||||
<flap0 start="0.04" end="0.51" lift="1.5" drag="1.2"/>
|
||||
<flap1 start="0.54" end="0.86" lift="1.3" drag="1.2"/>
|
||||
<spoiler start="0.54" end="0.86" lift="0.1" drag="20.0"/>
|
||||
|
||||
<control-input axis="/controls/flight/flaps" control="FLAP0"/>
|
||||
<control-input axis="/controls/flight/aileron" control="FLAP1" split="true"/>
|
||||
<control-input axis="/controls/flight/aileron-trim" control="FLAP1" split="true"/>
|
||||
<control-input axis="/controls/flight/spoilers" control="SPOILER"/>
|
||||
|
||||
<control-output control="FLAP0" side="left"
|
||||
prop="/surface-positions/left-flap-pos-norm"/>
|
||||
<control-output control="FLAP0" side="right"
|
||||
prop="/surface-positions/right-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-output control="SPOILER" side="left"
|
||||
prop="/surface-positions/left-spoiler-pos-norm"/>
|
||||
<control-output control="SPOILER" side="right"
|
||||
prop="/surface-positions/right-spoiler-pos-norm"/>
|
||||
|
||||
<control-speed control="FLAP0" transition-time="5"/>
|
||||
<control-speed control="SPOILER" transition-time="0.5"/>
|
||||
|
||||
</wing>
|
||||
|
||||
<hstab x="-15.5" y="0.4" z="0.4" taper="0.0" effectiveness="3"
|
||||
length="2.5" chord="2" sweep="0.0" dihedral="0.0" camber="0">
|
||||
<stall aoa="20" width="5" peak="1.5"/>
|
||||
<flap0 start="0" end="1" lift="1.5" drag="1.2"/>
|
||||
<control-input axis="/controls/flight/elevator" control="FLAP0"/>
|
||||
<control-input axis="/controls/flight/elevator-trim" control="FLAP0"/>
|
||||
<control-output control="FLAP0" prop="/surface-positions/elevator-pos-norm"/>
|
||||
</hstab>
|
||||
|
||||
<vstab x="-15.0" y="2.5" z="-0.9" taper="0.7" effectiveness="2"
|
||||
length="2.8" chord="2.0" sweep="0.0">
|
||||
<stall aoa="16" width="5" peak="1.5"/>
|
||||
<flap0 start="0" end="1" lift="1.3" drag="1.3"/>
|
||||
<control-input axis="/controls/flight/rudder" control="FLAP0" invert="true"/>
|
||||
<control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm"/>
|
||||
</vstab>
|
||||
|
||||
<vstab x="-15.0" y="-2.5" z="-0.9" taper="0.7" effectiveness="2"
|
||||
length="2.8" chord="2.0" sweep="0.0">
|
||||
<stall aoa="16" width="5" peak="1.5"/>
|
||||
<flap0 start="0" end="1" lift="1.3" drag="1.3"/>
|
||||
<control-input axis="/controls/flight/rudder" control="FLAP0" invert="true"/>
|
||||
<control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm"/>
|
||||
</vstab>
|
||||
|
||||
<!-- Engines and tanks -->
|
||||
<jet x="-11.8" y="-1.5" z="1.0" mass="1000" thrust="9065">
|
||||
<control-input axis="/controls/engines/engine[0]/throttle" control="THROTTLE"/>
|
||||
</jet>
|
||||
|
||||
<jet x="-11.8" y="1.5" z="1.0" mass="1000" thrust="9065">
|
||||
<control-input axis="/controls/engines/engine[1]/throttle" control="THROTTLE"/>
|
||||
</jet>
|
||||
|
||||
<tank x="-8.5" y="-1.5" z="0.0" jet="true" capacity="2000"/>
|
||||
<tank x="-8.5" y="1.5" z="0.0" jet="true" capacity="2000"/>
|
||||
<tank x="-8.5" y="0" z="0.0" jet="true" capacity="6700"/>
|
||||
|
||||
<!-- Undercarriage -->
|
||||
<!-- nose -->
|
||||
<gear x="-2.9" y="0.4" z="-2.8" retract-time="7" compression="0.7">
|
||||
<control-input axis="/controls/flight/rudder" control="STEER" square="true"/>
|
||||
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
|
||||
<control-speed control="EXTEND" transition-time="7"/>
|
||||
<control-output control="EXTEND" prop="/gear/gear/position-norm"/>
|
||||
</gear>
|
||||
|
||||
<!-- left main -->
|
||||
<gear x="-9.0" y="2.5" z="-2.8" retract-time="7" compression="0.6">
|
||||
<control-input axis="/controls/gear/wheel[1]/brake" control="BRAKE"/>
|
||||
<control-input axis="/controls/gear/parking-brake" control="BRAKE"/>
|
||||
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
|
||||
<control-speed control="EXTEND" transition-time="7"/>
|
||||
<control-output control="EXTEND" prop="/gear/gear[1]/position-norm"/>
|
||||
</gear>
|
||||
|
||||
<!-- right main -->
|
||||
<gear x="-9.0" y="-2.5" z="-2.8" retract-time="7" compression="0.6">
|
||||
<control-input axis="/controls/gear/wheel[2]/brake" control="BRAKE"/>
|
||||
<control-input axis="/controls/gear/parking-brake" control="BRAKE"/>
|
||||
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
|
||||
<control-speed control="EXTEND" transition-time="7"/>
|
||||
<control-output control="EXTEND" prop="/gear/gear[2]/position-norm"/>
|
||||
</gear>
|
||||
|
||||
<!-- Canopy -->
|
||||
<gear x="-2.6" y="0.0" z="1.4" retract-time="7" compression="0.6">
|
||||
<control-input axis="/controls/gear/parking-brake" control="EXTEND"/>
|
||||
<control-speed control="EXTEND" transition-time="5"/>
|
||||
<control-output control="EXTEND" prop="/canopy/position-norm"/>
|
||||
</gear>
|
||||
|
||||
<!-- Ballast -->
|
||||
<ballast x="-3.5" y="0" z="1.0" mass="2000"/> <!-- Armored cockpit -->
|
||||
<ballast x="-4.0" y="0" z="-1.0" mass="4000"/> <!-- Gun -->
|
||||
<ballast x="-5.0" y="0" z="0.0" mass="1000"/> <!-- avionics -->
|
||||
|
||||
</airplane>
|
||||
|
|
@ -1,143 +0,0 @@
|
|||
<!-- A10 yasim config. This is a hack and not an authentic
|
||||
representation of the aircraft. Having said that, the
|
||||
numbers, where I could find them, roughly match those of
|
||||
the original aircraft.
|
||||
Lee Elliott. leee-fgfs@spatial.freeserve.co.uk
|
||||
-->
|
||||
|
||||
<airplane mass="37700">
|
||||
|
||||
<!-- Approach configuration -->
|
||||
<approach speed="110" aoa="8">
|
||||
<control-setting axis="/controls/engines/engine[0]/throttle" value="0.5"/>
|
||||
<control-setting axis="/controls/engines/engine[1]/throttle" value="0.5"/>
|
||||
<control-setting axis="/controls/flight/flaps" value="1.0"/>
|
||||
<control-setting axis="/controls/gear/gear-down" value="1"/>
|
||||
</approach>
|
||||
|
||||
<!-- Cruise configuration -->
|
||||
<cruise speed="380" alt="0">
|
||||
<control-setting axis="/controls/engines/engine[0]/throttle" value="1.0"/>
|
||||
<control-setting axis="/controls/engines/engine[1]/throttle" value="1.0"/>
|
||||
<control-setting axis="/controls/flight/flaps" value="0.0"/>
|
||||
<control-setting axis="/controls/gear/gear-down" value="0"/>
|
||||
</cruise>
|
||||
|
||||
<cockpit x="-3.5" y="0.0" z="1.2"/>
|
||||
|
||||
<fuselage ax="0" ay="0" az="0" bx="-16.26" by="0" bz="0"
|
||||
width="1.4"/>
|
||||
|
||||
<!-- Left Engine -->
|
||||
<fuselage ax="-10" ay="1.50" az="1" bx="-13.5" by="1.50" bz="0.8"
|
||||
width="1.5"/>
|
||||
|
||||
<!-- Right Engine -->
|
||||
<fuselage ax="-10" ay="-1.50" az="1" bx="-13.5" by="-1.50" bz="0.8"
|
||||
width="1.5"/>
|
||||
|
||||
<wing x="-8.8" y="0.5" z="-0.5" taper="0.6" incidence="-1.0"
|
||||
length="8.3" chord="3.1" sweep="0.0" dihedral="3.0" camber="0.006">
|
||||
<stall aoa="17" width="6" peak="1.3"/>
|
||||
<flap0 start="0.04" end="0.51" lift="1.5" drag="1.2"/>
|
||||
<flap1 start="0.54" end="0.86" lift="1.3" drag="1.2"/>
|
||||
<spoiler start="0.54" end="0.86" lift="0.1" drag="20.0"/>
|
||||
|
||||
<control-input axis="/controls/flight/flaps" control="FLAP0"/>
|
||||
<control-input axis="/controls/flight/aileron" control="FLAP1" split="true"/>
|
||||
<control-input axis="/controls/flight/aileron-trim" control="FLAP1" split="true"/>
|
||||
<control-input axis="/controls/flight/spoilers" control="SPOILER"/>
|
||||
|
||||
<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-output control="SPOILER" side="left"
|
||||
prop="/surface-positions/left-spoiler-pos-norm"/>
|
||||
<control-output control="SPOILER" side="right"
|
||||
prop="/surface-positions/right-spoiler-pos-norm"/>
|
||||
|
||||
<control-speed control="FLAP0" transition-time="5"/>
|
||||
<control-speed control="SPOILER" transition-time="0.5"/>
|
||||
|
||||
</wing>
|
||||
|
||||
<hstab x="-15.5" y="0.4" z="0.4" taper="0.0" effectiveness="3"
|
||||
length="2.5" chord="2" sweep="0.0" dihedral="0.0" camber="0">
|
||||
<stall aoa="18" width="5" peak="1.5"/>
|
||||
<flap0 start="0" end="1" lift="1.5" drag="1.2"/>
|
||||
<control-input axis="/controls/flight/elevator" control="FLAP0"/>
|
||||
<control-input axis="/controls/flight/elevator-trim" control="FLAP0"/>
|
||||
<control-output control="FLAP0" prop="/surface-positions/elevator-pos-norm"/>
|
||||
</hstab>
|
||||
|
||||
<vstab x="-15.0" y="2.5" z="-0.9" taper="0.7" effectiveness="2"
|
||||
length="2.8" chord="2.0" sweep="0.0">
|
||||
<stall aoa="16" width="5" peak="1.5"/>
|
||||
<flap0 start="0" end="1" lift="1.3" drag="1.3"/>
|
||||
<control-input axis="/controls/flight/rudder" control="FLAP0" invert="true"/>
|
||||
<control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm"/>
|
||||
</vstab>
|
||||
|
||||
<vstab x="-15.0" y="-2.5" z="-0.9" taper="0.7" effectiveness="2"
|
||||
length="2.8" chord="2.0" sweep="0.0">
|
||||
<stall aoa="16" width="5" peak="1.5"/>
|
||||
<flap0 start="0" end="1" lift="1.3" drag="1.3"/>
|
||||
<control-input axis="/controls/flight/rudder" control="FLAP0" invert="true"/>
|
||||
<control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm"/>
|
||||
</vstab>
|
||||
|
||||
<!-- Engines and tanks -->
|
||||
<jet x="-11.8" y="-1.5" z="1.0" mass="1000" thrust="9065">
|
||||
<control-input axis="/controls/engines/engine[0]/throttle" control="THROTTLE"/>
|
||||
</jet>
|
||||
|
||||
<jet x="-11.8" y="1.5" z="1.0" mass="1000" thrust="9065">
|
||||
<control-input axis="/controls/engines/engine[1]/throttle" control="THROTTLE"/>
|
||||
</jet>
|
||||
|
||||
<tank x="-8.5" y="-1.5" z="0.0" jet="true" capacity="2000"/>
|
||||
<tank x="-8.5" y="1.5" z="0.0" jet="true" capacity="2000"/>
|
||||
<tank x="-8.5" y="0" z="0.0" jet="true" capacity="6700"/>
|
||||
|
||||
<!-- Undercarriage -->
|
||||
<!-- nose -->
|
||||
<gear x="-2.9" y="0.4" z="-2.8" retract-time="7" compression="0.7">
|
||||
<control-input axis="/controls/flight/rudder" control="STEER" square="true"/>
|
||||
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
|
||||
<control-speed control="EXTEND" transition-time="7"/>
|
||||
<control-output control="EXTEND" prop="/gear/gear/position-norm"/>
|
||||
</gear>
|
||||
|
||||
<!-- left main -->
|
||||
<gear x="-9.0" y="2.5" z="-2.8" retract-time="7" compression="0.6">
|
||||
<control-input axis="/controls/gear/wheel[0]/brake" control="BRAKE"/>
|
||||
<control-input axis="/controls/gear/parking-brake" control="BRAKE"/>
|
||||
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
|
||||
<control-speed control="EXTEND" transition-time="7"/>
|
||||
<control-output control="EXTEND" prop="/gear/gear[0]/position-norm"/>
|
||||
</gear>
|
||||
|
||||
<!-- right main -->
|
||||
<gear x="-9.0" y="-2.5" z="-2.8" retract-time="7" compression="0.6">
|
||||
<control-input axis="/controls/gear/wheel[1]/brake" control="BRAKE"/>
|
||||
<control-input axis="/controls/gear/parking-brake" control="BRAKE"/>
|
||||
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
|
||||
<control-speed control="EXTEND" transition-time="7"/>
|
||||
<control-output control="EXTEND" prop="/gear/gear[1]/position-norm"/>
|
||||
</gear>
|
||||
|
||||
<!-- Canopy -->
|
||||
<gear x="-2.6" y="0.0" z="1.4" retract-time="7" compression="0.6">
|
||||
<control-input axis="/controls/gear/parking-brake" control="EXTEND"/>
|
||||
<control-speed control="EXTEND" transition-time="5"/>
|
||||
<control-output control="EXTEND" prop="/canopy/position-norm"/>
|
||||
</gear>
|
||||
|
||||
<!-- Ballast -->
|
||||
<ballast x="-3.5" y="0" z="1.0" mass="2000"/> <!-- Armored cockpit -->
|
||||
<ballast x="-4.0" y="0" z="-1.0" mass="4000"/> <!-- Gun -->
|
||||
<ballast x="-5.0" y="0" z="0.0" mass="1000"/> <!-- avionics -->
|
||||
|
||||
</airplane>
|
||||
|
|
@ -1,155 +0,0 @@
|
|||
<!-- A10 yasim config. This is a hack and not an authentic
|
||||
representation of the aircraft. Having said that, the
|
||||
numbers, where I could find them, roughly match those of
|
||||
the original aircraft.
|
||||
Lee Elliott. leee-fgfs@spatial.freeserve.co.uk
|
||||
-->
|
||||
|
||||
<airplane mass="37700">
|
||||
|
||||
<!-- Approach configuration -->
|
||||
<approach speed="110" aoa="8">
|
||||
<control-setting axis="/controls/engines/engine[0]/throttle" value="0.5"/>
|
||||
<control-setting axis="/controls/engines/engine[1]/throttle" value="0.5"/>
|
||||
<control-setting axis="/controls/flight/flaps" value="1.0"/>
|
||||
<control-setting axis="/controls/gear/gear-down" value="1"/>
|
||||
</approach>
|
||||
|
||||
<!-- Cruise configuration -->
|
||||
<cruise speed="380" alt="0">
|
||||
<control-setting axis="/controls/engines/engine[0]/throttle" value="1.0"/>
|
||||
<control-setting axis="/controls/engines/engine[1]/throttle" value="1.0"/>
|
||||
<control-setting axis="/controls/flight/flaps" value="0.0"/>
|
||||
<control-setting axis="/controls/gear/gear-down" value="0"/>
|
||||
</cruise>
|
||||
|
||||
<cockpit x="4.5" y="0.0" z="1.2"/>
|
||||
|
||||
<fuselage ax="8" ay="0" az="0" bx="-8.26" by="0" bz="0"
|
||||
width="1.4"/>
|
||||
|
||||
<!-- Left Engine -->
|
||||
<fuselage ax="-2" ay="1.50" az="1" bx="-5.5" by="1.50" bz="0.8"
|
||||
width="1.5"/>
|
||||
|
||||
<!-- Right Engine -->
|
||||
<fuselage ax="-2" ay="-1.50" az="1" bx="-5.5" by="-1.50" bz="0.8"
|
||||
width="1.5"/>
|
||||
|
||||
<wing x="-0.8" y="0.5" z="-0.5" taper="0.6" incidence="-1.0"
|
||||
length="8.3" chord="3.1" sweep="0.0" dihedral="3.0" camber="0.006">
|
||||
<stall aoa="17" width="6" peak="1.3"/>
|
||||
<flap0 start="0.04" end="0.51" lift="1.5" drag="1.2"/>
|
||||
<flap1 start="0.54" end="0.86" lift="1.3" drag="1.2"/>
|
||||
<spoiler start="0.54" end="0.86" lift="0.1" drag="20.0"/>
|
||||
|
||||
<control-input axis="/controls/flight/flaps" control="FLAP0"/>
|
||||
<control-input axis="/controls/flight/aileron" control="FLAP1" split="true"/>
|
||||
<control-input axis="/controls/flight/aileron-trim" control="FLAP1" split="true"/>
|
||||
<control-input axis="/controls/flight/spoilers" control="SPOILER"/>
|
||||
|
||||
<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-output control="SPOILER" side="left"
|
||||
prop="/surface-positions/left-spoiler-pos-norm"/>
|
||||
<control-output control="SPOILER" side="right"
|
||||
prop="/surface-positions/right-spoiler-pos-norm"/>
|
||||
|
||||
<control-speed control="FLAP0" transition-time="5"/>
|
||||
<control-speed control="SPOILER" transition-time="0.5"/>
|
||||
|
||||
</wing>
|
||||
|
||||
<hstab x="-7.5" y="0.4" z="0.4" taper="0.0" effectiveness="3"
|
||||
length="2.5" chord="2" sweep="0.0" dihedral="0.0" camber="0">
|
||||
<stall aoa="18" width="5" peak="1.5"/>
|
||||
<flap0 start="0" end="1" lift="1.5" drag="1.2"/>
|
||||
<control-input axis="/controls/flight/elevator" control="FLAP0"/>
|
||||
<control-input axis="/controls/flight/elevator-trim" control="FLAP0"/>
|
||||
<control-output control="FLAP0" prop="/surface-positions/elevator-pos-norm"/>
|
||||
</hstab>
|
||||
|
||||
<vstab x="-7.0" y="2.5" z="-0.9" taper="0.7" effectiveness="2"
|
||||
length="2.8" chord="2.0" sweep="0.0">
|
||||
<stall aoa="16" width="5" peak="1.5"/>
|
||||
<flap0 start="0" end="1" lift="1.3" drag="1.3"/>
|
||||
<control-input axis="/controls/flight/rudder" control="FLAP0" invert="true"/>
|
||||
<control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm"/>
|
||||
</vstab>
|
||||
|
||||
<vstab x="-7.0" y="-2.5" z="-0.9" taper="0.7" effectiveness="2"
|
||||
length="2.8" chord="2.0" sweep="0.0">
|
||||
<stall aoa="16" width="5" peak="1.5"/>
|
||||
<flap0 start="0" end="1" lift="1.3" drag="1.3"/>
|
||||
<control-input axis="/controls/flight/rudder" control="FLAP0" invert="true"/>
|
||||
<control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm"/>
|
||||
</vstab>
|
||||
|
||||
<!-- Engines and tanks -->
|
||||
<jet x="-3.8" y="-1.5" z="1.0" mass="1000" thrust="9065">
|
||||
<control-input axis="/controls/engines/engine[0]/throttle" control="THROTTLE"/>
|
||||
</jet>
|
||||
|
||||
<jet x="-3.8" y="1.5" z="1.0" mass="1000" thrust="9065">
|
||||
<control-input axis="/controls/engines/engine[1]/throttle" control="THROTTLE"/>
|
||||
</jet>
|
||||
|
||||
<tank x="-0.5" y="-1.5" z="0.0" jet="true" capacity="2000"/>
|
||||
<tank x="-0.5" y="1.5" z="0.0" jet="true" capacity="2000"/>
|
||||
<tank x="-0.5" y="0" z="0.0" jet="true" capacity="6700"/>
|
||||
<!-- Ferry Tanks -->
|
||||
<tank x="-0.5" y="1.29" z="-0.7" jet="true" capacity="4032"/>
|
||||
<tank x="-0.5" y="0" z="-0.7" jet="true" capacity="4032"/>
|
||||
<tank x="-0.5" y="-1.29" z="-0.7" jet="true" capacity="4032"/>
|
||||
|
||||
<!-- Undercarriage -->
|
||||
<!-- nose -->
|
||||
<gear x="5.1" y="0.4" z="-2.8" retract-time="7" compression="0.7">
|
||||
<control-input axis="/controls/flight/rudder" control="STEER" square="true"/>
|
||||
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
|
||||
<control-speed control="EXTEND" transition-time="7"/>
|
||||
<control-output control="EXTEND" prop="/gear/gear/position-norm"/>
|
||||
</gear>
|
||||
|
||||
<!-- left main -->
|
||||
<gear x="-1.0" y="2.5" z="-2.8" retract-time="7" compression="0.6">
|
||||
<control-input axis="/controls/gear/wheel[0]/brake" control="BRAKE"/>
|
||||
<control-input axis="/controls/gear/parking-brake" control="BRAKE"/>
|
||||
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
|
||||
<control-speed control="EXTEND" transition-time="7"/>
|
||||
<control-output control="EXTEND" prop="/gear/gear[0]/position-norm"/>
|
||||
</gear>
|
||||
|
||||
<!-- right main -->
|
||||
<gear x="-1.0" y="-2.5" z="-2.8" retract-time="7" compression="0.6">
|
||||
<control-input axis="/controls/gear/wheel[1]/brake" control="BRAKE"/>
|
||||
<control-input axis="/controls/gear/parking-brake" control="BRAKE"/>
|
||||
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
|
||||
<control-speed control="EXTEND" transition-time="7"/>
|
||||
<control-output control="EXTEND" prop="/gear/gear[1]/position-norm"/>
|
||||
</gear>
|
||||
|
||||
<!-- Canopy -->
|
||||
<gear x="5.4" y="0.0" z="1.4" retract-time="7" compression="0.6">
|
||||
<control-input axis="/controls/gear/parking-brake" control="EXTEND"/>
|
||||
<control-speed control="EXTEND" transition-time="5"/>
|
||||
<control-output control="EXTEND" prop="/canopy/position-norm"/>
|
||||
</gear>
|
||||
|
||||
<!-- Ballast -->
|
||||
<ballast x="4.5" y="0" z="1.0" mass="2000"/> <!-- Armored cockpit -->
|
||||
<ballast x="4.0" y="0" z="-1.0" mass="4000"/> <!-- Gun -->
|
||||
<ballast x="3.0" y="0" z="0.0" mass="1000"/> <!-- avionics -->
|
||||
|
||||
<!-- Ferry Tanks -->
|
||||
<fuselage ax="1.1" ay="0.0" az="-1.2" bx="-2.9" by="0.0" bz="-1.2"
|
||||
width="0.8"/>
|
||||
<fuselage ax="1.1" ay="1.29" az="-1.2" bx="-2.9" by="1.29" bz="-1.2"
|
||||
width="0.8"/>
|
||||
<fuselage ax="1.1" ay="-1.29" az="-1.2" bx="-2.9" by="-1.29" bz="-1.2"
|
||||
width="0.8"/>
|
||||
|
||||
</airplane>
|
||||
|
|
@ -1,223 +0,0 @@
|
|||
<!-- A10 yasim config. This is a hack and not an authentic
|
||||
representation of the aircraft. Having said that, the
|
||||
numbers, where I could find them, roughly match those of
|
||||
the original aircraft.
