diff --git a/A318-100-CFM.xml b/A318-100-CFM.xml
index 0a0c8cac..8efc7527 100644
--- a/A318-100-CFM.xml
+++ b/A318-100-CFM.xml
@@ -4,585 +4,585 @@
xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance"
xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
-<fileheader>
- <author>Joshua Davidson (it0uchpods)</author>
- <version>Pre V1.0</version>
- <description>A3XX FDE</description>
-</fileheader>
+ <fileheader>
+ <author>Joshua Davidson (it0uchpods)</author>
+ <version>Pre V1.0</version>
+ <description>A3XX FDE</description>
+ </fileheader>
-<metrics>
- <wingarea unit="FT2"> 1319.79 </wingarea>
- <wingspan unit="FT" > 111.26 </wingspan>
- <wing_incidence> 1.03 </wing_incidence>
- <chord unit="FT" > 13.76 </chord>
- <htailarea unit="FT2"> 334.24 </htailarea>
- <htailarm unit="FT" > 57.88 </htailarm>
- <vtailarea unit="FT2"> 248.79 </vtailarea>
- <vtailarm unit="FT" > 57.33 </vtailarm>
+ <metrics>
+ <wingarea unit="FT2"> 1319.79 </wingarea>
+ <wingspan unit="FT" > 111.26 </wingspan>
+ <wing_incidence> 1.03 </wing_incidence>
+ <chord unit="FT" > 13.76 </chord>
+ <htailarea unit="FT2"> 334.24 </htailarea>
+ <htailarm unit="FT" > 57.88 </htailarm>
+ <vtailarea unit="FT2"> 248.79 </vtailarea>
+ <vtailarm unit="FT" > 57.33 </vtailarm>
- <location name="AERORP" unit="IN">
- <x> 700.00 </x>
- <y> 0 </y>
- <z> 0.00 </z>
- </location>
+ <location name="AERORP" unit="IN">
+ <x> 700.00 </x>
+ <y> 0 </y>
+ <z> 0.00 </z>
+ </location>
- <location name="EYEPOINT" unit="IN">
- <x> 80 </x>
- <y> -30 </y>
- <z> 70 </z>
- </location>
+ <location name="EYEPOINT" unit="IN">
+ <x> 80 </x>
+ <y> -30 </y>
+ <z> 70 </z>
+ </location>
- <location name="VRP" unit="IN">
- <x> 661.1 </x>
- <y> 0 </y>
- <z> -37 </z>
- </location>
+ <location name="VRP" unit="IN">
+ <x> 661.1 </x>
+ <y> 0 </y>
+ <z> -37 </z>
+ </location>
- </metrics>
+ </metrics>
- <mass_balance>
- <ixx unit="SLUG*FT2"> 611903</ixx>
- <iyy unit="SLUG*FT2">1735389</iyy>
- <izz unit="SLUG*FT2">2301293</izz>
+ <mass_balance>
+ <ixx unit="SLUG*FT2"> 611903</ixx>
+ <iyy unit="SLUG*FT2">1735389</iyy>
+ <izz unit="SLUG*FT2">2301293</izz>
- <ixy unit="SLUG*FT2">0</ixy>
- <ixz unit="SLUG*FT2">0</ixz>
- <iyz unit="SLUG*FT2">0</iyz>
- <emptywt unit="LBS">80431</emptywt>
+ <ixy unit="SLUG*FT2">0</ixy>
+ <ixz unit="SLUG*FT2">0</ixz>
+ <iyz unit="SLUG*FT2">0</iyz>
+ <emptywt unit="LBS">80431</emptywt>
- <location name="CG" unit="IN">
- <x> 652.00 </x>
- <y> 0 </y>
- <z> 0.00 </z>
- </location>
+ <location name="CG" unit="IN">
+ <x> 652.00 </x>
+ <y> 0 </y>
+ <z> 0.00 </z>
+ </location>
- <pointmass name="Cockpit Crew">
- <weight unit="LBS">400</weight>
- <!-- MAX: 400lbs, two pilots-->
- <location name="POINTMASS" unit="IN">
- <x>200</x>
- <y>0</y>
- <z>0</z>
- </location>
- </pointmass>
- <pointmass name="Engine 1">
- <weight unit="LBS">5200.7</weight>
- <location name="POINTMASS" unit="IN">
- <x>530.86</x>
- <y>-5.755</y>
- <z>-78.56019</z>
- </location>
- </pointmass>
- <pointmass name="Engine 2">
- <weight unit="LBS">5200.7</weight>
- <location name="POINTMASS" unit="IN">
- <x>530.86</x>
- <y>5.755</y>
- <z>-78.56019</z>
- </location>
- </pointmass>
- <pointmass name="PAX 0A (60 seats)">
- <weight unit="LBS">6600</weight>
- <!-- MAX: 13200lbs, 60 seats -->
- <location name="POINTMASS" unit="IN">
- <x>470.1711</x>
- <y>0</y>
- <z>0</z>
- </location>
- </pointmass>
- <pointmass name="PAX 0B (60 seats)">
- <weight unit="LBS">6600</weight>
- <!-- MAX: 13200lbs, 60 seats -->
- <location name="POINTMASS" unit="IN">
- <x>809.5669</x>
- <y>0</y>
- <z>0</z>
- </location>
- </pointmass>
- <pointmass name="PAX 0C (54 seats)">
- <weight unit="LBS">5940</weight>
- <!-- MAX: 11880lbs, 54 seats -->
- <location name="POINTMASS" unit="IN">
- <x>1163.2729</x>
- <y>0</y>
- <z>0</z>
- </location>
- </pointmass>
- <pointmass name="Cargo Hold 1">
- <weight unit="LBS">2000</weight>
- <!-- MAX: 7500.126lbs -->
- <location name="POINTMASS" unit="IN">
- <x>383.4792</x>
- <y>0</y>
- <z>-29.5</z>
- <!-- 1.5m and now half of it for the center point of the load -->
- </location>
- </pointmass>
- <!-- Cargo Hold 2 doesn't exist, that is the center tank -->
- <pointmass name="Cargo Hold 3">
- <weight unit="LBS">2000</weight>
- <!-- MAX: 5384.414lbs -->
- <location name="POINTMASS" unit="IN">
- <x>849.1324</x>
- <y>0</y>
- <z>-29.5</z>
- </location>
- </pointmass>
- <pointmass name="Cargo Hold 4">
- <weight unit="LBS">1500</weight>
- <!-- MAX: 4651.754lbs -->
- <location name="POINTMASS" unit="IN">
- <x>931.0653</x>
- <y>0</y>
- <z>-29.5</z>
- </location>
- </pointmass>
- <pointmass name="Cargo Hold 5">
- <weight unit="LBS">2000</weight>
- <!-- MAX: 3300.320lbs -->
- <location name="POINTMASS" unit="IN">
- <x>1068.2634</x>
- <y>0</y>
- <z>0</z>
- <!-- Cargo Hold #5 sits higher on the range of the cabin deck, it's only loadable with lifter -->
- </location>
- </pointmass>
+ <pointmass name="Cockpit Crew">
+ <weight unit="LBS">400</weight>
+ <!-- MAX: 400lbs, two pilots-->
+ <location name="POINTMASS" unit="IN">
+ <x>200</x>
+ <y>0</y>
+ <z>0</z>
+ </location>
+ </pointmass>
+ <pointmass name="Engine 1">
+ <weight unit="LBS">5200.7</weight>
+ <location name="POINTMASS" unit="IN">
+ <x>530.86</x>
+ <y>-5.755</y>
+ <z>-78.56019</z>
+ </location>
+ </pointmass>
+ <pointmass name="Engine 2">
+ <weight unit="LBS">5200.7</weight>
+ <location name="POINTMASS" unit="IN">
+ <x>530.86</x>
+ <y>5.755</y>
+ <z>-78.56019</z>
+ </location>
+ </pointmass>
+ <pointmass name="PAX 0A (60 seats)">
+ <weight unit="LBS">6600</weight>
+ <!-- MAX: 13200lbs, 60 seats -->
+ <location name="POINTMASS" unit="IN">
+ <x>470.1711</x>
+ <y>0</y>
+ <z>0</z>
+ </location>
+ </pointmass>
+ <pointmass name="PAX 0B (60 seats)">
+ <weight unit="LBS">6600</weight>
+ <!-- MAX: 13200lbs, 60 seats -->
+ <location name="POINTMASS" unit="IN">
+ <x>809.5669</x>
+ <y>0</y>
+ <z>0</z>
+ </location>
+ </pointmass>
+ <pointmass name="PAX 0C (54 seats)">
+ <weight unit="LBS">5940</weight>
+ <!-- MAX: 11880lbs, 54 seats -->
+ <location name="POINTMASS" unit="IN">
+ <x>1163.2729</x>
+ <y>0</y>
+ <z>0</z>
+ </location>
+ </pointmass>
+ <pointmass name="Cargo Hold 1">
+ <weight unit="LBS">2000</weight>
+ <!-- MAX: 7500.126lbs -->
+ <location name="POINTMASS" unit="IN">
+ <x>383.4792</x>
+ <y>0</y>
+ <z>-29.5</z>
+ <!-- 1.5m and now half of it for the center point of the load -->
+ </location>
+ </pointmass>
+ <!-- Cargo Hold 2 doesn't exist, that is the center tank -->
+ <pointmass name="Cargo Hold 3">
+ <weight unit="LBS">2000</weight>
+ <!-- MAX: 5384.414lbs -->
+ <location name="POINTMASS" unit="IN">
+ <x>849.1324</x>
+ <y>0</y>
+ <z>-29.5</z>
+ </location>
+ </pointmass>
+ <pointmass name="Cargo Hold 4">
+ <weight unit="LBS">1500</weight>
+ <!-- MAX: 4651.754lbs -->
+ <location name="POINTMASS" unit="IN">
+ <x>931.0653</x>
+ <y>0</y>
+ <z>-29.5</z>
+ </location>
+ </pointmass>
+ <pointmass name="Cargo Hold 5">
+ <weight unit="LBS">2000</weight>
+ <!-- MAX: 3300.320lbs -->
+ <location name="POINTMASS" unit="IN">
+ <x>1068.2634</x>
+ <y>0</y>
+ <z>0</z>
+ <!-- Cargo Hold #5 sits higher on the range of the cabin deck, it's only loadable with lifter -->
+ </location>
+ </pointmass>
- </mass_balance>
+ </mass_balance>
- <ground_reactions>
- <!-- REF-1 page 165 + 271 -->
- <contact type="BOGEY" name="NOSE_LG">
- <location unit="IN">
- <x> 197.6772 </x>
- <y> 0 </y>
- <z> -137.9617 </z>
- </location>
- <static_friction> 0.8 </static_friction>
- <dynamic_friction> 0.5 </dynamic_friction>
- <rolling_friction> 0.02 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 30935.5 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 16978.5 </damping_coeff>
- <max_steer unit="DEG"> 70 </max_steer>
- <!-- REF-1 page 133 -->
- <brake_group> NOSE </brake_group>
- <retractable>1</retractable>
- </contact>
- <contact type="BOGEY" name="LEFT_MLG">
- <location unit="IN">
- <!--<x> 699.9243 </x>-->
- <x> 695.3149 </x>
- <y> -149.4094 </y>
- <z> -150.4824 </z>
- </location>
- <!-- <static_friction> 0.5 </static_friction> WHAT??? less static than dinamyc friction?-->
- <static_friction> 0.8 </static_friction>
- <dynamic_friction> 0.5 </dynamic_friction>
- <rolling_friction> 0.02 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 59785 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 23957 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> LEFT </brake_group>
- <retractable>1</retractable>
- </contact>
- <contact type="BOGEY" name="RIGHT_MLG">
- <location unit="IN">
- <!-- <x> 697.3425 </x> It should be right left simetric
- <x> 699.9243 </x> -->
- <x> 695.3149 </x>
- <y> 149.4094 </y>
- <z> -150.4824 </z>
- </location>
- <!-- <static_friction> 0.5 </static_friction> WHAT??? less static than dinamyc friction?-->
- <static_friction> 0.8 </static_friction>
- <dynamic_friction> 0.5 </dynamic_friction>
- <rolling_friction> 0.02 </rolling_friction>
- <!--spring_coeff unit="LBS/FT"> 169785 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 33957 </damping_coeff-->
- <spring_coeff unit="LBS/FT"> 59785 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 23957 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> RIGHT </brake_group>
- <retractable>1</retractable>
- </contact>
+ <ground_reactions>
+ <!-- REF-1 page 165 + 271 -->
+ <contact type="BOGEY" name="NOSE_LG">
+ <location unit="IN">
+ <x> 197.6772 </x>
+ <y> 0 </y>
+ <z> -137.9617 </z>
+ </location>
+ <static_friction> 0.8 </static_friction>
+ <dynamic_friction> 0.5 </dynamic_friction>
+ <rolling_friction> 0.02 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 30935.5 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 16978.5 </damping_coeff>
+ <max_steer unit="DEG"> 70 </max_steer>
+ <!-- REF-1 page 133 -->
+ <brake_group> NOSE </brake_group>
+ <retractable>1</retractable>
+ </contact>
+ <contact type="BOGEY" name="LEFT_MLG">
+ <location unit="IN">
+ <!--<x> 699.9243 </x>-->
+ <x> 695.3149 </x>
+ <y> -149.4094 </y>
+ <z> -150.4824 </z>
+ </location>
+ <!-- <static_friction> 0.5 </static_friction> WHAT??? less static than dinamyc friction?-->
+ <static_friction> 0.8 </static_friction>
+ <dynamic_friction> 0.5 </dynamic_friction>
+ <rolling_friction> 0.02 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 59785 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 23957 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> LEFT </brake_group>
+ <retractable>1</retractable>
+ </contact>
+ <contact type="BOGEY" name="RIGHT_MLG">
+ <location unit="IN">
+ <!-- <x> 697.3425 </x> It should be right left simetric
+ <x> 699.9243 </x> -->
+ <x> 695.3149 </x>
+ <y> 149.4094 </y>
+ <z> -150.4824 </z>
+ </location>
+ <!-- <static_friction> 0.5 </static_friction> WHAT??? less static than dinamyc friction?-->
+ <static_friction> 0.8 </static_friction>
+ <dynamic_friction> 0.5 </dynamic_friction>
+ <rolling_friction> 0.02 </rolling_friction>
+ <!--spring_coeff unit="LBS/FT"> 169785 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 33957 </damping_coeff-->
+ <spring_coeff unit="LBS/FT"> 59785 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 23957 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> RIGHT </brake_group>
+ <retractable>1</retractable>
+ </contact>
- <contact type="STRUCTURE" name="NOSE_1">
- <location unit="IN">
- <x> 37.7953 </x>
- <y> 0 </y>
- <z> -38.1374 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="NOSE_2">
- <location unit="IN">
- <x> 128.1102 </x>
- <y> 0 </y>
- <z> -55.0271 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="CENTER_1">
- <location unit="IN">
- <x> 274.0157 </x>
- <y> 0 </y>
- <z> -60.0665 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="CENTER_2">
- <location unit="IN">
- <x> 930 </x>
- <y> 0 </y>
- <z> -60.0665 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
+ <contact type="STRUCTURE" name="NOSE_1">
+ <location unit="IN">
+ <x> 37.7953 </x>
+ <y> 0 </y>
+ <z> -38.1374 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="NOSE_2">
+ <location unit="IN">
+ <x> 128.1102 </x>
+ <y> 0 </y>
+ <z> -55.0271 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="CENTER_1">
+ <location unit="IN">
+ <x> 274.0157 </x>
+ <y> 0 </y>
+ <z> -60.0665 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="CENTER_2">
+ <location unit="IN">
+ <x> 930 </x>
+ <y> 0 </y>
+ <z> -60.0665 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
- <contact type="STRUCTURE" name="ENG_1">
- <location unit="IN">
- <x>589.735</x>
- <y>-226.575</y>
- <z>-95.567</z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="ENG_2">
- <location unit="IN">
- <x>589.735</x>
- <y>226.575</y>
- <z>-95.567</z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.5 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
+ <contact type="STRUCTURE" name="ENG_1">
+ <location unit="IN">
+ <x>589.735</x>
+ <y>-226.575</y>
+ <z>-95.567</z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="ENG_2">
+ <location unit="IN">
+ <x>589.735</x>
+ <y>226.575</y>
+ <z>-95.567</z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.5 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
- <contact type="STRUCTURE" name="TAIL_1">
- <location unit="IN">
- <x> 1097.9921 </x>
- <y> 0 </y>
- <z> -44.7722 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="TAIL_2">
- <location unit="IN">
- <x> 1225 </x>
- <y> 0 </y>
- <z> -18.8067 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="TAIL_3">
- <location unit="IN">
- <x> 1341.6142 </x>
- <y> 0 </y>
- <z> -10.2599 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="TAIL_4">
- <location unit="IN">
- <x> 1469.0945 </x>
- <y> 0 </y>
- <z> 47.4138 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 1 </dynamic_friction>
- <rolling_friction> 1 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="WING_TIP_1">
- <location unit="IN">
- <x> 838.8898 </x>
- <y> -667.5197 </y>
- <z> 35.7926 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="WING_TIP_2">
- <location unit="IN">
- <x> 838.8898 </x>
- <y> 667.5197 </y>
- <z> 35.7926 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 1 </dynamic_friction>
- <rolling_friction> 1 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- </ground_reactions>
+ <contact type="STRUCTURE" name="TAIL_1">
+ <location unit="IN">
+ <x> 1097.9921 </x>
+ <y> 0 </y>
+ <z> -44.7722 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="TAIL_2">
+ <location unit="IN">
+ <x> 1225 </x>
+ <y> 0 </y>
+ <z> -18.8067 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="TAIL_3">
+ <location unit="IN">
+ <x> 1341.6142 </x>
+ <y> 0 </y>
+ <z> -10.2599 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="TAIL_4">
+ <location unit="IN">
+ <x> 1469.0945 </x>
+ <y> 0 </y>
+ <z> 47.4138 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 1 </dynamic_friction>
+ <rolling_friction> 1 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="WING_TIP_1">
+ <location unit="IN">
+ <x> 838.8898 </x>
+ <y> -667.5197 </y>
+ <z> 35.7926 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="WING_TIP_2">
+ <location unit="IN">
+ <x> 838.8898 </x>
+ <y> 667.5197 </y>
+ <z> 35.7926 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 1 </dynamic_friction>
+ <rolling_friction> 1 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ </ground_reactions>
-<propulsion>
+ <propulsion>
- <engine file="cfm56_5b9">
- <location unit="IN">
- <x> 620.0683 </x>
- <y> -226.575 </y>
- <z> -45.567 </z>
- </location>
- <orient unit="DEG">
- <roll> 0.0 </roll>
- <pitch> 2.2 </pitch>
- <yaw> 1 </yaw>
- </orient>
- <feed>7</feed>
- <thruster file="direct">
+ <engine file="cfm56_5b9">
<location unit="IN">
- <x> 655.4820 </x>
- <y> -226.575 </y>
- <z> 0.000 </z>
+ <x> 620.0683 </x>
+ <y> -226.575 </y>
+ <z> -45.567 </z>
</location>
<orient unit="DEG">
- <roll> 0.0 </roll>
- <pitch> 2.2 </pitch>
- <yaw> 1 </yaw>
+ <roll> 0.0 </roll>
+ <pitch> 2.2 </pitch>
+ <yaw> 1 </yaw>
</orient>
- </thruster>
- </engine>
+ <feed>7</feed>
+ <thruster file="direct">
+ <location unit="IN">
+ <x> 655.4820 </x>
+ <y> -226.575 </y>
+ <z> 0.000 </z>
+ </location>
+ <orient unit="DEG">
+ <roll> 0.0 </roll>
+ <pitch> 2.2 </pitch>
+ <yaw> 1 </yaw>
+ </orient>
+ </thruster>
+ </engine>
- <engine file="cfm56_5b9">
- <location unit="IN">
- <x> 620.0683 </x>
- <y> 226.575 </y>
- <z> -45.567 </z>
- </location>
- <orient unit="DEG">
- <roll> 0.0 </roll>
- <pitch> 2.2 </pitch>
- <yaw> -1 </yaw>
- </orient>
- <feed>8</feed>
- <thruster file="direct">
+ <engine file="cfm56_5b9">
<location unit="IN">
- <x> 655.4820 </x>
- <y> 226.575 </y>
- <z> 0.000 </z>
+ <x> 620.0683 </x>
+ <y> 226.575 </y>
+ <z> -45.567 </z>
</location>
<orient unit="DEG">
- <roll> 0.0 </roll>
- <pitch> 2.2 </pitch>
- <yaw> -1 </yaw>
+ <roll> 0.0 </roll>
