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Move *-set.xml and Aircraft-yasim/*.xml into their individual aircraft

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subdirectories in yet another step towards making aircraft more self
contained rather than potentially spread out.
This commit is contained in:
curt 2003-09-20 03:57:12 +00:00
parent 788adc9e6b
commit 98804a6793
30 changed files with 189 additions and 3371 deletions
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133
Aircraft-yasim/747.xml
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<airplane mass="400000">
<!-- Approach configuration -->
<approach speed="136" aoa="7">
<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/slats" value="1.0"/>
<control-setting axis="/controls/gear/gear-down" value="1"/>
</approach>
<!-- Cruise configuration -->
<cruise speed="490" alt="36000">
<control-setting axis="/controls/engines/engine[0]/throttle" value="0.75"/>
<control-setting axis="/controls/engines/engine[1]/throttle" value="0.75"/>
<control-setting axis="/controls/flight/flaps" value="0.0"/>
<control-setting axis="/controls/gear/gear-down" value="0"/>
</cruise>
<cockpit x="19.08" y="1.81" z="15.06"/>
<fuselage ax="24.5" ay="0" az="0" bx="-45.36" by="0.00" bz="2.41"
width="6" taper="0.3" midpoint="0.2"/>
<wing x="-2" y="3.01" z="-1.45" length="33.72" chord="13.25" sweep="33"
taper=".27" dihedral="7" camber="0.15" incidence="-0.7">
<stall aoa="12" width="2" peak="2"/>
<flap0 start="0" end=".56" lift="1.8" drag="1.2"/>
<flap1 start=".64" end=".88" lift="1.3" drag="1.2"/>
<slat start="0" end="1" aoa="2" drag="1.1"/>
<spoiler start="0.2" end="0.6" lift="0.3" drag="2.0"/>
<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/slats" control="SLAT"/>
<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-speed control="FLAP0" transition-time="10"/>
</wing>
<hstab x="-38.13" y="1.81" z="1.81" chord="8.43" length="10.84" taper=".29"
sweep="28" dihedral="7" camber="-0.1" effectiveness="2.3">
<stall aoa="15" width="2" 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="-38.13" y="0.00" z="3.61" chord="12.04" length="12.04" taper="0.3"
sweep="33">
<stall aoa="15" width="2" peak="1.5"/>
<flap0 start="0" end="1" lift="1.2" drag="1.3"/>
<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>
<!-- The CF6 engines are rated at 60000 lbs thrust, flat rated to 33 -->
<!-- degrees C. Corrected to YASim's standard atmosphere temperature -->
<!-- of 288.2 kelvins, that gives 63737 lbs of nominal thrust. -->
<jet x="-10.43" y="16.26" z="-1.20" mass="8000" thrust="63737">
<control-input axis="/controls/engines/engine[0]/throttle" control="THROTTLE"/>
</jet>
<jet x="-2" y="12.65" z="-2.41" mass="8000" thrust="63737">
<control-input axis="/controls/engines/engine[0]/throttle" control="THROTTLE"/>
</jet>
<jet x="-2" y="-12.65" z="-2.41" mass="8000" thrust="63737">
<control-input axis="/controls/engines/engine[1]/throttle" control="THROTTLE"/>
</jet>
<jet x="-10.43" y="-16.26" z="-1.20" mass="8000" thrust="63737">
<control-input axis="/controls/engines/engine[1]/throttle" control="THROTTLE"/>
</jet>
<!-- nose -->
<gear x="19.08" y="0.00" z="-5.42"
compression="0.75" spring="0.7" damp="4">
<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-speed control="EXTEND" transition-time="7"/>
</gear>
<gear x="-4.65" y="5.42" z="-5.42" compression="1.1"> <!-- fwd left main -->
<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>
<gear x="-6.82" y="1.81" z="-5.42" compression="1.1"> <!-- rear left main -->
<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[2]/position-norm"/>
<control-speed control="EXTEND" transition-time="7"/>
</gear>
<gear x="-6.82" y="-1.81" z="-5.42" compression="1.1"> <!-- rear right main -->
<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[3]/position-norm"/>
<control-speed control="EXTEND" transition-time="7"/>
</gear>
<gear x="-4.65" y="-5.42" z="-5.42" compression="1.1"> <!-- fwd right main -->
<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[4]/position-norm"/>
<control-speed control="EXTEND" transition-time="7"/>
</gear>
<tank x="-2" y="0" z="-1.45" jet="true" capacity="128000"/>
<tank x="-5.6" y="8" z="-1.45" jet="true" capacity="128000"/>
<tank x="-5.6" y="-8" z="-1.45" jet="true" capacity="128000"/>
<ballast x="18.5" y="0" z="2.4" mass="30000"/> <!-- hump -->
<ballast x="12.5" y="0" z="2.4" mass="40000"/> <!-- hump -->
<ballast x="6.5" y="0" z="2.4" mass="40000"/> <!-- hump -->
<ballast x="0.5" y="0" z="2.4" mass="30000"/> <!-- hump -->
</airplane>

