diff --git a/Aircraft-yasim/747.xml b/Aircraft-yasim/747.xml deleted file mode 100644 index 153ea73d2..000000000 --- a/Aircraft-yasim/747.xml +++ /dev/null @@ -1,133 +0,0 @@ -<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> diff --git a/Aircraft-yasim/README.j3cub b/Aircraft-yasim/README.j3cub deleted file mode 100644 index f1f7f26bd..000000000 --- a/Aircraft-yasim/README.j3cub +++ /dev/null @@ -1,233 +0,0 @@ -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 diff --git a/Aircraft-yasim/README.p51d b/Aircraft-yasim/README.p51d deleted file mode 100644 index d087b6975..000000000 --- a/Aircraft-yasim/README.p51d +++ /dev/null @@ -1,60 +0,0 @@ -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 diff --git a/Aircraft-yasim/README.pa28-161 b/Aircraft-yasim/README.pa28-161 deleted file mode 100644 index 968a9bfc1..000000000 --- a/Aircraft-yasim/README.pa28-161 +++ /dev/null @@ -1,43 +0,0 @@ -PIPER WARRIOR II PERFORMANCE DATA -================================= - -These numbers apply to the 160 hp variant of the Warrior II; they come -from the Piper POH. - -Speeds ------- - Vne (never exceed): 160 KIAS - Vno (max. cruise): 126 KIAS - Vfe (max. flaps): 103 KIAS - Va (maneuvering): 111 KIAS (2440 lb) - 88 KIAS (1531 lb) - Vs (clean stall): 50 KIAS - Vso (flaps stall): 44 KIAS - Vglide (best glide): 73 KIAS - Vx (best climb angle): 63 KIAS - Vy (best climb rate): 79 KIAS - Enroute climb: 87 KIAS - Approach (no flaps): 70 KIAS - Approach (full flaps): 63 KIAS - - Cruise (75%, 8000 ft): 124 KTAS (107 KIAS) - Cruise (55%, 8000 ft): 103 KTAS (89 KIAS) - -Power ------ - Take off: full - Climb: full - 75% power at 8,000 ft: 2665 rpm - 75% power at 4,000 ft: 2570 rpm - 75% power at sea level: 2480 rpm - 55% power at 12,000 ft: 2470 rpm - 55% power at 8,000 ft: 2375 rpm - 55% power at 4,000 ft: 2285 rpm - 55% power at sea level: 2195 rpm - -Fuel ----- - Total fuel: 50 gal US - Usable fuel: 48 gal US - Grade: 100LL/100 (Avgas) - GPH (75%, 8000 ft): 10.0 gph - GPH (55%, 8000 ft): 7.0 gph diff --git a/Aircraft-yasim/a10-yasim.xml b/Aircraft-yasim/a10-yasim.xml deleted file mode 100755 index 1fb071f54..000000000 --- a/Aircraft-yasim/a10-yasim.xml +++ /dev/null @@ -1,146 +0,0 @@ -<!-- A10 yasim config. This is a hack and not an authentic - representation of the aircraft. Having said that, the - numbers, where I could find them, roughly match those of - the original aircraft. - Lee Elliott. leee-fgfs@spatial.freeserve.co.uk ---> - -<airplane mass="37700"> - -<!-- Approach configuration --> -<approach speed="110" aoa="7"> - <control-setting axis="/controls/engines/engine[0]/throttle" value="0.5"/> - <control-setting axis="/controls/engines/engine[1]/throttle" value="0.5"/> - <control-setting axis="/controls/flight/flaps" value="1.0"/> - <control-setting axis="/controls/gear/gear-down" value="1"/> -</approach> - -<!-- Cruise configuration --> -<cruise speed="380" alt="0"> - <control-setting axis="/controls/engines/engine[0]/throttle" value="1.0"/> - <control-setting axis="/controls/engines/engine[1]/throttle" value="1.0"/> - <control-setting axis="/controls/flight/flaps" value="0.0"/> - <control-setting axis="/controls/gear/gear-down" value="0"/> -</cruise> - -<cockpit x="-3.5" y="0.0" z="1.2"/> - -<fuselage ax="0" ay="0" az="0" bx="-16.26" by="0" bz="0" - width="1.4"/> - -<!-- Left Engine --> -<fuselage ax="-10" ay="1.50" az="1" bx="-13.5" by="1.50" bz="0.8" - width="1.5"/> - -<!-- Right Engine --> -<fuselage ax="-10" ay="-1.50" az="1" bx="-13.5" by="-1.50" bz="0.8" - width="1.5"/> - -<wing x="-8.8" y="0.5" z="-0.5" taper="0.6" incidence="-1" - length="8.3" chord="3.1" sweep="0.0" dihedral="3.0" camber="0"> - <stall aoa="14" width="6" peak="1.3"/> - <flap0 start="0.04" end="0.51" lift="1.5" drag="1.2"/> - <flap1 start="0.54" end="0.86" lift="1.3" drag="1.2"/> - <spoiler start="0.54" end="0.86" lift="0.1" drag="20.0"/> - - <control-input axis="/controls/flight/flaps" control="FLAP0"/> - <control-input axis="/controls/flight/aileron" control="FLAP1" split="true"/> - <control-input axis="/controls/flight/aileron-trim" control="FLAP1" split="true"/> - <control-input axis="/controls/flight/spoilers" control="SPOILER"/> - - <control-output control="FLAP0" side="left" - prop="/surface-positions/left-flap-pos-norm"/> - <control-output control="FLAP0" side="right" - prop="/surface-positions/right-flap-pos-norm"/> - <control-output