+ <pitch> 2.2 </pitch>
+ <yaw> -1 </yaw>
</orient>
- </thruster>
- </engine>
+ <feed>8</feed>
+ <thruster file="direct">
+ <location unit="IN">
+ <x> 655.4820 </x>
+ <y> 226.575 </y>
+ <z> 0.000 </z>
+ </location>
+ <orient unit="DEG">
+ <roll> 0.0 </roll>
+ <pitch> 2.2 </pitch>
+ <yaw> -1 </yaw>
+ </orient>
+ </thruster>
+ </engine>
- <tank type="FUEL"> <!-- Left Tank (Wing tip Ventilation Surge) 0 -->
- <location unit="IN">
- <x> 783.0709 </x>
- <y> -574.4148 </y>
- <z> 3.1080 </z>
- </location>
- <capacity unit="LBS"> 412 </capacity><!-- need review --> <!-- would be 1 percent of max load per each wing, 412 each. Needs temp rise of 20C at max load to fill -->
- <contents unit="LBS"> 0 </contents>
-
- <priority>4</priority>
- <type>JET-A1</type>
- <temperature>50</temperature>
- </tank>
- <tank type="FUEL"> <!-- Left Tank (Outer) 1 -->
- <location unit="IN">
- <x> 739.5669 </x>
- <y> -457.4259 </y>
- <z> -8.0898 </z>
- </location>
- <capacity unit="LBS"> 1520.00 </capacity><!-- need review -->
- <contents unit="LBS"> 1520 </contents><!-- outer filled first than inner -->
- <standpipe unit="LBS">21</standpipe><!-- minimun fuel on pipes -->
- <priority>2</priority>
- <type>JET-A1</type>
- <temperature>50</temperature>
- </tank>
- <tank type="FUEL"> <!-- Left Tank (Inner) 2 -->
- <location unit="IN">
- <x> 652.5591 </x>
- <y> -236.2992 </y>
- <z> -33.9470 </z>
- </location>
- <capacity unit="LBS"> 11982 </capacity><!-- correct by FCOM -->
- <contents unit="LBS"> 4480 </contents>
- <standpipe unit="LBS">31</standpipe><!-- minimun fuel on pipes -->
- <priority>3</priority>
- <type>JET-A1</type>
- <temperature>50</temperature>
- </tank>
- <tank type="FUEL"> <!-- Center Tank 3 -->
- <location unit="IN">
- <x> 522.0473 </x>
- <y> 0 </y>
- <z> -47.0 </z>
- </location>
- <capacity unit="LBS"> 14281 </capacity><!-- correct by FCOM -->
- <contents unit="LBS"> 0 </contents> <!-- wing tanks always filled first -->
- <standpipe unit="LBS">43</standpipe><!-- minimun fuel on pipes -->
- <priority>1</priority>
- <type>JET-A1</type>
- <temperature>50</temperature>
- </tank>
- <tank type="FUEL"> <!-- Right Tank (Inner) 4 -->
- <location unit="IN">
- <x> 652.5591 </x>
- <y> 236.2992 </y>
- <z> -33.9470 </z>
- </location>
- <capacity unit="LBS"> 11982 </capacity><!-- correct by FCOM -->
- <contents unit="LBS"> 4480 </contents>
- <standpipe unit="LBS">31</standpipe><!-- minimum fuel on pipes -->
- <priority>3</priority>
- <type>JET-A1</type>
- <temperature>50</temperature>
- </tank>
- <tank type="FUEL"> <!-- Right Tank (Outer) 5 -->
- <location unit="IN">
- <x> 739.5669 </x>
- <y> 457.4259 </y>
- <z> -8.0898 </z>
- </location>
- <capacity unit="LBS"> 1520 </capacity><!-- correct by FCOM -->
- <contents unit="LBS"> 1520 </contents><!-- outer filled before inner -->
- <standpipe unit="LBS">21</standpipe><!-- minimun fuel on pipes -->
- <priority>2</priority>
- <type>JET-A1</type>
- <temperature>50</temperature>
- </tank>
- <tank type="FUEL"> <!-- Right Tank (Wing tip Ventilation Surge) 6 -->
- <location unit="IN">
- <x> 783.0709 </x>
- <y> 574.4148 </y>
- <z> 3.1080 </z>
- </location>
- <capacity unit="LBS"> 412 </capacity><!-- need review --> <!-- 1 percent of max, see left surge tank, is 412 lb each -->
- <contents unit="LBS"> 0 </contents>
- <priority>4</priority>
- <type>JET-A1</type>
- <temperature>50</temperature>
- </tank>
- <tank type="FUEL"> <!-- LEFT FUEL PIPES (Engine 1 feed from this) -->
- <location unit="IN">
- <x>589.735</x>
- <y>-226.575</y>
- <z>-45.567</z>
- </location>
- <capacity unit="LBS"> 100 </capacity><!-- need review -->
- <contents unit="LBS"> 0 </contents>
- <priority>1</priority>
- <type>JET-A1</type>
- </tank>
- <tank type="FUEL"> <!-- RIGHT FUEL PIPES (Engine 2 feed from this) -->
- <location unit="IN">
- <x>589.735</x>
- <y>226.575</y>
- <z>-45.567</z>
- </location>
- <capacity unit="LBS"> 100 </capacity><!-- need review -->
- <contents unit="LBS"> 0 </contents>
- <priority>1</priority>
- <type>JET-A1</type>
- </tank>
-</propulsion>
+ <tank type="FUEL"> <!-- Left Tank (Wing tip Ventilation Surge) 0 -->
+ <location unit="IN">
+ <x> 783.0709 </x>
+ <y> -574.4148 </y>
+ <z> 3.1080 </z>
+ </location>
+ <capacity unit="LBS"> 412 </capacity><!-- need review --> <!-- would be 1 percent of max load per each wing, 412 each. Needs temp rise of 20C at max load to fill -->
+ <contents unit="LBS"> 0 </contents>
+
+ <priority>4</priority>
+ <type>JET-A1</type>
+ <temperature>50</temperature>
+ </tank>
+ <tank type="FUEL"> <!-- Left Tank (Outer) 1 -->
+ <location unit="IN">
+ <x> 739.5669 </x>
+ <y> -457.4259 </y>
+ <z> -8.0898 </z>
+ </location>
+ <capacity unit="LBS"> 1520.00 </capacity><!-- need review -->
+ <contents unit="LBS"> 1520 </contents><!-- outer filled first than inner -->
+ <standpipe unit="LBS">21</standpipe><!-- minimun fuel on pipes -->
+ <priority>2</priority>
+ <type>JET-A1</type>
+ <temperature>50</temperature>
+ </tank>
+ <tank type="FUEL"> <!-- Left Tank (Inner) 2 -->
+ <location unit="IN">
+ <x> 652.5591 </x>
+ <y> -236.2992 </y>
+ <z> -33.9470 </z>
+ </location>
+ <capacity unit="LBS"> 11982 </capacity><!-- correct by FCOM -->
+ <contents unit="LBS"> 4480 </contents>
+ <standpipe unit="LBS">31</standpipe><!-- minimun fuel on pipes -->
+ <priority>3</priority>
+ <type>JET-A1</type>
+ <temperature>50</temperature>
+ </tank>
+ <tank type="FUEL"> <!-- Center Tank 3 -->
+ <location unit="IN">
+ <x> 522.0473 </x>
+ <y> 0 </y>
+ <z> -47.0 </z>
+ </location>
+ <capacity unit="LBS"> 14281 </capacity><!-- correct by FCOM -->
+ <contents unit="LBS"> 0 </contents> <!-- wing tanks always filled first -->
+ <standpipe unit="LBS">43</standpipe><!-- minimun fuel on pipes -->
+ <priority>1</priority>
+ <type>JET-A1</type>
+ <temperature>50</temperature>
+ </tank>
+ <tank type="FUEL"> <!-- Right Tank (Inner) 4 -->
+ <location unit="IN">
+ <x> 652.5591 </x>
+ <y> 236.2992 </y>
+ <z> -33.9470 </z>
+ </location>
+ <capacity unit="LBS"> 11982 </capacity><!-- correct by FCOM -->
+ <contents unit="LBS"> 4480 </contents>
+ <standpipe unit="LBS">31</standpipe><!-- minimum fuel on pipes -->
+ <priority>3</priority>
+ <type>JET-A1</type>
+ <temperature>50</temperature>
+ </tank>
+ <tank type="FUEL"> <!-- Right Tank (Outer) 5 -->
+ <location unit="IN">
+ <x> 739.5669 </x>
+ <y> 457.4259 </y>
+ <z> -8.0898 </z>
+ </location>
+ <capacity unit="LBS"> 1520 </capacity><!-- correct by FCOM -->
+ <contents unit="LBS"> 1520 </contents><!-- outer filled before inner -->
+ <standpipe unit="LBS">21</standpipe><!-- minimun fuel on pipes -->
+ <priority>2</priority>
+ <type>JET-A1</type>
+ <temperature>50</temperature>
+ </tank>
+ <tank type="FUEL"> <!-- Right Tank (Wing tip Ventilation Surge) 6 -->
+ <location unit="IN">
+ <x> 783.0709 </x>
+ <y> 574.4148 </y>
+ <z> 3.1080 </z>
+ </location>
+ <capacity unit="LBS"> 412 </capacity><!-- need review --> <!-- 1 percent of max, see left surge tank, is 412 lb each -->
+ <contents unit="LBS"> 0 </contents>
+ <priority>4</priority>
+ <type>JET-A1</type>
+ <temperature>50</temperature>
+ </tank>
+ <tank type="FUEL"> <!-- LEFT FUEL PIPES (Engine 1 feed from this) -->
+ <location unit="IN">
+ <x>589.735</x>
+ <y>0</y>
+ <z>-45.567</z>
+ </location>
+ <capacity unit="LBS"> 100 </capacity><!-- need review -->
+ <contents unit="LBS"> 0 </contents>
+ <priority>1</priority>
+ <type>JET-A1</type>
+ </tank>
+ <tank type="FUEL"> <!-- RIGHT FUEL PIPES (Engine 2 feed from this) -->
+ <location unit="IN">
+ <x>589.735</x>
+ <y>0</y>
+ <z>-45.567</z>
+ </location>
+ <capacity unit="LBS"> 100 </capacity><!-- need review -->
+ <contents unit="LBS"> 0 </contents>
+ <priority>1</priority>
+ <type>JET-A1</type>
+ </tank>
+ </propulsion>
-<system file="pushback" />
-<system file="fuel" />
-<system file="glass-effect1" />
-<system file="fmgc" />
-<system file="fcs" />
+ <system file="pushback" />
+ <system file="fuel" />
+ <system file="glass-effect1" />
+ <system file="fmgc" />
+ <system file="fcs" />
-<flight_control name="none"/>
+ <flight_control name="none"/>
-<aerodynamics file="Systems/a318-aerodynamics.xml" />
+ <aerodynamics file="Systems/a318-aerodynamics.xml" />
-<external_reactions>
- <force name="pushback" frame="BODY">
- <location unit="IN">
- <x>294</x>
- <y>0</y>
- <z>-149</z>
- </location>
- <direction>
- <x>1</x>
- <y>0</y>
- <z>0</z>
- </direction>
- </force>
-</external_reactions>
+ <external_reactions>
+ <force name="pushback" frame="BODY">
+ <location unit="IN">
+ <x>294</x>
+ <y>0</y>
+ <z>-149</z>
+ </location>
+ <direction>
+ <x>1</x>
+ <y>0</y>
+ <z>0</z>
+ </direction>
+ </force>
+ </external_reactions>
</fdm_config>
diff --git a/A319-100-CFM.xml b/A319-100-CFM.xml
index 18d4ce2d..ed89c42c 100644
--- a/A319-100-CFM.xml
+++ b/A319-100-CFM.xml
@@ -4,585 +4,585 @@
xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance"
xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
-<fileheader>
- <author>Joshua Davidson (it0uchpods)</author>
- <version>Pre V1.0</version>
- <description>A3XX FDE</description>
-</fileheader>
+ <fileheader>
+ <author>Joshua Davidson (it0uchpods)</author>
+ <version>Pre V1.0</version>
+ <description>A3XX FDE</description>
+ </fileheader>
-<metrics>
- <wingarea unit="FT2"> 1319.79 </wingarea>
- <wingspan unit="FT" > 111.26 </wingspan>
- <wing_incidence> 1.03 </wing_incidence>
- <chord unit="FT" > 13.76 </chord>
- <htailarea unit="FT2"> 334.24 </htailarea>
- <htailarm unit="FT" > 57.88 </htailarm>
- <vtailarea unit="FT2"> 248.79 </vtailarea>
- <vtailarm unit="FT" > 57.33 </vtailarm>
+ <metrics>
+ <wingarea unit="FT2"> 1319.79 </wingarea>
+ <wingspan unit="FT" > 111.26 </wingspan>
+ <wing_incidence> 1.03 </wing_incidence>
+ <chord unit="FT" > 13.76 </chord>
+ <htailarea unit="FT2"> 334.24 </htailarea>
+ <htailarm unit="FT" > 57.88 </htailarm>
+ <vtailarea unit="FT2"> 248.79 </vtailarea>
+ <vtailarm unit="FT" > 57.33 </vtailarm>
- <location name="AERORP" unit="IN">
- <x> 700.00 </x>
- <y> 0 </y>
- <z> 0.00 </z>
- </location>
+ <location name="AERORP" unit="IN">
+ <x> 700.00 </x>
+ <y> 0 </y>
+ <z> 0.00 </z>
+ </location>
- <location name="EYEPOINT" unit="IN">
- <x> 80 </x>
- <y> -30 </y>
- <z> 70 </z>
- </location>
+ <location name="EYEPOINT" unit="IN">
+ <x> 80 </x>
+ <y> -30 </y>
+ <z> 70 </z>
+ </location>
- <location name="VRP" unit="IN">
- <x> 661.1 </x>
- <y> 0 </y>
- <z> -37 </z>
- </location>
+ <location name="VRP" unit="IN">
+ <x> 661.1 </x>
+ <y> 0 </y>
+ <z> -37 </z>
+ </location>
- </metrics>
+ </metrics>
- <mass_balance>
- <ixx unit="SLUG*FT2"> 611903</ixx>
- <iyy unit="SLUG*FT2">1735389</iyy>
- <izz unit="SLUG*FT2">2301293</izz>
+ <mass_balance>
+ <ixx unit="SLUG*FT2"> 611903</ixx>
+ <iyy unit="SLUG*FT2">1735389</iyy>
+ <izz unit="SLUG*FT2">2301293</izz>
- <ixy unit="SLUG*FT2">0</ixy>
- <ixz unit="SLUG*FT2">0</ixz>
- <iyz unit="SLUG*FT2">0</iyz>
- <emptywt unit="LBS">80431</emptywt>
+ <ixy unit="SLUG*FT2">0</ixy>
+ <ixz unit="SLUG*FT2">0</ixz>
+ <iyz unit="SLUG*FT2">0</iyz>
+ <emptywt unit="LBS">80431</emptywt>
- <location name="CG" unit="IN">
- <x> 652.00 </x>
- <y> 0 </y>
- <z> 0.00 </z>
- </location>
+ <location name="CG" unit="IN">
+ <x> 652.00 </x>
+ <y> 0 </y>
+ <z> 0.00 </z>
+ </location>
- <pointmass name="Cockpit Crew">
- <weight unit="LBS">400</weight>
- <!-- MAX: 400lbs, two pilots-->
- <location name="POINTMASS" unit="IN">
- <x>200</x>
- <y>0</y>
- <z>0</z>
- </location>
- </pointmass>
- <pointmass name="Engine 1">
- <weight unit="LBS">5200.7</weight>
- <location name="POINTMASS" unit="IN">
- <x>530.86</x>
- <y>-5.755</y>
- <z>-78.56019</z>
- </location>
- </pointmass>
- <pointmass name="Engine 2">
- <weight unit="LBS">5200.7</weight>
- <location name="POINTMASS" unit="IN">
- <x>530.86</x>
- <y>5.755</y>
- <z>-78.56019</z>
- </location>
- </pointmass>
- <pointmass name="PAX 0A (60 seats)">
- <weight unit="LBS">6600</weight>
- <!-- MAX: 13200lbs, 60 seats -->
- <location name="POINTMASS" unit="IN">
- <x>470.1711</x>
- <y>0</y>
- <z>0</z>
- </location>
- </pointmass>
- <pointmass name="PAX 0B (60 seats)">
- <weight unit="LBS">6600</weight>
- <!-- MAX: 13200lbs, 60 seats -->
- <location name="POINTMASS" unit="IN">
- <x>809.5669</x>
- <y>0</y>
- <z>0</z>
- </location>
- </pointmass>
- <pointmass name="PAX 0C (54 seats)">
- <weight unit="LBS">5940</weight>
- <!-- MAX: 11880lbs, 54 seats -->
- <location name="POINTMASS" unit="IN">
- <x>1163.2729</x>
- <y>0</y>
- <z>0</z>
- </location>
- </pointmass>
- <pointmass name="Cargo Hold 1">
- <weight unit="LBS">2000</weight>
- <!-- MAX: 7500.126lbs -->
- <location name="POINTMASS" unit="IN">
- <x>383.4792</x>
- <y>0</y>
- <z>-29.5</z>
- <!-- 1.5m and now half of it for the center point of the load -->
- </location>
- </pointmass>
- <!-- Cargo Hold 2 doesn't exist, that is the center tank -->
- <pointmass name="Cargo Hold 3">
- <weight unit="LBS">2000</weight>
- <!-- MAX: 5384.414lbs -->
- <location name="POINTMASS" unit="IN">
- <x>849.1324</x>
- <y>0</y>
- <z>-29.5</z>
- </location>
- </pointmass>
- <pointmass name="Cargo Hold 4">
- <weight unit="LBS">1500</weight>
- <!-- MAX: 4651.754lbs -->
- <location name="POINTMASS" unit="IN">
- <x>931.0653</x>
- <y>0</y>
- <z>-29.5</z>
- </location>
- </pointmass>
- <pointmass name="Cargo Hold 5">
- <weight unit="LBS">2000</weight>
- <!-- MAX: 3300.320lbs -->
- <location name="POINTMASS" unit="IN">
- <x>1068.2634</x>
- <y>0</y>
- <z>0</z>
- <!-- Cargo Hold #5 sits higher on the range of the cabin deck, it's only loadable with lifter -->
- </location>
- </pointmass>
+ <pointmass name="Cockpit Crew">
+ <weight unit="LBS">400</weight>
+ <!-- MAX: 400lbs, two pilots-->
+ <location name="POINTMASS" unit="IN">
+ <x>200</x>
+ <y>0</y>
+ <z>0</z>
+ </location>
+ </pointmass>
+ <pointmass name="Engine 1">
+ <weight unit="LBS">5200.7</weight>
+ <location name="POINTMASS" unit="IN">
+ <x>530.86</x>
+ <y>-5.755</y>
+ <z>-78.56019</z>
+ </location>
+ </pointmass>
+ <pointmass name="Engine 2">
+ <weight unit="LBS">5200.7</weight>
+ <location name="POINTMASS" unit="IN">
+ <x>530.86</x>
+ <y>5.755</y>
+ <z>-78.56019</z>
+ </location>
+ </pointmass>
+ <pointmass name="PAX 0A (60 seats)">
+ <weight unit="LBS">6600</weight>
+ <!-- MAX: 13200lbs, 60 seats -->
+ <location name="POINTMASS" unit="IN">
+ <x>470.1711</x>
+ <y>0</y>
+ <z>0</z>
+ </location>
+ </pointmass>
+ <pointmass name="PAX 0B (60 seats)">
+ <weight unit="LBS">6600</weight>
+ <!-- MAX: 13200lbs, 60 seats -->
+ <location name="POINTMASS" unit="IN">
+ <x>809.5669</x>
+ <y>0</y>
+ <z>0</z>
+ </location>
+ </pointmass>
+ <pointmass name="PAX 0C (54 seats)">
+ <weight unit="LBS">5940</weight>
+ <!-- MAX: 11880lbs, 54 seats -->
+ <location name="POINTMASS" unit="IN">
+ <x>1163.2729</x>
+ <y>0</y>
+ <z>0</z>
+ </location>
+ </pointmass>
+ <pointmass name="Cargo Hold 1">
+ <weight unit="LBS">2000</weight>
+ <!-- MAX: 7500.126lbs -->
+ <location name="POINTMASS" unit="IN">
+ <x>383.4792</x>
+ <y>0</y>
+ <z>-29.5</z>
+ <!-- 1.5m and now half of it for the center point of the load -->
+ </location>
+ </pointmass>
+ <!-- Cargo Hold 2 doesn't exist, that is the center tank -->
+ <pointmass name="Cargo Hold 3">
+ <weight unit="LBS">2000</weight>
+ <!-- MAX: 5384.414lbs -->
+ <location name="POINTMASS" unit="IN">
+ <x>849.1324</x>
+ <y>0</y>
+ <z>-29.5</z>
+ </location>
+ </pointmass>
+ <pointmass name="Cargo Hold 4">
+ <weight unit="LBS">1500</weight>
+ <!-- MAX: 4651.754lbs -->
+ <location name="POINTMASS" unit="IN">
+ <x>931.0653</x>
+ <y>0</y>
+ <z>-29.5</z>
+ </location>
+ </pointmass>
+ <pointmass name="Cargo Hold 5">
+ <weight unit="LBS">2000</weight>
+ <!-- MAX: 3300.320lbs -->
+ <location name="POINTMASS" unit="IN">
+ <x>1068.2634</x>
+ <y>0</y>
+ <z>0</z>
+ <!-- Cargo Hold #5 sits higher on the range of the cabin deck, it's only loadable with lifter -->
+ </location>
+ </pointmass>
- </mass_balance>
+ </mass_balance>
- <ground_reactions>
- <!-- REF-1 page 165 + 271 -->
- <contact type="BOGEY" name="NOSE_LG">
- <location unit="IN">
- <x> 197.6772 </x>
- <y> 0 </y>
- <z> -137.9617 </z>
- </location>
- <static_friction> 0.8 </static_friction>
- <dynamic_friction> 0.5 </dynamic_friction>
- <rolling_friction> 0.02 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 30935.5 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 16978.5 </damping_coeff>
- <max_steer unit="DEG"> 70 </max_steer>
- <!-- REF-1 page 133 -->
- <brake_group> NOSE </brake_group>
- <retractable>1</retractable>
- </contact>
- <contact type="BOGEY" name="LEFT_MLG">
- <location unit="IN">
- <!--<x> 699.9243 </x>-->
- <x> 695.3149 </x>
- <y> -149.4094 </y>
- <z> -150.4824 </z>
- </location>
- <!-- <static_friction> 0.5 </static_friction> WHAT??? less static than dinamyc friction?-->