233
Aircraft-yasim/README.j3cub
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PIPER J3 CUB PERFORMANCE DATA
=============================
[This information is copied from the 1946 J3C-65 owner's handbook.]
FLYING HINTS
The Piper Cub Special represents more than 15 years of diligent
aircraft engineering and manufacturing experience. Its simplicity of
design and construction, its low operating and maintenance costs, its
inherent stability, ruggedness, and its outstanding safety and ease of
flying, have made it the most popular airplane in aviation history.
The Piper Cub Special is the time-tested product of millions of hours
of flying under all conceivable conditions both in the military and in
peace time.
There are hints on starting, flying, stopping, and other related
topics that are important to the owner who wants to conserve his
airplane -- keep it in maximum airworthy condition -- and enjoy a full
measure of flying satisfaction.
First, each pilot should become familiar enough with his Piper Cub
Special that he can accomplish a satisfactory pre-flight inspection.
This check is simple and requires only a few minutes. See Section IX
for check list. Daily check of airplane prior to flight should be the
first in a number of safe flying habits the pilot should acquire.
A. BEFORE STARTING ENGINE
(1) Make routine check of gasoline supply. Visible fuel gauge is
integral part of gas tank cap; it will not show number of gallons but
will show proportion of fuel in tank by length of rod which extends
upward from cap. A full tank of 12 U.S. gallons will be indicated by
11 inches of rod extending beyond cap. Keep gas gauge rod clean and
smooth with crocus cloth for accuracy and freedom of movement.
(2) Check oil level in engine sump by removing oil cap and gauge. Oil
stick should indicate oil level up to index mark of 4 quarts.
(3) Check freedom of movement of flight and engine controls.
B. STARTING ENGINE
(1) Chock wheels, or have occupant who is familiar with controls set
brakes in cabin.
(2) Ignition switch OFF. Verify.
(3) Set throttle approximately 1/10 open.
(4) Push fuel shut-off ON.
(5) Turn propeller through several times.
(6) Turn ignition switch ON.
(7) Start engine by pulling propeller through with a snap.
CAUTION -- Always handle propeller as if switch were "ON." Stand as
far in front of propeller as possible. Use both hands and grasp one
blad approximately midway from tip. Do not overgrasp blade. Do not
wear long, loose clothing. Make sure footing is sure to preclude
possibility of feet slipping.
(8) If engine does not start, turn switch OFF. Turn primer knob to
unlock, pull out, pump three or four times, then reseat primer and
lock by turning in opposite direction. In extremely cold weather a
few strokes of the primer as the engine starts will enable it to keep
running. NOTE -- Avoid excessive priming as it causes raw gasoline to
wash lubricating oil from engine cylinder walls. Do not prime warm
engine.
(9) Repeat starting procedures 6, 7.
(10) If engine loads up and refuses to start, turn ignition switch
"OFF,", open throttle wide and turn propeller through backwards
several times to unload excessive gas mixture in cylinders. Then
close throttle and repeat starting procedure.
C. ENGINE WARM-UP
(1) As soon as engine starts, advance throttle slightly to idle at 700
R.P.M. Check engine instruments. If oil pressure gauge does not
indicate pressure within 30 seconds, stop engine immediately, check
and correct trouble before any further operation. Oil temperature
during operating should not rise above 200° F. and oil pressure should
not fall below 30 pounds. With engine warm, idling speed should be
550-600 R.P.M.
(2) Rev engine up to 2100 R.P.M. on both magnetos. Switch to LEFT and
RIGHT magnetos. R.P.M. drop should not be over 75 R.P.M. CAUTION
--Do not operate engine on either single magneto for more than 30
seconds at a time, as this tends to foul the non-operating spark plugs
in the ignition circuit of the magneto that is switched off.
D. STOPPING ENGINE
(1) Never cut switch immediately after landing as this causes engine
to cool too rapidly.
(2) Idle engine, especially in high temperature operating conditions,
for several minutes. It is advisable to switch to each magneto for 30
second intervals to allow gradual cooling of engine. This helps to
prevent overheating of spark plug insulators and will lessen tendency
for "after-firing."
(3) Check for carburetor heat OFF during idling.
E. TAXIING
(1) Open throttle to start airplane in motion; then close throttle to
a setting sufficient to keep airplane rolling. Do not keep throttle
advanced so that it is necessary to control taxi speed of airplane
with brakes. This causes unnecessary wear and tear on brakes and
tires.
(2) Taxi slowly (speed of a fast walk) controlling direction with
rudder which is connected to a steerable tail wheel. Use brakes only
for positive, precision ground control when necessary.
(3) Taxi upwind with stick back; downwind with stick foreward. When
ground winds are in excess of 15 M.P.H., turn into wind using ailerons
in direction of turn; apply ailerons away from the turn when turning
downwind. This procedure helps to prevent the wind "picking up" a
wing during windy, gusty conditions. Always make ground turns slowly.
F. GENERAL FLYING
(1) For takeoff use full throttle, heading into wind. Airplane loaded
will become airborne at approximately 39 M.P.H. Best climb speed is
an indicated 55 M.P.H.
(2) Indicated R.P.M. for cruising speed of 73 M.P.H. is 2150.
Take-off R.P.M. is 2300. Do not fly at full throttle over 3 minutes.
(3) Use CARBURETOR AIR HEAT when engine runs "rough" and tachometer
shows drop in R.P.M. which may be due to ice forming in carburetor.
Tachometer should recover to within 50 R.P.M. below normal when using
carburetor heat. Push heater to "OFF" position, and if icing
condition has been cleared, R.P.M. should return to normal. Continued
use of carburetor heat will only cause increased fuel consumption and
loss of power.
(4) Maximum permissible diving speed is 122 M.P.H.
G. APPROACH AND LANDING
(1) Push carburetor heat ON prior to throttling back for glide, or for
any other flight maneuver.
(2) Glide between 50-60 M.P.H. depending upon loading of airplane and
gust conditions.
NOTE -- "Clear" engine by opening throttle gently, every 200-250 feet
of descent during a long glide so that engine temperature will be
maintained.
Throttle action on the part of the pilot should be smooth and gentle
at all times.
H. PARKING AND MOORING
(1) After termination of flight, enter flying time in aircraft and
engine log books.
(2) Turn ignition and fuel OFF.
(3) Chcok the wheels of airplane.
(4) If airplane is not to be flown for some time, it should be
hangared or tied down. Use good quality 1/2" - 5/8" diameter rope.
Secure to lift assist handle at aft end of fuselage; also at upper end
of both front wing lift struts where they attach to wing. Make sure
that rope passes between aileron cable and lift strut. Mooring ropes,
when airplane is tied down, should have no slack.
(5) Lock aileron and elevator controls by wrapping front seat belt
completely around rear control stick, tighten and buckle.
(6) Under excessively wind conditions, airplane should be tailed into
wind for mooring.
[Here is my older information.]
These are the only numbers I could find. They are for a J3 Cub with
an 85HP engine rather than 65 hp, so some adjustments may be
necessary. The source is
http://www.evergreenfs.com/planedata.htm
Speeds
------
Best rate of climb (Vy): 65 mph (57 kt)
Best angle of climb (Vx): 55 mph (48 kt)
Cruise: 70 mph (61 kt)
Never-exceed (Vne): 122 mph (106 kt)
Best Glide (Vglide): 60 mph (52 kt)
Stall (Vs): 38 mph (33 kt)
Maneuvering (Va): 70 mph (61 kt)
Approach: 50-60 mph (44-52 kt)
Power
-----
Take off: full
Climb: 50 rpm below full
Cruise: 2300 rpm
Approach: 1200 rpm
Practice stalls: 1200 rpm
Distances
---------
Take-off: 450-800 ft
Landing: 200-800 ft
Fuel
----
Total fuel: 12 gal US
Usable fuel: 12 gal US
Grade: 80/87
GPH: 5 gal US/hr