|
||||
Lee Elliott. leee-fgfs@spatial.freeserve.co.uk
|
||||
-->
|
||||
|
||||
<airplane mass="45860">
|
||||
|
||||
<!-- Approach configuration -->
|
||||
<approach speed="110" aoa="8">
|
||||
<control-setting axis="/controls/engines/engine[0]/throttle" value="0.5"/>
|
||||
<control-setting axis="/controls/engines/engine[1]/throttle" value="0.5"/>
|
||||
<control-setting axis="/controls/flight/flaps" value="1.0"/>
|
||||
<control-setting axis="/controls/gear/gear-down" value="1"/>
|
||||
</approach>
|
||||
|
||||
<!-- Cruise configuration -->
|
||||
<cruise speed="380" alt="0">
|
||||
<control-setting axis="/controls/engines/engine[0]/throttle" value="1.0"/>
|
||||
<control-setting axis="/controls/engines/engine[1]/throttle" value="1.0"/>
|
||||
<control-setting axis="/controls/flight/flaps" value="0.0"/>
|
||||
<control-setting axis="/controls/gear/gear-down" value="0"/>
|
||||
</cruise>
|
||||
|
||||
<cockpit x="-3.5" y="0.0" z="1.2"/>
|
||||
|
||||
<fuselage ax="0" ay="0" az="0" bx="-16.26" by="0" bz="0"
|
||||
width="1.4"/>
|
||||
|
||||
<!-- Left Engine -->
|
||||
<fuselage ax="-10" ay="1.50" az="1" bx="-13.5" by="1.50" bz="0.8"
|
||||
width="1.5"/>
|
||||
|
||||
<!-- Right Engine -->
|
||||
<fuselage ax="-10" ay="-1.50" az="1" bx="-13.5" by="-1.50" bz="0.8"
|
||||
width="1.5"/>
|
||||
|
||||
<wing x="-8.8" y="0.5" z="-0.5" taper="0.6" incidence="-1.0"
|
||||
length="8.3" chord="3.1" sweep="0.0" dihedral="3.0" camber="0.006">
|
||||
<stall aoa="17" width="6" peak="1.3"/>
|
||||
<flap0 start="0.04" end="0.51" lift="1.5" drag="1.2"/>
|
||||
<flap1 start="0.54" end="0.86" lift="1.3" drag="1.2"/>
|
||||
<spoiler start="0.54" end="0.86" lift="0.1" drag="20.0"/>
|
||||
|
||||
<control-input axis="/controls/flight/flaps" control="FLAP0"/>
|
||||
<control-input axis="/controls/flight/aileron" control="FLAP1" split="true"/>
|
||||
<control-input axis="/controls/flight/aileron-trim" control="FLAP1" split="true"/>
|
||||
<control-input axis="/controls/flight/spoilers" control="SPOILER"/>
|
||||
|
||||
<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-output control="SPOILER" side="left"
|
||||
prop="/surface-positions/left-spoiler-pos-norm"/>
|
||||
<control-output control="SPOILER" side="right"
|
||||
prop="/surface-positions/right-spoiler-pos-norm"/>
|
||||
|
||||
<control-speed control="FLAP0" transition-time="5"/>
|
||||
<control-speed control="SPOILER" transition-time="0.5"/>
|
||||
|
||||
</wing>
|
||||
|
||||
<hstab x="-15.5" y="0.4" z="0.4" taper="0.0" effectiveness="3"
|
||||
length="2.5" chord="2" sweep="0.0" dihedral="0.0" camber="0">
|
||||
<stall aoa="18" width="5" peak="1.5"/>
|
||||
<flap0 start="0" end="1" lift="1.5" drag="1.2"/>
|
||||
<control-input axis="/controls/flight/elevator" control="FLAP0"/>
|
||||
<control-input axis="/controls/flight/elevator-trim" control="FLAP0"/>
|
||||
<control-output control="FLAP0" prop="/surface-positions/elevator-pos-norm"/>
|
||||
</hstab>
|
||||
|
||||
<vstab x="-15.0" y="2.5" z="-0.9" taper="0.7" effectiveness="2"
|
||||
length="2.8" chord="2.0" sweep="0.0">
|
||||
<stall aoa="16" width="5" peak="1.5"/>
|
||||
<flap0 start="0" end="1" lift="1.3" drag="1.3"/>
|
||||
<control-input axis="/controls/flight/rudder" control="FLAP0" invert="true"/>
|
||||
<control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm"/>
|
||||
</vstab>
|
||||
|
||||
<vstab x="-15.0" y="-2.5" z="-0.9" taper="0.7" effectiveness="2"
|
||||
length="2.8" chord="2.0" sweep="0.0">
|
||||
<stall aoa="16" width="5" peak="1.5"/>
|
||||
<flap0 start="0" end="1" lift="1.3" drag="1.3"/>
|
||||
<control-input axis="/controls/flight/rudder" control="FLAP0" invert="true"/>
|
||||
<control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm"/>
|
||||
</vstab>
|
||||
|
||||
<!-- Engines and tanks -->
|
||||
<jet x="-11.8" y="-1.5" z="1.0" mass="1000" thrust="9065">
|
||||
<control-input axis="/controls/engines/engine[0]/throttle" control="THROTTLE"/>
|
||||
</jet>
|
||||
|
||||
<jet x="-11.8" y="1.5" z="1.0" mass="1000" thrust="9065">
|
||||
<control-input axis="/controls/engines/engine[1]/throttle" control="THROTTLE"/>
|
||||
</jet>
|
||||
|
||||
<tank x="-8.5" y="-1.5" z="0.0" jet="true" capacity="2000"/>
|
||||
<tank x="-8.5" y="1.5" z="0.0" jet="true" capacity="2000"/>
|
||||
<tank x="-8.5" y="0" z="0.0" jet="true" capacity="6700"/>
|
||||
|
||||
<!-- Undercarriage -->
|
||||
<!-- nose -->
|
||||
<gear x="-2.9" y="0.4" z="-2.8" retract-time="7" compression="0.8">
|
||||
<control-input axis="/controls/flight/rudder" control="STEER" square="true"/>
|
||||
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
|
||||
<control-speed control="EXTEND" transition-time="7"/>
|
||||
<control-output control="EXTEND" prop="/gear/gear/position-norm"/>
|
||||
</gear>
|
||||
|
||||
<!-- left main -->
|
||||
<gear x="-9.0" y="2.5" z="-2.8" retract-time="7" compression="0.6">
|
||||
<control-input axis="/controls/gear/wheel[0]/brake" control="BRAKE"/>
|
||||
<control-input axis="/controls/gear/parking-brake" control="BRAKE"/>
|
||||
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
|
||||
<control-speed control="EXTEND" transition-time="7"/>
|
||||
<control-output control="EXTEND" prop="/gear/gear[0]/position-norm"/>
|
||||
</gear>
|
||||
|
||||
<!-- right main -->
|
||||
<gear x="-9.0" y="-2.5" z="-2.8" retract-time="7" compression="0.6">
|
||||
<control-input axis="/controls/gear/wheel[1]/brake" control="BRAKE"/>
|
||||
<control-input axis="/controls/gear/parking-brake" control="BRAKE"/>
|
||||
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
|
||||
<control-speed control="EXTEND" transition-time="7"/>
|
||||
<control-output control="EXTEND" prop="/gear/gear[1]/position-norm"/>
|
||||
</gear>
|
||||
|
||||
<!-- Canopy -->
|
||||
<gear x="-2.6" y="0.0" z="1.4" retract-time="7" compression="0.6">
|
||||
<control-input axis="/controls/gear/parking-brake" control="EXTEND"/>
|
||||
<control-speed control="EXTEND" transition-time="5"/>
|
||||
<control-output control="EXTEND" prop="/canopy/position-norm"/>
|
||||
</gear>
|
||||
|
||||
<!-- Ballast -->
|
||||
<ballast x="-3.5" y="0" z="1.0" mass="2000"/> <!-- C/pit + Pilot -->
|
||||
<ballast x="-4.0" y="0" z="-1.0" mass="4000"/> <!-- Gun -->
|
||||
<ballast x="-5.0" y="0" z="0.0" mass="1000"/> <!-- avionics -->
|
||||
|
||||
<!-- Weapons load -->
|
||||
|
||||
<!-- AGM65 x 16 objects and ballast (Left to Right) -->
|
||||
<!-- Positioned just ahead of the aircraft CG (x) - y and z locs approximate -->
|
||||
|
||||
<!-- Left Wing Outer AGM65 -->
|
||||
<fuselage ax="-7.65" ay="4.71" az="-0.47" bx="-10.15" by="4.71" bz="-0.35" width="0.35"/>
|
||||
<ballast x="-8.9" y="4.71" z="-0.41" mass="485"/>
|
||||
|
||||
<!-- Left Wing Mid Cluster Outer AGM65 -->
|
||||
<fuselage ax="-7.65" ay="3.89" az="-0.53" bx="-10.15" by="3.89" bz="-0.41" width="0.35"/>
|
||||
<ballast x="-8.9" y="3.89" z="-0.47" mass="485"/>
|
||||
|
||||
<!-- Left Wing Mid Cluster Mid AGM65 -->
|
||||
<fuselage ax="-7.65" ay="3.59" az="-0.96" bx="-10.15" by="3.59" bz="-0.84" width="0.35"/>
|
||||
<ballast x="-8.9" y="3.89" z="-0.90" mass="485"/>
|
||||
|
||||
<!-- Left Wing Mid Cluster Inner AGM65 -->
|
||||
<fuselage ax="-7.65" ay="3.21" az="-0.59" bx="-10.15" by="3.21" bz="-0.47" width="0.35"/>
|
||||
<ballast x="-8.9" y="3.21" z="-0.53" mass="485"/>
|
||||
|
||||
<!-- Left Wing Inner Cluster Outer AGM65 -->
|
||||
<fuselage ax="-7.65" ay="1.97" az="-0.65" bx="-10.15" by="1.97" bz="-0.53" width="0.35"/>
|
||||
<ballast x="-8.9" y="1.97" z="-0.59" mass="485"/>
|
||||
|
||||
<!-- Left Wing Inner Cluster Mid AGM65 -->
|
||||
<fuselage ax="-7.65" ay="1.63" az="-1.05" bx="-10.15" by="1.63" bz="-0.93" width="0.35"/>
|
||||
<ballast x="-8.9" y="1.63" z="-0.99" mass="485"/>
|
||||
|
||||
<!-- Left Wing Inner Cluster Inner AGM65 -->
|
||||
<fuselage ax="-7.65" ay="1.29" az="-0.65" bx="-10.15" by="1.29" bz="-0.53" width="0.35"/>
|
||||
<ballast x="-8.9" y="1.29" z="-0.59" mass="485"/>
|
||||
|
||||
<!-- Left Fuselage AGM65 -->
|
||||
<fuselage ax="-7.65" ay="0.53" az="-0.70" bx="-10.15" by="0.53" bz="-0.58" width="0.35"/>
|
||||
<ballast x="-8.9" y="0.53" z="-0.64" mass="485"/>
|
||||
|
||||
<!-- Right Wing Outer AGM65 -->
|
||||
<fuselage ax="-7.65" ay="-4.71" az="-0.47" bx="-10.15" by="-4.71" bz="-0.35" width="0.35"/>
|
||||
<ballast x="-8.9" y="-4.71" z="-0.41" mass="485"/>
|
||||
|
||||
<!-- Right Wing Mid Cluster Outer AGM65 -->
|
||||
<fuselage ax="-7.65" ay="-3.89" az="-0.53" bx="-10.15" by="-3.89" bz="-0.41" width="0.35"/>
|
||||
<ballast x="-8.9" y="-3.89" z="-0.47" mass="485"/>
|
||||
|
||||
<!-- Right Wing Mid Cluster Mid AGM65 -->
|
||||
<fuselage ax="-7.65" ay="-3.59" az="-0.96" bx="-10.15" by="-3.59" bz="-0.84" width="0.35"/>
|
||||
<ballast x="-8.9" y="-3.89" z="-0.90" mass="485"/>
|
||||
|
||||
<!-- Right Wing Mid Cluster Inner AGM65 -->
|
||||
<fuselage ax="-7.65" ay="-3.21" az="-0.59" bx="-10.15" by="-3.21" bz="-0.47" width="0.35"/>
|
||||
<ballast x="-8.9" y="-3.21" z="-0.53" mass="485"/>
|
||||
|
||||
<!-- Right Wing Inner Cluster Outer AGM65 -->
|
||||
<fuselage ax="-7.65" ay="-1.97" az="-0.65" bx="-10.15" by="-1.97" bz="-0.53" width="0.35"/>
|
||||
<ballast x="-8.9" y="-1.97" z="-0.59" mass="485"/>
|
||||
|
||||
<!-- Right Wing Inner Cluster Mid AGM65 -->
|
||||
<fuselage ax="-7.65" ay="-1.63" az="-1.05" bx="-10.15" by="-1.63" bz="-0.93" width="0.35"/>
|
||||
<ballast x="-8.9" y="-1.63" z="-0.99" mass="485"/>
|
||||
|
||||
<!-- Right Wing Inner Cluster Inner AGM65 -->
|
||||
<fuselage ax="-7.65" ay="-1.29" az="-0.65" bx="-10.15" by="-1.29" bz="-0.53" width="0.35"/>
|
||||
<ballast x="-8.9" y="-1.29" z="-0.59" mass="485"/>
|
||||
|
||||
<!-- Right Fuselage AGM65 -->
|
||||
<fuselage ax="-7.65" ay="-0.53" az="-0.70" bx="-10.15" by="-0.53" bz="-0.58" width="0.35"/>
|
||||
<ballast x="-8.9" y="-0.53" z="-0.64" mass="485"/>
|
||||
|
||||
<!-- AIM9 x 2 objects and ballast (guessed) - (Left to Right) -->
|
||||
<!-- Positioned ahead of the aircraft CG (x) - y and z locs approximate -->
|
||||
|
||||
<!-- Left Wing AIM9 -->
|
||||
<fuselage ax="-6.9" ay="5.76" az="-0.27" bx="-9.9" by="5.76" bz="-0.15" width="0.13"/>
|
||||
<ballast x="-8.9" y="5.76" z="-0.21" mass="200"/>
|
||||
|
||||
<!-- Right Wing AIM9 -->
|
||||
<fuselage ax="-6.9" ay="-5.76" az="-0.27" bx="-9.9" by="-5.76" bz="-0.15" width="0.13"/>
|
||||
<ballast x="-8.9" y="-5.76" z="-0.21" mass="200"/>
|
||||
|
||||
</airplane>
|
||||
|
|
@ -1,122 +0,0 @@
|
|||
<airplane mass="9853">
|
||||
|
||||
<!-- Approach configuration -->
|
||||
<approach speed="130" aoa="13.5">
|
||||
<control-setting axis="/controls/engines/engine[0]/throttle" value="0.2"/>
|
||||
<control-setting axis="/controls/flight/flaps" value="1.0"/>
|
||||
<control-setting axis="/controls/gear/gear-down" value="1"/>
|
||||
</approach>
|
||||
|
||||
<!-- Cruise configuration. This number is for an A-4F (595mph/FL340) -->
|
||||
<cruise speed="585" alt="34000">
|
||||
<control-setting axis="/controls/engines/engine[0]/throttle" value="0.8"/>
|
||||
<control-setting axis="/controls/flight/flaps" value="0.0"/>
|
||||
<control-setting axis="/controls/gear/gear-down" value="0"/>
|
||||
</cruise>
|
||||
|
||||
<cockpit x="2.71" y="0.0" z="0.67"/>
|
||||
|
||||
<fuselage ax="5.61" ay="0" az="-0.66" bx="-6.59" by="0" bz=".64"
|
||||
width="2.0" taper="0.5" midpoint="0.3"/>
|
||||
|
||||
<wing x="-0.79" y=".55" z="-0.33" taper=".186"
|
||||
length="4.04" chord="3.95" sweep="28" dihedral="0" camber="0.02">
|
||||
<stall aoa="27" width="10" peak="1.3"/>
|
||||
<flap0 start="0.0" end="0.5" lift="1.3" drag="1.2"/>
|
||||
<flap1 start="0.5" end="1.0" lift="1.2" drag="1.2"/>
|
||||
<control-input axis="/controls/flight/flaps" control="FLAP0"/>
|
||||
<control-input axis="/controls/flight/aileron" control="FLAP1" split="true"/>
|
||||
<control-input axis="/controls/flight/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="-5.4" y="0" z="1.05" taper=".3" effectiveness="1.99"
|
||||
length="2.02" chord="2.02" sweep="26">
|
||||
<stall aoa="27" width="10" peak="1.5"/>
|
||||
<flap0 start="0" end="1" lift="1.6" drag="1.2"/>
|
||||
<control-input axis="/controls/flight/elevator" control="FLAP0"/>
|
||||
<control-input axis="/controls/flight/elevator-trim" control="FLAP0"/>
|
||||
<control-output control="FLAP0" prop="/surface-positions/elevator-pos-norm"/>
|
||||
</hstab>
|
||||
|
||||
<vstab x="-5.4" y="0" z="1.05" taper=".176"
|
||||
length="2.57" chord="3.11" sweep="28" effectiveness="1.5">
|
||||
<stall aoa="27" width="10" peak="1.5"/>
|
||||
<flap0 start="0" end="1" lift="1.15" drag="1.2"/>
|
||||
<control-input axis="/controls/flight/rudder" control="FLAP0" invert="true"/>
|
||||
<control-input axis="/controls/flight/rudder-trim" control="FLAP0" invert="true"/>
|
||||
<control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm"
|
||||
min="1" max="-1"/>
|
||||
</vstab>
|
||||
|
||||
<!-- P&W J52-P-6A turbojet, 8500 lbs sea level thrust -->
|
||||
<jet x="0.61" y="0" z="0.11" mass="1800" thrust="8500" n1-max="106"
|
||||
exhaust-speed="2000">
|
||||
<control-input axis="/controls/engines/engine[0]/throttle" control="THROTTLE"/>
|
||||
</jet>
|
||||
|
||||
<!-- nose -->
|
||||
<gear x="3.32" y="0" z="-2.26" retract-time="7" compression=".96">
|
||||
<control-input axis="/controls/flight/rudder" control="STEER" square="true"
|
||||
src0="-1" src1="1" dst0="-0.9" dst1="0.9"/>
|
||||
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
|
||||
<control-output control="EXTEND" prop="/gear/gear[0]/position-norm"/>
|
||||
<control-speed control="EXTEND" transition-time="7"/>
|
||||
</gear>
|
||||
|
||||
<!-- left main -->
|
||||
<gear x="-1.39" y="1.19" z="-1.89" retract-time="7" compression=".78"
|
||||
damp="2">
|
||||
<control-input axis="/controls/gear/wheel[0]/brake" control="BRAKE"/>
|
||||
<control-input axis="/controls/gear/parking-brake" control="BRAKE"/>
|
||||
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
|
||||
<control-output control="EXTEND" prop="/gear/gear[1]/position-norm"/>
|
||||
<control-speed control="EXTEND" transition-time="7"/>
|
||||
<control-speed control="BRAKE" transition-time="2"/>
|
||||
</gear>
|
||||
|
||||
<!-- right main -->
|
||||
<gear x="-1.39" y="-1.19" z="-1.89" retract-time="7" compression=".78"
|
||||
damp="2">
|
||||
<control-input axis="/controls/gear/wheel[1]/brake" control="BRAKE"/>
|
||||
<control-input axis="/controls/gear/parking-brake" control="BRAKE"/>
|
||||
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
|
||||
<control-output control="EXTEND" prop="/gear/gear[2]/position-norm"/>
|
||||
<control-speed control="EXTEND" transition-time="7"/>
|
||||
<control-speed control="BRAKE" transition-time="2"/>
|
||||
</gear>
|
||||
|
||||
<!-- A4-M had 800 gallons of in-fuselage fuel capacity in three tanks,
|
||||
one in each wing and one behind the cockpit. TA-4F had "only" 100
|
||||
gallons in the fuselage due to the second seat, so the wings must
|
||||
have 0-350 gallons each. Call the tanks 260/280/260 gallons, and
|
||||
use 6.72 lbs/gal for Jet-A fuel. BUT: this is an A-4E, which had
|
||||
770 gallons. Figure that the extra 30 all went into an expanded
|
||||
center tank underneath the new "hump" in the fuselage. -->
|
||||
<tank x="0.11" y="0" z="0.17" jet="true" capacity="1678"/>
|
||||
<tank x="-0.39" y="1" z="-0.33" jet="true" capacity="1750"/>
|
||||
<tank x="-0.39" y="-1" z="-0.33" jet="true" capacity="1750"/>
|
||||
|
||||
<ballast x="4.11" y="0" z="0.67" mass="450"/> <!-- cockpit -->
|
||||
<ballast x="2.61" y="0" z="0.67" mass="450"/> <!-- cockpit -->
|
||||
|
||||
<!-- The early A-4's had five pylons. One 3500lbs center for a tank,
|
||||
two inboard pylons holding 2250lbs, and two 1000lbs outboard
|
||||
pylons. -->
|
||||
<weight x="-0.39" y="0" z="-1.33" size="1.5"
|
||||
mass-prop="/yasim/a4/weights/center-lbs"/>
|
||||
<weight x="-0.79" y="2" z="-1.33" size="1"
|
||||
mass-prop="/yasim/a4/weights/left-inboard-lbs"/>
|
||||
<weight x="-0.79" y="-2" z="-1.33" size="1"
|
||||
mass-prop="/yasim/a4/weights/right-inboard-lbs"/>
|
||||
<weight x="-1.39" y="3" z="-1.33" size="1"
|
||||
mass-prop="/yasim/a4/weights/left-outboard-lbs"/>
|
||||
<weight x="-1.39" y="-3" z="-1.33" size="1"
|
||||
mass-prop="/yasim/a4/weights/right-outboard-lbs"/>
|
||||
|
||||
</airplane>
|
||||
|
|
@ -1,289 +0,0 @@
|
|||
<!-- B52-F yasim config.