control="FLAP1" side="left" - prop="/surface-positions/left-aileron-pos-norm"/> - <control-output control="FLAP1" side="right" - prop="/surface-positions/right-aileron-pos-norm"/> - <control-output control="SPOILER" side="left" - prop="/surface-positions/left-spoiler-pos-norm"/> - <control-output control="SPOILER" side="right" - prop="/surface-positions/right-spoiler-pos-norm"/> - - <control-speed control="FLAP0" transition-time="5"/> - <control-speed control="SPOILER" transition-time="0.5"/> - -</wing> - -<hstab x="-15.5" y="0.4" z="0.4" taper="0.0" effectiveness="3" - length="2.5" chord="2" sweep="0.0" dihedral="0.0" camber="0"> - <stall aoa="20" width="5" peak="1.5"/> - <flap0 start="0" end="1" lift="1.5" drag="1.2"/> - <control-input axis="/controls/flight/elevator" control="FLAP0"/> - <control-input axis="/controls/flight/elevator-trim" control="FLAP0"/> - <control-output control="FLAP0" prop="/surface-positions/elevator-pos-norm"/> -</hstab> - -<vstab x="-15.0" y="2.5" z="-0.9" taper="0.7" effectiveness="2" - length="2.8" chord="2.0" sweep="0.0"> - <stall aoa="16" width="5" peak="1.5"/> - <flap0 start="0" end="1" lift="1.3" drag="1.3"/> - <control-input axis="/controls/flight/rudder" control="FLAP0" invert="true"/> - <control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm"/> -</vstab> - -<vstab x="-15.0" y="-2.5" z="-0.9" taper="0.7" effectiveness="2" - length="2.8" chord="2.0" sweep="0.0"> - <stall aoa="16" width="5" peak="1.5"/> - <flap0 start="0" end="1" lift="1.3" drag="1.3"/> - <control-input axis="/controls/flight/rudder" control="FLAP0" invert="true"/> - <control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm"/> -</vstab> - -<!-- Engines and tanks --> -<jet x="-11.8" y="-1.5" z="1.0" mass="1000" thrust="9065"> - <control-input axis="/controls/engines/engine[0]/throttle" control="THROTTLE"/> -</jet> - -<jet x="-11.8" y="1.5" z="1.0" mass="1000" thrust="9065"> - <control-input axis="/controls/engines/engine[1]/throttle" control="THROTTLE"/> -</jet> - -<tank x="-8.5" y="-1.5" z="0.0" jet="true" capacity="2000"/> -<tank x="-8.5" y="1.5" z="0.0" jet="true" capacity="2000"/> -<tank x="-8.5" y="0" z="0.0" jet="true" capacity="6700"/> - -<!-- Undercarriage --> -<!-- nose --> -<gear x="-2.9" y="0.4" z="-2.8" retract-time="7" compression="0.7"> - <control-input axis="/controls/flight/rudder" control="STEER" square="true"/> - <control-input axis="/controls/gear/gear-down" control="EXTEND"/> - <control-speed control="EXTEND" transition-time="7"/> - <control-output control="EXTEND" prop="/gear/gear/position-norm"/> -</gear> - -<!-- left main --> -<gear x="-9.0" y="2.5" z="-2.8" retract-time="7" compression="0.6"> - <control-input axis="/controls/gear/wheel[1]/brake" control="BRAKE"/> - <control-input axis="/controls/gear/parking-brake" control="BRAKE"/> - <control-input axis="/controls/gear/gear-down" control="EXTEND"/> - <control-speed control="EXTEND" transition-time="7"/> - <control-output control="EXTEND" prop="/gear/gear[1]/position-norm"/> -</gear> - -<!-- right main --> -<gear x="-9.0" y="-2.5" z="-2.8" retract-time="7" compression="0.6"> - <control-input axis="/controls/gear/wheel[2]/brake" control="BRAKE"/> - <control-input axis="/controls/gear/parking-brake" control="BRAKE"/> - <control-input axis="/controls/gear/gear-down" control="EXTEND"/> - <control-speed control="EXTEND" transition-time="7"/> - <control-output control="EXTEND" prop="/gear/gear[2]/position-norm"/> -</gear> - -<!-- Canopy --> -<gear x="-2.6" y="0.0" z="1.4" retract-time="7" compression="0.6"> - <control-input axis="/controls/gear/parking-brake" control="EXTEND"/> - <control-speed control="EXTEND" transition-time="5"/> - <control-output control="EXTEND" prop="/canopy/position-norm"/> -</gear> - -<!-- Ballast --> -<ballast x="-3.5" y="0" z="1.0" mass="2000"/> <!-- Armored cockpit --> -<ballast x="-4.0" y="0" z="-1.0" mass="4000"/> <!-- Gun --> -<ballast x="-5.0" y="0" z="0.0" mass="1000"/> <!