diff --git a/Aircraft-yasim/747.xml b/Aircraft-yasim/747.xml index feebe7638..3be382564 100644 --- a/Aircraft-yasim/747.xml +++ b/Aircraft-yasim/747.xml @@ -1,124 +1,127 @@ -<airplane mass="400000"> - -<!-- Approach configuration --> -<approach speed="136" aoa="7"> - <control-setting axis="/controls/throttle[0]" value="0.2"/> - <control-setting axis="/controls/throttle[1]" value="0.2"/> - <control-setting axis="/controls/flaps" value="1.0"/> - <control-setting axis="/controls/slats" value="1.0"/> - <control-setting axis="/controls/gear-down" value="1"/> -</approach> - -<!-- Cruise configuration --> -<cruise speed="530" alt="41000"> - <control-setting axis="/controls/throttle[0]" value="1.0"/> - <control-setting axis="/controls/throttle[1]" value="1.0"/> - <control-setting axis="/controls/flaps" value="0.0"/> - <control-setting axis="/controls/gear-down" value="0"/> -</cruise> - -<cockpit x="-5.42" y="1.81" z="15.06"/> - -<fuselage ax="0" ay="0" az="0" bx="-69.86" by="0.00" bz="2.41" - width="6" taper="0.3" midpoint="0.2"/> - -<wing x="-26.50" y="3.01" z="-1.45" length="33.72" chord="13.25" sweep="33" - taper=".27" dihedral="7" camber="0.1"> - <stall aoa="15" width="2" peak="1.5"/> - <flap0 start="0" end=".56" lift="1.8" drag="3"/> - <flap1 start=".64" end=".88" lift="1.3" drag="1.5"/> - <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/flaps" control="FLAP0"/> - <control-input axis="/controls/aileron" control="FLAP1" split="true"/> - <control-input axis="/controls/aileron-trim" control="FLAP1" split="true"/> - <control-input axis="/controls/slats" control="SLAT"/> - <control-input axis="/controls/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="-62.63" y="1.81" z="1.81" chord="8.43" length="10.84" taper=".29" - sweep="28" dihedral="7" effectiveness="1.9"> - <stall aoa="15" width="2" peak="1.5"/> - <flap0 start="0" end="1" lift="1.4" drag="1.8"/> - <control-input axis="/controls/elevator" control="FLAP0"/> - <control-input axis="/controls/elevator-trim" control="FLAP0"/> - <control-output control="FLAP0" prop="/surface-positions/elevator-pos-norm"/> -</hstab> - -<vstab x="-62.63" 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/rudder" control="FLAP0" invert="true"/> - <control-input axis="/controls/rudder-trim" control="FLAP0" invert="true"/> - <control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm" - min="1" max="-1"/> -</vstab> - -<jet x="-34.93" y="16.26" z="-1.20" mass="8000" thrust="60000"> - <control-input axis="/controls/throttle[0]" control="THROTTLE"/> -</jet> - -<jet x="-26.50" y="12.65" z="-2.41" mass="8000" thrust="60000"> - <control-input axis="/controls/throttle[0]" control="THROTTLE"/> -</jet> - -<jet x="-26.50" y="-12.65" z="-2.41" mass="8000" thrust="60000"> - <control-input axis="/controls/throttle[1]" control="THROTTLE"/> -</jet> - -<jet x="-34.93" y="-16.26" z="-1.20" mass="8000" thrust="60000"> - <control-input axis="/controls/throttle[1]" control="THROTTLE"/> -</jet> - -<gear x="-5.42" y="0.00" z="-5.42" compression="2"> <!-- nose --> - <control-input axis="/controls/rudder" control="STEER" square="true"/> - <control-input axis="/controls/gear-down" control="EXTEND"/> - <control-output control="EXTEND" prop="/gear/gear[0]/position-norm"/> - <control-speed control="EXTEND" transition-time="7"/> -</gear> - -<gear x="-29.15" y="5.42" z="-5.42" compression="2"> <!