|
||||
|
||||
Notes.
|
||||
|
||||
B-52F with full fuel load, no weapon load.
|
||||
|
||||
This config cannot be regarded as an accurate representation
|
||||
of a B-52F. I've used the real numbers, where I've been able
|
||||
to find them, but a lot of this config is semi-educated
|
||||
guesswork. I think all the bits are in the right places but
|
||||
many of the numbers were obtained either by measuring a h/c
|
||||
of the 3-view I used as a template for modelling or by reading
|
||||
them out of my 3d modeller.
|
||||
|
||||
The B52s had all moving tailplanes (9 deg up & 4 deg down) and
|
||||
these cannot be represented correctly using yasim at the moment,
|
||||
so in that respect this config is definitely a hack.
|
||||
|
||||
Lee Elliott. leee-fgfs@spatial.freeserve.co.uk
|
||||
-->
|
||||
|
||||
<airplane mass="173599">
|
||||
|
||||
<!-- Approach configuration -->
|
||||
<approach speed="100" aoa="1.0">
|
||||
<control-setting axis="/controls/engines/engine[0]/throttle" value="0.4"/>
|
||||
<control-setting axis="/controls/engines/engine[1]/throttle" value="0.4"/>
|
||||
<control-setting axis="/controls/engines/engine[2]/throttle" value="0.4"/>
|
||||
<control-setting axis="/controls/engines/engine[3]/throttle" value="0.4"/>
|
||||
<control-setting axis="/controls/engines/engine[4]/throttle" value="0.4"/>
|
||||
<control-setting axis="/controls/engines/engine[5]/throttle" value="0.4"/>
|
||||
<control-setting axis="/controls/engines/engine[6]/throttle" value="0.4"/>
|
||||
<control-setting axis="/controls/engines/engine[7]/throttle" value="0.4"/>
|
||||
<control-setting axis="/controls/engines/engine[0]/afterburner" value="0.0"/>
|
||||
<control-setting axis="/controls/engines/engine[1]/afterburner" value="0.0"/>
|
||||
<control-setting axis="/controls/engines/engine[2]/afterburner" value="0.0"/>
|
||||
<control-setting axis="/controls/engines/engine[3]/afterburner" value="0.0"/>
|
||||
<control-setting axis="/controls/engines/engine[4]/afterburner" value="0.0"/>
|
||||
<control-setting axis="/controls/engines/engine[5]/afterburner" value="0.0"/>
|
||||
<control-setting axis="/controls/engines/engine[6]/afterburner" value="0.0"/>
|
||||
<control-setting axis="/controls/engines/engine[7]/afterburner" value="0.0"/>
|
||||
<control-setting axis="/controls/flight/flaps" value="1.0"/>
|
||||
<control-setting axis="/controls/flight/spoilers" value="0.0"/>
|
||||
<control-setting axis="/controls/gear/gear-down" value="1"/>
|
||||
</approach>
|
||||
|
||||
<!-- Cruise configuration -->
|
||||
<!-- I found the following performance figures
|
||||
638 mph (554 kt) @ 21000 ft
|
||||
570 mph (495 kt) @ 46500 ft
|
||||
523 mph (454 kt) cruising speed (no alt specified)
|
||||
|
||||
The service ceiling at combat weight (291570 lbs) is 46700 ft and I
|
||||
assume that's at the cruise speed (454 kt)
|
||||
|
||||
I've not been able to get a solution that solves using 495 kt @ 46500 ft
|
||||
and using the figure of 554 kt @ 21000 ft results in the a/c not being
|
||||
able to climb nearly high enough so the numbers specified are currently
|
||||
the best compromise I've found so far.
|
||||
-->
|
||||
<cruise speed="554" alt="21000">
|
||||
<control-setting axis="/controls/engines/engine[0]/throttle" value="0.6"/>
|
||||
<control-setting axis="/controls/engines/engine[1]/throttle" value="0.6"/>
|
||||
<control-setting axis="/controls/engines/engine[2]/throttle" value="0.6"/>
|
||||
<control-setting axis="/controls/engines/engine[3]/throttle" value="0.6"/>
|
||||
<control-setting axis="/controls/engines/engine[4]/throttle" value="0.6"/>
|
||||
<control-setting axis="/controls/engines/engine[5]/throttle" value="0.6"/>
|
||||
<control-setting axis="/controls/engines/engine[6]/throttle" value="0.6"/>
|
||||
<control-setting axis="/controls/engines/engine[7]/throttle" value="0.6"/>
|
||||
<control-setting axis="/controls/engines/engine[0]/afterburner" value="0.0"/>
|
||||
<control-setting axis="/controls/engines/engine[1]/afterburner" value="0.0"/>
|
||||
<control-setting axis="/controls/engines/engine[2]/afterburner" value="0.0"/>
|
||||
<control-setting axis="/controls/engines/engine[3]/afterburner" value="0.0"/>
|
||||
<control-setting axis="/controls/engines/engine[4]/afterburner" value="0.0"/>
|
||||
<control-setting axis="/controls/engines/engine[5]/afterburner" value="0.0"/>
|
||||
<control-setting axis="/controls/engines/engine[6]/afterburner" value="0.0"/>
|
||||
<control-setting axis="/controls/engines/engine[7]/afterburner" value="0.0"/>
|
||||
<control-setting axis="/controls/flight/flaps" value="0.0"/>
|
||||
<control-setting axis="/controls/flight/spoilers" value="0.0"/>
|
||||
<control-setting axis="/controls/gear/gear-down" value="0"/>
|
||||
</cruise>
|
||||
|
||||
<cockpit x="-2.2" y="0.0" z="2.0"/>
|
||||
|
||||
<fuselage ax="0" ay="0" az="0" bx="-49.05" by="0" bz=".64"
|
||||
width="3.2" taper="0.5" midpoint="0.3"/>
|
||||
|
||||
<!-- Wing incidence was set at 6 degrees because the tandem u/c meant
|
||||
that the aircraft couldn't rotate in the conventional fashion. I
|
||||
found lots of references to the sweep angle of 35 degrees but
|
||||
none of them stated the chord point for it i.e. leading edge or
|
||||
quarter-chord. As yasim uses mid-chord I've subtracted 0.5 degree
|
||||
as a fudge factor.
|
||||
|
||||
Yasim also only allows for one [real] flap entry per wing so I've
|
||||
used a single spane but reduced it's length by the width of the
|
||||
aileron, which I've located outboard of the flaps.
|
||||
-->
|
||||
<wing x="-16.0" y="1.6" z="1.2" taper="0.4" incidence="6"
|
||||
length="31.1" chord="10.0" sweep="34.5" dihedral="-1.0" camber="0.16">
|
||||
<stall aoa="18.0" width="3" peak="1.3"/>
|
||||
<flap0 start="0.0" end="0.62" lift="1.45" drag="2.2"/>
|
||||
<flap1 start="0.62" end="0.7" lift="1.3" drag="1.3"/>
|
||||
<spoiler start="0.5" end="0.75" lift="0.0" drag="1.8"/>
|
||||
|
||||
<control-input axis="/controls/flight/flaps" control="FLAP0"/>
|
||||
<control-input axis="/controls/flight/aileron" control="FLAP1" split="true"/>
|
||||
<control-input axis="/controls/flight/spoilers" control="SPOILER"/>
|
||||
|
||||
<control-output control="FLAP0" side="left" prop="/surface-positions/left-flap-pos-norm"/>
|
||||
<control-output control="FLAP0" side="right" prop="/surface-positions/right-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-output control="SPOILER" side="left" prop="/surface-positions/left-spoiler-pos-norm"/>
|
||||
<control-output control="SPOILER" side="right" prop="/surface-positions/right-spoiler-pos-norm"/>
|
||||
|
||||
<control-speed control="FLAP0" transition-time="45"/>
|
||||
<control-speed control="FLAP1" transition-time="0.5"/>
|
||||
<control-speed control="SPOILER" transition-time="0.5"/>
|
||||
</wing>
|
||||
|
||||
<!-- The hstab/elevators are nearly deltas ao I've given them a high
|
||||
stall AoA figure.
|
||||
-->
|
||||
<hstab x="-41.5" y="1.0" z="0.8" taper="0.25" effectiveness="1.0"
|
||||
length="7.5" chord="7.5" sweep="40.0" dihedral="0.0" camber="0.01">
|
||||
<stall aoa="25.0" width="3" peak="1.5"/>
|
||||
<flap0 start="0" end="1" lift="1.3" drag="1.4"/>
|
||||
<control-input axis="/controls/flight/elevator" control="FLAP0"/>
|
||||
<control-input axis="/controls/flight/elevator-trim" control="FLAP0"/>
|
||||
<control-output control="FLAP0" prop="/surface-positions/elevator-pos-norm"/>
|
||||
<control-speed control="FLAP0" transition-time="0.5"/>
|
||||
</hstab>
|
||||
|
||||
<vstab x="-41.5" y="0" z="2.0" taper="0.4"
|
||||
length="8.5" chord="7.5" sweep="35.0">
|
||||
<stall aoa="20.0" width="3" peak="1.5"/>
|
||||
<flap0 start="0" end="1" lift="1.15" drag="1.3"/>
|
||||
<control-input axis="/controls/flight/rudder" control="FLAP0" invert="true"/>
|
||||
<control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm"/>
|
||||
</vstab>
|
||||
|
||||
<!-- Engine entries -->
|
||||
<!-- I've used the dry thrust rating of the J57-P-43WA turbojet (11200 lb)
|
||||
here instead of the wet-thrust (13500 lb). This will make take offs a
|
||||
little more sluggish but is about equivilent of a B-52B with wet-thrust.
|
||||
This model is a little heavier though.
|
||||
|
||||
I couldn't find a weight for the engines and have guessed at 4000lb
|
||||
-->
|
||||
<!-- Left wing engines -->
|
||||
<!-- Left Outer Left -->
|
||||
<jet x="-23.0" y="20.0" z="-1.0" mass="4000" tsfc="0.7" thrust="11200" afterburner="13500">
|
||||
<control-input axis="/controls/engines/engine[0]/throttle" control="THROTTLE"/>
|
||||
<control-input axis="/controls/engines/engine[0]/afterburner" control="REHEAT"/>
|
||||
</jet>
|
||||
|
||||
<!-- Left Outer Right -->
|
||||
<jet x="-23.0" y="18.0" z="-1.0" mass="4000" tsfc="0.7" thrust="11200" afterburner="13500">
|
||||
<control-input axis="/controls/engines/engine[1]/throttle" control="THROTTLE"/>
|
||||
<control-input axis="/controls/engines/engine[0]/afterburner" control="REHEAT"/>
|
||||
</jet>
|
||||
|
||||
<!-- Left Inner Left -->
|
||||
<jet x="-15.0" y="12.0" z="-1.0" mass="4000" tsfc="0.7" thrust="11200" afterburner="13500">
|
||||
<control-input axis="/controls/engines/engine[2]/throttle" control="THROTTLE"/>
|
||||
<control-input axis="/controls/engines/engine[0]/afterburner" control="REHEAT"/>
|
||||
</jet>
|
||||
|
||||
<!-- Left Inner Right -->
|
||||
<jet x="-15.0" y="10.0" z="-1.0" mass="4000" tsfc="0.7" thrust="11200" afterburner="13500">
|
||||
<control-input axis="/controls/engines/engine[3]/throttle" control="THROTTLE"/>
|
||||
<control-input axis="/controls/engines/engine[0]/afterburner" control="REHEAT"/>
|
||||
</jet>
|
||||
|
||||
<!-- Right wing engines -->
|
||||
<!-- Right Inner Left -->
|
||||
<jet x="-15.0" y="-10.0" z="-1.0" mass="4000" tsfc="0.7" thrust="11200" afterburner="13500">
|
||||
<control-input axis="/controls/engines/engine[4]/throttle" control="THROTTLE"/>
|
||||
<control-input axis="/controls/engines/engine[0]/afterburner" control="REHEAT"/>
|
||||
</jet>
|
||||
|
||||
<!-- Right Inner Right -->
|
||||
<jet x="-15.0" y="-12.0" z="-1.0" mass="4000" tsfc="0.7" thrust="11200" afterburner="13500">
|
||||
<control-input axis="/controls/engines/engine[5]/throttle" control="THROTTLE"/>
|
||||
<control-input axis="/controls/engines/engine[0]/afterburner" control="REHEAT"/>
|
||||
</jet>
|
||||
|
||||
<!-- Right Outer Left -->
|
||||
<jet x="-23.0" y="-18.0" z="-1.0" mass="4000" tsfc="0.7" thrust="11200" afterburner="13500">
|
||||
<control-input axis="/controls/engines/engine[6]/throttle" control="THROTTLE"/>
|
||||
<control-input axis="/controls/engines/engine[0]/afterburner" control="REHEAT"/>
|
||||
</jet>
|
||||
|
||||
<!-- Right Outer Right -->
|
||||
<jet x="-23.0" y="-20.0" z="-1.0" mass="4000" tsfc="0.7" thrust="11200" afterburner="13500">
|
||||
<control-input axis="/controls/engines/engine[7]/throttle" control="THROTTLE"/>
|
||||
<control-input axis="/controls/engines/engine[0]/afterburner" control="REHEAT"/>
|
||||
</jet>
|
||||
|
||||
<!-- Landing Gear -->
|
||||
<!-- Front Left -->
|
||||
<gear x="-13.2" y="2.0" z="-2.9" retract-time="7" compression="1.0">
|
||||
<control-input axis="/controls/flight/rudder" control="STEER" square="true"/>
|
||||
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
|
||||
<control-input axis="/controls/gear/gear[0]/wheel[0]/brake" control="BRAKE"/>
|
||||
<control-input axis="/controls/gear/gear[0]/wheel[1]/brake" control="BRAKE"/>
|
||||
<control-input axis="/controls/gear/parking-brake" control="BRAKE"/>
|
||||
<control-speed control="EXTEND" transition-time="7"/>
|
||||
<control-speed control="BRAKE" transition-time="0.7"/>
|
||||
<control-output control="EXTEND" prop="/gear/gear[0]/position-norm"/>
|
||||
</gear>
|
||||
|
||||
<!-- Front Right -->
|
||||
<gear x="-13.2" y="-2.0" z="-2.9" retract-time="7" compression="1.0">
|
||||
<control-input axis="/controls/flight/rudder" control="STEER" square="true"/>
|
||||
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
|
||||
<control-input axis="/controls/gear/gear[1]/wheel[0]/brake" control="BRAKE"/>
|
||||
<control-input axis="/controls/gear/gear[1]/wheel[1]/brake" control="BRAKE"/>
|
||||
<control-input axis="/controls/gear/parking-brake" control="BRAKE"/>
|
||||
<control-speed control="EXTEND" transition-time="7"/>
|
||||
<control-speed control="BRAKE" transition-time="0.7"/>
|
||||
<control-output control="EXTEND" prop="/gear/gear[1]/position-norm"/>
|
||||
</gear>
|
||||
|
||||
<!-- Rear Left -->
|
||||
<gear x="-28.0" y="2.0" z="-2.9" retract-time="7" compression="1.0">
|
||||
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
|
||||
<control-input axis="/controls/gear/gear[2]/wheel[0]/brake" control="BRAKE"/>
|
||||
<control-input axis="/controls/gear/gear[2]/wheel[1]/brake" control="BRAKE"/>
|
||||
<control-input axis="/controls/gear/parking-brake" control="BRAKE"/>
|
||||
<control-speed control="EXTEND" transition-time="7"/>
|
||||
<control-speed control="BRAKE" transition-time="0.7"/>
|
||||
<control-output control="EXTEND" prop="/gear/gear[2]/position-norm"/>
|
||||
</gear>
|
||||
|
||||
<!-- Rear Right -->
|
||||
<gear x="-28.0" y="-2.0" z="-2.9" retract-time="7" compression="1.0">
|
||||
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
|
||||
<control-input axis="/controls/gear/gear[3]/wheel[0]/brake" control="BRAKE"/>
|
||||
<control-input axis="/controls/gear/gear[3]/wheel[1]/brake" control="BRAKE"/>
|
||||
<control-input axis="/controls/gear/parking-brake" control="BRAKE"/>
|
||||
<control-speed control="EXTEND" transition-time="7"/>
|
||||
<control-speed control="BRAKE" transition-time="0.7"/>
|
||||
<control-output control="EXTEND" prop="/gear/gear[3]/position-norm"/>
|
||||
</gear>
|
||||
|
||||
<!-- Left Wing -->
|
||||
<gear x="-31.0" y="23.0" z="-2.0" retract-time="5" compression="2.5">
|
||||
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
|
||||
<control-speed control="EXTEND" transition-time="5"/>
|
||||
<control-output control="EXTEND" prop="/gear/gear[4]/position-norm"/>
|
||||
</gear>
|
||||
|
||||
<!-- Right Wing -->
|
||||
<gear x="-31.0" y="-23.0" z="-2.0" retract-time="5" compression="2.5">
|
||||
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
|
||||
<control-speed control="EXTEND" transition-time="5"/>
|
||||
<control-output control="EXTEND" prop="/gear/gear[5]/position-norm"/>
|
||||
</gear>
|
||||
|
||||
<!-- Fuel tanks -->
|
||||
<!-- Total fuel for the F model was 41553 gal incl the external tanks
|
||||
|
||||
There are a total of ten internal tanks, three located in the wings
|
||||
and four along the top of the fuselage above the bomb bay. I don't
|
||||
know what percentage was held in the wings vs. the fuselage but I'm
|
||||
guessing that more was held in the fuselage tank than half of the
|
||||
wing tank total.
|
||||
|
||||
There are also two external wing tanks holding 3000 gal each.
|
||||
|
||||
fgfs seems to convert gal to lbs using a ratio of 1:6 giving a total
|
||||
of 249318 lb of fuel, of which 18000 lb are in each external tank.
|
||||
That leaves 213318 of fuel to be distributed in the wings and
|
||||
fuselage.