-- avionics --> - -</airplane> diff --git a/Aircraft-yasim/a10cl-yasim.xml b/Aircraft-yasim/a10cl-yasim.xml deleted file mode 100644 index 475a9918b..000000000 --- a/Aircraft-yasim/a10cl-yasim.xml +++ /dev/null @@ -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> diff --git a/Aircraft-yasim/a10fl-yasim.xml b/Aircraft-yasim/a10fl-yasim.xml deleted file mode 100755 index ac8eb3821..000000000 --- a/Aircraft-yasim/a10fl-yasim.xml +++ /dev/null @@ -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> diff --git a/Aircraft-yasim/a10wl-yasim.xml b/Aircraft-yasim/a10wl-yasim.xml deleted file mode 100644 index 6f41ba73e..000000000 --- a/Aircraft-yasim/a10wl-yasim.xml +++ /dev/null @@ -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> diff --git a/Aircraft-yasim/a4.xml b/Aircraft-yasim/a4.xml deleted file mode 100644 index 9701aeb40..000000000 --- a/Aircraft-yasim/a4.xml +++ /dev/null @@ -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> diff --git a/Aircraft-yasim/b52-yasim.xml b/Aircraft-yasim/b52-yasim.xml deleted file mode 100755 index 7b8675d02..000000000 --- a/Aircraft-yasim/b52-yasim.xml +++ /dev/null @@ -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> diff --git a/Aircraft-yasim/c172.xml b/Aircraft-yasim/c172.xml deleted file mode 100644 index 3b6dda405..000000000 --- a/Aircraft-yasim/c172.xml +++ /dev/null @@ -1,93 +0,0 @@ -<airplane mass="1950"> - -<!-- Approach configuration --> -<approach speed="47" aoa="16"> - <control-setting axis="/controls/engines/engine[0]/throttle" value="0.3"/> - <control-setting axis="/controls/engines/engine[0]/mixture" value="1.0"/> - <control-setting axis="/controls/flight/flaps" value="1.0"/> -</approach> - -<!-- Cruise configuration --> -<cruise speed="123" alt="0"> - <control-setting axis="/controls/engines/engine[0]/throttle" value="1.0"/> - <control-setting axis="/controls/engines/engine[0]/mixture" value="1.0"/> - <control-setting axis="/controls/flight/flaps" value="0.0"/> -</cruise> - -<cockpit x="-1.88" y=".33" z="0.6"/> - -<fuselage ax="-.17" ay="0" az="-.51" bx="-7.16" by="0" bz=".17" - width="1.5" taper="0.2" midpoint="0.3"/> - -<wing x="-2.47" y=".51" z=".68" taper=".78" - length="5.37" chord="1.54" sweep="0" dihedral="1" camber="0.1"> - <stall aoa="16" width="6" peak="1.5"/> - <flap0 start="0" end=".38" lift="1.5" drag="1.2"/> - <flap1 start=".78" end="1" lift="1.5" drag="1.2"/> - <control-input axis="/controls/flight/flaps" control="FLAP0"/> - <control-input axis="/controls/flight/aileron" control="FLAP1" split="true"/> - <control-input axis="/controls/flight/aileron-trim" control="FLAP1" split="true"/> - <control-output control="FLAP0" prop="/surface-positions/flap-pos-norm"/> - <control-output control="FLAP1" side="left" - prop="/surface-positions/left-aileron-pos-norm"/> - <control-output control="FLAP1" side="right" - prop="/surface-positions/right-aileron-pos-norm"/> - <control-speed control="FLAP0" transition-time="6"/> -</wing> - -<hstab x="-7.16" y="0.08" z=".17" taper=".63" effectiveness="2" - length="1.71" chord="1.36" sweep="0"> - <stall aoa="18" width="4" peak="1.5"/> - <flap0 start="0" end="1" lift="1.7" drag="1.2"/> - <control-input axis="/controls/flight/elevator" control="FLAP0"/> - <control-input axis="/controls/flight/elevator-trim" control="FLAP0"/> - <control-output control="FLAP0" prop="/surface-positions/elevator-pos-norm"/> -</hstab> - -<vstab x="-7.16" y="0" z=".17" taper=".5" - length="1.71" chord="1.54" sweep="20"> - <stall aoa="16" width="4" peak="1.5"/> - <flap0 start="0" end="1" lift="1.3" drag="1.2"/> - <control-input axis="/controls/flight/rudder" control="FLAP0" invert="true"/> - <control-input axis="/controls/flight/rudder-trim" control="FLAP0" invert="true"/> - <control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm" - min="1" max="-1"/> -</vstab> - -<propeller radius="1.0" - cruise-speed="86" cruise-rpm="2200" - cruise-alt="10000" cruise-power="99" - takeoff-power="140.8" takeoff-rpm="2200" - eng-power="160" eng-rpm="2500" - x="-.6" y="0" z="0" mass="400" moment="8"> - <actionpt x="0" y="0" z="0"/> - <control-input axis="/controls/engines/engine[0]/throttle" control="THROTTLE"/> - <control-input axis="/controls/engines/engine[0]/starter" control="STARTER"/> - <control-input axis="/controls/engines/engine[0]/magnetos" control="MAGNETOS"/> - <control-input axis="/controls/engines/engine[0]/mixture" control="MIXTURE"/> -</propeller> - -<gear x="-1" y="0" z="-1.5" compression=".4"> <!-- nose --> - <control-input axis="/controls/flight/rudder" control="STEER" - src0="-1.0" src1="1.0" - dst0="-0.1" dst1="0.1"/> -</gear> - -<gear x="-2.82" y="1.15" z="-1.36" compression=".3"> <!-- left main --> - <control-input axis="/controls/gear/wheel[0]/brake" control="BRAKE" split="true"/> - <control-input axis="/controls/gear/parking-brake" control="BRAKE" split="true"/> -</gear> - -<gear x="-2.82" y="-1.15" z="-1.36" compression=".3"> <!