- <static_friction> 0.8 </static_friction>
- <dynamic_friction> 0.5 </dynamic_friction>
- <rolling_friction> 0.02 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 59785 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 23957 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> LEFT </brake_group>
- <retractable>1</retractable>
- </contact>
- <contact type="BOGEY" name="RIGHT_MLG">
- <location unit="IN">
- <!-- <x> 697.3425 </x> It should be right left simetric
- <x> 699.9243 </x> -->
- <x> 695.3149 </x>
- <y> 149.4094 </y>
- <z> -150.4824 </z>
- </location>
- <!-- <static_friction> 0.5 </static_friction> WHAT??? less static than dinamyc friction?-->
- <static_friction> 0.8 </static_friction>
- <dynamic_friction> 0.5 </dynamic_friction>
- <rolling_friction> 0.02 </rolling_friction>
- <!--spring_coeff unit="LBS/FT"> 169785 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 33957 </damping_coeff-->
- <spring_coeff unit="LBS/FT"> 59785 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 23957 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> RIGHT </brake_group>
- <retractable>1</retractable>
- </contact>
+ <ground_reactions>
+ <!-- REF-1 page 165 + 271 -->
+ <contact type="BOGEY" name="NOSE_LG">
+ <location unit="IN">
+ <x> 197.6772 </x>
+ <y> 0 </y>
+ <z> -137.9617 </z>
+ </location>
+ <static_friction> 0.8 </static_friction>
+ <dynamic_friction> 0.5 </dynamic_friction>
+ <rolling_friction> 0.02 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 30935.5 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 16978.5 </damping_coeff>
+ <max_steer unit="DEG"> 70 </max_steer>
+ <!-- REF-1 page 133 -->
+ <brake_group> NOSE </brake_group>
+ <retractable>1</retractable>
+ </contact>
+ <contact type="BOGEY" name="LEFT_MLG">
+ <location unit="IN">
+ <!--<x> 699.9243 </x>-->
+ <x> 695.3149 </x>
+ <y> -149.4094 </y>
+ <z> -150.4824 </z>
+ </location>
+ <!-- <static_friction> 0.5 </static_friction> WHAT??? less static than dinamyc friction?-->
+ <static_friction> 0.8 </static_friction>
+ <dynamic_friction> 0.5 </dynamic_friction>
+ <rolling_friction> 0.02 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 59785 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 23957 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> LEFT </brake_group>
+ <retractable>1</retractable>
+ </contact>
+ <contact type="BOGEY" name="RIGHT_MLG">
+ <location unit="IN">
+ <!-- <x> 697.3425 </x> It should be right left simetric
+ <x> 699.9243 </x> -->
+ <x> 695.3149 </x>
+ <y> 149.4094 </y>
+ <z> -150.4824 </z>
+ </location>
+ <!-- <static_friction> 0.5 </static_friction> WHAT??? less static than dinamyc friction?-->
+ <static_friction> 0.8 </static_friction>
+ <dynamic_friction> 0.5 </dynamic_friction>
+ <rolling_friction> 0.02 </rolling_friction>
+ <!--spring_coeff unit="LBS/FT"> 169785 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 33957 </damping_coeff-->
+ <spring_coeff unit="LBS/FT"> 59785 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 23957 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> RIGHT </brake_group>
+ <retractable>1</retractable>
+ </contact>
- <contact type="STRUCTURE" name="NOSE_1">
- <location unit="IN">
- <x> 37.7953 </x>
- <y> 0 </y>
- <z> -38.1374 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="NOSE_2">
- <location unit="IN">
- <x> 128.1102 </x>
- <y> 0 </y>
- <z> -55.0271 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="CENTER_1">
- <location unit="IN">
- <x> 274.0157 </x>
- <y> 0 </y>
- <z> -60.0665 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="CENTER_2">
- <location unit="IN">
- <x> 930 </x>
- <y> 0 </y>
- <z> -60.0665 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
+ <contact type="STRUCTURE" name="NOSE_1">
+ <location unit="IN">
+ <x> 37.7953 </x>
+ <y> 0 </y>
+ <z> -38.1374 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="NOSE_2">
+ <location unit="IN">
+ <x> 128.1102 </x>
+ <y> 0 </y>
+ <z> -55.0271 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="CENTER_1">
+ <location unit="IN">
+ <x> 274.0157 </x>
+ <y> 0 </y>
+ <z> -60.0665 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="CENTER_2">
+ <location unit="IN">
+ <x> 930 </x>
+ <y> 0 </y>
+ <z> -60.0665 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
- <contact type="STRUCTURE" name="ENG_1">
- <location unit="IN">
- <x>589.735</x>
- <y>-226.575</y>
- <z>-95.567</z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="ENG_2">
- <location unit="IN">
- <x>589.735</x>
- <y>226.575</y>
- <z>-95.567</z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.5 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
+ <contact type="STRUCTURE" name="ENG_1">
+ <location unit="IN">
+ <x>589.735</x>
+ <y>-226.575</y>
+ <z>-95.567</z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="ENG_2">
+ <location unit="IN">
+ <x>589.735</x>
+ <y>226.575</y>
+ <z>-95.567</z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.5 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
- <contact type="STRUCTURE" name="TAIL_1">
- <location unit="IN">
- <x> 1097.9921 </x>
- <y> 0 </y>
- <z> -44.7722 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="TAIL_2">
- <location unit="IN">
- <x> 1225 </x>
- <y> 0 </y>
- <z> -18.8067 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="TAIL_3">
- <location unit="IN">
- <x> 1341.6142 </x>
- <y> 0 </y>
- <z> -10.2599 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="TAIL_4">
- <location unit="IN">
- <x> 1469.0945 </x>
- <y> 0 </y>
- <z> 47.4138 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 1 </dynamic_friction>
- <rolling_friction> 1 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="WING_TIP_1">
- <location unit="IN">
- <x> 838.8898 </x>
- <y> -667.5197 </y>
- <z> 35.7926 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="WING_TIP_2">
- <location unit="IN">
- <x> 838.8898 </x>
- <y> 667.5197 </y>
- <z> 35.7926 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 1 </dynamic_friction>
- <rolling_friction> 1 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- </ground_reactions>
+ <contact type="STRUCTURE" name="TAIL_1">
+ <location unit="IN">
+ <x> 1097.9921 </x>
+ <y> 0 </y>
+ <z> -44.7722 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="TAIL_2">
+ <location unit="IN">
+ <x> 1225 </x>
+ <y> 0 </y>
+ <z> -18.8067 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="TAIL_3">
+ <location unit="IN">
+ <x> 1341.6142 </x>
+ <y> 0 </y>
+ <z> -10.2599 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="TAIL_4">
+ <location unit="IN">
+ <x> 1469.0945 </x>
+ <y> 0 </y>
+ <z> 47.4138 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 1 </dynamic_friction>
+ <rolling_friction> 1 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="WING_TIP_1">
+ <location unit="IN">
+ <x> 838.8898 </x>
+ <y> -667.5197 </y>
+ <z> 35.7926 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="WING_TIP_2">
+ <location unit="IN">
+ <x> 838.8898 </x>
+ <y> 667.5197 </y>
+ <z> 35.7926 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 1 </dynamic_friction>
+ <rolling_friction> 1 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ </ground_reactions>
-<propulsion>
+ <propulsion>
- <engine file="cfm56_5b6">
- <location unit="IN">
- <x> 620.0683 </x>
- <y> -226.575 </y>
- <z> -45.567 </z>
- </location>
- <orient unit="DEG">
- <roll> 0.0 </roll>
- <pitch> 2.2 </pitch>
- <yaw> 1 </yaw>
- </orient>
- <feed>7</feed>
- <thruster file="direct">
+ <engine file="cfm56_5b6">
<location unit="IN">
- <x> 655.4820 </x>
- <y> -226.575 </y>
- <z> 0.000 </z>
+ <x> 620.0683 </x>
+ <y> -226.575 </y>
+ <z> -45.567 </z>
</location>
<orient unit="DEG">
- <roll> 0.0 </roll>
- <pitch> 2.2 </pitch>
- <yaw> 1 </yaw>
+ <roll> 0.0 </roll>
+ <pitch> 2.2 </pitch>
+ <yaw> 1 </yaw>
</orient>
- </thruster>
- </engine>
+ <feed>7</feed>
+ <thruster file="direct">
+ <location unit="IN">
+ <x> 655.4820 </x>
+ <y> -226.575 </y>
+ <z> 0.000 </z>
+ </location>
+ <orient unit="DEG">
+ <roll> 0.0 </roll>
+ <pitch> 2.2 </pitch>
+ <yaw> 1 </yaw>
+ </orient>
+ </thruster>
+ </engine>
- <engine file="cfm56_5b6">
- <location unit="IN">
- <x> 620.0683 </x>
- <y> 226.575 </y>
- <z> -45.567 </z>
- </location>
- <orient unit="DEG">
- <roll> 0.0 </roll>
- <pitch> 2.2 </pitch>
- <yaw> -1 </yaw>
- </orient>
- <feed>8</feed>
- <thruster file="direct">
+ <engine file="cfm56_5b6">
<location unit="IN">
- <x> 655.4820 </x>
- <y> 226.575 </y>
- <z> 0.000 </z>
+ <x> 620.0683 </x>
+ <y> 226.575 </y>
+ <z> -45.567 </z>
</location>
<orient unit="DEG">
- <roll> 0.0 </roll>
- <pitch> 2.2 </pitch>
- <yaw> -1 </yaw>
+ <roll> 0.0 </roll>
+ <pitch> 2.2 </pitch>
+ <yaw> -1 </yaw>
</orient>
- </thruster>
- </engine>
+ <feed>8</feed>
+ <thruster file="direct">
+ <location unit="IN">
+ <x> 655.4820 </x>
+ <y> 226.575 </y>
+ <z> 0.000 </z>
+ </location>
+ <orient unit="DEG">
+ <roll> 0.0 </roll>
+ <pitch> 2.2 </pitch>
+ <yaw> -1 </yaw>
+ </orient>
+ </thruster>
+ </engine>
- <tank type="FUEL"> <!-- Left Tank (Wing tip Ventilation Surge) 0 -->
- <location unit="IN">
- <x> 783.0709 </x>
- <y> -574.4148 </y>
- <z> 3.1080 </z>
- </location>
- <capacity unit="LBS"> 412 </capacity><!-- need review --> <!-- would be 1 percent of max load per each wing, 412 each. Needs temp rise of 20C at max load to fill -->
- <contents unit="LBS"> 0 </contents>
-
- <priority>4</priority>
- <type>JET-A1</type>
- <temperature>50</temperature>
- </tank>
- <tank type="FUEL"> <!-- Left Tank (Outer) 1 -->
- <location unit="IN">
- <x> 739.5669 </x>
- <y> -457.4259 </y>
- <z> -8.0898 </z>
- </location>
- <capacity unit="LBS"> 1520.00 </capacity><!-- need review -->
- <contents unit="LBS"> 1520 </contents><!-- outer filled first than inner -->
- <standpipe unit="LBS">21</standpipe><!-- minimun fuel on pipes -->
- <priority>2</priority>
- <type>JET-A1</type>
- <temperature>50</temperature>
- </tank>
- <tank type="FUEL"> <!-- Left Tank (Inner) 2 -->
- <location unit="IN">
- <x> 652.5591 </x>
- <y> -236.2992 </y>
- <z> -33.9470 </z>
- </location>
- <capacity unit="LBS"> 11982 </capacity><!-- correct by FCOM -->
- <contents unit="LBS"> 4480 </contents>
- <standpipe unit="LBS">31</standpipe><!-- minimun fuel on pipes -->
- <priority>3</priority>
- <type>JET-A1</type>
- <temperature>50</temperature>
- </tank>
- <tank type="FUEL"> <!-- Center Tank 3 -->
- <location unit="IN">
- <x> 522.0473 </x>
- <y> 0 </y>
- <z> -47.0 </z>
- </location>
- <capacity unit="LBS"> 14281 </capacity><!-- correct by FCOM -->
- <contents unit="LBS"> 0 </contents> <!-- wing tanks always filled first -->
- <standpipe unit="LBS">43</standpipe><!-- minimun fuel on pipes -->
- <priority>1</priority>
- <type>JET-A1</type>
- <temperature>50</temperature>
- </tank>
- <tank type="FUEL"> <!-- Right Tank (Inner) 4 -->
- <location unit="IN">
- <x> 652.5591 </x>
- <y> 236.2992 </y>
- <z> -33.9470 </z>
- </location>
- <capacity unit="LBS"> 11982 </capacity><!-- correct by FCOM -->
- <contents unit="LBS"> 4480 </contents>
- <standpipe unit="LBS">31</standpipe><!-- minimum fuel on pipes -->
- <priority>3</priority>
- <type>JET-A1</type>
- <temperature>50</temperature>
- </tank>
- <tank type="FUEL"> <!-- Right Tank (Outer) 5 -->
- <location unit="IN">
- <x> 739.5669 </x>
- <y> 457.4259 </y>
- <z> -8.0898 </z>
- </location>
- <capacity unit="LBS"> 1520 </capacity><!-- correct by FCOM -->
- <contents unit="LBS"> 1520 </contents><!-- outer filled before inner -->
- <standpipe unit="LBS">21</standpipe><!-- minimun fuel on pipes -->
- <priority>2</priority>
- <type>JET-A1</type>
- <temperature>50</temperature>
- </tank>
- <tank type="FUEL"> <!-- Right Tank (Wing tip Ventilation Surge) 6 -->
- <location unit="IN">
- <x> 783.0709 </x>
- <y> 574.4148 </y>
- <z> 3.1080 </z>
- </location>
- <capacity unit="LBS"> 412 </capacity><!-- need review --> <!-- 1 percent of max, see left surge tank, is 412 lb each -->
- <contents unit="LBS"> 0 </contents>
- <priority>4</priority>
- <type>JET-A1</type>
- <temperature>50</temperature>
- </tank>
- <tank type="FUEL"> <!-- LEFT FUEL PIPES (Engine 1 feed from this) -->
- <location unit="IN">
- <x>589.735</x>
- <y>-226.575</y>
- <z>-45.567</z>
- </location>
- <capacity unit="LBS"> 100 </capacity><!-- need review -->
- <contents unit="LBS"> 0 </contents>
- <priority>1</priority>
- <type>JET-A1</type>
- </tank>
- <tank type="FUEL"> <!-- RIGHT FUEL PIPES (Engine 2 feed from this) -->
- <location unit="IN">
- <x>589.735</x>
- <y>226.575</y>
- <z>-45.567</z>
- </location>
- <capacity unit="LBS"> 100 </capacity><!-- need review -->
- <contents unit="LBS"> 0 </contents>
- <priority>1</priority>
- <type>JET-A1</type>
- </tank>
-</propulsion>
+ <tank type="FUEL"> <!-- Left Tank (Wing tip Ventilation Surge) 0 -->
+ <location unit="IN">
+ <x> 783.0709 </x>
+ <y> -574.4148 </y>
+ <z> 3.1080 </z>
+ </location>
+ <capacity unit="LBS"> 412 </capacity><!-- need review --> <!-- would be 1 percent of max load per each wing, 412 each. Needs temp rise of 20C at max load to fill -->
+ <contents unit="LBS"> 0 </contents>
+
+ <priority>4</priority>
+ <type>JET-A1</type>
+ <temperature>50</temperature>
+ </tank>
+ <tank type="FUEL"> <!-- Left Tank (Outer) 1 -->
+ <location unit="IN">
+ <x> 739.5669 </x>
+ <y> -457.4259 </y>
+ <z> -8.0898 </z>
+ </location>
+ <capacity unit="LBS"> 1520.00 </capacity><!-- need review -->
+ <contents unit="LBS"> 1520 </contents><!-- outer filled first than inner -->
+ <standpipe unit="LBS">21</standpipe><!-- minimun fuel on pipes -->
+ <priority>2</priority>
+ <type>JET-A1</type>
+ <temperature>50</temperature>
+ </tank>
+ <tank type="FUEL"> <!-- Left Tank (Inner) 2 -->
+ <location unit="IN">
+ <x> 652.5591 </x>
+ <y> -236.2992 </y>
+ <z> -33.9470 </z>
+ </location>
+ <capacity unit="LBS"> 11982 </capacity><!-- correct by FCOM -->
+ <contents unit="LBS"> 4480 </contents>
+ <standpipe unit="LBS">31</standpipe><!-- minimun fuel on pipes -->
+ <priority>3</priority>
+ <type>JET-A1</type>
+ <temperature>50</temperature>
+ </tank>
+ <tank type="FUEL"> <!-- Center Tank 3 -->
+ <location unit="IN">
+ <x> 522.0473 </x>
+ <y> 0 </y>
+ <z> -47.0 </z>
+ </location>
+ <capacity unit="LBS"> 14281 </capacity><!-- correct by FCOM -->
+ <contents unit="LBS"> 0 </contents> <!-- wing tanks always filled first -->
+ <standpipe unit="LBS">43</standpipe><!-- minimun fuel on pipes -->
+ <priority>1</priority>
+ <type>JET-A1</type>
+ <temperature>50</temperature>
+ </tank>
+ <tank type="FUEL"> <!-- Right Tank (Inner) 4 -->
+ <location unit="IN">
+ <x> 652.5591 </x>
+ <y> 236.2992 </y>
+ <z> -33.9470 </z>
+ </location>
+ <capacity unit="LBS"> 11982 </capacity><!-- correct by FCOM -->
+ <contents unit="LBS"> 4480 </contents>
+ <standpipe unit="LBS">31</standpipe><!-- minimum fuel on pipes -->
+ <priority>3</priority>
+ <type>JET-A1</type>
+ <temperature>50</temperature>
+ </tank>
+ <tank type="FUEL"> <!-- Right Tank (Outer) 5 -->
+ <location unit="IN">
+ <x> 739.5669 </x>
+ <y> 457.4259 </y>
+ <z> -8.0898 </z>
+ </location>
+ <capacity unit="LBS"> 1520 </capacity><!-- correct by FCOM -->
+ <contents unit="LBS"> 1520 </contents><!-- outer filled before inner -->
+ <standpipe unit="LBS">21</standpipe><!-- minimun fuel on pipes -->
+ <priority>2</priority>
+ <type>JET-A1</type>
+ <temperature>50</temperature>
+ </tank>
+ <tank type="FUEL"> <!-- Right Tank (Wing tip Ventilation Surge) 6 -->
+ <location unit="IN">
+ <x> 783.0709 </x>
+ <y> 574.4148 </y>
+ <z> 3.1080 </z>
+ </location>
+ <capacity unit="LBS"> 412 </capacity><!-- need review --> <!-- 1 percent of max, see left surge tank, is 412 lb each -->
+ <contents unit="LBS"> 0 </contents>
+ <priority>4</priority>
+ <type>JET-A1</type>
+ <temperature>50</temperature>
+ </tank>
+ <tank type="FUEL"> <!-- LEFT FUEL PIPES (Engine 1 feed from this) -->
+ <location unit="IN">
+ <x>589.735</x>
+ <y>0</y>
+ <z>-45.567</z>
+ </location>
+ <capacity unit="LBS"> 100 </capacity><!-- need review -->
+ <contents unit="LBS"> 0 </contents>
+ <priority>1</priority>
+ <type>JET-A1</type>
+ </tank>
+ <tank type="FUEL"> <!-- RIGHT FUEL PIPES (Engine 2 feed from this) -->
+ <location unit="IN">
+ <x>589.735</x>
+ <y>0</y>
+ <z>-45.567</z>
+ </location>
+ <capacity unit="LBS"> 100 </capacity><!-- need review -->
+ <contents unit="LBS"> 0 </contents>
+ <priority>1</priority>
+ <type>JET-A1</type>
+ </tank>
+ </propulsion>
-<system file="pushback" />
-<system file="fuel" />
-<system file="glass-effect1" />
-<system file="fmgc" />
-<system file="fcs" />
+ <system file="pushback" />
+ <system file="fuel" />
+ <system file="glass-effect1" />
+ <system file="fmgc" />
+ <system file="fcs" />
-<flight_control name="none"/>
+ <flight_control name="none"/>