|
||||
-->
|
||||
<tank x="-20.0" y="10.0" z="2.0" capacity="70000"/>
|
||||
<tank x="-20.0" y="-10.0" z="2.0" capacity="70000"/>
|
||||
<tank x="-20.0" y="0.0" z="2.3" capacity="73318"/>
|
||||
<tank x="-30.0" y="28.0" z="1.5" capacity="18000"/>
|
||||
<tank x="-30.0" y="-28.0" z="1.5" capacity="18000"/>
|
||||
|
||||
<!-- This is to level the aircraft on the ground
|
||||
-->
|
||||
|
||||
<ballast x="-4.0" y="0" z="0" mass="20000"/>
|
||||
|
||||
</airplane>
|
||||
|
|
@ -1,93 +0,0 @@
|
|||
<airplane mass="1950">
|
||||
|
||||
<!-- Approach configuration -->
|
||||
<approach speed="47" aoa="16">
|
||||
<control-setting axis="/controls/engines/engine[0]/throttle" value="0.3"/>
|
||||
<control-setting axis="/controls/engines/engine[0]/mixture" value="1.0"/>
|
||||
<control-setting axis="/controls/flight/flaps" value="1.0"/>
|
||||
</approach>
|
||||
|
||||
<!-- Cruise configuration -->
|
||||
<cruise speed="123" alt="0">
|
||||
<control-setting axis="/controls/engines/engine[0]/throttle" value="1.0"/>
|
||||
<control-setting axis="/controls/engines/engine[0]/mixture" value="1.0"/>
|
||||
<control-setting axis="/controls/flight/flaps" value="0.0"/>
|
||||
</cruise>
|
||||
|
||||
<cockpit x="-1.88" y=".33" z="0.6"/>
|
||||
|
||||
<fuselage ax="-.17" ay="0" az="-.51" bx="-7.16" by="0" bz=".17"
|
||||
width="1.5" taper="0.2" midpoint="0.3"/>
|
||||
|
||||
<wing x="-2.47" y=".51" z=".68" taper=".78"
|
||||
length="5.37" chord="1.54" sweep="0" dihedral="1" camber="0.1">
|
||||
<stall aoa="16" width="6" peak="1.5"/>
|
||||
<flap0 start="0" end=".38" lift="1.5" drag="1.2"/>
|
||||
<flap1 start=".78" end="1" lift="1.5" drag="1.2"/>
|
||||
<control-input axis="/controls/flight/flaps" control="FLAP0"/>
|
||||
<control-input axis="/controls/flight/aileron" control="FLAP1" split="true"/>
|
||||
<control-input axis="/controls/flight/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="6"/>
|
||||
</wing>
|
||||
|
||||
<hstab x="-7.16" y="0.08" z=".17" taper=".63" effectiveness="2"
|
||||
length="1.71" chord="1.36" sweep="0">
|
||||
<stall aoa="18" width="4" peak="1.5"/>
|
||||
<flap0 start="0" end="1" lift="1.7" drag="1.2"/>
|
||||
<control-input axis="/controls/flight/elevator" control="FLAP0"/>
|
||||
<control-input axis="/controls/flight/elevator-trim" control="FLAP0"/>
|
||||
<control-output control="FLAP0" prop="/surface-positions/elevator-pos-norm"/>
|
||||
</hstab>
|
||||
|
||||
<vstab x="-7.16" y="0" z=".17" taper=".5"
|
||||
length="1.71" chord="1.54" sweep="20">
|
||||
<stall aoa="16" width="4" peak="1.5"/>
|
||||
<flap0 start="0" end="1" lift="1.3" drag="1.2"/>
|
||||
<control-input axis="/controls/flight/rudder" control="FLAP0" invert="true"/>
|
||||
<control-input axis="/controls/flight/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="86" cruise-rpm="2200"
|
||||
cruise-alt="10000" cruise-power="99"
|
||||
takeoff-power="140.8" takeoff-rpm="2200"
|
||||
eng-power="160" eng-rpm="2500"
|
||||
x="-.6" y="0" z="0" mass="400" moment="8">
|
||||
<actionpt x="0" y="0" z="0"/>
|
||||
<control-input axis="/controls/engines/engine[0]/throttle" control="THROTTLE"/>
|
||||
<control-input axis="/controls/engines/engine[0]/starter" control="STARTER"/>
|
||||
<control-input axis="/controls/engines/engine[0]/magnetos" control="MAGNETOS"/>
|
||||
<control-input axis="/controls/engines/engine[0]/mixture" control="MIXTURE"/>
|
||||
</propeller>
|
||||
|
||||
<gear x="-1" y="0" z="-1.5" compression=".4"> <!-- nose -->
|
||||
<control-input axis="/controls/flight/rudder" control="STEER"
|
||||
src0="-1.0" src1="1.0"
|
||||
dst0="-0.1" dst1="0.1"/>
|
||||
</gear>
|
||||
|
||||
<gear x="-2.82" y="1.15" z="-1.36" compression=".3"> <!-- left main -->
|
||||
<control-input axis="/controls/gear/wheel[0]/brake" control="BRAKE" split="true"/>
|
||||
<control-input axis="/controls/gear/parking-brake" control="BRAKE" split="true"/>
|
||||
</gear>
|
||||
|
||||
<gear x="-2.82" y="-1.15" z="-1.36" compression=".3"> <!-- left main -->
|
||||
<control-input axis="/controls/gear/wheel[1]/brake" control="BRAKE" split="true"/>
|
||||
<control-input axis="/controls/gear/parking-brake" control="BRAKE" split="true"/>
|
||||
</gear>
|
||||
|
||||
<tank x="-2.47" y="1.36" z=".68" capacity="75"/>
|
||||
<tank x="-2.47" y="-1.36" z=".68" capacity="75"/>
|
||||
|
||||
<ballast x="-2.0" y=".33" z="0" mass="180"/> <!-- pilot -->
|
||||
<ballast x="-2.0" y="-.33" z="0" mass="180"/> <!-- passenger -->
|
||||
<ballast x="-1.0" y="-.33" z="0" mass="200"/> <!-- cockpit -->
|
||||
|
||||
</airplane>
|
||||
|
|
@ -1,129 +0,0 @@
|
|||
<airplane mass="3903">
|
||||
|
||||
<approach speed="70" aoa="16">
|
||||
<control-setting axis="/controls/engines/engine[0]/throttle" value="0.4"/>
|
||||
<control-setting axis="/controls/engines/engine[1]/throttle" value="0.4"/>
|
||||
<control-setting axis="/controls/engines/engine[0]/mixture" value="1.0"/>
|
||||
<control-setting axis="/controls/engines/engine[1]/mixture" value="1.0"/>
|
||||
<control-setting axis="/controls/engines/engine[0]/propeller-pitch" value="0.5"/>
|
||||
<control-setting axis="/controls/engines/engine[1]/propeller-pitch" value="0.5"/>
|
||||
<control-setting axis="/controls/flight/flaps" value="1.0"/>
|
||||
<control-setting axis="/controls/gear/gear-down" value="1"/>
|
||||
</approach>
|
||||
<cruise speed="223" alt="20000">
|
||||
<control-setting axis="/controls/engines/engine[0]/throttle" value="1.0"/>
|
||||
<control-setting axis="/controls/engines/engine[1]/throttle" value="1.0"/>
|
||||
<control-setting axis="/controls/engines/engine[0]/mixture" value="1.0"/>
|
||||
<control-setting axis="/controls/engines/engine[1]/mixture" value="1.0"/>
|
||||
<control-setting axis="/controls/engines/engine[0]/propeller-pitch" value="1.0"/>
|
||||
<control-setting axis="/controls/engines/engine[1]/propeller-pitch" value="1.0"/>
|
||||
<control-setting axis="/controls/flight/flaps" value="0.0"/>
|
||||
<control-setting axis="/controls/gear/gear-down" value="0"/>
|
||||
</cruise>
|
||||
|
||||
<cockpit x="-2.78" y="0.26" z="0.95"/>
|
||||
|
||||
<fuselage ax="0.00" ay="0" az="0" bx="-9.50" by="0" bz="0"
|
||||
width="1.5" taper="0" midpoint="0.4"/>
|
||||
|
||||
<wing x="-3.65" y="0.62" z="-0.18" length ="4.68" chord ="1.68"
|
||||
sweep="0" dihedral="5" taper="0.8" camber="0.1">
|
||||
<stall aoa="16" width="4" peak="1.5"/>
|
||||
<flap0 start="0" end=".5" lift="1.5" drag="1.2"/>
|
||||
<flap1 start=".55" end=".94" lift="1.3" drag="1.2"/>
|
||||
<control-input axis="/controls/flight/flaps" control="FLAP0"/>
|
||||
<control-speed control="FLAP0" transition-time="5"/>
|
||||
<control-output control="FLAP0" prop="/surface-positions/flap-pos-norm"/>
|
||||
<control-input axis="/controls/flight/aileron" control="FLAP1" split="true"/>
|
||||
<control-input axis="/controls/flight/aileron-trim" control="FLAP1" split="true"/>
|
||||
<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="-8.33" y="0.22" z="0.07" length ="2.34" chord ="1.24"
|
||||
sweep="0" dihedral="0" taper="0.6">
|
||||
<stall aoa="16" width="4" peak="1.5"/>
|
||||
<flap0 start="0" end="1" lift="1.68" drag="1.2"/>
|
||||
<control-input axis="/controls/flight/elevator" control="FLAP0"/>
|
||||
<control-input axis="/controls/flight/elevator-trim" control="FLAP0"/>
|
||||
<control-output control="FLAP0" prop="/surface-positions/elevator-pos-norm"/>
|
||||
</hstab>
|
||||
|
||||
<vstab x="-8.26" y="0.00" z="0.26" length ="2.16" chord ="1.61"
|
||||
sweep="36" taper="0.5">
|
||||
<stall aoa="16" width="4" peak="1.5"/>
|
||||
<flap0 start="0" end="1" lift="1.3" drag="1.2"/>
|
||||
<control-input axis="/controls/flight/rudder" control="FLAP0" invert="true"/>
|
||||
<control-input axis="/controls/flight/rudder-trim" control="FLAP0" invert="true"/>
|
||||
<control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm"/>
|
||||
</vstab>
|
||||
|
||||
<!-- Late model 310's had 50 gallon tip tanks, and 31.5 gallon wing
|
||||
tanks. Some also had nacelle tanks, but those aren't modeled
|
||||
here -->
|
||||
<tank x="-3.62" y="5.30" z="0.44" capacity="300"/>
|
||||
<tank x="-3.62" y="1.02" z="-0.15" capacity="189"/>
|
||||
<tank x="-3.62" y="-1.02" z="-0.15" capacity="189"/>
|
||||
<tank x="-3.62" y="-5.30" z="0.44" capacity="300"/>
|
||||
|
||||
<gear x="0.00" y="0.00" z="-1.35" compression=".5" retract-time="7">
|
||||
<control-input axis="/controls/flight/rudder" control="STEER"/>
|
||||
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
|
||||
<control-speed control="EXTEND" transition-time="7"/>
|
||||
<control-output control="EXTEND" prop="/gear/gear[2]/position-norm"/>
|
||||
</gear>
|
||||
|
||||
<gear x="-4.02" y="1.32" z="-1.35" compression=".5" retract-time="7">
|
||||
<control-input axis="/controls/gear/wheel[0]/brake" control="BRAKE"/>
|
||||
<control-input axis="/controls/gear/parking-brake" control="BRAKE"/>
|
||||
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
|
||||
<control-speed control="EXTEND" transition-time="6.2"/>
|
||||
<control-output control="EXTEND" prop="/gear/gear[0]/position-norm"/>
|
||||
</gear>
|
||||
|
||||
<gear x="-4.02" y="-1.32" z="-1.35" compression=".5" retract-time="7">
|
||||
<control-input axis="/controls/gear/wheel[1]/brake" control="BRAKE"/>
|
||||
<control-input axis="/controls/gear/parking-brake" control="BRAKE"/>
|
||||
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
|
||||
<control-speed control="EXTEND" transition-time="6"/>
|
||||
<control-output control="EXTEND" prop="/gear/gear[1]/position-norm"/>
|
||||
</gear>
|
||||
|
||||
<propeller x="-2.56" y="1.83" z="0.07"
|
||||
mass="800" moment="12" radius="1.0"
|
||||
eng-power="285" eng-rpm="2700"
|
||||
turbo-mul="2" wastegate-mp="40"
|
||||
cruise-power="157" cruise-speed="195"
|
||||
cruise-rpm="2100" cruise-alt="20000"
|
||||
min-rpm="1600" max-rpm="2700">
|
||||
<actionpt x="-1.53" y="1.83" z="0.07"/>
|
||||
<control-input axis="/controls/engines/engine[0]/throttle" control="THROTTLE"/>
|
||||
<control-input axis="/controls/engines/engine[0]/starter" control="STARTER"/>
|
||||
<control-input axis="/controls/engines/engine[0]/magnetos" control="MAGNETOS"/>
|
||||
<control-input axis="/controls/engines/engine[0]/mixture" control="MIXTURE"/>
|
||||
<control-input axis="/controls/engines/engine[0]/propeller-pitch" control="ADVANCE"/>
|
||||
</propeller>
|
||||
|
||||
<propeller x="-2.56" y="-1.83" z="0.07"
|
||||
mass="800" moment="12" radius="1.0"
|
||||
eng-power="285" eng-rpm="2700"
|
||||
turbo-mul="2" wastegate-mp="40"
|
||||
cruise-power="157" cruise-speed="195"
|
||||
cruise-rpm="2100" cruise-alt="20000"
|
||||
min-rpm="1600" max-rpm="2700">
|
||||
<actionpt x="-1.53" y="-1.83" z="0.07"/>
|
||||
<control-input axis="/controls/engines/engine[1]/throttle" control="THROTTLE"/>
|
||||
<control-input axis="/controls/engines/engine[1]/starter" control="STARTER"/>
|
||||
<control-input axis="/controls/engines/engine[1]/magnetos" control="MAGNETOS"/>
|
||||
<control-input axis="/controls/engines/engine[1]/mixture" control="MIXTURE"/>
|
||||
<control-input axis="/controls/engines/engine[1]/propeller-pitch" control="ADVANCE"/>
|
||||
</propeller>
|
||||
|
||||
<ballast x="-2.78" y="0.26" z="0.0" mass="180"/> <!-- pilot -->
|
||||
<ballast x="-2.2" y="0" z="0.0" mass="240"/> <!-- cockpit -->
|
||||
|
||||
<weight x="-4.24" y="0" z="0" mass-prop="/yasim/c310/passenger-lbs"/>
|
||||
|
||||
</airplane>
|
||||
|
|
@ -1,124 +0,0 @@
|
|||
<airplane mass="16865">
|
||||
|
||||
<approach speed="58" aoa="13">
|
||||
<control-setting axis="/controls/engines/engine[0]/throttle" value="0.4"/>
|
||||
<control-setting axis="/controls/engines/engine[1]/throttle" value="0.4"/>
|
||||
<control-setting axis="/controls/engines/engine[0]/mixture" value="1.0"/>
|
||||
<control-setting axis="/controls/engines/engine[1]/mixture" value="1.0"/>
|
||||
<control-setting axis="/controls/engines/engine[0]/propeller-pitch" value="0.5"/>
|
||||
<control-setting axis="/controls/engines/engine[1]/propeller-pitch" value="0.5"/>
|
||||
<control-setting axis="/controls/flight/flaps" value="1.0"/>
|
||||
<control-setting axis="/controls/gear/gear-down" value="1"/>
|
||||
</approach>
|
||||
<cruise speed="180" alt="23200">
|
||||
<control-setting axis="/controls/engines/engine[0]/throttle" value="1.0"/>
|
||||
<control-setting axis="/controls/engines/engine[1]/throttle" value="1.0"/>
|
||||
<control-setting axis="/controls/engines/engine[0]/mixture" value="1.0"/>
|
||||
<control-setting axis="/controls/engines/engine[1]/mixture" value="1.0"/>
|
||||
<control-setting axis="/controls/engines/engine[0]/propeller-pitch" value="1.0"/>
|
||||
<control-setting axis="/controls/engines/engine[1]/propeller-pitch" value="1.0"/>
|
||||
<control-setting axis="/controls/engines/engine[0]/boost" value="1.0"/>
|
||||
<control-setting axis="/controls/engines/engine[1]/boost" value="1.0"/>
|
||||
<control-setting axis="/controls/flight/flaps" value="0.0"/>
|
||||
<control-setting axis="/controls/gear/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" twist="-3">
|
||||
<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/flight/flaps" control="FLAP0"/>
|
||||
<control-input axis="/controls/flight/aileron" control="FLAP1" split="true"/>
|
||||
<control-input axis="/controls/flight/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="1.2"
|
||||
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/flight/elevator" control="FLAP0" effectiveness="0.3"/>
|
||||
<control-input axis="/controls/flight/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/flight/rudder" control="FLAP0" effectiveness="2.0" invert="true"/>
|
||||
<control-input axis="/controls/flight/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/engines/engine[0]/throttle" control="THROTTLE"/>
|
||||
<control-input axis="/controls/engines/engine[0]/starter" control="STARTER"/>
|
||||
<control-input axis="/controls/engines/engine[0]/magnetos" control="MAGNETOS"/>
|
||||
<control-input axis="/controls/engines/engine[0]/mixture" control="MIXTURE"/>
|
||||
<control-input axis="/controls/engines/engine[0]/propeller-pitch" control="ADVANCE"/>
|
||||
<control-input axis="/controls/engines/engine[0]/boost" 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/engines/engine[1]/throttle" control="THROTTLE"/>
|
||||
<control-input axis="/controls/engines/engine[1]/starter" control="STARTER"/>
|
||||
<control-input axis="/controls/engines/engine[1]/magnetos" control="MAGNETOS"/>
|
||||
<control-input axis="/controls/engines/engine[1]/mixture" control="MIXTURE"/>
|
||||
<control-input axis="/controls/engines/engine[1]/propeller-pitch" control="ADVANCE"/>
|
||||
<control-input axis="/controls/engines/engine[1]/boost" 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/gear/tailwheel-lock" control="CASTERING"/>
|
||||
</gear>
|
||||
|
||||
<gear x="-6.08" y="2.52" z="-3.49" compression="1" retract-time="7" spring="2">
|
||||
<control-input axis="/controls/gear/parking-brake" control="BRAKE"/>
|
||||
<control-input axis="/controls/gear/wheel[0]/brake" control="BRAKE"/>
|
||||
<control-input axis="/controls/gear/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" spring="2">
|
||||
<control-input axis="/controls/gear/parking-brake" control="BRAKE"/>
|
||||
<control-input axis="/controls/gear/wheel[1]/brake" control="BRAKE"/>
|
||||
<control-input axis="/controls/gear/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>
|
||||
|
|
@ -1,170 +0,0 @@
|
|||
<!-- The Harrier has a zillion variants. Where possible, the numbers
|
||||
here are based on the Sea Harrier FRS.Mk.1, the initial version
|
||||
for the Royal Navy of Falklands fame. -->
|
||||
|
||||
<airplane mass="14052">
|
||||
|
||||
<!-- Approach configuration -->
|
||||
<approach speed="160" aoa="8">
|
||||
<control-setting axis="/controls/engines/engine[0]/throttle" value="0.2"/>
|
||||
<control-setting axis="/controls/flight/flaps" value="1.0"/>
|
||||
<control-setting axis="/controls/gear/gear-down" value="1"/>
|
||||
</approach>
|
||||
|
||||
<!-- Cruise configuration -->
|
||||
<cruise speed="716" alt="39000">
|
||||
<control-setting axis="/controls/engines/engine[0]/throttle" value="1.0"/>
|
||||
<control-setting axis="/controls/flight/flaps" value="0.0"/>
|
||||
<control-setting axis="/controls/gear/gear-down" value="0"/>
|
||||
</cruise>
|
||||
|
||||
<cockpit x="-3.15" y="0.00" z="1.48"/>
|
||||
|
||||
<fuselage ax="0.00" ay="0.00" az="0.00"
|
||||
bx="-15.57" by="0.00" bz="1.11"
|
||||
width="1.6" taper="0.1" midpoint="0.3"/>
|
||||
|
||||
<wing x="-7.32" y="0.46" z="0.93" length="3.71" chord="3.15"
|
||||
taper=".294" sweep="28" dihedral="-11" camber="0.05">
|
||||
<stall aoa="21" width="8" peak="1.3"/>
|
||||
<flap0 start="0.11" end="0.56" lift="1.5" drag="1.2"/>
|
||||
<flap1 start="0.56" end="0.91" lift="1.2" drag="1.2"/>
|
||||
<control-input axis="/controls/flight/flaps" control="FLAP0"/>
|
||||
<control-input axis="/controls/flight/aileron" control="FLAP1" split="true"/>
|
||||
<control-input axis="/controls/flight/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="-12.23" y="0.00" z="0.93" length="2.04" chord="1.48"
|
||||
taper=".313" sweep="24.5" dihedral="-12">
|
||||
<stall aoa="20" width="7" peak="1.5"/>
|
||||
<flap0 start="0" end="1" lift="1.7" drag="1.2"/>
|
||||
<control-input axis="/controls/flight/elevator" control="FLAP0"/>
|
||||
<control-input axis="/controls/flight/elevator-trim" control="FLAP0"/>
|
||||
<control-output control="FLAP0" prop="/surface-positions/elevator-pos-norm"/>
|
||||
</hstab>
|
||||
|
||||
<vstab x="-12.51" y="0.00" z="1.20" length="2.78" chord="2.41"
|
||||
taper=".308" sweep="23.5">
|
||||
<stall aoa="20" width="7" peak="1.5"/>
|
||||
<flap0 start="0.12" end="0.88" lift="1.2" drag="1.2"/>
|
||||
<control-input axis="/controls/flight/rudder" control="FLAP0" invert="true"/>
|
||||
<control-input axis="/controls/flight/rudder-trim" control="FLAP0" invert="true"/>
|
||||
<control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm"
|
||||
min="1" max="-1"/>
|
||||
</vstab>
|
||||
|
||||
<jet x="-6.12" y="0" z="0.56" mass="3000" thrust="21500" rotate="-99">
|
||||
<actionpt x="-7.452" y="0" z="0.671"/>
|
||||
<control-input axis="/controls/engines/engine[0]/throttle" control="THROTTLE"/>
|
||||
<control-input axis="/controls/engines/engine[0]/mixture" control="VECTOR"
|
||||
src0="0" src1="1" dst0="1" dst1="0"/>
|
||||
</jet>
|
||||
|
||||
<!-- Harriers have little "reactor" jets to change the aircraft's
|
||||
orientation during hover. I've been unable to find a good
|
||||
reference for where these are, exactly. I've chosen to put the
|
||||
pitch and yaw jets in the tail, and the roll jets point down from
|
||||
the wingtips. This makes logical sense, but I'd be pleased if
|
||||
anyone can find better info. -->
|
||||
|
||||
<!-- tail jets: left yaw, right yaw and pitch down -->
|
||||
<thruster x="-15" y="0" z="1" vx="0" vy="1" vz="0" thrust="200">
|
||||
<control-input axis="/controls/flight/rudder" control="THROTTLE"
|
||||
src0="0" src1="1" dst0="0" dst1="1"/>
|
||||
<control-input axis="/orientation/yaw-rate-degps" control="THROTTLE"
|
||||
src0="-5" src1="0" dst0="0.3" dst1="0"/>
|
||||
</thruster>
|
||||
<thruster x="-15" y="0" z="1" vx="0" vy="-1" vz="0" thrust="200">
|
||||
<control-input axis="/controls/flight/rudder" control="THROTTLE"
|
||||
src0="-1" src1="0" dst0="1" dst1="0"/>
|
||||
<control-input axis="/orientation/yaw-rate-degps" control="THROTTLE"
|
||||
src0="0" src1="5" dst0="0" dst1="0.3"/>
|
||||
</thruster>
|
||||
<thruster x="-15" y="0" z="1" vx="0" vy="0" vz="1" thrust="200">
|
||||
<control-input axis="/controls/flight/elevator" control="THROTTLE"
|
||||
src0="0" src1="1" dst0="0" dst1="1"/>
|
||||
<control-input axis="/orientation/pitch-rate-degps" control="THROTTLE"
|
||||
src0="0" src1="2" dst0="0" dst1="0.3"/>
|
||||
</thruster>
|
||||
|
||||
<!-- wingtip jets for roll -->
|
||||
<thruster x="-9.2" y="3.34" z="0" vx="0" vy="0" vz="1" thrust="200">
|
||||
<control-input axis="/controls/flight/aileron" control="THROTTLE"
|
||||
src0="0" src1="1" dst0="0" dst1="1"/>
|
||||
<control-input axis="/orientation/roll-rate-degps" control="THROTTLE"
|
||||
src0="-2" src1="0" dst0="0.3" dst1="0"/>
|
||||
</thruster>
|
||||
<thruster x="-9.2" y="3.34" z="0" vx="0" vy="0" vz="-1" thrust="200">
|
||||
<control-input axis="/controls/flight/aileron" control="THROTTLE"
|
||||
src0="-1" src1="0" dst0="1" dst1="0"/>
|
||||
<control-input axis="/orientation/roll-rate-degps" control="THROTTLE"
|
||||
src0="0" src1="2" dst0="0" dst1="0.3"/>
|
||||
</thruster>
|
||||
<thruster x="-9.2" y="-3.34" z="0" vx="0" vy="0" vz="1" thrust="200">
|
||||
<control-input axis="/controls/flight/aileron" control="THROTTLE"
|
||||
src0="-1" src1="0" dst0="1" dst1="0"/>
|
||||
<control-input axis="/orientation/roll-rate-degps" control="THROTTLE"
|
||||
src0="0" src1="2" dst0="0" dst1="0.3"/>
|
||||
</thruster>
|
||||
<thruster x="-9.2" y="-3.34" z="0" vx="0" vy="0" vz="-1" thrust="200">
|
||||
<control-input axis="/controls/flight/aileron" control="THROTTLE"
|
||||
src0="0" src1="1" dst0="0" dst1="1"/>
|
||||
<control-input axis="/orientation/roll-rate-degps" control="THROTTLE"
|
||||
src0="-2" src1="0" dst0="0.3" dst1="0"/>
|
||||
</thruster>
|
||||
|
||||
<!-- nose jet for pitch up -->
|
||||
<thruster x="0" y="0" z="0" vx="0" vy="0" vz="1" thrust="200">
|
||||
<control-input axis="/controls/flight/elevator" control="THROTTLE"
|
||||
src0="-1" src1="0" dst0="1" dst1="0"/>
|
||||
<control-input axis="/orientation/pitch-rate-degps" control="THROTTLE"
|
||||
src0="-2" src1="0" dst0="0.3" dst1="0"/>
|
||||
</thruster>
|
||||
|
||||
|
||||
<!-- Forward main -->
|
||||
<gear x="-4.91" y="0.00" z="-2.0" compression="0.75">
|
||||
<control-input axis="/controls/flight/rudder" control="STEER" square="true"/>
|
||||
<control-input axis="/controls/gear/wheel[0]/brake" control="BRAKE"/>
|
||||
<control-input axis="/controls/gear/parking-brake" control="BRAKE"/>
|
||||
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
|
||||
<control-output control="EXTEND" prop="/gear/gear[0]/position-norm"/>
|
||||
<control-speed control="EXTEND" transition-time="7"/>
|
||||
</gear>
|
||||
|
||||
<!-- Rear main -->
|
||||
<gear x="-8.25" y="0.00" z="-1.5" compression="0.25">
|
||||
<control-input axis="/controls/gear/wheel[0]/brake" control="BRAKE"/>
|
||||
<control-input axis="/controls/gear/parking-brake" control="BRAKE"/>
|
||||
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
|
||||
<control-output control="EXTEND" prop="/gear/gear[1]/position-norm"/>
|
||||
<control-speed control="EXTEND" transition-time="7"/>
|
||||
</gear>
|
||||
|
||||
<!-- Wingtip gear -->
|
||||
<gear x="-8.90" y="3.24" z="-1.41" compression="0.25" castering="1">
|
||||
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
|
||||
<control-output control="EXTEND" prop="/gear/gear[2]/position-norm"/>
|
||||
<control-speed control="EXTEND" transition-time="7"/>
|
||||
</gear>
|
||||
|
||||
<gear x="-8.90" y="-3.24" z="-1.41" compression="0.25" castering="1">
|
||||
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
|
||||
<control-output control="EXTEND" prop="/gear/gear[3]/position-norm"/>
|
||||
<control-speed control="EXTEND" transition-time="7"/>
|
||||
</gear>
|
||||
|
||||
<!-- This capacity is right, but I'm not sure what the tank
|
||||
configuration of a FRS.Mk.1 is. Just put it all at the wing
|
||||
root. -->
|
||||
<tank x="-7.32" y="0" z="0.5" jet="true" capacity="5049"/>
|
||||
|
||||
<ballast x="-2" y="0" z="0" mass="600"/>
|
||||
|
||||
|
||||
</airplane>
|
||||
|
|
@ -1,174 +0,0 @@
|
|||
<!-- I took these data from the book "Sodobna letala in helikopterji"
|
||||
(Jelko Kacin, 1986). About the aerodynamics, it is mostly a guess
|
||||
work. I took a base model from Douglas A-4, and modified it for J-22.