-- left main --> - <control-input axis="/controls/gear/wheel[1]/brake" control="BRAKE" split="true"/> - <control-input axis="/controls/gear/parking-brake" control="BRAKE" split="true"/> -</gear> - -<tank x="-2.47" y="1.36" z=".68" capacity="75"/> -<tank x="-2.47" y="-1.36" z=".68" capacity="75"/> - -<ballast x="-2.0" y=".33" z="0" mass="180"/> <!-- pilot --> -<ballast x="-2.0" y="-.33" z="0" mass="180"/> <!-- passenger --> -<ballast x="-1.0" y="-.33" z="0" mass="200"/> <!-- cockpit --> - -</airplane> diff --git a/Aircraft-yasim/c310.xml b/Aircraft-yasim/c310.xml deleted file mode 100644 index 7899393e5..000000000 --- a/Aircraft-yasim/c310.xml +++ /dev/null @@ -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> diff --git a/Aircraft-yasim/dc3.xml b/Aircraft-yasim/dc3.xml deleted file mode 100644 index 220fcec0b..000000000 --- a/Aircraft-yasim/dc3.xml +++ /dev/null @@ -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> diff --git a/Aircraft-yasim/harrier.xml b/Aircraft-yasim/harrier.xml deleted file mode 100644 index 4b873279f..000000000 --- a/Aircraft-yasim/harrier.xml +++ /dev/null @@ -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> diff --git a/Aircraft-yasim/j22-yasim.xml b/Aircraft-yasim/j22-yasim.xml deleted file mode 100644 index fe05a2095..000000000 --- a/Aircraft-yasim/j22-yasim.xml +++ /dev/null @@ -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> diff --git a/Aircraft-yasim/j3cub.xml b/Aircraft-yasim/j3cub.xml deleted file mode 100644 index 37ebad7a4..000000000 --- a/Aircraft-yasim/j3cub.xml +++ /dev/null @@ -1,141 +0,0 @@ -<?xml version="1.0"?> - -<!-- -************************************************************************ -YASim aerodynamic model for a Piper J3 Cub. -Started 2002-08-15 by David Megginson. - -This aerodynamic model is based on three-views, unauthoritative -performance data, and wild guesses. These sites provided particularly -useful information or were simply fun to visit: - -Performance data: - http://www.marss.com/cub.htm -Weight and balance: - http://www.danford.net/balance.htm -Three-view: - http://www.fiddlersgreen.net/aircraft/private/j3cub/j3cub_info/j3_info.htm -Useless but fun free paper model: - http://www.fiddlersgreen.net/aircraft/private/j3cub/j3cub.htm -Useless but fun 1945 Piper Cub ad from FLYING: - http://www.fiddlersgreen.net/aircraft/private/j3cub/j3cub_info/piperad.jpg - -The reference datum for measurements is the leading edge of the wing, -since it is what the weight-and-balance site above uses. -************************************************************************ ---> - -<!-- - 680lb empty weight. - --> -<!-- FIXME: this includes the engine; is that correct? --> -<airplane mass="680"> - -<!-- Approach configuration --> -<approach speed="20" aoa="15"> - <control-setting axis="/controls/engines/engine[0]/throttle" value="0.5"/> - <control-setting axis="/controls/engines/engine[0]/mixture" value="1.0"/> -</approach> - -<!-- Cruise configuration --> -<cruise speed="64" alt="0"> - <control-setting axis="/controls/engines/engine[0]/throttle" value="0.75"/> - <control-setting axis="/controls/engines/engine[0]/mixture" value="0.75"/> - <control-setting axis="/controls/flight/elevator-trim" value="0.1"/> -</cruise> - -<!-- pilot's eyepoint --> -<cockpit x="-0.23" y="0" z="-0.30"/> - -<fuselage ax="1.37" ay="0" az="-0.71" bx="-4.81" by="0" bz="-0.65" - width="0.71" taper="0.16" midpoint="0.17"/> - -<!-- - I treat it as a perfectly rectangular wing for now. Note that - the dihedral is exaggerated to simulate hull-interference effects - on a high-wing aircraft; once YASim models that properly, the - angle should be reduced to something like 2 degrees. - - Note that the J3 Cub has no flaps. With a stall speed of 25kt, who - needs them? From what I've read, the ailerons add lots of drag. ---> -<wing x="-0.80" y="0.42" z="0.0" taper="1.0" incidence="2" twist="-3" - length="4.87" chord="1.60" sweep="0" dihedral="5" camber="0.1"> - <stall aoa="18" width="4" peak="1.5"/> - <flap0 start=".31" end="0.85" lift="1.5" drag="1.4"/> - <control-input axis="/controls/flight/aileron" control="FLAP0" split="true"/> - <control-input axis="/controls/flight/aileron-trim" control="FLAP0" split="true"/> - <control-output control="FLAP0" side="left" - prop="/surface-positions/left-aileron-pos-norm"/> - <control-output control="FLAP0" side="right" - prop="/surface-positions/right-aileron-pos-norm"/> -</wing> - -<hstab x="-4.87" y="0.05" z="-0.42" taper="0.8" effectiveness="1.24" - length="1.49" chord="1.13" sweep="0"> - <stall aoa="16" width="4" peak="1.5"/> - <flap0 start="0" end="1" lift="1.4" drag="1.2"/> - <control-input axis="/controls/flight/elevator" control="FLAP0"/> - <control-input axis="/controls/flight/elevator-trim" control="FLAP0"/> - <control-output control="FLAP0" prop="/surface-positions/elevator-pos-norm"/> -</hstab> - -<!