-<aerodynamics file="Systems/a319-aerodynamics.xml" />
+ <aerodynamics file="Systems/a319-aerodynamics.xml" />
-<external_reactions>
- <force name="pushback" frame="BODY">
- <location unit="IN">
- <x>294</x>
- <y>0</y>
- <z>-149</z>
- </location>
- <direction>
- <x>1</x>
- <y>0</y>
- <z>0</z>
- </direction>
- </force>
-</external_reactions>
+ <external_reactions>
+ <force name="pushback" frame="BODY">
+ <location unit="IN">
+ <x>294</x>
+ <y>0</y>
+ <z>-149</z>
+ </location>
+ <direction>
+ <x>1</x>
+ <y>0</y>
+ <z>0</z>
+ </direction>
+ </force>
+ </external_reactions>
</fdm_config>
diff --git a/A319-100-IAE.xml b/A319-100-IAE.xml
index b59a8cf8..4990949b 100644
--- a/A319-100-IAE.xml
+++ b/A319-100-IAE.xml
@@ -4,585 +4,585 @@
xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance"
xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
-<fileheader>
- <author>Joshua Davidson (it0uchpods)</author>
- <version>Pre V1.0</version>
- <description>A3XX FDE</description>
-</fileheader>
+ <fileheader>
+ <author>Joshua Davidson (it0uchpods)</author>
+ <version>Pre V1.0</version>
+ <description>A3XX FDE</description>
+ </fileheader>
-<metrics>
- <wingarea unit="FT2"> 1319.79 </wingarea>
- <wingspan unit="FT" > 111.26 </wingspan>
- <wing_incidence> 1.03 </wing_incidence>
- <chord unit="FT" > 13.76 </chord>
- <htailarea unit="FT2"> 334.24 </htailarea>
- <htailarm unit="FT" > 57.88 </htailarm>
- <vtailarea unit="FT2"> 248.79 </vtailarea>
- <vtailarm unit="FT" > 57.33 </vtailarm>
+ <metrics>
+ <wingarea unit="FT2"> 1319.79 </wingarea>
+ <wingspan unit="FT" > 111.26 </wingspan>
+ <wing_incidence> 1.03 </wing_incidence>
+ <chord unit="FT" > 13.76 </chord>
+ <htailarea unit="FT2"> 334.24 </htailarea>
+ <htailarm unit="FT" > 57.88 </htailarm>
+ <vtailarea unit="FT2"> 248.79 </vtailarea>
+ <vtailarm unit="FT" > 57.33 </vtailarm>
- <location name="AERORP" unit="IN">
- <x> 700.00 </x>
- <y> 0 </y>
- <z> 0.00 </z>
- </location>
+ <location name="AERORP" unit="IN">
+ <x> 700.00 </x>
+ <y> 0 </y>
+ <z> 0.00 </z>
+ </location>
- <location name="EYEPOINT" unit="IN">
- <x> 80 </x>
- <y> -30 </y>
- <z> 70 </z>
- </location>
+ <location name="EYEPOINT" unit="IN">
+ <x> 80 </x>
+ <y> -30 </y>
+ <z> 70 </z>
+ </location>
- <location name="VRP" unit="IN">
- <x> 661.1 </x>
- <y> 0 </y>
- <z> -37 </z>
- </location>
+ <location name="VRP" unit="IN">
+ <x> 661.1 </x>
+ <y> 0 </y>
+ <z> -37 </z>
+ </location>
- </metrics>
+ </metrics>
- <mass_balance>
- <ixx unit="SLUG*FT2"> 611903</ixx>
- <iyy unit="SLUG*FT2">1735389</iyy>
- <izz unit="SLUG*FT2">2301293</izz>
+ <mass_balance>
+ <ixx unit="SLUG*FT2"> 611903</ixx>
+ <iyy unit="SLUG*FT2">1735389</iyy>
+ <izz unit="SLUG*FT2">2301293</izz>
- <ixy unit="SLUG*FT2">0</ixy>
- <ixz unit="SLUG*FT2">0</ixz>
- <iyz unit="SLUG*FT2">0</iyz>
- <emptywt unit="LBS">80431</emptywt>
+ <ixy unit="SLUG*FT2">0</ixy>
+ <ixz unit="SLUG*FT2">0</ixz>
+ <iyz unit="SLUG*FT2">0</iyz>
+ <emptywt unit="LBS">80431</emptywt>
- <location name="CG" unit="IN">
- <x> 652.00 </x>
- <y> 0 </y>
- <z> 0.00 </z>
- </location>
+ <location name="CG" unit="IN">
+ <x> 652.00 </x>
+ <y> 0 </y>
+ <z> 0.00 </z>
+ </location>
- <pointmass name="Cockpit Crew">
- <weight unit="LBS">400</weight>
- <!-- MAX: 400lbs, two pilots-->
- <location name="POINTMASS" unit="IN">
- <x>200</x>
- <y>0</y>
- <z>0</z>
- </location>
- </pointmass>
- <pointmass name="Engine 1">
- <weight unit="LBS">5200.7</weight>
- <location name="POINTMASS" unit="IN">
- <x>530.86</x>
- <y>-5.755</y>
- <z>-78.56019</z>
- </location>
- </pointmass>
- <pointmass name="Engine 2">
- <weight unit="LBS">5200.7</weight>
- <location name="POINTMASS" unit="IN">
- <x>530.86</x>
- <y>5.755</y>
- <z>-78.56019</z>
- </location>
- </pointmass>
- <pointmass name="PAX 0A (60 seats)">
- <weight unit="LBS">6600</weight>
- <!-- MAX: 13200lbs, 60 seats -->
- <location name="POINTMASS" unit="IN">
- <x>470.1711</x>
- <y>0</y>
- <z>0</z>
- </location>
- </pointmass>
- <pointmass name="PAX 0B (60 seats)">
- <weight unit="LBS">6600</weight>
- <!-- MAX: 13200lbs, 60 seats -->
- <location name="POINTMASS" unit="IN">
- <x>809.5669</x>
- <y>0</y>
- <z>0</z>
- </location>
- </pointmass>
- <pointmass name="PAX 0C (54 seats)">
- <weight unit="LBS">5940</weight>
- <!-- MAX: 11880lbs, 54 seats -->
- <location name="POINTMASS" unit="IN">
- <x>1163.2729</x>
- <y>0</y>
- <z>0</z>
- </location>
- </pointmass>
- <pointmass name="Cargo Hold 1">
- <weight unit="LBS">2000</weight>
- <!-- MAX: 7500.126lbs -->
- <location name="POINTMASS" unit="IN">
- <x>383.4792</x>
- <y>0</y>
- <z>-29.5</z>
- <!-- 1.5m and now half of it for the center point of the load -->
- </location>
- </pointmass>
- <!-- Cargo Hold 2 doesn't exist, that is the center tank -->
- <pointmass name="Cargo Hold 3">
- <weight unit="LBS">2000</weight>
- <!-- MAX: 5384.414lbs -->
- <location name="POINTMASS" unit="IN">
- <x>849.1324</x>
- <y>0</y>
- <z>-29.5</z>
- </location>
- </pointmass>
- <pointmass name="Cargo Hold 4">
- <weight unit="LBS">1500</weight>
- <!-- MAX: 4651.754lbs -->
- <location name="POINTMASS" unit="IN">
- <x>931.0653</x>
- <y>0</y>
- <z>-29.5</z>
- </location>
- </pointmass>
- <pointmass name="Cargo Hold 5">
- <weight unit="LBS">2000</weight>
- <!-- MAX: 3300.320lbs -->
- <location name="POINTMASS" unit="IN">
- <x>1068.2634</x>
- <y>0</y>
- <z>0</z>
- <!-- Cargo Hold #5 sits higher on the range of the cabin deck, it's only loadable with lifter -->
- </location>
- </pointmass>
+ <pointmass name="Cockpit Crew">
+ <weight unit="LBS">400</weight>
+ <!-- MAX: 400lbs, two pilots-->
+ <location name="POINTMASS" unit="IN">
+ <x>200</x>
+ <y>0</y>
+ <z>0</z>
+ </location>
+ </pointmass>
+ <pointmass name="Engine 1">
+ <weight unit="LBS">5200.7</weight>
+ <location name="POINTMASS" unit="IN">
+ <x>530.86</x>
+ <y>-5.755</y>
+ <z>-78.56019</z>
+ </location>
+ </pointmass>
+ <pointmass name="Engine 2">
+ <weight unit="LBS">5200.7</weight>
+ <location name="POINTMASS" unit="IN">
+ <x>530.86</x>
+ <y>5.755</y>
+ <z>-78.56019</z>
+ </location>
+ </pointmass>
+ <pointmass name="PAX 0A (60 seats)">
+ <weight unit="LBS">6600</weight>
+ <!-- MAX: 13200lbs, 60 seats -->
+ <location name="POINTMASS" unit="IN">
+ <x>470.1711</x>
+ <y>0</y>
+ <z>0</z>
+ </location>
+ </pointmass>
+ <pointmass name="PAX 0B (60 seats)">
+ <weight unit="LBS">6600</weight>
+ <!-- MAX: 13200lbs, 60 seats -->
+ <location name="POINTMASS" unit="IN">
+ <x>809.5669</x>
+ <y>0</y>
+ <z>0</z>
+ </location>
+ </pointmass>
+ <pointmass name="PAX 0C (54 seats)">
+ <weight unit="LBS">5940</weight>
+ <!-- MAX: 11880lbs, 54 seats -->
+ <location name="POINTMASS" unit="IN">
+ <x>1163.2729</x>
+ <y>0</y>
+ <z>0</z>
+ </location>
+ </pointmass>
+ <pointmass name="Cargo Hold 1">
+ <weight unit="LBS">2000</weight>
+ <!-- MAX: 7500.126lbs -->
+ <location name="POINTMASS" unit="IN">
+ <x>383.4792</x>
+ <y>0</y>
+ <z>-29.5</z>
+ <!-- 1.5m and now half of it for the center point of the load -->
+ </location>
+ </pointmass>
+ <!-- Cargo Hold 2 doesn't exist, that is the center tank -->
+ <pointmass name="Cargo Hold 3">
+ <weight unit="LBS">2000</weight>
+ <!-- MAX: 5384.414lbs -->
+ <location name="POINTMASS" unit="IN">
+ <x>849.1324</x>
+ <y>0</y>
+ <z>-29.5</z>
+ </location>
+ </pointmass>
+ <pointmass name="Cargo Hold 4">
+ <weight unit="LBS">1500</weight>
+ <!-- MAX: 4651.754lbs -->
+ <location name="POINTMASS" unit="IN">
+ <x>931.0653</x>
+ <y>0</y>
+ <z>-29.5</z>
+ </location>
+ </pointmass>
+ <pointmass name="Cargo Hold 5">
+ <weight unit="LBS">2000</weight>
+ <!-- MAX: 3300.320lbs -->
+ <location name="POINTMASS" unit="IN">
+ <x>1068.2634</x>
+ <y>0</y>
+ <z>0</z>
+ <!-- Cargo Hold #5 sits higher on the range of the cabin deck, it's only loadable with lifter -->
+ </location>
+ </pointmass>
- </mass_balance>
+ </mass_balance>
- <ground_reactions>
- <!-- REF-1 page 165 + 271 -->
- <contact type="BOGEY" name="NOSE_LG">
- <location unit="IN">
- <x> 197.6772 </x>
- <y> 0 </y>
- <z> -137.9617 </z>
- </location>
- <static_friction> 0.8 </static_friction>
- <dynamic_friction> 0.5 </dynamic_friction>
- <rolling_friction> 0.02 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 30935.5 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 16978.5 </damping_coeff>
- <max_steer unit="DEG"> 70 </max_steer>
- <!-- REF-1 page 133 -->
- <brake_group> NOSE </brake_group>
- <retractable>1</retractable>
- </contact>
- <contact type="BOGEY" name="LEFT_MLG">
- <location unit="IN">
- <!--<x> 699.9243 </x>-->
- <x> 695.3149 </x>
- <y> -149.4094 </y>
- <z> -150.4824 </z>
- </location>
- <!-- <static_friction> 0.5 </static_friction> WHAT??? less static than dinamyc friction?-->
- <static_friction> 0.8 </static_friction>
- <dynamic_friction> 0.5 </dynamic_friction>
- <rolling_friction> 0.02 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 59785 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 23957 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> LEFT </brake_group>
- <retractable>1</retractable>
- </contact>
- <contact type="BOGEY" name="RIGHT_MLG">
- <location unit="IN">
- <!-- <x> 697.3425 </x> It should be right left simetric
- <x> 699.9243 </x> -->
- <x> 695.3149 </x>
- <y> 149.4094 </y>
- <z> -150.4824 </z>
- </location>
- <!-- <static_friction> 0.5 </static_friction> WHAT??? less static than dinamyc friction?-->
- <static_friction> 0.8 </static_friction>
- <dynamic_friction> 0.5 </dynamic_friction>
- <rolling_friction> 0.02 </rolling_friction>
- <!--spring_coeff unit="LBS/FT"> 169785 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 33957 </damping_coeff-->
- <spring_coeff unit="LBS/FT"> 59785 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 23957 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> RIGHT </brake_group>
- <retractable>1</retractable>
- </contact>
+ <ground_reactions>
+ <!-- REF-1 page 165 + 271 -->
+ <contact type="BOGEY" name="NOSE_LG">
+ <location unit="IN">
+ <x> 197.6772 </x>
+ <y> 0 </y>
+ <z> -137.9617 </z>
+ </location>
+ <static_friction> 0.8 </static_friction>
+ <dynamic_friction> 0.5 </dynamic_friction>
+ <rolling_friction> 0.02 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 30935.5 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 16978.5 </damping_coeff>
+ <max_steer unit="DEG"> 70 </max_steer>
+ <!-- REF-1 page 133 -->
+ <brake_group> NOSE </brake_group>
+ <retractable>1</retractable>
+ </contact>
+ <contact type="BOGEY" name="LEFT_MLG">
+ <location unit="IN">
+ <!--<x> 699.9243 </x>-->
+ <x> 695.3149 </x>
+ <y> -149.4094 </y>
+ <z> -150.4824 </z>
+ </location>
+ <!-- <static_friction> 0.5 </static_friction> WHAT??? less static than dinamyc friction?-->
+ <static_friction> 0.8 </static_friction>
+ <dynamic_friction> 0.5 </dynamic_friction>
+ <rolling_friction> 0.02 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 59785 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 23957 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> LEFT </brake_group>
+ <retractable>1</retractable>
+ </contact>
+ <contact type="BOGEY" name="RIGHT_MLG">
+ <location unit="IN">
+ <!-- <x> 697.3425 </x> It should be right left simetric
+ <x> 699.9243 </x> -->
+ <x> 695.3149 </x>
+ <y> 149.4094 </y>
+ <z> -150.4824 </z>
+ </location>
+ <!-- <static_friction> 0.5 </static_friction> WHAT??? less static than dinamyc friction?-->
+ <static_friction> 0.8 </static_friction>
+ <dynamic_friction> 0.5 </dynamic_friction>
+ <rolling_friction> 0.02 </rolling_friction>
+ <!--spring_coeff unit="LBS/FT"> 169785 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 33957 </damping_coeff-->
+ <spring_coeff unit="LBS/FT"> 59785 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 23957 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> RIGHT </brake_group>
+ <retractable>1</retractable>
+ </contact>
- <contact type="STRUCTURE" name="NOSE_1">
- <location unit="IN">
- <x> 37.7953 </x>
- <y> 0 </y>
- <z> -38.1374 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="NOSE_2">
- <location unit="IN">
- <x> 128.1102 </x>
- <y> 0 </y>
- <z> -55.0271 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="CENTER_1">
- <location unit="IN">
- <x> 274.0157 </x>
- <y> 0 </y>
- <z> -60.0665 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="CENTER_2">
- <location unit="IN">
- <x> 930 </x>
- <y> 0 </y>
- <z> -60.0665 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
+ <contact type="STRUCTURE" name="NOSE_1">
+ <location unit="IN">
+ <x> 37.7953 </x>
+ <y> 0 </y>
+ <z> -38.1374 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="NOSE_2">
+ <location unit="IN">
+ <x> 128.1102 </x>
+ <y> 0 </y>
+ <z> -55.0271 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="CENTER_1">
+ <location unit="IN">
+ <x> 274.0157 </x>
+ <y> 0 </y>
+ <z> -60.0665 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="CENTER_2">
+ <location unit="IN">
+ <x> 930 </x>
+ <y> 0 </y>
+ <z> -60.0665 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
- <contact type="STRUCTURE" name="ENG_1">
- <location unit="IN">
- <x>589.735</x>
- <y>-226.575</y>
- <z>-95.567</z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="ENG_2">
- <location unit="IN">
- <x>589.735</x>
- <y>226.575</y>
- <z>-95.567</z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.5 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
+ <contact type="STRUCTURE" name="ENG_1">
+ <location unit="IN">
+ <x>589.735</x>
+ <y>-226.575</y>
+ <z>-95.567</z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="ENG_2">
+ <location unit="IN">
+ <x>589.735</x>
+ <y>226.575</y>
+ <z>-95.567</z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.5 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
- <contact type="STRUCTURE" name="TAIL_1">
- <location unit="IN">
- <x> 1097.9921 </x>
- <y> 0 </y>
- <z> -44.7722 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="TAIL_2">
- <location unit="IN">
- <x> 1225 </x>
- <y> 0 </y>
- <z> -18.8067 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="TAIL_3">
- <location unit="IN">
- <x> 1341.6142 </x>
- <y> 0 </y>
- <z> -10.2599 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="TAIL_4">
- <location unit="IN">
- <x> 1469.0945 </x>
- <y> 0 </y>
- <z> 47.4138 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 1 </dynamic_friction>
- <rolling_friction> 1 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="WING_TIP_1">
- <location unit="IN">
- <x> 838.8898 </x>
- <y> -667.5197 </y>
- <z> 35.7926 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="WING_TIP_2">
- <location unit="IN">
- <x> 838.8898 </x>
- <y> 667.5197 </y>
- <z> 35.7926 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 1 </dynamic_friction>
- <rolling_friction> 1 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- </ground_reactions>
+ <contact type="STRUCTURE" name="TAIL_1">
+ <location unit="IN">
+ <x> 1097.9921 </x>
+ <y> 0 </y>
+ <z> -44.7722 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="TAIL_2">
+ <location unit="IN">
+ <x> 1225 </x>
+ <y> 0 </y>
+ <z> -18.8067 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="TAIL_3">
+ <location unit="IN">
+ <x> 1341.6142 </x>
+ <y> 0 </y>
+ <z> -10.2599 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="TAIL_4">
+ <location unit="IN">
+ <x> 1469.0945 </x>
+ <y> 0 </y>
+ <z> 47.4138 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 1 </dynamic_friction>
+ <rolling_friction> 1 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="WING_TIP_1">
+ <location unit="IN">
+ <x> 838.8898 </x>
+ <y> -667.5197 </y>
+ <z> 35.7926 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="WING_TIP_2">
+ <location unit="IN">
+ <x> 838.8898 </x>
+ <y> 667.5197 </y>
+ <z> 35.7926 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 1 </dynamic_friction>
+ <rolling_friction> 1 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ </ground_reactions>
-<propulsion>
+ <propulsion>
- <engine file="v2527_a5">
- <location unit="IN">
- <x> 620.0683 </x>
- <y> -226.575 </y>
- <z> -45.567 </z>
- </location>
- <orient unit="DEG">
- <roll> 0.0 </roll>
- <pitch> 2.2 </pitch>
- <yaw> 1 </yaw>
- </orient>
- <feed>7</feed>
- <thruster file="direct">
+ <engine file="v2527_a5">
<location unit="IN">
- <x> 655.4820 </x>
- <y> -226.575 </y>
- <z> 0.000 </z>
+ <x> 620.0683 </x>
+ <y> -226.575 </y>
+ <z> -45.567 </z>
</location>
<orient unit="DEG">
- <roll> 0.0 </roll>
- <pitch> 2.2 </pitch>
- <yaw> 1 </yaw>
+ <roll> 0.0 </roll>
+ <pitch> 2.2 </pitch>
+ <yaw> 1 </yaw>
</orient>
- </thruster>
- </engine>
+ <feed>7</feed>
+ <thruster file="direct">
+ <location unit="IN">
+ <x> 655.4820 </x>
+ <y> -226.575 </y>
+ <z> 0.000 </z>
+ </location>
+ <orient unit="DEG">
+ <roll> 0.0 </roll>
+ <pitch> 2.2 </pitch>