|
||||
-->
|
||||
|
||||
<!-- The empy aircraft mass is 5720 kg (12613 lbs), max fuel mass is about
|
||||
2950 kg (6505 lbs), max aircraft weight is 11300 kg (24917 lbs)
|
||||
accordingly to the sources
|
||||
-->
|
||||
<airplane mass="12613"> <!-- clean weight without fuel -->
|
||||
|
||||
<!-- Approach configuration -->
|
||||
<approach speed="130" aoa="6.5">
|
||||
<control-setting axis="/controls/engines/engine[0]/throttle" value="0.15"/>
|
||||
<control-setting axis="/controls/engines/engine[1]/throttle" value="0.15"/>
|
||||
<control-setting axis="/controls/engines/engine[0]/afterburner" value="0"/>
|
||||
<control-setting axis="/controls/engines/engine[1]/afterburner" value="0"/>
|
||||
<control-setting axis="/controls/flight/flaps" value="1"/>
|
||||
<control-setting axis="/controls/gear/gear-down" value="1"/>
|
||||
</approach>
|
||||
|
||||
<!-- Cruise configuration -->
|
||||
<cruise speed="540" alt="55000">
|
||||
<control-setting axis="/controls/engines/engine[0]/throttle" value="1"/>
|
||||
<control-setting axis="/controls/engines/engine[1]/throttle" value="1"/>
|
||||
<control-setting axis="/controls/engines/engine[0]/afterburner" value="0"/>
|
||||
<control-setting axis="/controls/engines/engine[1]/afterburner" value="0"/>
|
||||
<control-setting axis="/controls/flight/flaps" value="0.0"/>
|
||||
<control-setting axis="/controls/gear/gear-down" value="0"/>
|
||||
</cruise>
|
||||
|
||||
<cockpit x="4.089" y="0.0" z="0.920"/>
|
||||
|
||||
<!-- Fuselage -->
|
||||
<fuselage ax="7.718" ay="0.0" az="-0.300"
|
||||
bx="-5.518" by="0.0" bz="0.0"
|
||||
width="1" taper="0.5" midpoint="0.55"/>
|
||||
|
||||
<wing x="0.548" y="0.740" z="0.349" taper="0.286" incidence="0.25" idrag="1.3"
|
||||
length="5.72" chord="4.25" sweep="37.44" dihedral="0" camber="0.01" twist="-2.37">
|
||||
<stall aoa="27" width="10" peak="1.5"/>
|
||||
<flap0 start="0.0" end="0.5" lift="1.2" drag="1.3"/>
|
||||
<flap1 start="0.5" end="1.0" lift="1.2" drag="1.3"/>
|
||||
<control-input axis="/controls/flight/flaps" control="FLAP0"/>
|
||||
<control-input axis="/controls/flight/aileron" control="FLAP1" split="true"/>
|
||||
<control-input axis="/controls/flight/aileron-trim" control="FLAP1" split="true"/>
|
||||
<control-input axis="/controls/flight/spoilers" control="FLAP0"/>
|
||||
<control-input axis="/controls/flight/spoilers" control="FLAP1" invert="true"/>
|
||||
<control-output control="FLAP0" prop="/surface-positions/left-flap-pos-norm"/>
|
||||
<control-output control="FLAP0" prop="/surface-positions/right-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="2"/>
|
||||
<control-speed control="FLAP1" transition-time="0.5"/>
|
||||
</wing>
|
||||
|
||||
<!-- Back wings -->
|
||||
<hstab x="-4.44" y="0.689" z="-0.176" length="2.02" chord="4"
|
||||
taper="0.11" sweep="0" dihedral="40" camber="0.01" effectiveness="1.85">
|
||||
<stall aoa="24" width="2" peak="1.3"/>
|
||||
<flap0 start="0" end="1" lift="1.25" drag="1.4"/>
|
||||
|
||||
<control-input axis="/controls/flight/elevator" control="FLAP0"/>
|
||||
<control-input axis="/controls/flight/elevator-trim" control="FLAP0"/>
|
||||
<control-output control="FLAP0" prop="/surface-positions/elevator-pos-norm"/>
|
||||
|
||||
<control-speed control="FLAP0" transition-time="0.8"/>
|
||||
</hstab>
|
||||
|
||||
<!--
|
||||
<hstab x="-4.44" y="0.689" z="-0.176" taper="0.3" effectiveness="1.85"
|
||||
length="2.02" chord="2.02" sweep="0">
|
||||
<stall aoa="27" width="10" peak="1.5"/>
|
||||
<flap0 start="0" end="1" lift="1.5" drag="1.2"/>
|
||||
<control-input axis="/controls/flight/elevator" control="FLAP0"/>
|
||||
<control-input axis="/controls/flight/elevator-trim" control="FLAP0"/>
|
||||
<control-output control="FLAP0" prop="/surface-positions/elevator-pos-norm"/>
|
||||
<control-output control="FLAP0" side="left" prop="/surface-positions/left-elevator-pos-norm"/>
|
||||
<control-output control="FLAP0" side="right" prop="/surface-positions/right-elevator-pos-norm"/>
|
||||
<control-speed control="FLAP0" transition-time="0.5"/>
|
||||
</hstab>
|
||||
-->
|
||||
|
||||
<!-- Vertical stabilizator -->
|
||||
<vstab x="4.0" y="0" z="0.57" taper="0.176"
|
||||
length="3.13" chord="2.7" sweep="53.7" effectiveness="1.5">
|
||||
<stall aoa="27" width="10" peak="1.5"/>
|
||||
<flap0 start="0" end="1" lift="1.15" drag="1.2"/>
|
||||
<control-input axis="/controls/flight/rudder" control="FLAP0"/>
|
||||
<control-input axis="/controls/flight/rudder-trim" control="FLAP0"/>
|
||||
<control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm"
|
||||
min="1" max="-1"/>
|
||||
</vstab>
|
||||
|
||||
<!-- Viper Mk-632-41 R with 17,5 kN (22,5 kN w/ afterburner) thrust -->
|
||||
<!-- I couldn't find a figure for the mass so it's guess work.
|
||||
-->
|
||||
<jet x="-3.689" y="0.321" z="-0.072" mass="1900" thrust="3934" afterburner="5057">
|
||||
<control-input axis="/controls/engines/engine[0]/throttle" control="THROTTLE"/>
|
||||
<control-input axis="/controls/engines/engine[0]/afterburner" control="REHEAT"/>
|
||||
</jet>
|
||||
|
||||
<jet x="-3.689" y="-0.321" z="-0.072" mass="1900" thrust="3934" afterburner="5057">
|
||||
<control-input axis="/controls/engines/engine[1]/throttle" control="THROTTLE"/>
|
||||
<control-input axis="/controls/engines/engine[1]/afterburner" control="REHEAT"/>
|
||||
</jet>
|
||||
|
||||
<!-- Nose -->
|
||||
<gear x="5.481" y="0.00" z="-1.880" compression="0.7" spring="2.0">
|
||||
<control-input axis="/controls/flight/rudder" control="STEER" square="true"/>
|
||||
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
|
||||
<control-output control="EXTEND" prop="/gear/gear[0]/position-norm"/>
|
||||
<control-output control="STEER" prop="/gear/gear[0]/steering-norm"/>
|
||||
<control-speed control="EXTEND" transition-time="5"/>
|
||||
</gear>
|
||||
|
||||
<!-- Left main -->
|
||||
<gear x="0.219" y="1.150" z="-1.879" compression="0.6" spring="1.5">
|
||||
<control-input axis="/controls/gear/wheel[0]/brake" control="BRAKE"/>
|
||||
<control-input axis="/controls/gear/parking-brake" control="BRAKE"/>
|
||||
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
|
||||
<control-output control="EXTEND" prop="/gear/gear[1]/position-norm"/>
|
||||
<control-speed control="EXTEND" transition-time="5"/>
|
||||
</gear>
|
||||
|
||||
<!-- Right main -->
|
||||
<gear x="0.219" y="-1.150" z="-1.879" compression="0.6" spring="1.5">
|
||||
<control-input axis="/controls/gear/wheel[1]/brake" control="BRAKE"/>
|
||||
<control-input axis="/controls/gear/parking-brake" control="BRAKE"/>
|
||||
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
|
||||
<control-output control="EXTEND" prop="/gear/gear[2]/position-norm"/>
|
||||
<control-speed control="EXTEND" transition-time="5"/>
|
||||
</gear>
|
||||
|
||||
<!-- Canopy -->
|
||||
<gear x="4.1" y="0.0" z="1.05" retract-time="6" compression="0.6">
|
||||
<control-input axis="/controls/gear/parking-brake" control="EXTEND"/>
|
||||
<control-speed control="EXTEND" transition-time="6"/>
|
||||
<control-output control="EXTEND" prop="/canopy/position-norm"/>
|
||||
</gear>
|
||||
|
||||
<!-- The capacities of seperated fuel tanks are a guess work-->
|
||||
<!-- Fuselage tank (behind the cockpit) -->
|
||||
<tank x="2.738" y="0" z="0.282" jet="true" capacity="1805"/>
|
||||
<!-- Left wing tank -->
|
||||
<tank x="-0.357" y="1.377" z="0.310" jet="true" capacity="2400"/>
|
||||
<!-- Right wing tank -->
|
||||
<tank x="-0.357" y="-1.377" z="0.310" jet="true" capacity="2400"/>
|
||||
|
||||
<!-- J-22 has five pylons. One 1770 lbs center for a tank,
|
||||
and 4 1105 lbs pylons on the wings
|
||||
-->
|
||||
|
||||
<weight x="2.201" y="0" z="-0.975" size="1"
|
||||
mass-prop="/yasim/j22/weights/center-lbs"/>
|
||||
<weight x="0.649" y="2.137" z="-0.001" size="1"
|
||||
mass-prop="/yasim/j22/weights/left-inboard-lbs"/>
|
||||
<weight x="0.649" y="-2.137" z="-0.001" size="1"
|
||||
mass-prop="/yasim/j22/weights/right-inboard-lbs"/>
|
||||
<weight x="-0.222" y="3.272" z="-0.072" size="1"
|
||||
mass-prop="/yasim/j22/weights/left-outboard-lbs"/>
|
||||
<weight x="-0.222" y="-3.272" z="-0.072" size="1"
|
||||
mass-prop="/yasim/j22/weights/right-outboard-lbs"/>
|
||||
|
||||
<!-- Some ballast stuff to reach correctly placed center of gravity point -->
|
||||
<!-- Avionics -->
|
||||
<ballast x="5.413" y="0" z="-0.16" mass="2000"/>
|
||||
<!-- Cockpit and radar -->
|
||||
<ballast x="5.171" y="0" z="0.207" mass="2500"/>
|
||||
<!-- Pilot -->
|
||||
<ballast x="4.312" y="0" z="0" mass="200"/>
|
||||
|
||||
</airplane>
|
||||
|
|
@ -1,141 +0,0 @@
|
|||
<?xml version="1.0"?>
|
||||
|
||||
<!--
|
||||
************************************************************************
|
||||
YASim aerodynamic model for a Piper J3 Cub.
|
||||
Started 2002-08-15 by David Megginson.
|
||||
|
||||
This aerodynamic model is based on three-views, unauthoritative
|
||||
performance data, and wild guesses. These sites provided particularly
|
||||
useful information or were simply fun to visit:
|
||||
|
||||
Performance data:
|
||||
http://www.marss.com/cub.htm
|
||||
Weight and balance:
|
||||
http://www.danford.net/balance.htm
|
||||
Three-view:
|
||||
http://www.fiddlersgreen.net/aircraft/private/j3cub/j3cub_info/j3_info.htm
|
||||
Useless but fun free paper model:
|
||||
http://www.fiddlersgreen.net/aircraft/private/j3cub/j3cub.htm
|
||||
Useless but fun 1945 Piper Cub ad from FLYING:
|
||||
http://www.fiddlersgreen.net/aircraft/private/j3cub/j3cub_info/piperad.jpg
|
||||
|
||||
The reference datum for measurements is the leading edge of the wing,
|
||||
since it is what the weight-and-balance site above uses.
|
||||
************************************************************************
|
||||
-->
|
||||
|
||||
<!--
|
||||
680lb empty weight.
|
||||
-->
|
||||
<!-- FIXME: this includes the engine; is that correct? -->
|
||||
<airplane mass="680">
|
||||
|
||||
<!-- Approach configuration -->
|
||||
<approach speed="20" aoa="15">
|
||||
<control-setting axis="/controls/engines/engine[0]/throttle" value="0.5"/>
|
||||
<control-setting axis="/controls/engines/engine[0]/mixture" value="1.0"/>
|
||||
</approach>
|
||||
|
||||
<!-- Cruise configuration -->
|
||||
<cruise speed="64" alt="0">
|
||||
<control-setting axis="/controls/engines/engine[0]/throttle" value="0.75"/>
|
||||
<control-setting axis="/controls/engines/engine[0]/mixture" value="0.75"/>
|
||||
<control-setting axis="/controls/flight/elevator-trim" value="0.1"/>
|
||||
</cruise>
|
||||
|
||||
<!-- pilot's eyepoint -->
|
||||
<cockpit x="-0.23" y="0" z="-0.30"/>
|
||||
|
||||
<fuselage ax="1.37" ay="0" az="-0.71" bx="-4.81" by="0" bz="-0.65"
|
||||
width="0.71" taper="0.16" midpoint="0.17"/>
|
||||
|
||||
<!--
|
||||
I treat it as a perfectly rectangular wing for now. Note that
|
||||
the dihedral is exaggerated to simulate hull-interference effects
|
||||
on a high-wing aircraft; once YASim models that properly, the
|
||||
angle should be reduced to something like 2 degrees.
|
||||
|
||||
Note that the J3 Cub has no flaps. With a stall speed of 25kt, who
|
||||
needs them? From what I've read, the ailerons add lots of drag.
|
||||
-->
|
||||
<wing x="-0.80" y="0.42" z="0.0" taper="1.0" incidence="2" twist="-3"
|
||||
length="4.87" chord="1.60" sweep="0" dihedral="5" camber="0.1">
|
||||
<stall aoa="18" width="4" peak="1.5"/>
|
||||
<flap0 start=".31" end="0.85" lift="1.5" drag="1.4"/>
|
||||
<control-input axis="/controls/flight/aileron" control="FLAP0" split="true"/>
|
||||
<control-input axis="/controls/flight/aileron-trim" control="FLAP0" split="true"/>
|
||||
<control-output control="FLAP0" side="left"
|
||||
prop="/surface-positions/left-aileron-pos-norm"/>
|
||||
<control-output control="FLAP0" side="right"
|
||||
prop="/surface-positions/right-aileron-pos-norm"/>
|
||||
</wing>
|
||||
|
||||
<hstab x="-4.87" y="0.05" z="-0.42" taper="0.8" effectiveness="1.24"
|
||||
length="1.49" chord="1.13" sweep="0">
|
||||
<stall aoa="16" width="4" peak="1.5"/>
|
||||
<flap0 start="0" end="1" lift="1.4" drag="1.2"/>
|
||||
<control-input axis="/controls/flight/elevator" control="FLAP0"/>
|
||||
<control-input axis="/controls/flight/elevator-trim" control="FLAP0"/>
|
||||
<control-output control="FLAP0" prop="/surface-positions/elevator-pos-norm"/>
|
||||
</hstab>
|
||||
|
||||
<!-- rudder has to be able to counteract aileron drag -->
|
||||
<vstab x="-4.87" y="0" z="-0.65" taper="0.38" effectiveness="2.0"
|
||||
length="1.31" chord="1.37" sweep="0" incidence="1.5">
|
||||
<stall aoa="16" width="4" peak="1.5"/>
|
||||
<flap0 start="0" end="1" lift="2.0" drag="1.2"/>
|
||||
<control-input axis="/controls/flight/rudder" control="FLAP0" invert="true"/>
|
||||
<control-input axis="/controls/flight/rudder-trim" control="FLAP0" invert="true"/>
|
||||
<control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm"
|
||||
min="1" max="-1"/>
|
||||
</vstab>
|
||||
|
||||
<!-- FIXME: engine mass (just a guess; it's a small engine) -->
|
||||
<!-- Assume 75% power at 8000ft -->
|
||||
<propeller radius="0.90"
|
||||
cruise-speed="70" cruise-rpm="2150"
|
||||
cruise-alt="8000" cruise-power="49"
|
||||
takeoff-power="55" takeoff-rpm="2300"
|
||||
eng-power="65" eng-rpm="2500"
|
||||
x="0.71" y="0" z="-0.65" mass="150" moment="4">
|
||||
<actionpt x="1.31" y="0" z="-0.65"/>
|
||||
<control-input axis="/controls/engines/engine[0]/throttle" control="THROTTLE"/>
|
||||
<control-input axis="/controls/engines/engine[0]/starter" control="STARTER"/>
|
||||
<control-input axis="/controls/engines/engine[0]/magnetos" control="MAGNETOS"/>
|
||||
<control-input axis="/controls/engines/engine[0]/mixture" control="MIXTURE"/>
|
||||
</propeller>
|
||||
|
||||
<gear x="-5.17" y="0" z="-0.71" compression="0.1">
|
||||
<control-input axis="/controls/flight/rudder" control="STEER"
|
||||
src0="-1.0" src1="1.0"
|
||||
dst0="0.5" dst1="-0.5"/>
|
||||
</gear>
|
||||
|
||||
<gear x="0" y="0.95" z="-1.96" compression="0.01"> <!-- left main -->
|
||||
<control-input axis="/controls/gear/wheel[0]/brake" control="BRAKE" split="true"/>
|
||||
<control-input axis="/controls/gear/parking-brake" control="BRAKE" split="true"/>
|
||||
</gear>
|
||||
|
||||
<gear x="0" y="-0.95" z="-1.96" compression="0.01"> <!-- right main -->
|
||||
<control-input axis="/controls/gear/wheel[1]/brake" control="BRAKE" split="true"/>
|
||||
<control-input axis="/controls/gear/parking-brake" control="BRAKE" split="true"/>
|
||||
</gear>
|
||||
|
||||
<!-- There's just one 12-gallon tank, right behind the engine (!!!) -->
|
||||
<tank x="-0.45" y="0" z="-0.89" capacity="72"/>
|
||||
|
||||
<!--
|
||||
Note the tandem seating; the x values (arms) come from the
|
||||
weight-and-balance page cited at the start.