-- rudder has to be able to counteract aileron drag --> -<vstab x="-4.87" y="0" z="-0.65" taper="0.38" effectiveness="2.0" - length="1.31" chord="1.37" sweep="0" incidence="1.5"> - <stall aoa="16" width="4" peak="1.5"/> - <flap0 start="0" end="1" lift="2.0" drag="1.2"/> - <control-input axis="/controls/flight/rudder" control="FLAP0" invert="true"/> - <control-input axis="/controls/flight/rudder-trim" control="FLAP0" invert="true"/> - <control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm" - min="1" max="-1"/> -</vstab> - -<!-- FIXME: engine mass (just a guess; it's a small engine) --> -<!-- Assume 75% power at 8000ft --> -<propeller radius="0.90" - cruise-speed="70" cruise-rpm="2150" - cruise-alt="8000" cruise-power="49" - takeoff-power="55" takeoff-rpm="2300" - eng-power="65" eng-rpm="2500" - x="0.71" y="0" z="-0.65" mass="150" moment="4"> - <actionpt x="1.31" y="0" z="-0.65"/> - <control-input axis="/controls/engines/engine[0]/throttle" control="THROTTLE"/> - <control-input axis="/controls/engines/engine[0]/starter" control="STARTER"/> - <control-input axis="/controls/engines/engine[0]/magnetos" control="MAGNETOS"/> - <control-input axis="/controls/engines/engine[0]/mixture" control="MIXTURE"/> -</propeller> - -<gear x="-5.17" y="0" z="-0.71" compression="0.1"> - <control-input axis="/controls/flight/rudder" control="STEER" - src0="-1.0" src1="1.0" - dst0="0.5" dst1="-0.5"/> -</gear> - -<gear x="0" y="0.95" z="-1.96" compression="0.01"> <!-- left main --> - <control-input axis="/controls/gear/wheel[0]/brake" control="BRAKE" split="true"/> - <control-input axis="/controls/gear/parking-brake" control="BRAKE" split="true"/> -</gear> - -<gear x="0" y="-0.95" z="-1.96" compression="0.01"> <!-- right main --> - <control-input axis="/controls/gear/wheel[1]/brake" control="BRAKE" split="true"/> - <control-input axis="/controls/gear/parking-brake" control="BRAKE" split="true"/> -</gear> - -<!-- There's just one 12-gallon tank, right behind the engine (!!!) --> -<tank x="-0.45" y="0" z="-0.89" capacity="72"/> - -<!-- - Note the tandem seating; the x values (arms) come from the - weight-and-balance page cited at the start. ---> - -<ballast x="-4.0" y="0" z="-0.70" mass="-75"/> - -<!-- pilot --> -<weight x="-0.91" y="0" z="-0.70" mass-prop="/yasim/j3cub/pilot-lb"/> - -<!-- passenger --> -<weight x="-0.23" y="0" z="-0.70" mass-prop="/yasim/j3cub/passenger-lb"/> - -</airplane> diff --git a/Aircraft-yasim/p51d.xml b/Aircraft-yasim/p51d.xml deleted file mode 100644 index 48bd1a4aa..000000000 --- a/Aircraft-yasim/p51d.xml +++ /dev/null @@ -1,166 +0,0 @@ -<?xml version="1.0"?> - -<!-- -************************************************************************ -YASim aerodynamic model for a P-51D mustang -Started 2003-04-24 by Jim Wilson - -This aerodynamic model is based on three-views, unauthoritative -performance data, and wild guesses. These sites provided particularly -useful information or were simply fun to visit: - -Performance data: -http://www.hq.nasa.gov/office/pao/History/SP-468/app-a2.htm -http://www.olympicflightmuseum.com/aircraft_gallery/p51d_mustang.htm -http://www.btinternet.com/~lee_mail/P51.html -http://www.sprucegoose.org/pdfs/planes/P51Mustang.pdf - -Weight and balance: -http://www.p51.wjackparker.com/P51_Additional_reference_material/x_maintenance.htm -http://www.nzfpm.co.nz/aircraft/p51d.htm -http://www.wpafb.af.mil/museum/engines/eng33.htm - -Three-view: -http://members.optushome.com.au/gjmustang/docs/3-View.html -(Note: I have local copies if this url becomes un-available) - -The reference datum for measurements is the nose. -************************************************************************ ---> - -<!-- Weight of everything but fuel (7010 empty) --> -<airplane mass="7190"> - -<!-- Approach configuration --> -<approach speed="87" aoa="13"> - <control-setting axis="/controls/engines/engine[0]/throttle" value="0.2"/> - <control-setting axis="/controls/engines/engine[0]/mixture" value="1.0"/> - <control-setting axis="/controls/engines/engine[0]/propeller-pitch" value="0.5"/> - <control-setting axis="/controls/flight/flaps" value="1.0"/> - <control-setting axis="/controls/gear/gear-down" value="1"/> -</approach> - -<!