+ <yaw> 1 </yaw>
+ </orient>
+ </thruster>
+ </engine>
- <engine file="v2527_a5">
- <location unit="IN">
- <x> 620.0683 </x>
- <y> 226.575 </y>
- <z> -45.567 </z>
- </location>
- <orient unit="DEG">
- <roll> 0.0 </roll>
- <pitch> 2.2 </pitch>
- <yaw> -1 </yaw>
- </orient>
- <feed>8</feed>
- <thruster file="direct">
+ <engine file="v2527_a5">
<location unit="IN">
- <x> 655.4820 </x>
- <y> 226.575 </y>
- <z> 0.000 </z>
+ <x> 620.0683 </x>
+ <y> 226.575 </y>
+ <z> -45.567 </z>
</location>
<orient unit="DEG">
- <roll> 0.0 </roll>
- <pitch> 2.2 </pitch>
- <yaw> -1 </yaw>
+ <roll> 0.0 </roll>
+ <pitch> 2.2 </pitch>
+ <yaw> -1 </yaw>
</orient>
- </thruster>
- </engine>
+ <feed>8</feed>
+ <thruster file="direct">
+ <location unit="IN">
+ <x> 655.4820 </x>
+ <y> 226.575 </y>
+ <z> 0.000 </z>
+ </location>
+ <orient unit="DEG">
+ <roll> 0.0 </roll>
+ <pitch> 2.2 </pitch>
+ <yaw> -1 </yaw>
+ </orient>
+ </thruster>
+ </engine>
- <tank type="FUEL"> <!-- Left Tank (Wing tip Ventilation Surge) 0 -->
- <location unit="IN">
- <x> 783.0709 </x>
- <y> -574.4148 </y>
- <z> 3.1080 </z>
- </location>
- <capacity unit="LBS"> 412 </capacity><!-- need review --> <!-- would be 1 percent of max load per each wing, 412 each. Needs temp rise of 20C at max load to fill -->
- <contents unit="LBS"> 0 </contents>
-
- <priority>4</priority>
- <type>JET-A1</type>
- <temperature>50</temperature>
- </tank>
- <tank type="FUEL"> <!-- Left Tank (Outer) 1 -->
- <location unit="IN">
- <x> 739.5669 </x>
- <y> -457.4259 </y>
- <z> -8.0898 </z>
- </location>
- <capacity unit="LBS"> 1520.00 </capacity><!-- need review -->
- <contents unit="LBS"> 1520 </contents><!-- outer filled first than inner -->
- <standpipe unit="LBS">21</standpipe><!-- minimun fuel on pipes -->
- <priority>2</priority>
- <type>JET-A1</type>
- <temperature>50</temperature>
- </tank>
- <tank type="FUEL"> <!-- Left Tank (Inner) 2 -->
- <location unit="IN">
- <x> 652.5591 </x>
- <y> -236.2992 </y>
- <z> -33.9470 </z>
- </location>
- <capacity unit="LBS"> 11982 </capacity><!-- correct by FCOM -->
- <contents unit="LBS"> 4480 </contents>
- <standpipe unit="LBS">31</standpipe><!-- minimun fuel on pipes -->
- <priority>3</priority>
- <type>JET-A1</type>
- <temperature>50</temperature>
- </tank>
- <tank type="FUEL"> <!-- Center Tank 3 -->
- <location unit="IN">
- <x> 522.0473 </x>
- <y> 0 </y>
- <z> -47.0 </z>
- </location>
- <capacity unit="LBS"> 14281 </capacity><!-- correct by FCOM -->
- <contents unit="LBS"> 0 </contents> <!-- wing tanks always filled first -->
- <standpipe unit="LBS">43</standpipe><!-- minimun fuel on pipes -->
- <priority>1</priority>
- <type>JET-A1</type>
- <temperature>50</temperature>
- </tank>
- <tank type="FUEL"> <!-- Right Tank (Inner) 4 -->
- <location unit="IN">
- <x> 652.5591 </x>
- <y> 236.2992 </y>
- <z> -33.9470 </z>
- </location>
- <capacity unit="LBS"> 11982 </capacity><!-- correct by FCOM -->
- <contents unit="LBS"> 4480 </contents>
- <standpipe unit="LBS">31</standpipe><!-- minimum fuel on pipes -->
- <priority>3</priority>
- <type>JET-A1</type>
- <temperature>50</temperature>
- </tank>
- <tank type="FUEL"> <!-- Right Tank (Outer) 5 -->
- <location unit="IN">
- <x> 739.5669 </x>
- <y> 457.4259 </y>
- <z> -8.0898 </z>
- </location>
- <capacity unit="LBS"> 1520 </capacity><!-- correct by FCOM -->
- <contents unit="LBS"> 1520 </contents><!-- outer filled before inner -->
- <standpipe unit="LBS">21</standpipe><!-- minimun fuel on pipes -->
- <priority>2</priority>
- <type>JET-A1</type>
- <temperature>50</temperature>
- </tank>
- <tank type="FUEL"> <!-- Right Tank (Wing tip Ventilation Surge) 6 -->
- <location unit="IN">
- <x> 783.0709 </x>
- <y> 574.4148 </y>
- <z> 3.1080 </z>
- </location>
- <capacity unit="LBS"> 412 </capacity><!-- need review --> <!-- 1 percent of max, see left surge tank, is 412 lb each -->
- <contents unit="LBS"> 0 </contents>
- <priority>4</priority>
- <type>JET-A1</type>
- <temperature>50</temperature>
- </tank>
- <tank type="FUEL"> <!-- LEFT FUEL PIPES (Engine 1 feed from this) -->
- <location unit="IN">
- <x>589.735</x>
- <y>-226.575</y>
- <z>-45.567</z>
- </location>
- <capacity unit="LBS"> 100 </capacity><!-- need review -->
- <contents unit="LBS"> 0 </contents>
- <priority>1</priority>
- <type>JET-A1</type>
- </tank>
- <tank type="FUEL"> <!-- RIGHT FUEL PIPES (Engine 2 feed from this) -->
- <location unit="IN">
- <x>589.735</x>
- <y>226.575</y>
- <z>-45.567</z>
- </location>
- <capacity unit="LBS"> 100 </capacity><!-- need review -->
- <contents unit="LBS"> 0 </contents>
- <priority>1</priority>
- <type>JET-A1</type>
- </tank>
-</propulsion>
+ <tank type="FUEL"> <!-- Left Tank (Wing tip Ventilation Surge) 0 -->
+ <location unit="IN">
+ <x> 783.0709 </x>
+ <y> -574.4148 </y>
+ <z> 3.1080 </z>
+ </location>
+ <capacity unit="LBS"> 412 </capacity><!-- need review --> <!-- would be 1 percent of max load per each wing, 412 each. Needs temp rise of 20C at max load to fill -->
+ <contents unit="LBS"> 0 </contents>
+
+ <priority>4</priority>
+ <type>JET-A1</type>
+ <temperature>50</temperature>
+ </tank>
+ <tank type="FUEL"> <!-- Left Tank (Outer) 1 -->
+ <location unit="IN">
+ <x> 739.5669 </x>
+ <y> -457.4259 </y>
+ <z> -8.0898 </z>
+ </location>
+ <capacity unit="LBS"> 1520.00 </capacity><!-- need review -->
+ <contents unit="LBS"> 1520 </contents><!-- outer filled first than inner -->
+ <standpipe unit="LBS">21</standpipe><!-- minimun fuel on pipes -->
+ <priority>2</priority>
+ <type>JET-A1</type>
+ <temperature>50</temperature>
+ </tank>
+ <tank type="FUEL"> <!-- Left Tank (Inner) 2 -->
+ <location unit="IN">
+ <x> 652.5591 </x>
+ <y> -236.2992 </y>
+ <z> -33.9470 </z>
+ </location>
+ <capacity unit="LBS"> 11982 </capacity><!-- correct by FCOM -->
+ <contents unit="LBS"> 4480 </contents>
+ <standpipe unit="LBS">31</standpipe><!-- minimun fuel on pipes -->
+ <priority>3</priority>
+ <type>JET-A1</type>
+ <temperature>50</temperature>
+ </tank>
+ <tank type="FUEL"> <!-- Center Tank 3 -->
+ <location unit="IN">
+ <x> 522.0473 </x>
+ <y> 0 </y>
+ <z> -47.0 </z>
+ </location>
+ <capacity unit="LBS"> 14281 </capacity><!-- correct by FCOM -->
+ <contents unit="LBS"> 0 </contents> <!-- wing tanks always filled first -->
+ <standpipe unit="LBS">43</standpipe><!-- minimun fuel on pipes -->
+ <priority>1</priority>
+ <type>JET-A1</type>
+ <temperature>50</temperature>
+ </tank>
+ <tank type="FUEL"> <!-- Right Tank (Inner) 4 -->
+ <location unit="IN">
+ <x> 652.5591 </x>
+ <y> 236.2992 </y>
+ <z> -33.9470 </z>
+ </location>
+ <capacity unit="LBS"> 11982 </capacity><!-- correct by FCOM -->
+ <contents unit="LBS"> 4480 </contents>
+ <standpipe unit="LBS">31</standpipe><!-- minimum fuel on pipes -->
+ <priority>3</priority>
+ <type>JET-A1</type>
+ <temperature>50</temperature>
+ </tank>
+ <tank type="FUEL"> <!-- Right Tank (Outer) 5 -->
+ <location unit="IN">
+ <x> 739.5669 </x>
+ <y> 457.4259 </y>
+ <z> -8.0898 </z>
+ </location>
+ <capacity unit="LBS"> 1520 </capacity><!-- correct by FCOM -->
+ <contents unit="LBS"> 1520 </contents><!-- outer filled before inner -->
+ <standpipe unit="LBS">21</standpipe><!-- minimun fuel on pipes -->
+ <priority>2</priority>
+ <type>JET-A1</type>
+ <temperature>50</temperature>
+ </tank>
+ <tank type="FUEL"> <!-- Right Tank (Wing tip Ventilation Surge) 6 -->
+ <location unit="IN">
+ <x> 783.0709 </x>
+ <y> 574.4148 </y>
+ <z> 3.1080 </z>
+ </location>
+ <capacity unit="LBS"> 412 </capacity><!-- need review --> <!-- 1 percent of max, see left surge tank, is 412 lb each -->
+ <contents unit="LBS"> 0 </contents>
+ <priority>4</priority>
+ <type>JET-A1</type>
+ <temperature>50</temperature>
+ </tank>
+ <tank type="FUEL"> <!-- LEFT FUEL PIPES (Engine 1 feed from this) -->
+ <location unit="IN">
+ <x>589.735</x>
+ <y>0</y>
+ <z>-45.567</z>
+ </location>
+ <capacity unit="LBS"> 100 </capacity><!-- need review -->
+ <contents unit="LBS"> 0 </contents>
+ <priority>1</priority>
+ <type>JET-A1</type>
+ </tank>
+ <tank type="FUEL"> <!-- RIGHT FUEL PIPES (Engine 2 feed from this) -->
+ <location unit="IN">
+ <x>589.735</x>
+ <y>0</y>
+ <z>-45.567</z>
+ </location>
+ <capacity unit="LBS"> 100 </capacity><!-- need review -->
+ <contents unit="LBS"> 0 </contents>
+ <priority>1</priority>
+ <type>JET-A1</type>
+ </tank>
+ </propulsion>
-<system file="pushback" />
-<system file="fuel" />
-<system file="glass-effect1" />
-<system file="fmgc" />
-<system file="fcs" />
+ <system file="pushback" />
+ <system file="fuel" />
+ <system file="glass-effect1" />
+ <system file="fmgc" />
+ <system file="fcs" />
-<flight_control name="none"/>
+ <flight_control name="none"/>
-<aerodynamics file="Systems/a319-aerodynamics.xml" />
+ <aerodynamics file="Systems/a319-aerodynamics.xml" />
-<external_reactions>
- <force name="pushback" frame="BODY">
- <location unit="IN">
- <x>294</x>
- <y>0</y>
- <z>-149</z>
- </location>
- <direction>
- <x>1</x>
- <y>0</y>
- <z>0</z>
- </direction>
- </force>
-</external_reactions>
+ <external_reactions>
+ <force name="pushback" frame="BODY">
+ <location unit="IN">
+ <x>294</x>
+ <y>0</y>
+ <z>-149</z>
+ </location>
+ <direction>
+ <x>1</x>
+ <y>0</y>
+ <z>0</z>
+ </direction>
+ </force>
+ </external_reactions>
</fdm_config>
diff --git a/A320-100-CFM.xml b/A320-100-CFM.xml
index a07d2223..c6552719 100644
--- a/A320-100-CFM.xml
+++ b/A320-100-CFM.xml
@@ -4,585 +4,585 @@
xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance"
xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
-<fileheader>
- <author>Joshua Davidson (it0uchpods)</author>
- <version>Pre V1.0</version>
- <description>A3XX FDE</description>
-</fileheader>
+ <fileheader>
+ <author>Joshua Davidson (it0uchpods)</author>
+ <version>Pre V1.0</version>
+ <description>A3XX FDE</description>
+ </fileheader>
-<metrics>
- <wingarea unit="FT2"> 1319.79 </wingarea>
- <wingspan unit="FT" > 111.26 </wingspan>
- <wing_incidence> 1.03 </wing_incidence>
- <chord unit="FT" > 13.76 </chord>
- <htailarea unit="FT2"> 334.24 </htailarea>
- <htailarm unit="FT" > 57.88 </htailarm>
- <vtailarea unit="FT2"> 248.79 </vtailarea>
- <vtailarm unit="FT" > 57.33 </vtailarm>
+ <metrics>
+ <wingarea unit="FT2"> 1319.79 </wingarea>
+ <wingspan unit="FT" > 111.26 </wingspan>
+ <wing_incidence> 1.03 </wing_incidence>
+ <chord unit="FT" > 13.76 </chord>
+ <htailarea unit="FT2"> 334.24 </htailarea>
+ <htailarm unit="FT" > 57.88 </htailarm>
+ <vtailarea unit="FT2"> 248.79 </vtailarea>
+ <vtailarm unit="FT" > 57.33 </vtailarm>
- <location name="AERORP" unit="IN">
- <x> 700.00 </x>
- <y> 0 </y>
- <z> 0.00 </z>
- </location>
+ <location name="AERORP" unit="IN">
+ <x> 700.00 </x>
+ <y> 0 </y>
+ <z> 0.00 </z>
+ </location>
- <location name="EYEPOINT" unit="IN">
- <x> 80 </x>
- <y> -30 </y>
- <z> 70 </z>
- </location>
+ <location name="EYEPOINT" unit="IN">
+ <x> 80 </x>
+ <y> -30 </y>
+ <z> 70 </z>
+ </location>
- <location name="VRP" unit="IN">
- <x> 661.1 </x>
- <y> 0 </y>
- <z> -37 </z>
- </location>
+ <location name="VRP" unit="IN">
+ <x> 661.1 </x>
+ <y> 0 </y>
+ <z> -37 </z>
+ </location>
- </metrics>
+ </metrics>
- <mass_balance>
- <ixx unit="SLUG*FT2"> 611903</ixx>
- <iyy unit="SLUG*FT2">1735389</iyy>
- <izz unit="SLUG*FT2">2301293</izz>
+ <mass_balance>
+ <ixx unit="SLUG*FT2"> 611903</ixx>
+ <iyy unit="SLUG*FT2">1735389</iyy>
+ <izz unit="SLUG*FT2">2301293</izz>
- <ixy unit="SLUG*FT2">0</ixy>
- <ixz unit="SLUG*FT2">0</ixz>
- <iyz unit="SLUG*FT2">0</iyz>
- <emptywt unit="LBS">80431</emptywt>
+ <ixy unit="SLUG*FT2">0</ixy>
+ <ixz unit="SLUG*FT2">0</ixz>
+ <iyz unit="SLUG*FT2">0</iyz>
+ <emptywt unit="LBS">80431</emptywt>
- <location name="CG" unit="IN">
- <x> 652.00 </x>
- <y> 0 </y>
- <z> 0.00 </z>
- </location>
+ <location name="CG" unit="IN">
+ <x> 652.00 </x>
+ <y> 0 </y>
+ <z> 0.00 </z>
+ </location>
- <pointmass name="Cockpit Crew">
- <weight unit="LBS">400</weight>
- <!-- MAX: 400lbs, two pilots-->
- <location name="POINTMASS" unit="IN">
- <x>200</x>
- <y>0</y>
- <z>0</z>
- </location>
- </pointmass>
- <pointmass name="Engine 1">
- <weight unit="LBS">5200.7</weight>
- <location name="POINTMASS" unit="IN">
- <x>530.86</x>
- <y>-5.755</y>
- <z>-78.56019</z>
- </location>
- </pointmass>
- <pointmass name="Engine 2">
- <weight unit="LBS">5200.7</weight>
- <location name="POINTMASS" unit="IN">
- <x>530.86</x>
- <y>5.755</y>
- <z>-78.56019</z>
- </location>
- </pointmass>
- <pointmass name="PAX 0A (60 seats)">
- <weight unit="LBS">6600</weight>
- <!-- MAX: 13200lbs, 60 seats -->
- <location name="POINTMASS" unit="IN">
- <x>470.1711</x>
- <y>0</y>
- <z>0</z>
- </location>
- </pointmass>
- <pointmass name="PAX 0B (60 seats)">
- <weight unit="LBS">6600</weight>
- <!-- MAX: 13200lbs, 60 seats -->
- <location name="POINTMASS" unit="IN">
- <x>809.5669</x>
- <y>0</y>
- <z>0</z>
- </location>
- </pointmass>
- <pointmass name="PAX 0C (54 seats)">
- <weight unit="LBS">5940</weight>
- <!-- MAX: 11880lbs, 54 seats -->
- <location name="POINTMASS" unit="IN">
- <x>1163.2729</x>
- <y>0</y>
- <z>0</z>
- </location>
- </pointmass>
- <pointmass name="Cargo Hold 1">
- <weight unit="LBS">2000</weight>
- <!-- MAX: 7500.126lbs -->
- <location name="POINTMASS" unit="IN">
- <x>383.4792</x>
- <y>0</y>
- <z>-29.5</z>
- <!-- 1.5m and now half of it for the center point of the load -->
- </location>
- </pointmass>
- <!-- Cargo Hold 2 doesn't exist, that is the center tank -->
- <pointmass name="Cargo Hold 3">
- <weight unit="LBS">2000</weight>
- <!-- MAX: 5384.414lbs -->
- <location name="POINTMASS" unit="IN">
- <x>849.1324</x>
- <y>0</y>
- <z>-29.5</z>
- </location>
- </pointmass>
- <pointmass name="Cargo Hold 4">
- <weight unit="LBS">1500</weight>
- <!-- MAX: 4651.754lbs -->
- <location name="POINTMASS" unit="IN">
- <x>931.0653</x>
- <y>0</y>
- <z>-29.5</z>
- </location>
- </pointmass>
- <pointmass name="Cargo Hold 5">
- <weight unit="LBS">2000</weight>
- <!-- MAX: 3300.320lbs -->
- <location name="POINTMASS" unit="IN">
- <x>1068.2634</x>
- <y>0</y>
- <z>0</z>
- <!-- Cargo Hold #5 sits higher on the range of the cabin deck, it's only loadable with lifter -->
- </location>
- </pointmass>
+ <pointmass name="Cockpit Crew">
+ <weight unit="LBS">400</weight>
+ <!-- MAX: 400lbs, two pilots-->
+ <location name="POINTMASS" unit="IN">
+ <x>200</x>
+ <y>0</y>
+ <z>0</z>
+ </location>
+ </pointmass>
+ <pointmass name="Engine 1">
+ <weight unit="LBS">5200.7</weight>
+ <location name="POINTMASS" unit="IN">
+ <x>530.86</x>
+ <y>-5.755</y>
+ <z>-78.56019</z>
+ </location>
+ </pointmass>
+ <pointmass name="Engine 2">
+ <weight unit="LBS">5200.7</weight>
+ <location name="POINTMASS" unit="IN">
+ <x>530.86</x>
+ <y>5.755</y>
+ <z>-78.56019</z>
+ </location>
+ </pointmass>
+ <pointmass name="PAX 0A (60 seats)">
+ <weight unit="LBS">6600</weight>
+ <!-- MAX: 13200lbs, 60 seats -->
+ <location name="POINTMASS" unit="IN">
+ <x>470.1711</x>
+ <y>0</y>
+ <z>0</z>
+ </location>
+ </pointmass>
+ <pointmass name="PAX 0B (60 seats)">
+ <weight unit="LBS">6600</weight>
+ <!-- MAX: 13200lbs, 60 seats -->
+ <location name="POINTMASS" unit="IN">
+ <x>809.5669</x>
+ <y>0</y>
+ <z>0</z>
+ </location>
+ </pointmass>
+ <pointmass name="PAX 0C (54 seats)">
+ <weight unit="LBS">5940</weight>
+ <!-- MAX: 11880lbs, 54 seats -->
+ <location name="POINTMASS" unit="IN">
+ <x>1163.2729</x>
+ <y>0</y>
+ <z>0</z>
+ </location>
+ </pointmass>
+ <pointmass name="Cargo Hold 1">
+ <weight unit="LBS">2000</weight>
+ <!-- MAX: 7500.126lbs -->
+ <location name="POINTMASS" unit="IN">
+ <x>383.4792</x>
+ <y>0</y>
+ <z>-29.5</z>
+ <!-- 1.5m and now half of it for the center point of the load -->
+ </location>
+ </pointmass>
+ <!-- Cargo Hold 2 doesn't exist, that is the center tank -->
+ <pointmass name="Cargo Hold 3">
+ <weight unit="LBS">2000</weight>
+ <!-- MAX: 5384.414lbs -->
+ <location name="POINTMASS" unit="IN">
+ <x>849.1324</x>
+ <y>0</y>
+ <z>-29.5</z>
+ </location>
+ </pointmass>
+ <pointmass name="Cargo Hold 4">
+ <weight unit="LBS">1500</weight>
+ <!-- MAX: 4651.754lbs -->
+ <location name="POINTMASS" unit="IN">
+ <x>931.0653</x>
+ <y>0</y>
+ <z>-29.5</z>
+ </location>
+ </pointmass>
+ <pointmass name="Cargo Hold 5">
+ <weight unit="LBS">2000</weight>
+ <!-- MAX: 3300.320lbs -->
+ <location name="POINTMASS" unit="IN">
+ <x>1068.2634</x>
+ <y>0</y>
+ <z>0</z>
+ <!-- Cargo Hold #5 sits higher on the range of the cabin deck, it's only loadable with lifter -->
+ </location>
+ </pointmass>
- </mass_balance>
+ </mass_balance>
- <ground_reactions>
- <!-- REF-1 page 165 + 271 -->
- <contact type="BOGEY" name="NOSE_LG">
- <location unit="IN">
- <x> 197.6772 </x>
- <y> 0 </y>
- <z> -137.9617 </z>
- </location>
- <static_friction> 0.8 </static_friction>
