From 36f9127650568da2c8914ad66b747941cdc211fa Mon Sep 17 00:00:00 2001
From: jimw <jimw>
Date: Mon, 3 Jun 2002 19:52:51 +0000
Subject: [PATCH] Updated with Andy's latest fix for 747.

---
 Aircraft-yasim/747.xml | 251 +++++++++++++++++++++--------------------
 1 file changed, 127 insertions(+), 124 deletions(-)

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>