-- Cruise configuration --> -<cruise speed="380" alt="25000"> - <control-setting axis="/controls/engines/engine[0]/throttle" value="1.00"/> - <control-setting axis="/controls/engines/engine[0]/mixture" value="1.00"/> - <control-setting axis="/controls/engines/engine[0]/propeller-pitch" value="1.0"/> - <control-setting axis="/controls/engines/engine[0]/boost" value="1.0"/> - <control-setting axis="/controls/flight/flaps" value="0.0"/> - <control-setting axis="/controls/gear/gear-down" value="0"/> -</cruise> - -<!-- pilot's eyepoint --> -<cockpit x="-4.495" y="0" z="0.689"/> - -<fuselage ax="0.0" ay="0.0" az="0.0" bx="-9.9" by="0.0" bz="0.0" - width="0.94" taper="0.38"/> - -<!-- -stall aoa not available -flap drag not available ---> -<wing x="-3.96" y="0.55" z="-0.60" taper="0.466" incidence="0" - length="5.16" chord="2.845" sweep="-3.5" dihedral="5" camber="0.1"> - <stall aoa="14" width="4" peak="1.5"/> - <flap0 start="0.024" end="0.543" lift="1.2" drag="1.8"/> - <flap1 start="0.543" end="0.94.5" lift="1.3" drag="1.4"/> - <control-input axis="/controls/flight/flaps" control="FLAP0"/> - <control-output control="FLAP0" prop="/surface-positions/flap-pos-norm"/> - <control-speed control="FLAP0" transition-time="5"/> - <control-input axis="/controls/flight/aileron" control="FLAP1" split="true"/> - <control-input axis="/controls/flight/aileron-trim" control="FLAP1" split="true"/> -</wing> - -<hstab x="-8.62" y="0.18" z="0.34" taper="0.639" effectiveness="3.5" - length="1.834" chord="1.256" sweep="0" incidence="2"> - <stall aoa="15" width="4" peak="1.5"/> - <flap0 start="0.0" end="1.8" lift="1.65" drag="1.2"/> - <control-input axis="/controls/flight/elevator" control="FLAP0"/> - <control-input axis="/controls/flight/elevator-trim" control="FLAP0"/> - <control-output control="FLAP0" prop="/surface-positions/elevator-pos-norm"/> -</hstab> - -<!-- rudder has to be able to counteract aileron drag --> -<vstab x="-9.30" y="0" z="-0.37" taper="0.432" effectiveness="3.5" - length="1.971" chord="2.65" sweep="25" incidence="-0.58"> - <stall aoa="15" width="4" peak="1.5"/> - <flap0 start="0" end="1" lift="1.3" drag="1.2"/> - <control-input axis="/controls/flight/rudder" square="true" control="FLAP0" invert="true"/> - <control-input axis="/controls/flight/rudder-trim" control="FLAP0" invert="true"/> - <control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm" - min="1" max="-1"/> -</vstab> - -<!-- moment calculated using formula submitted by Donald Simon: - MOI = # of Blades * (8.2*(10^-5))*(D^5), slug-ft^2 - then converted to kg-m^2 and finally square root to kg-m for torque value --> -<!-- wastegate setting should not apply. set here so that calculations would approximate. - YASim doesn't model gear supercharger. Have read various figures (turbo-mul) 4.0 to 5.8 for - running the second stage blower. Fixing this would probably give more reasonable - performance at lower altitude --> -<!-- cruise-rpm roughly estimated from documented gear ratio of 0.479 --> -<propeller x="-0.75" y="0" z="0" - radius="1.75" - mass="1690" moment="94.5" - eng-power="1590" eng-rpm="3000" - turbo-mul="4.0" wastegate-mp="61" - cruise-alt="21400" cruise-power="1370" - cruise-speed="380" cruise-rpm="2900" - manual-pitch="true" > - <actionpt x="-1.25" y="0" z="0"/> - <control-input axis="/controls/engines/engine[0]/throttle" control="THROTTLE"/> - <control-input axis="/controls/engines/engine[0]/starter" control="STARTER"/> - <control-input axis="/controls/engines/engine[0]/magnetos" control="MAGNETOS"/> - <control-input axis="/controls/engines/engine[0]/mixture" control="MIXTURE"/> - <control-input axis="/controls/engines/engine[0]/propeller-pitch" control="PROPPITCH" - src0="0" src1="1" dst0="0.40" dst1="0.82"/> - <control-input axis="/controls/engines/engine[0]/boost" control="BOOST"/> -</propeller> - -<!-- Tail wheel --> -<!-- tail wheel "steerable" in p-51d (in stick back locked position it actually should be limited to 6deg +/-) --> -<gear x="-7.90" y="0" z="-0.96" compression="0.2"> - <control-input axis="/controls/flight/rudder" control="STEER" square="true" - src0="-1.0" src1="1.0" - dst0="0.5" dst1="-0.5"/> -</gear> - - <!