- <dynamic_friction> 0.5 </dynamic_friction>
- <rolling_friction> 0.02 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 30935.5 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 16978.5 </damping_coeff>
- <max_steer unit="DEG"> 70 </max_steer>
- <!-- REF-1 page 133 -->
- <brake_group> NOSE </brake_group>
- <retractable>1</retractable>
- </contact>
- <contact type="BOGEY" name="LEFT_MLG">
- <location unit="IN">
- <!--<x> 699.9243 </x>-->
- <x> 695.3149 </x>
- <y> -149.4094 </y>
- <z> -150.4824 </z>
- </location>
- <!-- <static_friction> 0.5 </static_friction> WHAT??? less static than dinamyc friction?-->
- <static_friction> 0.8 </static_friction>
- <dynamic_friction> 0.5 </dynamic_friction>
- <rolling_friction> 0.02 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 59785 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 23957 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> LEFT </brake_group>
- <retractable>1</retractable>
- </contact>
- <contact type="BOGEY" name="RIGHT_MLG">
- <location unit="IN">
- <!-- <x> 697.3425 </x> It should be right left simetric
- <x> 699.9243 </x> -->
- <x> 695.3149 </x>
- <y> 149.4094 </y>
- <z> -150.4824 </z>
- </location>
- <!-- <static_friction> 0.5 </static_friction> WHAT??? less static than dinamyc friction?-->
- <static_friction> 0.8 </static_friction>
- <dynamic_friction> 0.5 </dynamic_friction>
- <rolling_friction> 0.02 </rolling_friction>
- <!--spring_coeff unit="LBS/FT"> 169785 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 33957 </damping_coeff-->
- <spring_coeff unit="LBS/FT"> 59785 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 23957 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> RIGHT </brake_group>
- <retractable>1</retractable>
- </contact>
+ <ground_reactions>
+ <!-- REF-1 page 165 + 271 -->
+ <contact type="BOGEY" name="NOSE_LG">
+ <location unit="IN">
+ <x> 197.6772 </x>
+ <y> 0 </y>
+ <z> -137.9617 </z>
+ </location>
+ <static_friction> 0.8 </static_friction>
+ <dynamic_friction> 0.5 </dynamic_friction>
+ <rolling_friction> 0.02 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 30935.5 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 16978.5 </damping_coeff>
+ <max_steer unit="DEG"> 70 </max_steer>
+ <!-- REF-1 page 133 -->
+ <brake_group> NOSE </brake_group>
+ <retractable>1</retractable>
+ </contact>
+ <contact type="BOGEY" name="LEFT_MLG">
+ <location unit="IN">
+ <!--<x> 699.9243 </x>-->
+ <x> 695.3149 </x>
+ <y> -149.4094 </y>
+ <z> -150.4824 </z>
+ </location>
+ <!-- <static_friction> 0.5 </static_friction> WHAT??? less static than dinamyc friction?-->
+ <static_friction> 0.8 </static_friction>
+ <dynamic_friction> 0.5 </dynamic_friction>
+ <rolling_friction> 0.02 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 59785 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 23957 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> LEFT </brake_group>
+ <retractable>1</retractable>
+ </contact>
+ <contact type="BOGEY" name="RIGHT_MLG">
+ <location unit="IN">
+ <!-- <x> 697.3425 </x> It should be right left simetric
+ <x> 699.9243 </x> -->
+ <x> 695.3149 </x>
+ <y> 149.4094 </y>
+ <z> -150.4824 </z>
+ </location>
+ <!-- <static_friction> 0.5 </static_friction> WHAT??? less static than dinamyc friction?-->
+ <static_friction> 0.8 </static_friction>
+ <dynamic_friction> 0.5 </dynamic_friction>
+ <rolling_friction> 0.02 </rolling_friction>
+ <!--spring_coeff unit="LBS/FT"> 169785 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 33957 </damping_coeff-->
+ <spring_coeff unit="LBS/FT"> 59785 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 23957 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> RIGHT </brake_group>
+ <retractable>1</retractable>
+ </contact>
- <contact type="STRUCTURE" name="NOSE_1">
- <location unit="IN">
- <x> 37.7953 </x>
- <y> 0 </y>
- <z> -38.1374 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="NOSE_2">
- <location unit="IN">
- <x> 128.1102 </x>
- <y> 0 </y>
- <z> -55.0271 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="CENTER_1">
- <location unit="IN">
- <x> 274.0157 </x>
- <y> 0 </y>
- <z> -60.0665 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="CENTER_2">
- <location unit="IN">
- <x> 930 </x>
- <y> 0 </y>
- <z> -60.0665 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
+ <contact type="STRUCTURE" name="NOSE_1">
+ <location unit="IN">
+ <x> 37.7953 </x>
+ <y> 0 </y>
+ <z> -38.1374 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="NOSE_2">
+ <location unit="IN">
+ <x> 128.1102 </x>
+ <y> 0 </y>
+ <z> -55.0271 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="CENTER_1">
+ <location unit="IN">
+ <x> 274.0157 </x>
+ <y> 0 </y>
+ <z> -60.0665 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="CENTER_2">
+ <location unit="IN">
+ <x> 930 </x>
+ <y> 0 </y>
+ <z> -60.0665 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
- <contact type="STRUCTURE" name="ENG_1">
- <location unit="IN">
- <x>589.735</x>
- <y>-226.575</y>
- <z>-95.567</z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="ENG_2">
- <location unit="IN">
- <x>589.735</x>
- <y>226.575</y>
- <z>-95.567</z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.5 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
+ <contact type="STRUCTURE" name="ENG_1">
+ <location unit="IN">
+ <x>589.735</x>
+ <y>-226.575</y>
+ <z>-95.567</z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="ENG_2">
+ <location unit="IN">
+ <x>589.735</x>
+ <y>226.575</y>
+ <z>-95.567</z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.5 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
- <contact type="STRUCTURE" name="TAIL_1">
- <location unit="IN">
- <x> 1097.9921 </x>
- <y> 0 </y>
- <z> -44.7722 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="TAIL_2">
- <location unit="IN">
- <x> 1225 </x>
- <y> 0 </y>
- <z> -18.8067 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="TAIL_3">
- <location unit="IN">
- <x> 1341.6142 </x>
- <y> 0 </y>
- <z> -10.2599 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="TAIL_4">
- <location unit="IN">
- <x> 1469.0945 </x>
- <y> 0 </y>
- <z> 47.4138 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 1 </dynamic_friction>
- <rolling_friction> 1 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="WING_TIP_1">
- <location unit="IN">
- <x> 838.8898 </x>
- <y> -667.5197 </y>
- <z> 35.7926 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="WING_TIP_2">
- <location unit="IN">
- <x> 838.8898 </x>
- <y> 667.5197 </y>
- <z> 35.7926 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 1 </dynamic_friction>
- <rolling_friction> 1 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- </ground_reactions>
+ <contact type="STRUCTURE" name="TAIL_1">
+ <location unit="IN">
+ <x> 1097.9921 </x>
+ <y> 0 </y>
+ <z> -44.7722 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="TAIL_2">
+ <location unit="IN">
+ <x> 1225 </x>
+ <y> 0 </y>
+ <z> -18.8067 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="TAIL_3">
+ <location unit="IN">
+ <x> 1341.6142 </x>
+ <y> 0 </y>
+ <z> -10.2599 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="TAIL_4">
+ <location unit="IN">
+ <x> 1469.0945 </x>
+ <y> 0 </y>
+ <z> 47.4138 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 1 </dynamic_friction>
+ <rolling_friction> 1 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="WING_TIP_1">
+ <location unit="IN">
+ <x> 838.8898 </x>
+ <y> -667.5197 </y>
+ <z> 35.7926 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="WING_TIP_2">
+ <location unit="IN">
+ <x> 838.8898 </x>
+ <y> 667.5197 </y>
+ <z> 35.7926 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 1 </dynamic_friction>
+ <rolling_friction> 1 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ </ground_reactions>
-<propulsion>
+ <propulsion>
- <engine file="cfm56_5a1">
- <location unit="IN">
- <x> 620.0683 </x>
- <y> -226.575 </y>
- <z> -45.567 </z>
- </location>
- <orient unit="DEG">
- <roll> 0.0 </roll>
- <pitch> 2.2 </pitch>
- <yaw> 1 </yaw>
- </orient>
- <feed>7</feed>
- <thruster file="direct">
+ <engine file="cfm56_5a1">
<location unit="IN">
- <x> 655.4820 </x>
- <y> -226.575 </y>
- <z> 0.000 </z>
+ <x> 620.0683 </x>
+ <y> -226.575 </y>
+ <z> -45.567 </z>
</location>
<orient unit="DEG">
- <roll> 0.0 </roll>
- <pitch> 2.2 </pitch>
- <yaw> 1 </yaw>
+ <roll> 0.0 </roll>
+ <pitch> 2.2 </pitch>
+ <yaw> 1 </yaw>
</orient>
- </thruster>
- </engine>
+ <feed>7</feed>
+ <thruster file="direct">
+ <location unit="IN">
+ <x> 655.4820 </x>
+ <y> -226.575 </y>
+ <z> 0.000 </z>
+ </location>
+ <orient unit="DEG">
+ <roll> 0.0 </roll>
+ <pitch> 2.2 </pitch>
+ <yaw> 1 </yaw>
+ </orient>
+ </thruster>
+ </engine>
- <engine file="cfm56_5a1">
- <location unit="IN">
- <x> 620.0683 </x>
- <y> 226.575 </y>
- <z> -45.567 </z>
- </location>
- <orient unit="DEG">
- <roll> 0.0 </roll>
- <pitch> 2.2 </pitch>
- <yaw> -1 </yaw>
- </orient>
- <feed>8</feed>
- <thruster file="direct">
+ <engine file="cfm56_5a1">
<location unit="IN">
- <x> 655.4820 </x>
- <y> 226.575 </y>
- <z> 0.000 </z>
+ <x> 620.0683 </x>
+ <y> 226.575 </y>
+ <z> -45.567 </z>
</location>
<orient unit="DEG">
- <roll> 0.0 </roll>
- <pitch> 2.2 </pitch>
- <yaw> -1 </yaw>
+ <roll> 0.0 </roll>
+ <pitch> 2.2 </pitch>
+ <yaw> -1 </yaw>
</orient>
- </thruster>
- </engine>
+ <feed>8</feed>
+ <thruster file="direct">
+ <location unit="IN">
+ <x> 655.4820 </x>
+ <y> 226.575 </y>
+ <z> 0.000 </z>
+ </location>
+ <orient unit="DEG">
+ <roll> 0.0 </roll>
+ <pitch> 2.2 </pitch>
+ <yaw> -1 </yaw>
+ </orient>
+ </thruster>
+ </engine>
- <tank type="FUEL"> <!-- Left Tank (Wing tip Ventilation Surge) 0 -->
- <location unit="IN">
- <x> 783.0709 </x>
- <y> -574.4148 </y>
- <z> 3.1080 </z>
- </location>
- <capacity unit="LBS"> 412 </capacity><!-- 1 percent of total capacity, needs 20C to be filled -->
- <contents unit="LBS"> 0 </contents>
-
- <priority>4</priority>
- <type>JET-A1</type>
- <temperature>50</temperature>
- </tank>
- <tank type="FUEL"> <!-- Left Tank (Outer) 1 -->
- <location unit="IN">
- <x> 739.5669 </x>
- <y> -457.4259 </y>
- <z> -8.0898 </z>
- </location>
- <capacity unit="LBS"> 1520.00 </capacity><!-- correct by FCOM -->
- <contents unit="LBS"> 1520 </contents><!-- outer filled first than inner -->
- <standpipe unit="LBS">21</standpipe><!-- minimun fuel on pipes -->
- <priority>2</priority>
- <type>JET-A1</type>
- <temperature>50</temperature>
- </tank>
- <tank type="FUEL"> <!-- Left Tank (Inner) 2 -->
- <location unit="IN">
- <x> 652.5591 </x>
- <y> -236.2992 </y>
- <z> -33.9470 </z>
- </location>
- <capacity unit="LBS"> 11982 </capacity><!-- correct by FCOM -->
- <contents unit="LBS"> 4480 </contents>
- <standpipe unit="LBS">31</standpipe><!-- minimun fuel on pipes -->
- <priority>3</priority>
- <type>JET-A1</type>
- <temperature>50</temperature>
- </tank>
- <tank type="FUEL"> <!-- Center Tank 3 -->
- <location unit="IN">
- <x> 522.0473 </x>
- <y> 0 </y>
- <z> -47.0 </z>
- </location>
- <capacity unit="LBS"> 14281 </capacity><!-- correct by FCOM -->
- <contents unit="LBS"> 0 </contents> <!-- wing tanks filled first -->
- <standpipe unit="LBS">43</standpipe><!-- minimun fuel on pipes -->
- <priority>1</priority>
- <type>JET-A1</type>
- <temperature>50</temperature>
- </tank>
- <tank type="FUEL"> <!-- Right Tank (Inner) 4 -->
- <location unit="IN">
- <x> 652.5591 </x>
- <y> 236.2992 </y>
- <z> -33.9470 </z>
- </location>
- <capacity unit="LBS"> 11982 </capacity><!-- correct by FCOM -->
- <contents unit="LBS"> 4480 </contents>
- <standpipe unit="LBS">31</standpipe><!-- minimum fuel on pipes -->
- <priority>3</priority>
- <type>JET-A1</type>
- <temperature>50</temperature>
- </tank>
- <tank type="FUEL"> <!-- Right Tank (Outer) 5 -->
- <location unit="IN">
- <x> 739.5669 </x>
- <y> 457.4259 </y>
- <z> -8.0898 </z>
- </location>
- <capacity unit="LBS"> 1520 </capacity><!-- need review -->
- <contents unit="LBS"> 1520 </contents><!-- outer tank filled first than inner tank -->
- <standpipe unit="LBS">21</standpipe><!-- minimun fuel on pipes -->
- <priority>2</priority>
- <type>JET-A1</type>
- <temperature>50</temperature>
- </tank>
- <tank type="FUEL"> <!-- Right Tank (Wing tip Ventilation Surge) 6 -->
- <location unit="IN">
- <x> 783.0709 </x>
- <y> 574.4148 </y>
- <z> 3.1080 </z>
- </location>
- <capacity unit="LBS"> 412 </capacity><!-- 1 percent of total fuel capacity, needs 20C-->
- <contents unit="LBS"> 0 </contents>
- <priority>4</priority>
- <type>JET-A1</type>
- <temperature>50</temperature>
- </tank>
- <tank type="FUEL"> <!-- LEFT FUEL PIPES (Engine 1 feed from this) -->
- <location unit="IN">
- <x>589.735</x>
- <y>-226.575</y>
- <z>-45.567</z>
- </location>
- <capacity unit="LBS"> 100 </capacity><!-- need review -->
- <contents unit="LBS"> 0 </contents>
- <priority>1</priority>
- <type>JET-A1</type>
- </tank>
- <tank type="FUEL"> <!-- RIGHT FUEL PIPES (Engine 2 feed from this) -->
- <location unit="IN">
- <x>589.735</x>
- <y>226.575</y>
- <z>-45.567</z>
- </location>
- <capacity unit="LBS"> 100 </capacity><!-- need review -->
- <contents unit="LBS"> 0 </contents>
- <priority>1</priority>
- <type>JET-A1</type>
- </tank>
-</propulsion>
+ <tank type="FUEL"> <!-- Left Tank (Wing tip Ventilation Surge) 0 -->
+ <location unit="IN">
+ <x> 783.0709 </x>
+ <y> -574.4148 </y>
+ <z> 3.1080 </z>
+ </location>
+ <capacity unit="LBS"> 412 </capacity><!-- 1 percent of total capacity, needs 20C to be filled -->
+ <contents unit="LBS"> 0 </contents>
+
+ <priority>4</priority>
+ <type>JET-A1</type>
+ <temperature>50</temperature>
+ </tank>
+ <tank type="FUEL"> <!-- Left Tank (Outer) 1 -->
+ <location unit="IN">
+ <x> 739.5669 </x>
+ <y> -457.4259 </y>
+ <z> -8.0898 </z>
+ </location>
+ <capacity unit="LBS"> 1520.00 </capacity><!-- correct by FCOM -->
+ <contents unit="LBS"> 1520 </contents><!-- outer filled first than inner -->
+ <standpipe unit="LBS">21</standpipe><!-- minimun fuel on pipes -->
+ <priority>2</priority>
+ <type>JET-A1</type>
+ <temperature>50</temperature>
+ </tank>
+ <tank type="FUEL"> <!-- Left Tank (Inner) 2 -->
+ <location unit="IN">
+ <x> 652.5591 </x>
+ <y> -236.2992 </y>
+ <z> -33.9470 </z>
+ </location>
+ <capacity unit="LBS"> 11982 </capacity><!-- correct by FCOM -->
+ <contents unit="LBS"> 4480 </contents>
+ <standpipe unit="LBS">31</standpipe><!-- minimun fuel on pipes -->
+ <priority>3</priority>
+ <type>JET-A1</type>
+ <temperature>50</temperature>
+ </tank>
+ <tank type="FUEL"> <!-- Center Tank 3 -->
+ <location unit="IN">
+ <x> 522.0473 </x>
+ <y> 0 </y>
+ <z> -47.0 </z>
+ </location>
+ <capacity unit="LBS"> 14281 </capacity><!-- correct by FCOM -->
+ <contents unit="LBS"> 0 </contents> <!-- wing tanks filled first -->
+ <standpipe unit="LBS">43</standpipe><!-- minimun fuel on pipes -->
+ <priority>1</priority>
+ <type>JET-A1</type>
+ <temperature>50</temperature>
+ </tank>
+ <tank type="FUEL"> <!-- Right Tank (Inner) 4 -->
+ <location unit="IN">
+ <x> 652.5591 </x>
+ <y> 236.2992 </y>
+ <z> -33.9470 </z>
+ </location>
+ <capacity unit="LBS"> 11982 </capacity><!-- correct by FCOM -->
+ <contents unit="LBS"> 4480 </contents>
+ <standpipe unit="LBS">31</standpipe><!-- minimum fuel on pipes -->
+ <priority>3</priority>
+ <type>JET-A1</type>
+ <temperature>50</temperature>
+ </tank>
+ <tank type="FUEL"> <!-- Right Tank (Outer) 5 -->
+ <location unit="IN">
+ <x> 739.5669 </x>
+ <y> 457.4259 </y>
+ <z> -8.0898 </z>
+ </location>
+ <capacity unit="LBS"> 1520 </capacity><!-- need review -->
+ <contents unit="LBS"> 1520 </contents><!-- outer tank filled first than inner tank -->
+ <standpipe unit="LBS">21</standpipe><!-- minimun fuel on pipes -->
+ <priority>2</priority>
+ <type>JET-A1</type>
+ <temperature>50</temperature>
+ </tank>
+ <tank type="FUEL"> <!-- Right Tank (Wing tip Ventilation Surge) 6 -->
+ <location unit="IN">
+ <x> 783.0709 </x>
+ <y> 574.4148 </y>
+ <z> 3.1080 </z>
+ </location>
+ <capacity unit="LBS"> 412 </capacity><!-- 1 percent of total fuel capacity, needs 20C-->
+ <contents unit="LBS"> 0 </contents>
+ <priority>4</priority>
+ <type>JET-A1</type>
+ <temperature>50</temperature>
+ </tank>
+ <tank type="FUEL"> <!-- LEFT FUEL PIPES (Engine 1 feed from this) -->
+ <location unit="IN">
+ <x>589.735</x>
+ <y>0</y>
+ <z>-45.567</z>
+ </location>
+ <capacity unit="LBS"> 100 </capacity><!-- need review -->
+ <contents unit="LBS"> 0 </contents>
+ <priority>1</priority>
+ <type>JET-A1</type>
+ </tank>
+ <tank type="FUEL"> <!-- RIGHT FUEL PIPES (Engine 2 feed from this) -->
+ <location unit="IN">
+ <x>589.735</x>
+ <y>0</y>
+ <z>-45.567</z>
+ </location>
+ <capacity unit="LBS"> 100 </capacity><!-- need review -->
+ <contents unit="LBS"> 0 </contents>