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Aircraft-yasim/README.p51d
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P-51D Information
=============
FLYING HINTS
NOTE: the yasim config file for this aircraft currently starts up with
the booster in 1st stage.
TAKE OFF:
Set prop pitch to full increased rpm.
Start engine with throttle at idle.
Set BOOST stage one (CTRL-b keybinding cycles through stage 0 (off), 1,
and 2). Default startup for p51-d should have stage one already on.
Set throttle to 40 inHG Manifold Pressure (MP).
Be ready to actuate rudder. When the tail first lifts, the torque will
pull the nose to the left.
After tail lifts off slowing move throttle to full open which with
stage 1 booster engaged should be about 61 inHG Manifold Pressure.
Hang on. Stay on top of rudder control with small adjustments or you'll
do a ground loop.
Rotate at 150 mph or so.
CLIMB:
Back off MP to 46 inHG.
Adjust propeller pitch to 2700 rpm.
Keep adding throttle as you climb to maintain 46 inHG until you hit full throttle.
At 18,000 feet turn on second stage (hit CTRL-b) and back off throttle to 46 inHG.
FLYING:
Trim and Cruise at about 2400 rpm.
Do not exceed 2700 rpm sustained.
Do not exceed 3000 rpm military power (aerobatics)
Do not exceed 3500 rpm in dives.
Do not exceed 61 inHG Mainfold Pressure (military power), except 71 inHG for
maximum of 7 minutes (war emergency power). Note that war emergency
power is not for flying fast, rather it is for dogfighting at < 200mph.
LANDING:
A single long sweeping turn from the downwind leg into a short approach
seems to work best. Make sure you are below 250mph before starting the
turn. Use forward slip as necessary to bleed off speed and altitude at the
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