|
||||
-->
|
||||
|
||||
<ballast x="-4.0" y="0" z="-0.70" mass="-75"/>
|
||||
|
||||
<!-- pilot -->
|
||||
<weight x="-0.91" y="0" z="-0.70" mass-prop="/yasim/j3cub/pilot-lb"/>
|
||||
|
||||
<!-- passenger -->
|
||||
<weight x="-0.23" y="0" z="-0.70" mass-prop="/yasim/j3cub/passenger-lb"/>
|
||||
|
||||
</airplane>
|
||||
|
|
@ -1,166 +0,0 @@
|
|||
<?xml version="1.0"?>
|
||||
|
||||
<!--
|
||||
************************************************************************
|
||||
YASim aerodynamic model for a P-51D mustang
|
||||
Started 2003-04-24 by Jim Wilson
|
||||
|
||||
This aerodynamic model is based on three-views, unauthoritative
|
||||
performance data, and wild guesses. These sites provided particularly
|
||||
useful information or were simply fun to visit:
|
||||
|
||||
Performance data:
|
||||
http://www.hq.nasa.gov/office/pao/History/SP-468/app-a2.htm
|
||||
http://www.olympicflightmuseum.com/aircraft_gallery/p51d_mustang.htm
|
||||
http://www.btinternet.com/~lee_mail/P51.html
|
||||
http://www.sprucegoose.org/pdfs/planes/P51Mustang.pdf
|
||||
|
||||
Weight and balance:
|
||||
http://www.p51.wjackparker.com/P51_Additional_reference_material/x_maintenance.htm
|
||||
http://www.nzfpm.co.nz/aircraft/p51d.htm
|
||||
http://www.wpafb.af.mil/museum/engines/eng33.htm
|
||||
|
||||
Three-view:
|
||||
http://members.optushome.com.au/gjmustang/docs/3-View.html
|
||||
(Note: I have local copies if this url becomes un-available)
|
||||
|
||||
The reference datum for measurements is the nose.
|
||||
************************************************************************
|
||||
-->
|
||||
|
||||
<!-- Weight of everything but fuel (7010 empty) -->
|
||||
<airplane mass="7190">
|
||||
|
||||
<!-- Approach configuration -->
|
||||
<approach speed="87" aoa="13">
|
||||
<control-setting axis="/controls/engines/engine[0]/throttle" value="0.2"/>
|
||||
<control-setting axis="/controls/engines/engine[0]/mixture" value="1.0"/>
|
||||
<control-setting axis="/controls/engines/engine[0]/propeller-pitch" value="0.5"/>
|
||||
<control-setting axis="/controls/flight/flaps" value="1.0"/>
|
||||
<control-setting axis="/controls/gear/gear-down" value="1"/>
|
||||
</approach>
|
||||
|
||||
<!-- Cruise configuration -->
|
||||
<cruise speed="380" alt="25000">
|
||||
<control-setting axis="/controls/engines/engine[0]/throttle" value="1.00"/>
|
||||
<control-setting axis="/controls/engines/engine[0]/mixture" value="1.00"/>
|
||||
<control-setting axis="/controls/engines/engine[0]/propeller-pitch" value="1.0"/>
|
||||
<control-setting axis="/controls/engines/engine[0]/boost" value="1.0"/>
|
||||
<control-setting axis="/controls/flight/flaps" value="0.0"/>
|
||||
<control-setting axis="/controls/gear/gear-down" value="0"/>
|
||||
</cruise>
|
||||
|
||||
<!-- pilot's eyepoint -->
|
||||
<cockpit x="-4.495" y="0" z="0.689"/>
|
||||
|
||||
<fuselage ax="0.0" ay="0.0" az="0.0" bx="-9.9" by="0.0" bz="0.0"
|
||||
width="0.94" taper="0.38"/>
|
||||
|
||||
<!--
|
||||
stall aoa not available
|
||||
flap drag not available
|
||||
-->
|
||||
<wing x="-3.96" y="0.55" z="-0.60" taper="0.466" incidence="0"
|
||||
length="5.16" chord="2.845" sweep="-3.5" dihedral="5" camber="0.1">
|
||||
<stall aoa="14" width="4" peak="1.5"/>
|
||||
<flap0 start="0.024" end="0.543" lift="1.2" drag="1.8"/>
|
||||
<flap1 start="0.543" end="0.94.5" lift="1.3" drag="1.4"/>
|
||||
<control-input axis="/controls/flight/flaps" control="FLAP0"/>
|
||||
<control-output control="FLAP0" prop="/surface-positions/flap-pos-norm"/>
|
||||
<control-speed control="FLAP0" transition-time="5"/>
|
||||
<control-input axis="/controls/flight/aileron" control="FLAP1" split="true"/>
|
||||
<control-input axis="/controls/flight/aileron-trim" control="FLAP1" split="true"/>
|
||||
</wing>
|
||||
|
||||
<hstab x="-8.62" y="0.18" z="0.34" taper="0.639" effectiveness="3.5"
|
||||
length="1.834" chord="1.256" sweep="0" incidence="2">
|
||||
<stall aoa="15" width="4" peak="1.5"/>
|
||||
<flap0 start="0.0" end="1.8" lift="1.65" drag="1.2"/>
|
||||
<control-input axis="/controls/flight/elevator" control="FLAP0"/>
|
||||
<control-input axis="/controls/flight/elevator-trim" control="FLAP0"/>
|
||||
<control-output control="FLAP0" prop="/surface-positions/elevator-pos-norm"/>
|
||||
</hstab>
|
||||
|
||||
<!-- rudder has to be able to counteract aileron drag -->
|
||||
<vstab x="-9.30" y="0" z="-0.37" taper="0.432" effectiveness="3.5"
|
||||
length="1.971" chord="2.65" sweep="25" incidence="-0.58">
|
||||
<stall aoa="15" width="4" peak="1.5"/>
|
||||
<flap0 start="0" end="1" lift="1.3" drag="1.2"/>
|
||||
<control-input axis="/controls/flight/rudder" square="true" control="FLAP0" invert="true"/>
|
||||
<control-input axis="/controls/flight/rudder-trim" control="FLAP0" invert="true"/>
|
||||
<control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm"
|
||||
min="1" max="-1"/>
|
||||
</vstab>
|
||||
|
||||
<!-- moment calculated using formula submitted by Donald Simon:
|
||||
MOI = # of Blades * (8.2*(10^-5))*(D^5), slug-ft^2
|
||||
then converted to kg-m^2 and finally square root to kg-m for torque value -->
|
||||
<!-- wastegate setting should not apply. set here so that calculations would approximate.
|
||||
YASim doesn't model gear supercharger. Have read various figures (turbo-mul) 4.0 to 5.8 for
|
||||
running the second stage blower. Fixing this would probably give more reasonable
|
||||
performance at lower altitude -->
|
||||
<!-- cruise-rpm roughly estimated from documented gear ratio of 0.479 -->
|
||||
<propeller x="-0.75" y="0" z="0"
|
||||
radius="1.75"
|
||||
mass="1690" moment="94.5"
|
||||
eng-power="1590" eng-rpm="3000"
|
||||
turbo-mul="4.0" wastegate-mp="61"
|
||||
cruise-alt="21400" cruise-power="1370"
|
||||
cruise-speed="380" cruise-rpm="2900"
|
||||
manual-pitch="true" >
|
||||
<actionpt x="-1.25" y="0" z="0"/>
|
||||
<control-input axis="/controls/engines/engine[0]/throttle" control="THROTTLE"/>
|
||||
<control-input axis="/controls/engines/engine[0]/starter" control="STARTER"/>
|
||||
<control-input axis="/controls/engines/engine[0]/magnetos" control="MAGNETOS"/>
|
||||
<control-input axis="/controls/engines/engine[0]/mixture" control="MIXTURE"/>
|
||||
<control-input axis="/controls/engines/engine[0]/propeller-pitch" control="PROPPITCH"
|
||||
src0="0" src1="1" dst0="0.40" dst1="0.82"/>
|
||||
<control-input axis="/controls/engines/engine[0]/boost" control="BOOST"/>
|
||||
</propeller>
|
||||
|
||||
<!-- Tail wheel -->
|
||||
<!-- tail wheel "steerable" in p-51d (in stick back locked position it actually should be limited to 6deg +/-) -->
|
||||
<gear x="-7.90" y="0" z="-0.96" compression="0.2">
|
||||
<control-input axis="/controls/flight/rudder" control="STEER" square="true"
|
||||
src0="-1.0" src1="1.0"
|
||||
dst0="0.5" dst1="-0.5"/>
|
||||
</gear>
|
||||
|
||||
<!-- left main -->
|
||||
<gear x="-2.79" y="1.81" z="-2.20" compression="0.4" spring="0.7" damp="3.0">
|
||||
<control-input axis="/controls/gear/wheel[0]/brake" control="BRAKE"/>
|
||||
<control-input axis="/controls/gear/parking-brake" control="BRAKE" split="true"/>
|
||||
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
|
||||
<control-speed control="EXTEND" transition-time="6"/>
|
||||
<control-output control="EXTEND" prop="/gear/gear[0]/position-norm"/>
|
||||
</gear>
|
||||
|
||||
<!-- right main -->
|
||||
<gear x="-2.79" y="-1.81" z="-2.20" compression="0.4" spring="0.7" damp="3.0">
|
||||
<control-input axis="/controls/gear/wheel[1]/brake" control="BRAKE"/>
|
||||
<control-input axis="/controls/gear/parking-brake" control="BRAKE" split="true"/>
|
||||
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
|
||||
<control-speed control="EXTEND" transition-time="6"/>
|
||||
<control-output control="EXTEND" prop="/gear/gear[1]/position-norm"/>
|
||||
</gear>
|
||||
|
||||
<!-- Guess on wing tank positions -->
|
||||
<tank x="-3.50" y="1.0" z="-0.61" capacity="726"/>
|
||||
<tank x="-3.50" y="-1.0" z="-0.61" capacity="726"/>
|
||||
<tank x="-6.50" y="0" z="0" capacity="671"/>
|
||||
|
||||
<!-- pilot -->
|
||||
<ballast x="-4.495" y="0" z="0.689" mass="180"/>
|
||||
|
||||
<!-- armament -->
|
||||
<!-- Had too much weight I think...disable until stall speed fixed
|
||||
<ballast x="-3.20" y="0.7" z="-0.60" mass="800"/>
|
||||
<ballast x="-3.20" y="-0.7" z="-0.60" mass="800"/>
|
||||
-->
|
||||
|
||||
<!-- prop -->
|
||||
<!--
|
||||
<ballast x="0.1" y="0" z="0.0" mass="200"/>
|
||||
-->
|
||||
|
||||
</airplane>
|
||||
|
|
@ -1,93 +0,0 @@
|
|||
<airplane mass="1480">
|
||||
|
||||
<!-- Approach configuration -->
|
||||
<approach speed="45" aoa="14">
|
||||
<control-setting axis="/controls/engines/engine[0]/throttle" value="0.0"/>
|
||||
<control-setting axis="/controls/engines/engine[0]/mixture" value="1.0"/>
|
||||
<control-setting axis="/controls/flight/flaps" value="0.0"/>
|
||||
</approach>
|
||||
|
||||
<!-- Cruise configuration -->
|
||||
<cruise speed="123" alt="7000">
|
||||
<control-setting axis="/controls/engines/engine[0]/throttle" value="1.0"/>
|
||||
<control-setting axis="/controls/engines/engine[0]/mixture" value="0.7"/>
|
||||
<control-setting axis="/controls/flight/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" incidence="2" twist="-2"
|
||||
length="4.5" chord="1.65" sweep="0" dihedral="5" camber="0.1">
|
||||
<stall aoa="18" width="2.0" peak="1.5"/>
|
||||
<flap0 start="0" end="0.5" lift="1.5" drag="1.5"/>
|
||||
<flap1 start="0.5" end="1.0" lift="1.2" drag="1.2"/>
|
||||
<control-input axis="/controls/flight/flaps" control="FLAP0"/>
|
||||
<control-input axis="/controls/flight/aileron" control="FLAP1" split="true"/>
|
||||
<control-input axis="/controls/flight/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" incidence="-1"
|
||||
length="1.9" chord="0.9" sweep="0">
|
||||
<stall aoa="17" width="4" peak="1.5"/>
|
||||
<flap0 start="0" end="1" lift="1.65" drag="1.2"/>
|
||||
<control-input axis="/controls/flight/elevator" control="FLAP0"/>
|
||||
<control-input axis="/controls/flight/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/flight/rudder" control="FLAP0" invert="true"/>
|
||||
<control-input axis="/controls/flight/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/engines/engine[0]/throttle" control="THROTTLE"/>
|
||||
<control-input axis="/controls/engines/engine[0]/starter" control="STARTER"/>
|
||||
<control-input axis="/controls/engines/engine[0]/magnetos" control="MAGNETOS"/>
|
||||
<control-input axis="/controls/engines/engine[0]/mixture" control="MIXTURE"/>
|
||||
</propeller>
|
||||
|
||||
<gear x="-1" y="0" z="-1.3" compression=".05"> <!-- nose -->
|
||||
<control-input axis="/controls/flight/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/gear/wheel[0]/brake" control="BRAKE" split="true"/>
|
||||
<control-input axis="/controls/gear/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/gear/wheel[1]/brake" control="BRAKE" split="true"/>
|
||||
<control-input axis="/controls/gear/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>
|
||||
|
|
@ -1,140 +0,0 @@
|
|||
<!-- Hawker Sea Hawk yasim config. This is a hack and not an
|
||||
authentic representation of the aircraft. Having said
|
||||
that, the numbers, where I could find them, roughly match
|
||||
those of the original aircraft.
|
||||
Lee Elliott. leee-fgfs@spatial.freeserve.co.uk
|
||||
-->
|
||||
|
||||
<airplane mass="9720">
|
||||
|
||||
<!-- Approach configuration.
|
||||
I couldn't find any approach data but I think that the way
|
||||
the aircraft sits tail down on it's u/c indicates that it
|
||||
must land at a fairly shallow AoA to avoid hitting tail
|
||||
first. The speed is a guess.
|
||||
|
||||
I could see no sign or mention of spoilers or airbrakes in any
|
||||
of the docs or pictures I found.
|
||||
-->
|
||||
<approach speed="110" aoa="4">
|
||||
<control-setting axis="/controls/engines/engine[0]/throttle" value="0.5"/>
|
||||
<control-setting axis="/controls/flight/flaps" value="1.0"/>
|
||||
<control-setting axis="/controls/gear/gear-down" value="1"/>
|
||||
</approach>
|
||||
|
||||
<!-- Cruise configuration.
|
||||
Max speed at sea level is 599 mph = 521 knots. The same source
|
||||
also quoted 587 mph at 'altitude'.
|
||||
-->
|
||||
<cruise speed="521" alt="0">
|
||||
<control-setting axis="/controls/engines/engine[0]/throttle" value="1.0"/>
|
||||
<control-setting axis="/controls/flight/flaps" value="0.0"/>
|
||||
<control-setting axis="/controls/gear/gear-down" value="0"/>
|
||||
</cruise>
|
||||
|
||||
<cockpit x="3.0" y="0.0" z="0.7"/>
|
||||
|
||||
<fuselage ax="5.10" ay="0" az="0" bx="5.88" by="0" bz="0"
|
||||
width="1.3"/>
|
||||
|
||||
<!-- The wing length is from tips to fuselage, including intakes.
|
||||
The aileron figures are probably too low but the roll rate seemed
|
||||
too high otherwise.
|
||||
-->
|
||||
<wing x="0.1" y="0.65" z="0.0" taper="0.5" incidence="0.0"
|
||||
length="5.3" chord="3.0" sweep="-3.0" dihedral="3.0" camber="0.006">
|
||||
<stall aoa="17" width="3" peak="1.3"/>
|
||||
<flap0 start="0.1" end="0.4" lift="1.4" drag="1.6"/>
|
||||
<flap1 start="0.4" end="0.95" lift="1.05" drag="1.2"/>
|
||||
|
||||
<control-input axis="/controls/flight/flaps" control="FLAP0"/>
|
||||
<control-input axis="/controls/flight/aileron" control="FLAP1" split="true"/>
|
||||
<control-input axis="/controls/flight/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-output control="SPOILER" side="right" prop="/surface-positions/right-spoiler-pos-norm"/> -->
|
||||
|
||||
<control-speed control="FLAP0" transition-time="5"/>
|
||||
<control-speed control="FLAP1" transition-time="0.5"/>
|
||||
</wing>
|
||||
|
||||
<hstab x="-5.2" y="0.10" z="0.76" taper="0.3" effectiveness="1.6"
|
||||
length="1.7" chord="1.2" sweep="0.0" dihedral="0.0" camber="0.0">
|
||||
<stall aoa="17" width="5" peak="1.5"/>
|
||||
<flap0 start="0" end="1" lift="1.5" drag="1.2"/>
|
||||
|
||||
<control-input axis="/controls/flight/elevator" control="FLAP0"/>
|
||||
<control-input axis="/controls/flight/elevator-trim" control="FLAP0"/>
|
||||
|
||||
<control-output control="FLAP0" prop="/surface-positions/elevator-pos-norm"/>
|
||||
|
||||
<control-speed control="FLAP0" transition-time="0.5"/>
|
||||
</hstab>
|
||||
|
||||
<vstab x="-5.2" y="0.0" z="0.2" taper="0.8"
|
||||
length="1.4" chord="1.8" sweep="10.0">
|
||||
<stall aoa="16" width="5" peak="1.5"/>
|
||||
<flap0 start="0" end="1" lift="1.15" drag="1.3"/>
|
||||
<control-input axis="/controls/flight/rudder" control="FLAP0" invert="true"/>
|
||||
|
||||
<control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm"/>
|
||||
|
||||
<control-speed control="FLAP0" transition-time="0.5"/>
|
||||
</vstab>
|
||||
|
||||
<!-- Engines and tanks.
|
||||
1 x Roll-Royce Nene 103. I've no idea how much it actually
|
||||
weighs.
|
||||
-->
|
||||
<jet x="0.3" y="0.0" z="0.0" mass="1000" thrust="5200">
|
||||
<control-input axis="/controls/engines/engine[0]/throttle" control="THROTTLE"/>
|
||||
</jet>
|
||||
<!-- Fuel tanks in front, behind and above (saddle tank - actually feeds into
|
||||
tank two in real life) the engine. -->
|
||||
<tank x="1.4" y="0.0" z="0.0" jet="true" capacity="2000"/>
|
||||
<tank x="-1.3" y="0.0" z="0.0" jet="true" capacity="2000"/>
|
||||
<tank x="0.5" y="0.0" z="0.5" jet="true" capacity="1200"/>
|
||||
|
||||
<!-- Undercarriage -->
|
||||
<!-- Front -->
|
||||
<gear x="4.0" y="0.0" z="-1.53" compression="0.7" spring="1.0">
|
||||
<control-input axis="/controls/flight/rudder" control="STEER" square="true"/>
|
||||
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
|
||||
<control-speed control="EXTEND" transition-time="7"/>
|
||||
<control-output control="EXTEND" prop="/gear/gear[0]/position-norm"/>
|
||||
<control-output control="STEER" prop="/gear/gear[0]/steering-norm"/>
|
||||
</gear>
|
||||
|
||||
<!-- Left Main -->
|
||||
<gear x="-0.09" y="1.4" z="-1.34" compression="0.7" spring="1.8">
|
||||
<control-input axis="/controls/gear/wheel[1]/brake" control="BRAKE"/>
|
||||
<control-input axis="/controls/gear/parking-brake" control="BRAKE"/>
|
||||
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
|
||||
<control-speed control="EXTEND" transition-time="7"/>
|
||||
<control-output control="EXTEND" prop="/gear/gear[1]/position-norm"/>
|
||||
</gear>
|
||||
|
||||
<!-- Right Main -->
|
||||
<gear x="-0.09" y="-1.4" z="-1.34" compression="0.7" spring="1.8">
|
||||
<control-input axis="/controls/gear/wheel[2]/brake" control="BRAKE"/>
|
||||
<control-input axis="/controls/gear/parking-brake" control="BRAKE"/>
|
||||
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
|
||||
<control-speed control="EXTEND" transition-time="7"/>
|
||||
<control-output control="EXTEND" prop="/gear/gear[2]/position-norm"/>
|
||||
</gear>
|
||||
|
||||
<!-- Canopy -->
|
||||
<gear x="3.0" y="0.0" z="0.6" compression="0.6">
|
||||
<control-input axis="/controls/gear/parking-brake" control="EXTEND"/>
|
||||
<control-speed control="EXTEND" transition-time="10"/>
|
||||
<control-output control="EXTEND" prop="/gear/canopy/position-norm"/>
|
||||
</gear>
|
||||
|
||||
<!-- Ballast -->
|
||||
<ballast x="3.0" y="0" z="1.0" mass="1200"/> <!-- C/pit + Pilot -->
|
||||
<ballast x="3.5" y="0" z="-0.5" mass="1000"/> <!-- Gun -->
|
||||
<ballast x="2.0" y="0" z="0.0" mass="1000"/> <!-- trim ballast -->
|
||||
|
||||
</airplane>
|
||||
|
|
@ -1,135 +0,0 @@
|
|||
<!-- Hawker Sea Hawk yasim config. This is a hack and not an
|
||||
authentic representation of the aircraft. Having said
|
||||
that, the numbers, where I could find them, roughly match
|
||||
those of the original aircraft.