+ <priority>1</priority>
+ <type>JET-A1</type>
+ </tank>
+ </propulsion>
-<system file="pushback" />
-<system file="fuel" />
-<system file="glass-effect1" />
-<system file="fmgc" />
-<system file="fcs" />
+ <system file="pushback" />
+ <system file="fuel" />
+ <system file="glass-effect1" />
+ <system file="fmgc" />
+ <system file="fcs" />
-<flight_control name="none"/>
+ <flight_control name="none"/>
-<aerodynamics file="Systems/a320-aerodynamics.xml" />
+ <aerodynamics file="Systems/a320-aerodynamics.xml" />
-<external_reactions>
- <force name="pushback" frame="BODY">
- <location unit="IN">
- <x>294</x>
- <y>0</y>
- <z>-149</z>
- </location>
- <direction>
- <x>1</x>
- <y>0</y>
- <z>0</z>
- </direction>
- </force>
-</external_reactions>
+ <external_reactions>
+ <force name="pushback" frame="BODY">
+ <location unit="IN">
+ <x>294</x>
+ <y>0</y>
+ <z>-149</z>
+ </location>
+ <direction>
+ <x>1</x>
+ <y>0</y>
+ <z>0</z>
+ </direction>
+ </force>
+ </external_reactions>
</fdm_config>
diff --git a/A320-200-CFM.xml b/A320-200-CFM.xml
index 3bf8a975..6301f228 100644
--- a/A320-200-CFM.xml
+++ b/A320-200-CFM.xml
@@ -559,32 +559,28 @@ xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
<type>JET-A1</type>
<temperature>50</temperature>
</tank>
- <tank type="FUEL">
- <!-- LEFT FUEL PIPES (Engine 1 feed from this) -->
- <location unit="IN">
- <x>589.735</x>
- <y>-226.575</y>
- <z>-45.567</z>
- </location>
- <capacity unit="LBS"> 100 </capacity>
- <!-- need review -->
- <contents unit="LBS"> 0 </contents>
- <priority>1</priority>
- <type>JET-A1</type>
- </tank>
- <tank type="FUEL">
- <!-- RIGHT FUEL PIPES (Engine 2 feed from this) -->
- <location unit="IN">
- <x>589.735</x>
- <y>226.575</y>
- <z>-45.567</z>
- </location>
- <capacity unit="LBS"> 100 </capacity>
- <!-- need review -->
- <contents unit="LBS"> 0 </contents>
- <priority>1</priority>
- <type>JET-A1</type>
- </tank>
+ <tank type="FUEL"> <!-- LEFT FUEL PIPES (Engine 1 feed from this) -->
+ <location unit="IN">
+ <x>589.735</x>
+ <y>0</y>
+ <z>-45.567</z>
+ </location>
+ <capacity unit="LBS"> 100 </capacity><!-- need review -->
+ <contents unit="LBS"> 0 </contents>
+ <priority>1</priority>
+ <type>JET-A1</type>
+ </tank>
+ <tank type="FUEL"> <!-- RIGHT FUEL PIPES (Engine 2 feed from this) -->
+ <location unit="IN">
+ <x>589.735</x>
+ <y>0</y>
+ <z>-45.567</z>
+ </location>
+ <capacity unit="LBS"> 100 </capacity><!-- need review -->
+ <contents unit="LBS"> 0 </contents>
+ <priority>1</priority>
+ <type>JET-A1</type>
+ </tank>
</propulsion>
<system file="pushback" />
diff --git a/A320-200-IAE.xml b/A320-200-IAE.xml
index ba8e08bb..9dfbaf1f 100644
--- a/A320-200-IAE.xml
+++ b/A320-200-IAE.xml
@@ -4,585 +4,585 @@
xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance"
xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
-<fileheader>
- <author>Joshua Davidson (it0uchpods)</author>
- <version>Pre V1.0</version>
- <description>A3XX FDE</description>
-</fileheader>
+ <fileheader>
+ <author>Joshua Davidson (it0uchpods)</author>
+ <version>Pre V1.0</version>
+ <description>A3XX FDE</description>
+ </fileheader>
-<metrics>
- <wingarea unit="FT2"> 1319.79 </wingarea>
- <wingspan unit="FT" > 111.26 </wingspan>
- <wing_incidence> 1.03 </wing_incidence>
- <chord unit="FT" > 13.76 </chord>
- <htailarea unit="FT2"> 334.24 </htailarea>
- <htailarm unit="FT" > 57.88 </htailarm>
- <vtailarea unit="FT2"> 248.79 </vtailarea>
- <vtailarm unit="FT" > 57.33 </vtailarm>
+ <metrics>
+ <wingarea unit="FT2"> 1319.79 </wingarea>
+ <wingspan unit="FT" > 111.26 </wingspan>
+ <wing_incidence> 1.03 </wing_incidence>
+ <chord unit="FT" > 13.76 </chord>
+ <htailarea unit="FT2"> 334.24 </htailarea>
+ <htailarm unit="FT" > 57.88 </htailarm>
+ <vtailarea unit="FT2"> 248.79 </vtailarea>
+ <vtailarm unit="FT" > 57.33 </vtailarm>
- <location name="AERORP" unit="IN">
- <x> 700.00 </x>
- <y> 0 </y>
- <z> 0.00 </z>
- </location>
+ <location name="AERORP" unit="IN">
+ <x> 700.00 </x>
+ <y> 0 </y>
+ <z> 0.00 </z>
+ </location>
- <location name="EYEPOINT" unit="IN">
- <x> 80 </x>
- <y> -30 </y>
- <z> 70 </z>
- </location>
+ <location name="EYEPOINT" unit="IN">
+ <x> 80 </x>
+ <y> -30 </y>
+ <z> 70 </z>
+ </location>
- <location name="VRP" unit="IN">
- <x> 661.1 </x>
- <y> 0 </y>
- <z> -37 </z>
- </location>
+ <location name="VRP" unit="IN">
+ <x> 661.1 </x>
+ <y> 0 </y>
+ <z> -37 </z>
+ </location>
- </metrics>
+ </metrics>
- <mass_balance>
- <ixx unit="SLUG*FT2"> 611903</ixx>
- <iyy unit="SLUG*FT2">1735389</iyy>
- <izz unit="SLUG*FT2">2301293</izz>
+ <mass_balance>
+ <ixx unit="SLUG*FT2"> 611903</ixx>
+ <iyy unit="SLUG*FT2">1735389</iyy>
+ <izz unit="SLUG*FT2">2301293</izz>
- <ixy unit="SLUG*FT2">0</ixy>
- <ixz unit="SLUG*FT2">0</ixz>
- <iyz unit="SLUG*FT2">0</iyz>
- <emptywt unit="LBS">80431</emptywt>
+ <ixy unit="SLUG*FT2">0</ixy>
+ <ixz unit="SLUG*FT2">0</ixz>
+ <iyz unit="SLUG*FT2">0</iyz>
+ <emptywt unit="LBS">80431</emptywt>
- <location name="CG" unit="IN">
- <x> 652.00 </x>
- <y> 0 </y>
- <z> 0.00 </z>
- </location>
+ <location name="CG" unit="IN">
+ <x> 652.00 </x>
+ <y> 0 </y>
+ <z> 0.00 </z>
+ </location>
- <pointmass name="Cockpit Crew">
- <weight unit="LBS">400</weight>
- <!-- MAX: 400lbs, two pilots-->
- <location name="POINTMASS" unit="IN">
- <x>200</x>
- <y>0</y>
- <z>0</z>
- </location>
- </pointmass>
- <pointmass name="Engine 1">
- <weight unit="LBS">5200.7</weight>
- <location name="POINTMASS" unit="IN">
- <x>530.86</x>
- <y>-5.755</y>
- <z>-78.56019</z>
- </location>
- </pointmass>
- <pointmass name="Engine 2">
- <weight unit="LBS">5200.7</weight>
- <location name="POINTMASS" unit="IN">
- <x>530.86</x>
- <y>5.755</y>
- <z>-78.56019</z>
- </location>
- </pointmass>
- <pointmass name="PAX 0A (60 seats)">
- <weight unit="LBS">6600</weight>
- <!-- MAX: 13200lbs, 60 seats -->
- <location name="POINTMASS" unit="IN">
- <x>470.1711</x>
- <y>0</y>
- <z>0</z>
- </location>
- </pointmass>
- <pointmass name="PAX 0B (60 seats)">
- <weight unit="LBS">6600</weight>
- <!-- MAX: 13200lbs, 60 seats -->
- <location name="POINTMASS" unit="IN">
- <x>809.5669</x>
- <y>0</y>
- <z>0</z>
- </location>
- </pointmass>
- <pointmass name="PAX 0C (54 seats)">
- <weight unit="LBS">5940</weight>
- <!-- MAX: 11880lbs, 54 seats -->
- <location name="POINTMASS" unit="IN">
- <x>1163.2729</x>
- <y>0</y>
- <z>0</z>
- </location>
- </pointmass>
- <pointmass name="Cargo Hold 1">
- <weight unit="LBS">2000</weight>
- <!-- MAX: 7500.126lbs -->
- <location name="POINTMASS" unit="IN">
- <x>383.4792</x>
- <y>0</y>
- <z>-29.5</z>
- <!-- 1.5m and now half of it for the center point of the load -->
- </location>
- </pointmass>
- <!-- Cargo Hold 2 doesn't exist, that is the center tank -->
- <pointmass name="Cargo Hold 3">
- <weight unit="LBS">2000</weight>
- <!-- MAX: 5384.414lbs -->
- <location name="POINTMASS" unit="IN">
- <x>849.1324</x>
- <y>0</y>
- <z>-29.5</z>
- </location>
- </pointmass>
- <pointmass name="Cargo Hold 4">
- <weight unit="LBS">1500</weight>
- <!-- MAX: 4651.754lbs -->
- <location name="POINTMASS" unit="IN">
- <x>931.0653</x>
- <y>0</y>
- <z>-29.5</z>
- </location>
- </pointmass>
- <pointmass name="Cargo Hold 5">
- <weight unit="LBS">2000</weight>
- <!-- MAX: 3300.320lbs -->
- <location name="POINTMASS" unit="IN">
- <x>1068.2634</x>
- <y>0</y>
- <z>0</z>
- <!-- Cargo Hold #5 sits higher on the range of the cabin deck, it's only loadable with lifter -->
- </location>
- </pointmass>
+ <pointmass name="Cockpit Crew">
+ <weight unit="LBS">400</weight>
+ <!-- MAX: 400lbs, two pilots-->
+ <location name="POINTMASS" unit="IN">
+ <x>200</x>
+ <y>0</y>
+ <z>0</z>
+ </location>
+ </pointmass>
+ <pointmass name="Engine 1">
+ <weight unit="LBS">5200.7</weight>
+ <location name="POINTMASS" unit="IN">
+ <x>530.86</x>
+ <y>-5.755</y>
+ <z>-78.56019</z>
+ </location>
+ </pointmass>
+ <pointmass name="Engine 2">
+ <weight unit="LBS">5200.7</weight>
+ <location name="POINTMASS" unit="IN">
+ <x>530.86</x>
+ <y>5.755</y>
+ <z>-78.56019</z>
+ </location>
+ </pointmass>
+ <pointmass name="PAX 0A (60 seats)">
+ <weight unit="LBS">6600</weight>
+ <!-- MAX: 13200lbs, 60 seats -->
+ <location name="POINTMASS" unit="IN">
+ <x>470.1711</x>
+ <y>0</y>
+ <z>0</z>
+ </location>
+ </pointmass>
+ <pointmass name="PAX 0B (60 seats)">
+ <weight unit="LBS">6600</weight>
+ <!-- MAX: 13200lbs, 60 seats -->
+ <location name="POINTMASS" unit="IN">
+ <x>809.5669</x>
+ <y>0</y>
+ <z>0</z>
+ </location>
+ </pointmass>
+ <pointmass name="PAX 0C (54 seats)">
+ <weight unit="LBS">5940</weight>
+ <!-- MAX: 11880lbs, 54 seats -->
+ <location name="POINTMASS" unit="IN">
+ <x>1163.2729</x>
+ <y>0</y>
+ <z>0</z>
+ </location>
+ </pointmass>
+ <pointmass name="Cargo Hold 1">
+ <weight unit="LBS">2000</weight>
+ <!-- MAX: 7500.126lbs -->
+ <location name="POINTMASS" unit="IN">
+ <x>383.4792</x>
+ <y>0</y>
+ <z>-29.5</z>
+ <!-- 1.5m and now half of it for the center point of the load -->
+ </location>
+ </pointmass>
+ <!-- Cargo Hold 2 doesn't exist, that is the center tank -->
+ <pointmass name="Cargo Hold 3">
+ <weight unit="LBS">2000</weight>
+ <!-- MAX: 5384.414lbs -->
+ <location name="POINTMASS" unit="IN">
+ <x>849.1324</x>
+ <y>0</y>
+ <z>-29.5</z>
+ </location>
+ </pointmass>
+ <pointmass name="Cargo Hold 4">
+ <weight unit="LBS">1500</weight>
+ <!-- MAX: 4651.754lbs -->
+ <location name="POINTMASS" unit="IN">
+ <x>931.0653</x>
+ <y>0</y>
+ <z>-29.5</z>
+ </location>
+ </pointmass>
+ <pointmass name="Cargo Hold 5">
+ <weight unit="LBS">2000</weight>
+ <!-- MAX: 3300.320lbs -->
+ <location name="POINTMASS" unit="IN">
+ <x>1068.2634</x>
+ <y>0</y>
+ <z>0</z>
+ <!-- Cargo Hold #5 sits higher on the range of the cabin deck, it's only loadable with lifter -->
+ </location>
+ </pointmass>
- </mass_balance>
+ </mass_balance>
- <ground_reactions>
- <!-- REF-1 page 165 + 271 -->
- <contact type="BOGEY" name="NOSE_LG">
- <location unit="IN">
- <x> 197.6772 </x>
- <y> 0 </y>
- <z> -137.9617 </z>
- </location>
- <static_friction> 0.8 </static_friction>
- <dynamic_friction> 0.5 </dynamic_friction>
- <rolling_friction> 0.02 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 30935.5 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 16978.5 </damping_coeff>
- <max_steer unit="DEG"> 70 </max_steer>
- <!-- REF-1 page 133 -->
- <brake_group> NOSE </brake_group>
- <retractable>1</retractable>
- </contact>
- <contact type="BOGEY" name="LEFT_MLG">
- <location unit="IN">
- <!--<x> 699.9243 </x>-->
- <x> 695.3149 </x>
- <y> -149.4094 </y>
- <z> -150.4824 </z>
- </location>
- <!-- <static_friction> 0.5 </static_friction> WHAT??? less static than dinamyc friction?-->
- <static_friction> 0.8 </static_friction>
- <dynamic_friction> 0.5 </dynamic_friction>
- <rolling_friction> 0.02 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 59785 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 23957 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> LEFT </brake_group>
- <retractable>1</retractable>
- </contact>
- <contact type="BOGEY" name="RIGHT_MLG">
- <location unit="IN">
- <!-- <x> 697.3425 </x> It should be right left simetric
- <x> 699.9243 </x> -->
- <x> 695.3149 </x>
- <y> 149.4094 </y>
- <z> -150.4824 </z>
- </location>
- <!-- <static_friction> 0.5 </static_friction> WHAT??? less static than dinamyc friction?-->
- <static_friction> 0.8 </static_friction>
- <dynamic_friction> 0.5 </dynamic_friction>
- <rolling_friction> 0.02 </rolling_friction>
- <!--spring_coeff unit="LBS/FT"> 169785 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 33957 </damping_coeff-->
- <spring_coeff unit="LBS/FT"> 59785 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 23957 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> RIGHT </brake_group>
- <retractable>1</retractable>
- </contact>
+ <ground_reactions>
+ <!-- REF-1 page 165 + 271 -->
+ <contact type="BOGEY" name="NOSE_LG">
+ <location unit="IN">
+ <x> 197.6772 </x>
+ <y> 0 </y>
+ <z> -137.9617 </z>
+ </location>
+ <static_friction> 0.8 </static_friction>
+ <dynamic_friction> 0.5 </dynamic_friction>
+ <rolling_friction> 0.02 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 30935.5 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 16978.5 </damping_coeff>
+ <max_steer unit="DEG"> 70 </max_steer>
+ <!-- REF-1 page 133 -->
+ <brake_group> NOSE </brake_group>
+ <retractable>1</retractable>
+ </contact>
+ <contact type="BOGEY" name="LEFT_MLG">
+ <location unit="IN">
+ <!--<x> 699.9243 </x>-->
+ <x> 695.3149 </x>
+ <y> -149.4094 </y>
+ <z> -150.4824 </z>
+ </location>
+ <!-- <static_friction> 0.5 </static_friction> WHAT??? less static than dinamyc friction?-->
+ <static_friction> 0.8 </static_friction>
+ <dynamic_friction> 0.5 </dynamic_friction>
+ <rolling_friction> 0.02 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 59785 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 23957 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> LEFT </brake_group>
+ <retractable>1</retractable>
+ </contact>
+ <contact type="BOGEY" name="RIGHT_MLG">
+ <location unit="IN">
+ <!-- <x> 697.3425 </x> It should be right left simetric
+ <x> 699.9243 </x> -->
+ <x> 695.3149 </x>
+ <y> 149.4094 </y>
+ <z> -150.4824 </z>
+ </location>
+ <!-- <static_friction> 0.5 </static_friction> WHAT??? less static than dinamyc friction?-->
+ <static_friction> 0.8 </static_friction>
+ <dynamic_friction> 0.5 </dynamic_friction>
+ <rolling_friction> 0.02 </rolling_friction>
+ <!--spring_coeff unit="LBS/FT"> 169785 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 33957 </damping_coeff-->
+ <spring_coeff unit="LBS/FT"> 59785 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 23957 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> RIGHT </brake_group>
+ <retractable>1</retractable>
+ </contact>
- <contact type="STRUCTURE" name="NOSE_1">
- <location unit="IN">
- <x> 37.7953 </x>
- <y> 0 </y>
- <z> -38.1374 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="NOSE_2">
- <location unit="IN">
- <x> 128.1102 </x>
- <y> 0 </y>
- <z> -55.0271 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="CENTER_1">
- <location unit="IN">
- <x> 274.0157 </x>
- <y> 0 </y>
- <z> -60.0665 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="CENTER_2">
- <location unit="IN">
- <x> 930 </x>
- <y> 0 </y>
- <z> -60.0665 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
+ <contact type="STRUCTURE" name="NOSE_1">
+ <location unit="IN">
+ <x> 37.7953 </x>
+ <y> 0 </y>
+ <z> -38.1374 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="NOSE_2">
+ <location unit="IN">
+ <x> 128.1102 </x>
+ <y> 0 </y>
+ <z> -55.0271 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="CENTER_1">
+ <location unit="IN">
+ <x> 274.0157 </x>
+ <y> 0 </y>
+ <z> -60.0665 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="CENTER_2">
+ <location unit="IN">
+ <x> 930 </x>
+ <y> 0 </y>
+ <z> -60.0665 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
- <contact type="STRUCTURE" name="ENG_1">
- <location unit="IN">
- <x>589.735</x>
- <y>-226.575</y>
- <z>-95.567</z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="ENG_2">
- <location unit="IN">
- <x>589.735</x>
- <y>226.575</y>
- <z>-95.567</z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.5 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
+ <contact type="STRUCTURE" name="ENG_1">
+ <location unit="IN">
+ <x>589.735</x>
+ <y>-226.575</y>
+ <z>-95.567</z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="ENG_2">
+ <location unit="IN">
+ <x>589.735</x>
+ <y>226.575</y>
+ <z>-95.567</z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.5 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
- <contact type="STRUCTURE" name="TAIL_1">
- <location unit="IN">
- <x> 1097.9921 </x>
- <y> 0 </y>
- <z> -44.7722 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="TAIL_2">
- <location unit="IN">
- <x> 1225 </x>
- <y> 0 </y>
- <z> -18.8067 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="TAIL_3">
- <location unit="IN">
- <x> 1341.6142 </x>
- <y> 0 </y>
- <z> -10.2599 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="TAIL_4">
- <location unit="IN">
- <x> 1469.0945 </x>
- <y> 0 </y>
- <z> 47.4138 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 1 </dynamic_friction>
- <rolling_friction> 1 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="WING_TIP_1">
- <location unit="IN">
- <x> 838.8898 </x>
- <y> -667.5197 </y>
- <z> 35.7926 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="WING_TIP_2">
- <location unit="IN">
- <x> 838.8898 </x>
- <y> 667.5197 </y>
- <z> 35.7926 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 1 </dynamic_friction>