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Aircraft-yasim/README.pa28-161
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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

146
Aircraft-yasim/a10-yasim.xml
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<!-- 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>

143
Aircraft-yasim/a10cl-yasim.xml
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@ -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>

155
Aircraft-yasim/a10fl-yasim.xml
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@ -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>

223
Aircraft-yasim/a10wl-yasim.xml
View file

@ -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>

122
Aircraft-yasim/a4.xml
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@ -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>

289
Aircraft-yasim/b52-yasim.xml
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@ -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>

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Aircraft-yasim/c172.xml
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<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>

129
Aircraft-yasim/c310.xml
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@ -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>

124
Aircraft-yasim/dc3.xml
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@ -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>

170
Aircraft-yasim/harrier.xml
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@ -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>

174
Aircraft-yasim/j22-yasim.xml
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@ -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>

141
Aircraft-yasim/j3cub.xml
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<?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>

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Aircraft-yasim/p51d.xml
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<?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>

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Aircraft-yasim/pa28-161.xml
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@ -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>

140
Aircraft-yasim/seahawk-WV908-yasim.xml
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@ -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>

135
Aircraft-yasim/seahawk-yasim.xml
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@ -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>

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Aircraft-yasim/seahawkpair-yasim.xml
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@ -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>

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Aircraft-yasim/tsr2-yasim.xml
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@ -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>

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Aircraft-yasim/yf23-yasim.xml
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@ -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>

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Aircraft/c172p/c172p-3d-jsbsim-set.xml Normal file
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<?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>

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Aircraft/c172p/c172p-3d-set.xml Normal file
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<?xml version="1.0"?>
<PropertyList include="c172p-3d-jsbsim-set.xml">
<sim>
<description>Alias for c172p-3d-jsbsim.</description>
</sim>
</PropertyList>

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Aircraft/c172p/c172p-base.xml Normal file
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<?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>

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Aircraft/c172p/c172p-jsbsim-base.xml Normal file
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<?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>

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Aircraft/c172p/c172p-jsbsim-set.xml Normal file
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<?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>

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Aircraft/c172p/c172p-set.xml Normal file
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<?xml version="1.0"?>
<PropertyList include="c172p-jsbsim-set.xml">
<sim>
<description>Alias for c172p-jsbsim.</description>
</sim>
</PropertyList>

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Aircraft/ufo/ufo-set.xml Normal file
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<?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>