-- fwd left main --> - <control-input axis="/controls/brakes[0]" control="BRAKE"/> - <control-input axis="/controls/gear-down" control="EXTEND"/> - <control-output control="EXTEND" prop="/gear/gear[1]/position-norm"/> - <control-speed control="EXTEND" transition-time="7"/> -</gear> - -<gear x="-31.32" y="1.81" z="-5.42" compression="2"> <!-- rear left main --> - <control-input axis="/controls/brakes[0]" control="BRAKE"/> - <control-input axis="/controls/gear-down" control="EXTEND"/> - <control-output control="EXTEND" prop="/gear/gear[2]/position-norm"/> - <control-speed control="EXTEND" transition-time="7"/> -</gear> - -<gear x="-31.32" y="-1.81" z="-5.42" compression="2"> <!-- rear right main --> - <control-input axis="/controls/brakes[1]" control="BRAKE"/> - <control-input axis="/controls/gear-down" control="EXTEND"/> - <control-output control="EXTEND" prop="/gear/gear[3]/position-norm"/> - <control-speed control="EXTEND" transition-time="7"/> -</gear> - -<gear x="-29.15" y="-5.42" z="-5.42" compression="2"> <!-- fwd right main --> - <control-input axis="/controls/brakes[1]" control="BRAKE"/> - <control-input axis="/controls/gear-down" control="EXTEND"/> - <control-output control="EXTEND" prop="/gear/gear[4]/position-norm"/> - <control-speed control="EXTEND" transition-time="7"/> -</gear> - -<tank x="-26.50" y="0" z="-1.45" jet="true" capacity="128000"/> -<tank x="-30.10" y="8" z="-1.45" jet="true" capacity="128000"/> -<tank x="-30.10" y="-8" z="-1.45" jet="true" capacity="128000"/> - -<ballast x="-6" y="0" z="2.4" mass="30000"/> <!-- hump --> -<ballast x="-12" y="0" z="2.4" mass="40000"/> <!-- hump --> -<ballast x="-18" y="0" z="2.4" mass="40000"/> <!-- hump --> -<ballast x="-24" y="0" z="2.4" mass="30000"/> <!-- hump --> - -</airplane> \ No newline at end of file +<airplane mass="400000"> + +<!-- Approach configuration --> +<approach speed="136" aoa="7"> + <control-setting axis="/controls/throttle[0]" value="0.2"/> + <control-setting axis="/controls/throttle[1]" value="0.2"/> + <control-setting axis="/controls/flaps" value="1.0"/> + <control-setting axis="/controls/slats" value="1.0"/> + <control-setting axis="/controls/gear-down" value="1"/> +</approach> + +<!-- Cruise configuration --> +<cruise speed="490" alt="36000"> + <control-setting axis="/controls/throttle[0]" value="0.75"/> + <control-setting axis="/controls/throttle[1]" value="0.75"/> + <control-setting axis="/controls/flaps" value="0.0"/> + <control-setting axis="/controls/gear-down" value="0"/> +</cruise> + +<cockpit x="-5.42" y="1.81" z="15.06"/> + +<fuselage ax="0" ay="0" az="0" bx="-69.86" by="0.00" bz="2.41" + width="6" taper="0.3" midpoint="0.2"/> + +<wing x="-26.50" 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="15" width="2" peak="1.5"/> + <flap0 start="0" end=".56" lift="1.8" drag="3"/> + <flap1 start=".64" end=".88" lift="1.3" drag="1.5"/> + <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/flaps" control="FLAP0"/> + <control-input axis="/controls/aileron" control="FLAP1" split="true"/> + <control-input axis="/controls/aileron-trim" control="FLAP1" split="true"/> + <control-input axis="/controls/slats" control="SLAT"/> + <control-input axis="/controls/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="-62.63" y="1.81" z="1.81" chord="8.43" length="10.84" taper=".29" + sweep="28" dihedral="7" camber="-0.1" effectiveness="1.5"> + <stall