|
||||
Lee Elliott. leee-fgfs@spatial.freeserve.co.uk
|
||||
-->
|
||||
|
||||
<airplane mass="9720">
|
||||
|
||||
<!-- Approach configuration.
|
||||
I couldn't find any approach data but I think that the way
|
||||
the aircraft sits tail down on it's u/c indicates that it
|
||||
must land at a fairly shallow AoA to avoid hitting tail
|
||||
first. The speed is a guess.
|
||||
|
||||
I could see no sign or mention of spoilers or airbrakes in any
|
||||
of the docs or pictures I found.
|
||||
-->
|
||||
<approach speed="110" aoa="7">
|
||||
<control-setting axis="/controls/engines/engine[0]/throttle" value="0.5"/>
|
||||
<control-setting axis="/controls/flight/flaps" value="1.0"/>
|
||||
<control-setting axis="/controls/gear/gear-down" value="1"/>
|
||||
</approach>
|
||||
|
||||
<!-- Cruise configuration.
|
||||
Max speed at sea level is 599 mph = 521 knots. The same source
|
||||
also quoted 587 mph at 'altitude'.
|
||||
-->
|
||||
<cruise speed="521" alt="0">
|
||||
<control-setting axis="/controls/engines/engine[0]/throttle" value="1.0"/>
|
||||
<control-setting axis="/controls/flight/flaps" value="0.0"/>
|
||||
<control-setting axis="/controls/gear/gear-down" value="0"/>
|
||||
</cruise>
|
||||
|
||||
<cockpit x="3.0" y="0.0" z="0.7"/>
|
||||
|
||||
<fuselage ax="5.10" ay="0" az="0" bx="5.88" by="0" bz="0"
|
||||
width="1.3"/>
|
||||
|
||||
<!-- The wing length is from tips to fuselage, including intakes.
|
||||
The aileron figures are probably too low but the roll rate seemed
|
||||
too high otherwise.
|
||||
-->
|
||||
<wing x="0.1" y="0.65" z="0.0" taper="0.5" incidence="0.0"
|
||||
length="5.3" chord="3.0" sweep="-3.0" dihedral="3.0" camber="0.006">
|
||||
<stall aoa="17" width="3" peak="1.3"/>
|
||||
<flap0 start="0.1" end="0.4" lift="1.4" drag="1.6"/>
|
||||
<flap1 start="0.4" end="0.95" lift="1.05" drag="1.2"/>
|
||||
|
||||
<control-input axis="/controls/flight/flaps" control="FLAP0"/>
|
||||
<control-input axis="/controls/flight/aileron" control="FLAP1" split="true"/>
|
||||
<control-input axis="/controls/flight/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-output control="SPOILER" side="right"
|
||||
prop="/surface-positions/right-spoiler-pos-norm"/> -->
|
||||
|
||||
<control-speed control="FLAP0" transition-time="5"/>
|
||||
|
||||
</wing>
|
||||
|
||||
<hstab x="-5.2" y="0.10" z="0.76" taper="0.3" effectiveness="1.6"
|
||||
length="1.7" chord="1.2" sweep="0.0" dihedral="0.0" camber="0.0">
|
||||
<stall aoa="17" width="5" peak="1.5"/>
|
||||
<flap0 start="0" end="1" lift="1.5" drag="1.2"/>
|
||||
<control-input axis="/controls/flight/elevator" control="FLAP0"/>
|
||||
<control-input axis="/controls/flight/elevator-trim" control="FLAP0"/>
|
||||
<control-output control="FLAP0" prop="/surface-positions/elevator-pos-norm"/>
|
||||
</hstab>
|
||||
|
||||
<vstab x="-5.2" y="0.0" z="0.2" taper="0.8"
|
||||
length="1.4" chord="1.8" sweep="10.0">
|
||||
<stall aoa="16" width="5" peak="1.5"/>
|
||||
<flap0 start="0" end="1" lift="1.15" drag="1.3"/>
|
||||
<control-input axis="/controls/flight/rudder" control="FLAP0" invert="true"/>
|
||||
<control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm"/>
|
||||
</vstab>
|
||||
|
||||
<!-- Engines and tanks.
|
||||
1 x Roll-Royce Nene 103. I've no idea how much it actually
|
||||
weighs.
|
||||
-->
|
||||
<jet x="0.3" y="0.0" z="0.0" mass="1000" thrust="5200">
|
||||
<control-input axis="/controls/engines/engine[0]/throttle" control="THROTTLE"/>
|
||||
</jet>
|
||||
<!-- Fuel tanks in front, behind and above (saddle tank - actually feeds into
|
||||
tank two in real life) the engine. -->
|
||||
<tank x="1.4" y="0.0" z="0.0" jet="true" capacity="2000"/>
|
||||
<tank x="-1.3" y="0.0" z="0.0" jet="true" capacity="2000"/>
|
||||
<tank x="0.5" y="0.0" z="0.5" jet="true" capacity="1200"/>
|
||||
|
||||
<!-- Undercarriage -->
|
||||
<!-- nose -->
|
||||
<gear x="4.0" y="0.0" z="-1.39" retract-time="7" compression="0.6">
|
||||
<control-input axis="/controls/flight/rudder" control="STEER" square="true"/>
|
||||
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
|
||||
<control-speed control="EXTEND" transition-time="7"/>
|
||||
<control-output control="EXTEND" prop="/gear/gear/position-norm"/>
|
||||
</gear>
|
||||
|
||||
<!-- left main -->
|
||||
<gear x="0.08" y="1.4" z="-1.3" retract-time="7" compression="0.6">
|
||||
<control-input axis="/controls/gear/wheel[0]/brake" control="BRAKE"/>
|
||||
<control-input axis="/controls/gear/parking-brake" control="BRAKE"/>
|
||||
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
|
||||
<control-speed control="EXTEND" transition-time="7"/>
|
||||
<control-output control="EXTEND" prop="/gear/gear[0]/position-norm"/>
|
||||
</gear>
|
||||
|
||||
<!-- right main -->
|
||||
<gear x="0.08" y="-1.4" z="-1.3" retract-time="7" compression="0.6">
|
||||
<control-input axis="/controls/gear/wheel[1]/brake" control="BRAKE"/>
|
||||
<control-input axis="/controls/gear/parking-brake" control="BRAKE"/>
|
||||
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
|
||||
<control-speed control="EXTEND" transition-time="7"/>
|
||||
<control-output control="EXTEND" prop="/gear/gear[1]/position-norm"/>
|
||||
</gear>
|
||||
|
||||
<!-- Canopy -->
|
||||
<gear x="3.0" y="0.0" z="0.6" retract-time="7" compression="0.6">
|
||||
<control-input axis="/controls/gear/parking-brake" control="EXTEND"/>
|
||||
<control-speed control="EXTEND" transition-time="10"/>
|
||||
<control-output control="EXTEND" prop="/canopy/position-norm"/>
|
||||
</gear>
|
||||
|
||||
<!-- Ballast -->
|
||||
<ballast x="3.0" y="0" z="1.0" mass="1200"/> <!-- C/pit + Pilot -->
|
||||
<ballast x="3.5" y="0" z="-0.5" mass="1000"/> <!-- Gun -->
|
||||
<ballast x="2.0" y="0" z="0.0" mass="1000"/> <!-- trim ballast -->
|
||||
|
||||
</airplane>
|
||||
|
|
@ -1,141 +0,0 @@
|
|||
<!-- Hawker Sea Hawk yasim config. This is a hack and not an
|
||||
authentic representation of the aircraft. Having said
|
||||
that, the numbers, where I could find them, roughly match
|
||||
those of the original aircraft.
|
||||
Lee Elliott. leee-fgfs@spatial.freeserve.co.uk
|
||||
-->
|
||||
|
||||
<airplane mass="9720">
|
||||
|
||||
<!-- Approach configuration.
|
||||
I couldn't find any approach data but I think that the way
|
||||
the aircraft sits tail down on it's u/c indicates that it
|
||||
must land at a fairly shallow AoA to avoid hitting tail
|
||||
first. The speed is a guess.
|
||||
|
||||
I could see no sign or mention of spoilers or airbrakes in any
|
||||
of the docs or pictures I found.
|
||||
-->
|
||||
<approach speed="110" aoa="7">
|
||||
<control-setting axis="/controls/engines/engine[0]/throttle" value="0.5"/>
|
||||
<control-setting axis="/controls/flight/flaps" value="1.0"/>
|
||||
<control-setting axis="/controls/gear/gear-down" value="1"/>
|
||||
</approach>
|
||||
|
||||
<!-- Cruise configuration.
|
||||
Max speed at sea level is 599 mph = 521 knots. The same source
|
||||
also quoted 587 mph at 'altitude'.
|
||||
-->
|
||||
<cruise speed="521" alt="0">
|
||||
<control-setting axis="/controls/engines/engine[0]/throttle" value="1.0"/>
|
||||
<control-setting axis="/controls/flight/flaps" value="0.0"/>
|
||||
<control-setting axis="/controls/gear/gear-down" value="0"/>
|
||||
</cruise>
|
||||
|
||||
<cockpit x="3.0" y="0.0" z="0.7"/>
|
||||
|
||||
<fuselage ax="5.10" ay="0" az="0" bx="5.88" by="0" bz="0"
|
||||
width="1.3"/>
|
||||
|
||||
<!-- The wing length is from tips to fuselage, including intakes.
|
||||
The aileron figures are probably too low but the roll rate seemed
|
||||
too high otherwise.
|
||||
-->
|
||||
<wing x="0.1" y="0.65" z="0.0" taper="0.5" incidence="0.0"
|
||||
length="5.3" chord="3.0" sweep="-3.0" dihedral="3.0" camber="0.006">
|
||||
<stall aoa="17" width="3" peak="1.3"/>
|
||||
<flap0 start="0.1" end="0.4" lift="1.4" drag="1.6"/>
|
||||
<flap1 start="0.4" end="0.95" lift="1.05" drag="1.2"/>
|
||||
|
||||
<control-input axis="/controls/flight/flaps" control="FLAP0"/>
|
||||
<control-input axis="/controls/flight/aileron" control="FLAP1" split="true"/>
|
||||
<control-input axis="/controls/flight/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-output control="SPOILER" side="right"
|
||||
prop="/surface-positions/right-spoiler-pos-norm"/> -->
|
||||
|
||||
<control-speed control="FLAP0" transition-time="5"/>
|
||||
|
||||
</wing>
|
||||
|
||||
<hstab x="-5.2" y="0.10" z="0.76" taper="0.3" effectiveness="1.6"
|
||||
length="1.7" chord="1.2" sweep="0.0" dihedral="0.0" camber="0.0">
|
||||
<stall aoa="17" width="5" peak="1.5"/>
|
||||
<flap0 start="0" end="1" lift="1.5" drag="1.2"/>
|
||||
<control-input axis="/controls/flight/elevator" control="FLAP0"/>
|
||||
<control-input axis="/controls/flight/elevator-trim" control="FLAP0"/>
|
||||
<control-output control="FLAP0" prop="/surface-positions/elevator-pos-norm"/>
|
||||
</hstab>
|
||||
|
||||
<vstab x="-5.2" y="0.0" z="0.2" taper="0.8"
|
||||
length="1.4" chord="1.8" sweep="10.0">
|
||||
<stall aoa="16" width="5" peak="1.5"/>
|
||||
<flap0 start="0" end="1" lift="1.15" drag="1.3"/>
|
||||
<control-input axis="/controls/flight/rudder" control="FLAP0" invert="true"/>
|
||||
<control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm"/>
|
||||
</vstab>
|
||||
|
||||
<!-- Engines and tanks.
|
||||
1 x Roll-Royce Nene 103. I've no idea how much it actually
|
||||
weighs.
|
||||
-->
|
||||
<jet x="0.3" y="0.0" z="0.0" mass="1000" thrust="5200">
|
||||
<control-input axis="/controls/engines/engine[0]/throttle" control="THROTTLE"/>
|
||||
</jet>
|
||||
<!-- Fuel tanks in front of and behind the engine.
|
||||
-->
|
||||
<tank x="1.4" y="0.0" z="0.0" jet="true" capacity="2600"/>
|
||||
<tank x="-1.3" y="0.0" z="0.0" jet="true" capacity="2600"/>
|
||||
|
||||
<!-- Undercarriage -->
|
||||
<!-- nose -->
|
||||
<gear x="4.0" y="0.0" z="-1.39" retract-time="7" compression="0.6">
|
||||
<control-input axis="/controls/flight/rudder" control="STEER" square="true"/>
|
||||
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
|
||||
<control-speed control="EXTEND" transition-time="7"/>
|
||||
<control-output control="EXTEND" prop="/gear/gear/position-norm"/>
|
||||
</gear>
|
||||
|
||||
<!-- left main -->
|
||||
<gear x="0.08" y="1.4" z="-1.3" retract-time="7" compression="0.6">
|
||||
<control-input axis="/controls/gear/wheel[0]/brake" control="BRAKE"/>
|
||||
<control-input axis="/controls/gear/parking-brake" control="BRAKE"/>
|
||||
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
|
||||
<control-speed control="EXTEND" transition-time="7"/>
|
||||
<control-output control="EXTEND" prop="/gear/gear[0]/position-norm"/>
|
||||
</gear>
|
||||
|
||||
<!-- right main -->
|
||||
<gear x="0.08" y="-1.4" z="-1.3" retract-time="7" compression="0.6">
|
||||
<control-input axis="/controls/gear/wheel[1]/brake" control="BRAKE"/>
|
||||
<control-input axis="/controls/gear/parking-brake" control="BRAKE"/>
|
||||
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
|
||||
<control-speed control="EXTEND" transition-time="7"/>
|
||||
<control-output control="EXTEND" prop="/gear/gear[1]/position-norm"/>
|
||||
</gear>
|
||||
|
||||
<!-- Canopy -->
|
||||
<gear x="3.0" y="0.0" z="0.6" retract-time="7" compression="0.6">
|
||||
<control-input axis="/controls/gear/parking-brake" control="EXTEND"/>
|
||||
<control-speed control="EXTEND" transition-time="10"/>
|
||||
<control-output control="EXTEND" prop="/canopy/position-norm"/>
|
||||
</gear>
|
||||
|
||||
<!-- Wingman -->
|
||||
<gear x="3.0" y="0.0" z="0.6" retract-time="7" compression="0.6">
|
||||
<control-input axis="/controls/autoflight/wingman" control="EXTEND"/>
|
||||
<control-speed control="EXTEND" transition-time="10"/>
|
||||
<control-output control="EXTEND" prop="/wingman/position-norm"/>
|
||||
</gear>
|
||||
|
||||
<!-- Ballast -->
|
||||
<ballast x="3.0" y="0" z="1.0" mass="1200"/> <!-- C/pit + Pilot -->
|
||||
<ballast x="3.5" y="0" z="-0.5" mass="1000"/> <!-- Gun -->
|
||||
<ballast x="2.0" y="0" z="0.0" mass="1000"/> <!-- trim ballast -->
|
||||
|
||||
</airplane>
|
||||
|
|
@ -1,139 +0,0 @@
|
|||
<!-- TSR2 yasim config. This is a hack and not an authentic
|
||||
representation of the aircraft. Having said that, the
|
||||
numbers, where I could find them, roughly match those of
|
||||
the original aircraft. Lee Elliott.
|
||||
|
||||
The ailerons are a hack on this fdm - the real aircraft
|
||||
use all moving tail planes for roll and this model had a
|
||||
very high roll rate so they've been made relatively
|
||||
ineffective and in the model/anim file the aileron surface
|
||||
positions actually operate on the tailplanes.
|
||||
-->
|
||||
|
||||
<airplane mass="54750">
|
||||
|
||||
<!-- Approach configuration -->
|
||||
<approach speed="130" aoa="10.0">
|
||||
<control-setting axis="/controls/engines/engine[0]/throttle" value="0.2"/>
|
||||
<control-setting axis="/controls/engines/engine[1]/throttle" value="0.2"/>
|
||||
<control-setting axis="/controls/flight/flaps" value="1.0"/>
|
||||
<control-setting axis="/controls/flight/spoiler" value="0.2"/>
|
||||
<control-setting axis="/controls/gear/gear-down" value="1"/>
|
||||
</approach>
|
||||
|
||||
<!-- Cruise configuration -->
|
||||
<!-- <cruise speed="840" alt="1000"> -->
|
||||
<cruise speed="1197" alt="35000">
|
||||
<control-setting axis="/controls/engines/engine[0]/throttle" value="1.0"/>
|
||||
<control-setting axis="/controls/engines/engine[1]/throttle" value="1.0"/>
|
||||
<control-setting axis="/controls/engines/engine[0]/afterburner" value="1.0"/>
|
||||
<control-setting axis="/controls/engines/engine[1]/afterburner" value="1.0"/>
|
||||
<control-setting axis="/controls/flight/flaps" value="0.0"/>
|
||||
<control-setting axis="/controls/gear/gear-down" value="0"/>
|
||||
</cruise>
|
||||
|
||||
<cockpit x="8.5" y="0.0" z="1.0"/>
|
||||
|
||||
<fuselage ax="13.0" ay="0" az="0" bx="-14.13" by="0" bz=".64"
|
||||
width="2.0" taper="0.5" midpoint="0.3"/>
|
||||
|
||||
<wing x="-3.0" y="1.5" z="1.7" taper="0.25"
|
||||
length="5.0" chord="6.0" sweep="50" dihedral="-1.0" camber="0.003">
|
||||
<stall aoa="35.0" width="3" peak="1.3"/>
|
||||
<flap0 start="0.0" end="0.9" lift="1.4" drag="1.2"/>
|
||||
<flap1 start="0.0" end="0.4" lift="1.05" drag="1.2"/>
|
||||
<spoiler start="0.54" end="0.86" lift="0.0" drag="20.0"/>
|
||||
|
||||
<control-input axis="/controls/flight/flaps" control="FLAP0"/>
|
||||
<control-input axis="/controls/flight/aileron" control="FLAP1" split="true"/>
|
||||
<control-input axis="/controls/flight/aileron-trim" control="FLAP1" split="true"/>
|
||||
<control-input axis="/controls/flight/spoilers" control="SPOILER"/>
|
||||
|
||||
<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-output control="SPOILER" side="left"
|
||||
prop="/surface-positions/left-spoiler-pos-norm"/>
|
||||
<control-output control="SPOILER" side="right"
|
||||
prop="/surface-positions/right-spoiler-pos-norm"/>
|
||||
|
||||
<control-speed control="FLAP0" transition-time="5"/>
|
||||
<control-speed control="FLAP1" transition-time="0.5"/>
|
||||
<control-speed control="SPOILER" transition-time="0.5"/>
|
||||
|
||||
</wing>
|
||||
|
||||
<hstab x="-10.0" y="1.0" z="0.5" taper=".2" effectiveness="2.0"
|
||||
length="3.0" chord="4.0" sweep="55" dihedral="0.0">
|
||||
<stall aoa="35.0" width="3" peak="1.5"/>
|
||||
<flap0 start="0" end="1" lift="1.4" drag="1.3"/>
|
||||
<control-input axis="/controls/flight/elevator" control="FLAP0"/>
|
||||
<control-input axis="/controls/flight/elevator-trim" control="FLAP0"/>
|
||||
<control-output control="FLAP0" prop="/surface-positions/elevator-pos-norm"/>
|
||||
<control-speed control="FLAP0" transition-time="0.5"/>
|
||||
</hstab>
|
||||
|
||||
<vstab x="-10.0" y="0" z="1.38" taper=".176" effectiveness="1.0"
|
||||
length="4.5" chord="4.0" sweep="50">
|
||||
<stall aoa="28.0" width="3" peak="1.5"/>
|
||||
<flap0 start="0" end="1" lift="1.15" drag="1.3"/>
|
||||
<control-input axis="/controls/flight/rudder" control="FLAP0" invert="true"/>
|
||||
<control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm"/>
|
||||
</vstab>
|
||||
|
||||
<!-- nose -->
|
||||
<gear x="3.0" y="0" z="-2.0" retract-time="7" compression="0.8">
|
||||
<control-input axis="/controls/flight/rudder" control="STEER" square="true"/>
|
||||
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
|
||||
<control-speed control="EXTEND" transition-time="7"/>
|
||||
<control-output control="EXTEND" prop="/gear/gear/position-norm"/>
|
||||
</gear>
|
||||
|
||||
<!-- left main -->
|
||||
<gear x="-4.0" y="2.5" z="-2.0" retract-time="7" compression="0.8">
|
||||
<control-input axis="/controls/gear/wheel[0]/brake" control="BRAKE"/>
|
||||
<control-input axis="/controls/gear/parking-brake" control="BRAKE"/>
|
||||
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
|
||||
<control-speed control="EXTEND" transition-time="7"/>
|
||||
<control-output control="EXTEND" prop="/gear/gear[0]/position-norm"/>
|
||||
</gear>
|
||||
|
||||
<!-- right main -->
|
||||
<gear x="-4.0" y="-2.5" z="-2.0" retract-time="7" compression="0.8">
|
||||
<control-input axis="/controls/gear/wheel[1]/brake" control="BRAKE"/>
|
||||
<control-input axis="/controls/gear/parking-brake" control="BRAKE"/>
|
||||
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
|
||||
<control-speed control="EXTEND" transition-time="7"/>
|
||||
<control-output control="EXTEND" prop="/gear/gear[1]/position-norm"/>
|
||||
</gear>
|
||||
|
||||
<!-- Canopy -->
|
||||
<gear x="3.0" y="0.0" z="0.6" retract-time="7" compression="0.6">
|
||||
<control-input axis="/controls/gear/parking-brake" control="EXTEND"/>
|
||||
<control-speed control="EXTEND" transition-time="10"/>
|
||||
<control-output control="EXTEND" prop="/canopy/position-norm"/>
|
||||
</gear>
|
||||
|
||||
<jet x="-8.0" y="-1.0" z="0.4" mass="4000" thrust="16600" afterburner="30600">
|
||||
<!-- <jet x="-22.0" y="-1.0" z=".44" mass="4000" thrust="30600"> -->
|
||||
<control-input axis="/controls/engines/engine[0]/throttle" control="THROTTLE"/>
|
||||
<control-input axis="/controls/engines/engine[0]/afterburner" control="REHEAT"/>
|
||||
</jet>
|
||||
|
||||
<jet x="-8.0" y="1.0" z="0.4" mass="4000" thrust="16600" afterburner="30600">
|
||||
<!-- <jet x="-22.0" y="1.0" z=".44" mass="4000" thrust="30600"> -->
|
||||
<control-input axis="/controls/engines/engine[1]/throttle" control="THROTTLE"/>
|
||||
<control-input axis="/controls/engines/engine[1]/afterburner" control="REHEAT"/>
|
||||
</jet>
|
||||
|
||||
<tank x="-2.0" y="0.0" z="0.5" jet="true" capacity="13000"/>
|
||||
<tank x="-3.0" y="2.5" z="1.7" jet="true" capacity="11000"/>
|
||||
<tank x="-3.0" y="-2.5" z="1.7" jet="true" capacity="11000"/>
|
||||
|
||||
<ballast x="8.5" y="0" z="0" mass="3000"/> <!-- Cockpit -->
|
||||
<ballast x="4.0" y="0" z="0" mass="3000"/> <!-- avionics -->
|
||||
<ballast x="-6.0" y="0" z="0" mass="100"/> <!-- Trim ballast -->
|
||||
|
||||
</airplane>
|
||||
|
|
@ -1,179 +0,0 @@
|
|||
<!-- There weren't many YF23s - just the two prototypes - and I
|
||||
couldn't find much 'hard' information so a lot of this fdm is
|
||||
guess work (GW).