-- left main --> -<gear x="-2.79" y="1.81" z="-2.20" compression="0.4" spring="0.7" damp="3.0"> - <control-input axis="/controls/gear/wheel[0]/brake" control="BRAKE"/> - <control-input axis="/controls/gear/parking-brake" control="BRAKE" split="true"/> - <control-input axis="/controls/gear/gear-down" control="EXTEND"/> - <control-speed control="EXTEND" transition-time="6"/> - <control-output control="EXTEND" prop="/gear/gear[0]/position-norm"/> -</gear> - - <!-- right main --> -<gear x="-2.79" y="-1.81" z="-2.20" compression="0.4" spring="0.7" damp="3.0"> - <control-input axis="/controls/gear/wheel[1]/brake" control="BRAKE"/> - <control-input axis="/controls/gear/parking-brake" control="BRAKE" split="true"/> - <control-input axis="/controls/gear/gear-down" control="EXTEND"/> - <control-speed control="EXTEND" transition-time="6"/> - <control-output control="EXTEND" prop="/gear/gear[1]/position-norm"/> -</gear> - -<!-- Guess on wing tank positions --> -<tank x="-3.50" y="1.0" z="-0.61" capacity="726"/> -<tank x="-3.50" y="-1.0" z="-0.61" capacity="726"/> -<tank x="-6.50" y="0" z="0" capacity="671"/> - -<!-- pilot --> -<ballast x="-4.495" y="0" z="0.689" mass="180"/> - -<!-- armament --> -<!-- Had too much weight I think...disable until stall speed fixed -<ballast x="-3.20" y="0.7" z="-0.60" mass="800"/> -<ballast x="-3.20" y="-0.7" z="-0.60" mass="800"/> ---> - -<!-- prop --> -<!-- -<ballast x="0.1" y="0" z="0.0" mass="200"/> ---> - -</airplane> diff --git a/Aircraft-yasim/pa28-161.xml b/Aircraft-yasim/pa28-161.xml deleted file mode 100644 index 8b49d4056..000000000 --- a/Aircraft-yasim/pa28-161.xml +++ /dev/null @@ -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> diff --git a/Aircraft-yasim/seahawk-WV908-yasim.xml b/Aircraft-yasim/seahawk-WV908-yasim.xml deleted file mode 100755 index 7473d4cbe..000000000 --- a/Aircraft-yasim/seahawk-WV908-yasim.xml +++ /dev/null @@ -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> diff --git a/Aircraft-yasim/seahawk-yasim.xml b/Aircraft-yasim/seahawk-yasim.xml deleted file mode 100755 index 35dc96fdf..000000000 --- a/Aircraft-yasim/seahawk-yasim.xml +++ /dev/null @@ -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> diff --git a/Aircraft-yasim/seahawkpair-yasim.xml b/Aircraft-yasim/seahawkpair-yasim.xml deleted file mode 100755 index 21da1aaf0..000000000 --- a/Aircraft-yasim/seahawkpair-yasim.xml +++ /dev/null @@ -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> diff --git a/Aircraft-yasim/tsr2-yasim.xml b/Aircraft-yasim/tsr2-yasim.xml deleted file mode 100755 index 706d4656a..000000000 --- a/Aircraft-yasim/tsr2-yasim.xml +++ /dev/null @@ -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> diff --git a/Aircraft-yasim/yf23-yasim.xml b/Aircraft-yasim/yf23-yasim.xml deleted file mode 100644 index afa0fc137..000000000 --- a/Aircraft-yasim/yf23-yasim.xml +++ /dev/null @@ -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> diff --git a/Aircraft/c172p/c172p-3d-jsbsim-set.xml b/Aircraft/c172p/c172p-3d-jsbsim-set.xml new file mode 100644 index 000000000..fe227d1ce --- /dev/null +++ b/Aircraft/c172p/c172p-3d-jsbsim-set.xml @@ -0,0 +1,37 @@ +<?xml version="1.0"?> +<!-- +************************************************************************ +JSBSim Cessna 172P with 3D cockpit. + +Started October 23 2001 by John Check, fgpanels@rockfish.net +************************************************************************ +--> + +<PropertyList include="c172p-jsbsim-base.xml"> + + <sim> + + <description>Cessna 172P (JSBSim, 3D cockpit)</description> + + <!-- hide the 2D panel --> + + <panel> + <visibility archive="y">false</visibility> + </panel> + + <!-- position the pilot viewpoint and angle --> + + <view> + <internal archive="y">true</internal> + <config> + <x-offset-m archive="y">-0.18</x-offset-m> + <y-offset-m archive="y">0.30</y-offset-m> + <z-offset-m archive="y">0.36</z-offset-m> + <pitch-offset-deg>-12</pitch-offset-deg> + </config> + </view> + + + </sim> + +</PropertyList> diff --git a/Aircraft/c172p/c172p-3d-set.xml b/Aircraft/c172p/c172p-3d-set.xml new file mode 100644 index 000000000..fc820a0b7 --- /dev/null +++ b/Aircraft/c172p/c172p-3d-set.xml @@ -0,0 +1,7 @@ +<?xml version="1.0"?> + +<PropertyList include="c172p-3d-jsbsim-set.xml"> + <sim> + <description>Alias for c172p-3d-jsbsim.</description> + </sim> +</PropertyList> diff --git a/Aircraft/c172p/c172p-base.xml b/Aircraft/c172p/c172p-base.xml new file mode 100644 index 000000000..7169736d9 --- /dev/null +++ b/Aircraft/c172p/c172p-base.xml @@ -0,0 +1,42 @@ +<?xml version="1.0"?