aoa="15" width="2" peak="1.5"/> + <flap0 start="0" end="1" lift="1.6" drag="1.8"/> + <control-input axis="/controls/elevator" control="FLAP0"/> + <control-input axis="/controls/elevator-trim" control="FLAP0"/> + <control-output control="FLAP0" prop="/surface-positions/elevator-pos-norm"/> +</hstab> + +<vstab x="-62.63" 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/rudder" control="FLAP0" invert="true"/> + <control-input axis="/controls/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="-34.93" y="16.26" z="-1.20" mass="8000" thrust="63737"> + <control-input axis="/controls/throttle[0]" control="THROTTLE"/> +</jet> + +<jet x="-26.50" y="12.65" z="-2.41" mass="8000" thrust="63737"> + <control-input axis="/controls/throttle[0]" control="THROTTLE"/> +</jet> + +<jet x="-26.50" y="-12.65" z="-2.41" mass="8000" thrust="63737"> + <control-input axis="/controls/throttle[1]" control="THROTTLE"/> +</jet> + +<jet x="-34.93" y="-16.26" z="-1.20" mass="8000" thrust="63737"> + <control-input axis="/controls/throttle[1]" control="THROTTLE"/> +</jet> + +<gear x="-5.42" y="0.00" z="-5.42" compression="2"> <!-- nose --> + <control-input axis="/controls/rudder" control="STEER" square="true"/> + <control-input axis="/controls/gear-down" control="EXTEND"/> + <control-output control="EXTEND" prop="/gear/gear[0]/position-norm"/> + <control-speed control="EXTEND" transition-time="7"/> +</gear> + +<gear x="-29.15" y="5.42" z="-5.42" compression="2"> <!-- fwd left main --> + <control-input axis="/controls/brakes[0]" control="BRAKE"/> + <control-input axis="/controls/gear-down" control="EXTEND"/> + <control-output control="EXTEND" prop="/gear/gear[1]/position-norm"/> + <control-speed control="EXTEND" transition-time="7"/> +</gear> + +<gear x="-31.32" y="1.81" z="-5.42" compression="2"> <!-- rear left main --> + <control-input axis="/controls/brakes[0]" control="BRAKE"/> + <control-input axis="/controls/gear-down" control="EXTEND"/> + <control-output control="EXTEND" prop="/gear/gear[2]/position-norm"/> + <control-speed control="EXTEND" transition-time="7"/> +</gear> + +<gear x="-31.32" y="-1.81" z="-5.42" compression="2"> <!-- rear right main --> + <control-input axis="/controls/brakes[1]" control="BRAKE"/> + <control-input axis="/controls/gear-down" control="EXTEND"/> + <control-output control="EXTEND" prop="/gear/gear[3]/position-norm"/> + <control-speed control="EXTEND" transition-time="7"/> +</gear> + +<gear x="-29.15" y="-5.42" z="-5.42" compression="2"> <!-- fwd right main --> + <control-input axis="/controls/brakes[1]" control="BRAKE"/> + <control-input axis="/controls/gear-down" control="EXTEND"/> + <control-output control="EXTEND" prop="/gear/gear[4]/position-norm"/> + <control-speed control="EXTEND" transition-time="7"/> +</gear> + +<tank x="-26.50" y="0" z="-1.45" jet="true" capacity="128000"/> +<tank x="-30.10" y="8" z="-1.45" jet="true" capacity="128000"/> +<tank x="-30.10" y="-8" z="-1.45" jet="true" capacity="128000"/> + +<ballast x="-6" y="0" z="2.4" mass="30000"/> <!-- hump --> +<ballast x="-12" y="0" z="2.4" mass="40000"/> <!-- hump --> +<ballast x="-18" y="0" z="2.4" mass="40000"/> <!-- hump --> +<ballast x="-24" y="0" z="2.4" mass="30000"/> <!-- hump --> + +</airplane>