|
||||
-->
|
||||
<!-- Max take off wieght is 64000lb but I imagine that this
|
||||
includes some weapons so I'm allocating 8000lb to his and
|
||||
subtracting it from the max wieght.
|
||||
|
||||
I got a figure of 24000lb for the fuel load from a web site.
|
||||
this seems rather high to me but until I can get a better
|
||||
figure it'll have to do.
|
||||
-->
|
||||
<airplane mass="32000">
|
||||
|
||||
<!-- Approach configuration -->
|
||||
<!-- From GW & photos -->
|
||||
<approach speed="130" aoa="5">
|
||||
<control-setting axis="/controls/engines/engine[0]/throttle" value="0.15"/>
|
||||
<control-setting axis="/controls/engines/engine[1]/throttle" value="0.15"/>
|
||||
<control-setting axis="/controls/engines/engine[0]/afterburner" value="0"/>
|
||||
<control-setting axis="/controls/engines/engine[1]/afterburner" value="0"/>
|
||||
<control-setting axis="/controls/flight/flaps" value="1"/>
|
||||
<control-setting axis="/controls/flight/slats" value="0"/>
|
||||
<control-setting axis="/controls/gear/gear-down" value="1"/>
|
||||
</approach>
|
||||
|
||||
<!-- Cruise configuration -->
|
||||
<cruise speed="600" alt="55000">
|
||||
<control-setting axis="/controls/engines/engine[0]/throttle" value="0.9"/>
|
||||
<control-setting axis="/controls/engines/engine[1]/throttle" value="0.9"/>
|
||||
<control-setting axis="/controls/engines/engine[0]/afterburner" value="0"/>
|
||||
<control-setting axis="/controls/engines/engine[1]/afterburner" value="0"/>
|
||||
<control-setting axis="/controls/flight/flaps" value="0.0"/>
|
||||
<control-setting axis="/controls/flight/slats" value="0"/>
|
||||
<control-setting axis="/controls/gear/gear-down" value="0"/>
|
||||
</cruise>
|
||||
|
||||
<cockpit x="5.70" y="0.00" z="1.26"/>
|
||||
|
||||
<!-- Fuselage entries for the fuselage proper and the two
|
||||
engine housings.
|
||||
-->
|
||||
<!-- Fuselage -->
|
||||
<fuselage ax="10.00" ay="0.00" az="0.00"
|
||||
bx="-2.00" by="0.00" bz="0.00"
|
||||
width="1.6" taper="0.5" midpoint="0.5"/>
|
||||
|
||||
<!-- Left engine housing -->
|
||||
<fuselage ax="-2.00" ay="1.80" az="0.00"
|
||||
bx="-8.00" by="1.20" bz="0.60"
|
||||
width="1.2" taper="0" midpoint="0.3"/>
|
||||
|
||||
<!-- Right engine housing -->
|
||||
<fuselage ax="-2.00" ay="-1.80" az="0.00"
|
||||
bx="-8.00" by="-1.20" bz="0.60"
|
||||
width="1.2" taper="0" midpoint="0.3"/>
|
||||
|
||||
<!-- Lots of guesswork here -->
|
||||
<wing x="-2.00" y="0.00" z="0.25" length="6.66" chord="12.00" taper="0.08"
|
||||
sweep="0" dihedral="0" camber="0.001" incidence="0.0" idrag="1.6">
|
||||
<stall aoa="25" width="3" peak="1.3"/>
|
||||
<flap0 start="0.36" end="0.63" lift="1.3" drag="1.8"/>
|
||||
<flap1 start="0.63" end="0.89" lift="1.2" drag="1.8"/>
|
||||
<slat start="0.36" end="0.89" aoa="6" drag="1.3"/>
|
||||
|
||||
<!-- Shortened wing that starts outboard of the engine intakes.
|
||||
<wing x="-2.00" y="2.40" z="0.25" length="4.2" chord="8.1"
|
||||
taper="0.19" sweep="0" dihedral="0" camber="0.0" incidence="0.0">
|
||||
<stall aoa="35" width="2" peak="1.3"/>
|
||||
<flap0 start="0.0" end="0.42" lift="1.5" drag="1.6"/>
|
||||
<flap1 start="0.42" end="0.833" lift="1.05" drag="1.3"/>
|
||||
-->
|
||||
<control-input axis="/controls/flight/flaps" control="FLAP0"/>
|
||||
<control-input axis="/controls/flight/aileron" control="FLAP1" split="true"/>
|
||||
<control-input axis="/controls/flight/aileron-trim" control="FLAP1" split="true"/>
|
||||
|
||||
<control-input axis="/controls/flight/slats" control="SLAT"/>
|
||||
|
||||
<control-input axis="/controls/flight/rudder" control="FLAP1" split="true" invert="true"/>
|
||||
|
||||
<control-input axis="/controls/flight/spoilers" control="FLAP0"/>
|
||||
<control-input axis="/controls/flight/spoilers" control="FLAP1" invert="true"/>
|
||||
|
||||
<control-output control="FLAP0" prop="/surface-positions/left-flap-pos-norm"/>
|
||||
<control-output control="FLAP0" prop="/surface-positions/right-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-output control="SLAT" side="left" prop="/surface-positions/left-slat-pos-norm"/>
|
||||
<control-output control="SLAT" side="right" prop="/surface-positions/right-slat-pos-norm"/>
|
||||
|
||||
<control-speed control="FLAP0" transition-time="2"/>
|
||||
<control-speed control="FLAP1" transition-time="0.5"/>
|
||||
<control-speed control="SLAT" transition-time="0.5"/>
|
||||
</wing>
|
||||
|
||||
<hstab x="-8.70" y="2.40" z="0.36" length="3.30" chord="5.10"
|
||||
taper="0.11" sweep="0" dihedral="40" camber="0.01" effectiveness="2">
|
||||
<stall aoa="24" width="2" peak="1.3"/>
|
||||
<flap0 start="0" end="1" lift="1.25" drag="1.4"/>
|
||||
|
||||
<control-input axis="/controls/flight/elevator" control="FLAP0"/>
|
||||
<control-input axis="/controls/flight/elevator-trim" control="FLAP0"/>
|
||||
|
||||
<control-input axis="/controls/flight/rudder" control="FLAP0" split="true" square="false" invert="true"/>
|
||||
|
||||
<control-output control="FLAP0" side="left" prop="/surface-positions/left-elevator-pos-norm"/>
|
||||
<control-output control="FLAP0" side="right" prop="/surface-positions/right-elevator-pos-norm"/>
|
||||
|
||||
<control-speed control="FLAP0" transition-time="0.5"/>
|
||||
</hstab>
|
||||
|
||||
<!-- I couldn't find a figure for the mass so it's guess work.
|
||||
-->
|
||||
<jet x="-6.26" y="1.20" z="0.60" mass="3000" thrust="24500" afterburner="35000">
|
||||
<control-input axis="/controls/engines/engine[0]/throttle" control="THROTTLE"/>
|
||||
<control-input axis="/controls/engines/engine[0]/afterburner" control="REHEAT"/>
|
||||
</jet>
|
||||
|
||||
<jet x="-6.26" y="-1.20" z="0.60" mass="3000" thrust="24500" afterburner="35000">
|
||||
<control-input axis="/controls/engines/engine[1]/throttle" control="THROTTLE"/>
|
||||
<control-input axis="/controls/engines/engine[1]/afterburner" control="REHEAT"/>
|
||||
</jet>
|
||||
|
||||
<!-- Front -->
|
||||
<gear x="5.25" y="0.00" z="-2.25" compression="0.65" spring="2.5">
|
||||
<control-input axis="/controls/flight/rudder" control="STEER" square="true"/>
|
||||
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
|
||||
<control-input axis="/controls/gear/gear[0]/wheel[0]/brake" control="BRAKE"/>
|
||||
<control-output control="EXTEND" prop="/gear/gear[0]/position-norm"/>
|
||||
<control-output control="STEER" prop="/gear/gear[0]/steering-norm"/>
|
||||
<control-speed control="EXTEND" transition-time="4"/>
|
||||
</gear>
|
||||
|
||||
<!-- Left main -->
|
||||
<gear x="-2.20" y="1.92" z="-2.9" compression="2.0" spring="2.5">
|
||||
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
|
||||
<control-input axis="/controls/gear/gear[1]/wheel[0]/brake" control="BRAKE"/>
|
||||
<control-output control="EXTEND" prop="/gear/gear[1]/position-norm"/>
|
||||
<control-speed control="EXTEND" transition-time="4"/>
|
||||
</gear>
|
||||
|
||||
<!-- Right main -->
|
||||
<gear x="-2.20" y="-1.92" z="-2.9" compression="2.0" spring="2.5">
|
||||
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
|
||||
<control-input axis="/controls/gear/gear[2]/wheel[0]/brake" control="BRAKE"/>
|
||||
<control-output control="EXTEND" prop="/gear/gear[2]/position-norm"/>
|
||||
<control-speed control="EXTEND" transition-time="4"/>
|
||||
</gear>
|
||||
|
||||
<!-- Canopy -->
|
||||
<gear x="4.1" y="0.0" z="1.05" retract-time="7" compression="0.6">
|
||||
<control-input axis="/controls/gear/parking-brake" control="EXTEND"/>
|
||||
<control-speed control="EXTEND" transition-time="10"/>
|
||||
<control-output control="EXTEND" prop="/canopy/position-norm"/>
|
||||
</gear>
|
||||
|
||||
<!-- The locations and capcities are guesswork. -->
|
||||
<!-- Fuselage tank -->
|
||||
<tank x="1.5" y="0" z="0.68" jet="true" capacity="8000"/>
|
||||
<!-- Left wing tank -->
|
||||
<tank x="-1.40" y="2" z="0.0" jet="true" capacity="8000"/>
|
||||
<!-- Right wing tank -->
|
||||
<tank x="-1.40" y="-2" z="0.0" jet="true" capacity="8000"/>
|
||||
|
||||
<!-- Avionics -->
|
||||
<ballast x="4" y="0" z="0.6" mass="3000"/>
|
||||
|
||||
<!-- Cockpit and radar -->
|
||||
<ballast x="7" y="0" z="0.2" mass="1500"/>
|
||||
|
||||
<!-- Pilot -->
|
||||
<ballast x="5.8" y="0" z="0.6" mass="200"/>
|
||||
|
||||
<!-- Trim ballast -->
|
||||
<ballast x="6" y="0" z="0.0" mass="2000"/>
|
||||
|
||||
</airplane>
|
||||
37
Aircraft/c172p/c172p-3d-jsbsim-set.xml
Normal file
37
Aircraft/c172p/c172p-3d-jsbsim-set.xml
Normal file
|
|
@ -0,0 +1,37 @@
|
|||
<?xml version="1.0"?>
|
||||
<!--
|
||||
************************************************************************
|
||||
JSBSim Cessna 172P with 3D cockpit.
|
||||
|
||||
Started October 23 2001 by John Check, fgpanels@rockfish.net
|
||||
************************************************************************
|
||||
-->
|
||||
|
||||
<PropertyList include="c172p-jsbsim-base.xml">
|
||||
|
||||
<sim>
|
||||
|
||||
<description>Cessna 172P (JSBSim, 3D cockpit)</description>
|
||||
|
||||
<!-- hide the 2D panel -->
|
||||
|
||||
<panel>
|
||||
<visibility archive="y">false</visibility>
|
||||
</panel>
|
||||
|
||||
<!-- position the pilot viewpoint and angle -->
|
||||
|
||||
<view>
|
||||
<internal archive="y">true</internal>
|
||||
<config>
|
||||
<x-offset-m archive="y">-0.18</x-offset-m>
|
||||
<y-offset-m archive="y">0.30</y-offset-m>
|
||||
<z-offset-m archive="y">0.36</z-offset-m>
|
||||
<pitch-offset-deg>-12</pitch-offset-deg>
|
||||
</config>
|
||||
</view>
|
||||
|
||||
|
||||
</sim>
|
||||
|
||||
</PropertyList>
|
||||
7
Aircraft/c172p/c172p-3d-set.xml
Normal file
7
Aircraft/c172p/c172p-3d-set.xml
Normal file
|
|
@ -0,0 +1,7 @@
|
|||
<?xml version="1.0"?>
|
||||
|
||||
<PropertyList include="c172p-3d-jsbsim-set.xml">
|
||||
<sim>
|
||||
<description>Alias for c172p-3d-jsbsim.</description>
|
||||
</sim>
|
||||
</PropertyList>
|
||||
42
Aircraft/c172p/c172p-base.xml
Normal file
42
Aircraft/c172p/c172p-base.xml
Normal file
|
|
@ -0,0 +1,42 @@
|
|||
<?xml version="1.0"?>
|
||||
<!--
|
||||
************************************************************************
|
||||
Common configuration for all C172P aircraft.
|
||||
************************************************************************
|
||||
-->
|
||||
|
||||
<PropertyList include="../c172/c172-base.xml">
|
||||
|
||||
<sim>
|
||||
|
||||
<model>
|
||||
<path archive="y">Aircraft/c172p/Models/c172p.xml</path>
|
||||
</model>
|
||||
|
||||
</sim>
|
||||
|
||||
<autopilot>
|
||||
<config>
|
||||
<min-climb-speed-kt type="float">70.0</min-climb-speed-kt>
|
||||
<best-climb-speed-kt type="float">75.0</best-climb-speed-kt>
|
||||
<target-climb-rate-fpm type="float">500.0</target-climb-rate-fpm>
|
||||
<target-descent-rate-fpm type="float">1000.0</target-descent-rate-fpm>
|
||||
<elevator-adj-factor type="float">4000.0</elevator-adj-factor>
|
||||
<integral-contribution type="float">0.01</integral-contribution>
|
||||
<zero-pitch-throttle type="float">0.45</zero-pitch-throttle>
|
||||
<zero-pitch-trim-full-throttle type="float">0.14</zero-pitch-trim-full-throttle>
|
||||
</config>
|
||||
</autopilot>
|
||||
|
||||
<consumables>
|
||||
<fuel>
|
||||
<tank n="0">
|
||||
<level-gal_us>20</level-gal_us>
|
||||
</tank>
|
||||
<tank n="1">
|
||||
<level-gal_us>20</level-gal_us>
|
||||
</tank>
|
||||
</fuel>
|
||||
</consumables>
|
||||
|
||||
</PropertyList>
|
||||
24
Aircraft/c172p/c172p-jsbsim-base.xml
Normal file
24
Aircraft/c172p/c172p-jsbsim-base.xml
Normal file
|
|
@ -0,0 +1,24 @@
|
|||
<?xml version="1.0"?>
|
||||
<!--
|
||||
************************************************************************
|
||||
Common configuration for JSBSim C172P aircraft.
|
||||
************************************************************************
|
||||
-->
|
||||
|
||||
<PropertyList include="c172p-base.xml">
|
||||
|
||||
<sim>
|
||||
<flight-model archive="y">jsb</flight-model>
|
||||
<aero archive="y">c172p</aero>
|
||||
</sim>
|
||||
|
||||
<!-- trim for level cruise -->
|
||||
|
||||
<controls>
|
||||
<flight>
|
||||
<aileron-trim>0.027</aileron-trim>
|
||||
<rudder-trim>0.0</rudder-trim>
|
||||
</flight>
|
||||
</controls>
|
||||
|
||||
</PropertyList>
|
||||
36
Aircraft/c172p/c172p-jsbsim-set.xml
Normal file
36
Aircraft/c172p/c172p-jsbsim-set.xml
Normal file
|
|
@ -0,0 +1,36 @@
|
|||
<?xml version="1.0"?>
|
||||
<!--
|
||||
************************************************************************
|
||||
JSBSim Cessna 172P with 2D panel.
|
||||
|
||||
Started October 23 2001 by John Check, fgpanels@rockfish.net
|
||||
************************************************************************
|
||||
-->
|
||||
|
||||
<PropertyList include="c172p-jsbsim-base.xml">
|
||||
|
||||
<sim>
|
||||
|
||||
<description>Cessna 172P (JSBSim, 2D panel).</description>
|
||||
|
||||
<!-- Use a 2D instrument panel -->
|
||||
|
||||
<panel>
|
||||
<path>Aircraft/c172/Panels/c172-vfr-panel.xml</path>
|
||||
<visibility archive="y">true</visibility>
|
||||
</panel>
|
||||
<panel_2>
|
||||
<path>Aircraft/c172/Panels/c172-trans-mini-panel.xml</path>
|
||||
</panel_2>
|
||||
|
||||
<!-- Look down a bit over the top of the panel -->
|
||||
|
||||
<view>
|
||||
<config>
|
||||
<pitch-offset-deg>-8</pitch-offset-deg>
|
||||
</config>
|
||||
</view>
|
||||
|
||||
</sim>
|
||||
|
||||
</PropertyList>
|
||||
7
Aircraft/c172p/c172p-set.xml
Normal file
7
Aircraft/c172p/c172p-set.xml
Normal file
|
|
@ -0,0 +1,7 @@
|
|||
<?xml version="1.0"?>
|
||||
|
||||
<PropertyList include="c172p-jsbsim-set.xml">
|
||||
<sim>
|
||||
<description>Alias for c172p-jsbsim.</description>
|
||||
</sim>
|
||||
</PropertyList>
|
||||
36
Aircraft/ufo/ufo-set.xml
Normal file
36
Aircraft/ufo/ufo-set.xml
Normal file
|
|
@ -0,0 +1,36 @@
|
|||
<?xml version="1.0"?>
|
||||
<!--
|
||||
************************************************************************
|
||||
Cessna 172 simulation config. This files ties together all the components
|
||||
used by FGFS to represent the C172. Components include the flight data
|
||||
model, instrument panel, and external 3D model.
|
||||
3D models can be downloaded from http://home.t-online.de/home/Wolfram.Kuss/
|
||||
|
||||
October 23 2001 John Check, fgpanels@rockfish.net
|
||||
************************************************************************
|
||||
-->
|
||||
|
||||
<PropertyList>
|
||||
|
||||
<sim>
|
||||
|
||||
<description>UFO from the 'White Project' of the UNESCO</description>
|
||||
|
||||
<flight-model>ufo</flight-model>
|
||||
|
||||
<sound>
|
||||
<audible>true</audible>
|
||||
<path>Aircraft/ufo/ufo-sound.xml</path>
|
||||
</sound>
|
||||
|
||||
<panel>
|
||||
<visibility>false</visibility>
|
||||
</panel>
|
||||
|
||||
<model>
|
||||
<path>Aircraft/ufo/Models/ufo.xml</path>
|
||||
</model>
|
||||
|
||||
</sim>
|
||||
|
||||
</PropertyList>
|
||||
Loading…
Reference in a new issue