> +<!-- +************************************************************************ +Common configuration for all C172P aircraft. +************************************************************************ +--> + +<PropertyList include="../c172/c172-base.xml"> + + <sim> + + <model> + <path archive="y">Aircraft/c172p/Models/c172p.xml</path> + </model> + + </sim> + + <autopilot> + <config> + <min-climb-speed-kt type="float">70.0</min-climb-speed-kt> + <best-climb-speed-kt type="float">75.0</best-climb-speed-kt> + <target-climb-rate-fpm type="float">500.0</target-climb-rate-fpm> + <target-descent-rate-fpm type="float">1000.0</target-descent-rate-fpm> + <elevator-adj-factor type="float">4000.0</elevator-adj-factor> + <integral-contribution type="float">0.01</integral-contribution> + <zero-pitch-throttle type="float">0.45</zero-pitch-throttle> + <zero-pitch-trim-full-throttle type="float">0.14</zero-pitch-trim-full-throttle> + </config> + </autopilot> + + <consumables> + <fuel> + <tank n="0"> + <level-gal_us>20</level-gal_us> + </tank> + <tank n="1"> + <level-gal_us>20</level-gal_us> + </tank> + </fuel> + </consumables> + +</PropertyList> diff --git a/Aircraft/c172p/c172p-jsbsim-base.xml b/Aircraft/c172p/c172p-jsbsim-base.xml new file mode 100644 index 000000000..ad8e57383 --- /dev/null +++ b/Aircraft/c172p/c172p-jsbsim-base.xml @@ -0,0 +1,24 @@ +<?xml version="1.0"?> +<!-- +************************************************************************ +Common configuration for JSBSim C172P aircraft. +************************************************************************ +--> + +<PropertyList include="c172p-base.xml"> + + <sim> + <flight-model archive="y">jsb</flight-model> + <aero archive="y">c172p</aero> + </sim> + + <!-- trim for level cruise --> + + <controls> + <flight> + <aileron-trim>0.027</aileron-trim> + <rudder-trim>0.0</rudder-trim> + </flight> + </controls> + +</PropertyList> diff --git a/Aircraft/c172p/c172p-jsbsim-set.xml b/Aircraft/c172p/c172p-jsbsim-set.xml new file mode 100644 index 000000000..860291cef --- /dev/null +++ b/Aircraft/c172p/c172p-jsbsim-set.xml @@ -0,0 +1,36 @@ +<?xml version="1.0"?> +<!-- +************************************************************************ +JSBSim Cessna 172P with 2D panel. + +Started October 23 2001 by John Check, fgpanels@rockfish.net +************************************************************************ +--> + +<PropertyList include="c172p-jsbsim-base.xml"> + + <sim> + + <description>Cessna 172P (JSBSim, 2D panel).</description> + + <!-- Use a 2D instrument panel --> + + <panel> + <path>Aircraft/c172/Panels/c172-vfr-panel.xml</path> + <visibility archive="y">true</visibility> + </panel> + <panel_2> + <path>Aircraft/c172/Panels/c172-trans-mini-panel.xml</path> + </panel_2> + + <!-- Look down a bit over the top of the panel --> + + <view> + <config> + <pitch-offset-deg>-8</pitch-offset-deg> + </config> + </view> + + </sim> + +</PropertyList> diff --git a/Aircraft/c172p/c172p-set.xml b/Aircraft/c172p/c172p-set.xml new file mode 100644 index 000000000..95cf781a0 --- /dev/null +++ b/Aircraft/c172p/c172p-set.xml @@ -0,0 +1,7 @@ +<?xml version="1.0"?> + +<PropertyList include="c172p-jsbsim-set.xml"> + <sim> + <description>Alias for c172p-jsbsim.</description> + </sim> +</PropertyList> diff --git a/Aircraft/ufo/ufo-set.xml b/Aircraft/ufo/ufo-set.xml new file mode 100644 index 000000000..7c70b3b48 --- /dev/null +++ b/Aircraft/ufo/ufo-set.xml @@ -0,0 +1,36 @@ +<?xml version="1.0"?> +<!-- +************************************************************************ +Cessna 172 simulation config. This files ties together all the components +used by FGFS to represent the C172. Components include the flight data +model, instrument panel, and external 3D model. +3D models can be downloaded from http://home.t-online.de/home/Wolfram.Kuss/ + +October 23 2001 John Check, fgpanels@rockfish.net +************************************************************************ +--> + +<PropertyList> + + <sim> + + <description>UFO from the 'White Project' of the UNESCO</description> + + <flight-model>ufo</flight-model> + + <sound> + <audible>true</audible> + <path>Aircraft/ufo/ufo-sound.xml</path> + </sound> + + <panel> + <visibility>false</visibility> + </panel> + + <model> + <path>Aircraft/ufo/Models/ufo.xml</path> + </model> + + </sim> + +</PropertyList>