- <rolling_friction> 1 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- </ground_reactions>
+ <contact type="STRUCTURE" name="TAIL_1">
+ <location unit="IN">
+ <x> 1097.9921 </x>
+ <y> 0 </y>
+ <z> -44.7722 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="TAIL_2">
+ <location unit="IN">
+ <x> 1225 </x>
+ <y> 0 </y>
+ <z> -18.8067 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="TAIL_3">
+ <location unit="IN">
+ <x> 1341.6142 </x>
+ <y> 0 </y>
+ <z> -10.2599 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="TAIL_4">
+ <location unit="IN">
+ <x> 1469.0945 </x>
+ <y> 0 </y>
+ <z> 47.4138 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 1 </dynamic_friction>
+ <rolling_friction> 1 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="WING_TIP_1">
+ <location unit="IN">
+ <x> 838.8898 </x>
+ <y> -667.5197 </y>
+ <z> 35.7926 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="WING_TIP_2">
+ <location unit="IN">
+ <x> 838.8898 </x>
+ <y> 667.5197 </y>
+ <z> 35.7926 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 1 </dynamic_friction>
+ <rolling_friction> 1 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ </ground_reactions>
-<propulsion>
+ <propulsion>
- <engine file="v2527_a5">
- <location unit="IN">
- <x> 620.0683 </x>
- <y> -226.575 </y>
- <z> -45.567 </z>
- </location>
- <orient unit="DEG">
- <roll> 0.0 </roll>
- <pitch> 2.2 </pitch>
- <yaw> 1 </yaw>
- </orient>
- <feed>7</feed>
- <thruster file="direct">
+ <engine file="v2527_a5">
<location unit="IN">
- <x> 655.4820 </x>
- <y> -226.575 </y>
- <z> 0.000 </z>
+ <x> 620.0683 </x>
+ <y> -226.575 </y>
+ <z> -45.567 </z>
</location>
<orient unit="DEG">
- <roll> 0.0 </roll>
- <pitch> 2.2 </pitch>
- <yaw> 1 </yaw>
+ <roll> 0.0 </roll>
+ <pitch> 2.2 </pitch>
+ <yaw> 1 </yaw>
</orient>
- </thruster>
- </engine>
+ <feed>7</feed>
+ <thruster file="direct">
+ <location unit="IN">
+ <x> 655.4820 </x>
+ <y> -226.575 </y>
+ <z> 0.000 </z>
+ </location>
+ <orient unit="DEG">
+ <roll> 0.0 </roll>
+ <pitch> 2.2 </pitch>
+ <yaw> 1 </yaw>
+ </orient>
+ </thruster>
+ </engine>
- <engine file="v2527_a5">
- <location unit="IN">
- <x> 620.0683 </x>
- <y> 226.575 </y>
- <z> -45.567 </z>
- </location>
- <orient unit="DEG">
- <roll> 0.0 </roll>
- <pitch> 2.2 </pitch>
- <yaw> -1 </yaw>
- </orient>
- <feed>8</feed>
- <thruster file="direct">
+ <engine file="v2527_a5">
<location unit="IN">
- <x> 655.4820 </x>
- <y> 226.575 </y>
- <z> 0.000 </z>
+ <x> 620.0683 </x>
+ <y> 226.575 </y>
+ <z> -45.567 </z>
</location>
<orient unit="DEG">
- <roll> 0.0 </roll>
- <pitch> 2.2 </pitch>
- <yaw> -1 </yaw>
+ <roll> 0.0 </roll>
+ <pitch> 2.2 </pitch>
+ <yaw> -1 </yaw>
</orient>
- </thruster>
- </engine>
+ <feed>8</feed>
+ <thruster file="direct">
+ <location unit="IN">
+ <x> 655.4820 </x>
+ <y> 226.575 </y>
+ <z> 0.000 </z>
+ </location>
+ <orient unit="DEG">
+ <roll> 0.0 </roll>
+ <pitch> 2.2 </pitch>
+ <yaw> -1 </yaw>
+ </orient>
+ </thruster>
+ </engine>
- <tank type="FUEL"> <!-- Left Tank (Wing tip Ventilation Surge) 0 -->
- <location unit="IN">
- <x> 783.0709 </x>
- <y> -574.4148 </y>
- <z> 3.1080 </z>
- </location>
- <capacity unit="LBS"> 412 </capacity><!-- 1 percent of total capacity, needs 20C to be filled -->
- <contents unit="LBS"> 0 </contents>
+ <tank type="FUEL"> <!-- Left Tank (Wing tip Ventilation Surge) 0 -->
+ <location unit="IN">
+ <x> 783.0709 </x>
+ <y> -574.4148 </y>
+ <z> 3.1080 </z>
+ </location>
+ <capacity unit="LBS"> 412 </capacity><!-- 1 percent of total capacity, needs 20C to be filled -->
+ <contents unit="LBS"> 0 </contents>
+
+ <priority>0</priority>
+ <type>JET-A1</type>
+ <temperature>50</temperature>
+ </tank>
+ <tank type="FUEL"> <!-- Left Tank (Outer) 1 -->
+ <location unit="IN">
+ <x> 739.5669 </x>
+ <y> -457.4259 </y>
+ <z> -8.0898 </z>
+ </location>
+ <capacity unit="LBS"> 1520.00 </capacity><!-- correct by FCOM -->
+ <contents unit="LBS"> 1520 </contents><!-- outer filled first than inner -->
+ <standpipe unit="LBS">21</standpipe><!-- minimun fuel on pipes -->
+ <priority>2</priority>
+ <type>JET-A1</type>
+ <temperature>50</temperature>
+ </tank>
+ <tank type="FUEL"> <!-- Left Tank (Inner) 2 -->
+ <location unit="IN">
+ <x> 652.5591 </x>
+ <y> -236.2992 </y>
+ <z> -33.9470 </z>
+ </location>
+ <capacity unit="LBS"> 11982 </capacity><!-- correct by FCOM -->
+ <contents unit="LBS"> 4480 </contents>
+ <standpipe unit="LBS">31</standpipe><!-- minimun fuel on pipes -->
+ <priority>3</priority>
+ <type>JET-A1</type>
+ <temperature>50</temperature>
+ </tank>
+ <tank type="FUEL"> <!-- Center Tank 3 -->
+ <location unit="IN">
+ <x> 522.0473 </x>
+ <y> 0 </y>
+ <z> -47.0 </z>
+ </location>
+ <capacity unit="LBS"> 14281 </capacity><!-- correct by FCOM -->
+ <contents unit="LBS"> 0 </contents> <!-- wing tanks filled first -->
+ <standpipe unit="LBS">43</standpipe><!-- minimun fuel on pipes -->
+ <priority>1</priority>
+ <type>JET-A1</type>
+ <temperature>50</temperature>
+ </tank>
+ <tank type="FUEL"> <!-- Right Tank (Inner) 4 -->
+ <location unit="IN">
+ <x> 652.5591 </x>
+ <y> 236.2992 </y>
+ <z> -33.9470 </z>
+ </location>
+ <capacity unit="LBS"> 11982 </capacity><!-- correct by FCOM -->
+ <contents unit="LBS"> 4480 </contents>
+ <standpipe unit="LBS">31</standpipe><!-- minimum fuel on pipes -->
+ <priority>3</priority>
+ <type>JET-A1</type>
+ <temperature>50</temperature>
+ </tank>
+ <tank type="FUEL"> <!-- Right Tank (Outer) 5 -->
+ <location unit="IN">
+ <x> 739.5669 </x>
+ <y> 457.4259 </y>
+ <z> -8.0898 </z>
+ </location>
+ <capacity unit="LBS"> 1520 </capacity><!-- need review -->
+ <contents unit="LBS"> 1520 </contents><!-- outer tank filled first than inner tank -->
+ <standpipe unit="LBS">21</standpipe><!-- minimun fuel on pipes -->
+ <priority>2</priority>
+ <type>JET-A1</type>
+ <temperature>50</temperature>
+ </tank>
+ <tank type="FUEL"> <!-- Right Tank (Wing tip Ventilation Surge) 6 -->
+ <location unit="IN">
+ <x> 783.0709 </x>
+ <y> 574.4148 </y>
+ <z> 3.1080 </z>
+ </location>
+ <capacity unit="LBS"> 412 </capacity><!-- 1 percent of total fuel capacity, needs 20C-->
+ <contents unit="LBS"> 0 </contents>
+ <priority>0</priority>
+ <type>JET-A1</type>
+ <temperature>50</temperature>
+ </tank>
+ <tank type="FUEL"> <!-- LEFT FUEL PIPES (Engine 1 feed from this) -->
+ <location unit="IN">
+ <x>589.735</x>
+ <y>0</y>
+ <z>-45.567</z>
+ </location>
+ <capacity unit="LBS"> 100 </capacity><!-- need review -->
+ <contents unit="LBS"> 0 </contents>
+ <priority>1</priority>
+ <type>JET-A1</type>
+ </tank>
+ <tank type="FUEL"> <!-- RIGHT FUEL PIPES (Engine 2 feed from this) -->
+ <location unit="IN">
+ <x>589.735</x>
+ <y>0</y>
+ <z>-45.567</z>
+ </location>
+ <capacity unit="LBS"> 100 </capacity><!-- need review -->
+ <contents unit="LBS"> 0 </contents>
+ <priority>1</priority>
+ <type>JET-A1</type>
+ </tank>
+ </propulsion>
+
+ <system file="pushback" />
+ <system file="fuel" />
+ <system file="glass-effect1" />
+ <system file="fmgc" />
+ <system file="fcs" />
+
+ <flight_control name="none"/>
- <priority>0</priority>
- <type>JET-A1</type>
- <temperature>50</temperature>
- </tank>
- <tank type="FUEL"> <!-- Left Tank (Outer) 1 -->
- <location unit="IN">
- <x> 739.5669 </x>
- <y> -457.4259 </y>
- <z> -8.0898 </z>
- </location>
- <capacity unit="LBS"> 1520.00 </capacity><!-- correct by FCOM -->
- <contents unit="LBS"> 1520 </contents><!-- outer filled first than inner -->
- <standpipe unit="LBS">21</standpipe><!-- minimun fuel on pipes -->
- <priority>2</priority>
- <type>JET-A1</type>
- <temperature>50</temperature>
- </tank>
- <tank type="FUEL"> <!-- Left Tank (Inner) 2 -->
- <location unit="IN">
- <x> 652.5591 </x>
- <y> -236.2992 </y>
- <z> -33.9470 </z>
- </location>
- <capacity unit="LBS"> 11982 </capacity><!-- correct by FCOM -->
- <contents unit="LBS"> 4480 </contents>
- <standpipe unit="LBS">31</standpipe><!-- minimun fuel on pipes -->
- <priority>3</priority>
- <type>JET-A1</type>
- <temperature>50</temperature>
- </tank>
- <tank type="FUEL"> <!-- Center Tank 3 -->
- <location unit="IN">
- <x> 522.0473 </x>
- <y> 0 </y>
- <z> -47.0 </z>
- </location>
- <capacity unit="LBS"> 14281 </capacity><!-- correct by FCOM -->
- <contents unit="LBS"> 0 </contents> <!-- wing tanks filled first -->
- <standpipe unit="LBS">43</standpipe><!-- minimun fuel on pipes -->
- <priority>1</priority>
- <type>JET-A1</type>
- <temperature>50</temperature>
- </tank>
- <tank type="FUEL"> <!-- Right Tank (Inner) 4 -->
- <location unit="IN">
- <x> 652.5591 </x>
- <y> 236.2992 </y>
- <z> -33.9470 </z>
- </location>
- <capacity unit="LBS"> 11982 </capacity><!-- correct by FCOM -->
- <contents unit="LBS"> 4480 </contents>
- <standpipe unit="LBS">31</standpipe><!-- minimum fuel on pipes -->
- <priority>3</priority>
- <type>JET-A1</type>
- <temperature>50</temperature>
- </tank>
- <tank type="FUEL"> <!-- Right Tank (Outer) 5 -->
- <location unit="IN">
- <x> 739.5669 </x>
- <y> 457.4259 </y>
- <z> -8.0898 </z>
- </location>
- <capacity unit="LBS"> 1520 </capacity><!-- need review -->
- <contents unit="LBS"> 1520 </contents><!-- outer tank filled first than inner tank -->
- <standpipe unit="LBS">21</standpipe><!-- minimun fuel on pipes -->
- <priority>2</priority>
- <type>JET-A1</type>
- <temperature>50</temperature>
- </tank>
- <tank type="FUEL"> <!-- Right Tank (Wing tip Ventilation Surge) 6 -->
- <location unit="IN">
- <x> 783.0709 </x>
- <y> 574.4148 </y>
- <z> 3.1080 </z>
- </location>
- <capacity unit="LBS"> 412 </capacity><!-- 1 percent of total fuel capacity, needs 20C-->
- <contents unit="LBS"> 0 </contents>
- <priority>0</priority>
- <type>JET-A1</type>
- <temperature>50</temperature>
- </tank>
- <tank type="FUEL"> <!-- LEFT FUEL PIPES (Engine 1 feed from this) -->
- <location unit="IN">
- <x>589.735</x>
- <y>-226.575</y>
- <z>-45.567</z>
- </location>
- <capacity unit="LBS"> 100 </capacity><!-- need review -->
- <contents unit="LBS"> 0 </contents>
- <priority>1</priority>
- <type>JET-A1</type>
- </tank>
- <tank type="FUEL"> <!-- RIGHT FUEL PIPES (Engine 2 feed from this) -->
- <location unit="IN">
- <x>589.735</x>
- <y>226.575</y>
- <z>-45.567</z>
- </location>
- <capacity unit="LBS"> 100 </capacity><!-- need review -->
- <contents unit="LBS"> 0 </contents>
- <priority>1</priority>
- <type>JET-A1</type>
- </tank>
-</propulsion>
+ <aerodynamics file="Systems/a320-aerodynamics.xml" />
-<system file="pushback" />
-<system file="fuel" />
-<system file="glass-effect1" />
-<system file="fmgc" />
-<system file="fcs" />
-
-<flight_control name="none"/>
-
-<aerodynamics file="Systems/a320-aerodynamics.xml" />
-
-<external_reactions>
- <force name="pushback" frame="BODY">
- <location unit="IN">
- <x>294</x>
- <y>0</y>
- <z>-149</z>
- </location>
- <direction>
- <x>1</x>
- <y>0</y>
- <z>0</z>
- </direction>
- </force>
-</external_reactions>
+ <external_reactions>
+ <force name="pushback" frame="BODY">
+ <location unit="IN">
+ <x>294</x>
+ <y>0</y>
+ <z>-149</z>
+ </location>
+ <direction>
+ <x>1</x>
+ <y>0</y>
+ <z>0</z>
+ </direction>
+ </force>
+ </external_reactions>
</fdm_config>
diff --git a/A320neo-CFM.xml b/A320neo-CFM.xml
index 039531f8..60d5141c 100644
--- a/A320neo-CFM.xml
+++ b/A320neo-CFM.xml
@@ -4,585 +4,585 @@
xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance"
xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
-<fileheader>
- <author>Joshua Davidson (it0uchpods)</author>
- <version>Pre V1.0</version>
- <description>A3XX FDE</description>
-</fileheader>
+ <fileheader>
+ <author>Joshua Davidson (it0uchpods)</author>
+ <version>Pre V1.0</version>
+ <description>A3XX FDE</description>
+ </fileheader>
-<metrics>
- <wingarea unit="FT2"> 1319.79 </wingarea>
- <wingspan unit="FT" > 111.26 </wingspan>
- <wing_incidence> 1.03 </wing_incidence>
- <chord unit="FT" > 13.76 </chord>
- <htailarea unit="FT2"> 334.24 </htailarea>
- <htailarm unit="FT" > 57.88 </htailarm>
- <vtailarea unit="FT2"> 248.79 </vtailarea>
- <vtailarm unit="FT" > 57.33 </vtailarm>
+ <metrics>
+ <wingarea unit="FT2"> 1319.79 </wingarea>
+ <wingspan unit="FT" > 111.26 </wingspan>
+ <wing_incidence> 1.03 </wing_incidence>
+ <chord unit="FT" > 13.76 </chord>
+ <htailarea unit="FT2"> 334.24 </htailarea>
+ <htailarm unit="FT" > 57.88 </htailarm>
+ <vtailarea unit="FT2"> 248.79 </vtailarea>
+ <vtailarm unit="FT" > 57.33 </vtailarm>
- <location name="AERORP" unit="IN">
- <x> 700.00 </x>
- <y> 0 </y>
- <z> 0.00 </z>
- </location>
+ <location name="AERORP" unit="IN">
+ <x> 700.00 </x>
+ <y> 0 </y>
+ <z> 0.00 </z>
+ </location>
- <location name="EYEPOINT" unit="IN">
- <x> 80 </x>
- <y> -30 </y>
- <z> 70 </z>
- </location>
+ <location name="EYEPOINT" unit="IN">
+ <x> 80 </x>
+ <y> -30 </y>
+ <z> 70 </z>
+ </location>
- <location name="VRP" unit="IN">
- <x> 661.1 </x>
- <y> 0 </y>
- <z> -37 </z>
- </location>
+ <location name="VRP" unit="IN">
+ <x> 661.1 </x>
+ <y> 0 </y>
+ <z> -37 </z>
+ </location>
- </metrics>
+ </metrics>
- <mass_balance>
- <ixx unit="SLUG*FT2"> 611903</ixx>
- <iyy unit="SLUG*FT2">1735389</iyy>
- <izz unit="SLUG*FT2">2301293</izz>
+ <mass_balance>
+ <ixx unit="SLUG*FT2"> 611903</ixx>
+ <iyy unit="SLUG*FT2">1735389</iyy>
+ <izz unit="SLUG*FT2">2301293</izz>
- <ixy unit="SLUG*FT2">0</ixy>
- <ixz unit="SLUG*FT2">0</ixz>
- <iyz unit="SLUG*FT2">0</iyz>
- <emptywt unit="LBS">80431</emptywt>
+ <ixy unit="SLUG*FT2">0</ixy>
+ <ixz unit="SLUG*FT2">0</ixz>
+ <iyz unit="SLUG*FT2">0</iyz>
+ <emptywt unit="LBS">80431</emptywt>
- <location name="CG" unit="IN">
- <x> 652.00 </x>
- <y> 0 </y>
- <z> 0.00 </z>
- </location>
+ <location name="CG" unit="IN">
+ <x> 652.00 </x>
+ <y> 0 </y>
+ <z> 0.00 </z>
+ </location>
- <pointmass name="Cockpit Crew">
- <weight unit="LBS">400</weight>
- <!-- MAX: 400lbs, two pilots-->
- <location name="POINTMASS" unit="IN">
- <x>200</x>
- <y>0</y>
- <z>0</z>
- </location>
- </pointmass>
- <pointmass name="Engine 1">
- <weight unit="LBS">5200.7</weight>
- <location name="POINTMASS" unit="IN">
- <x>530.86</x>
- <y>-5.755</y>
- <z>-78.56019</z>
- </location>
- </pointmass>
- <pointmass name="Engine 2">
- <weight unit="LBS">5200.7</weight>
- <location name="POINTMASS" unit="IN">
- <x>530.86</x>
- <y>5.755</y>
- <z>-78.56019</z>
- </location>
- </pointmass>
- <pointmass name="PAX 0A (60 seats)">
- <weight unit="LBS">6600</weight>
- <!-- MAX: 13200lbs, 60 seats -->
- <location name="POINTMASS" unit="IN">
- <x>470.1711</x>
- <y>0</y>
- <z>0</z>
- </location>
- </pointmass>
- <pointmass name="PAX 0B (60 seats)">
- <weight unit="LBS">6600</weight>
- <!-- MAX: 13200lbs, 60 seats -->
- <location name="POINTMASS" unit="IN">
- <x>809.5669</x>
- <y>0</y>
- <z>0</z>
- </location>
- </pointmass>
- <pointmass name="PAX 0C (54 seats)">
- <weight unit="LBS">5940</weight>
- <!-- MAX: 11880lbs, 54 seats -->
- <location name="POINTMASS" unit="IN">
- <x>1163.2729</x>
- <y>0</y>
- <z>0</z>
- </location>
- </pointmass>
- <pointmass name="Cargo Hold 1">
- <weight unit="LBS">2000</weight>
- <!-- MAX: 7500.126lbs -->
- <location name="POINTMASS" unit="IN">
- <x>383.4792</x>
- <y>0</y>
- <z>-29.5</z>
- <!-- 1.5m and now half of it for the center point of the load -->
- </location>
- </pointmass>
- <!-- Cargo Hold 2 doesn't exist, that is the center tank -->
- <pointmass name="Cargo Hold 3">
- <weight unit="LBS">2000</weight>
- <!-- MAX: 5384.414lbs -->
- <location name="POINTMASS" unit="IN">
- <x>849.1324</x>
- <y>0</y>
- <z>-29.5</z>
- </location>
- </pointmass>
- <pointmass name="Cargo Hold 4">
- <weight unit="LBS">1500</weight>
- <!-- MAX: 4651.754lbs -->
- <location name="POINTMASS" unit="IN">
- <x>931.0653</x>
- <y>0</y>
- <z>-29.5</z>
- </location>
- </pointmass>
- <pointmass name="Cargo Hold 5">
- <weight unit="LBS">2000</weight>
- <!-- MAX: 3300.320lbs -->
- <location name="POINTMASS" unit="IN">
- <x>1068.2634</x>
- <y>0</y>
- <z>0</z>
- <!-- Cargo Hold #5 sits higher on the range of the cabin deck, it's only loadable with lifter -->
- </location>
- </pointmass>
+ <pointmass name="Cockpit Crew">
+ <weight unit="LBS">400</weight>
+ <!-- MAX: 400lbs, two pilots-->
+ <location name="POINTMASS" unit="IN">
+ <x>200</x>
+ <y>0</y>
+ <z>0</z>
+ </location>
+ </pointmass>
+ <pointmass name="Engine 1">
+ <weight unit="LBS">5200.7</weight>
+ <location name="POINTMASS" unit="IN">
+ <x>530.86</x>
+ <y>-5.755</y>
+ <z>-78.56019</z>
+ </location>
+ </pointmass>
+ <pointmass name="Engine 2">
+ <weight unit="LBS">5200.7</weight>
+ <location name="POINTMASS" unit="IN">
+ <x>530.86</x>
+ <y>5.755</y>
+ <z>-78.56019</z>
+ </location>
+ </pointmass>
+ <pointmass name="PAX 0A (60 seats)">
+ <weight unit="LBS">6600</weight>
+ <!-- MAX: 13200lbs, 60 seats -->
+ <location name="POINTMASS" unit="IN">
+ <x>470.1711</x>
+ <y>0</y>
+ <z>0</z>
+ </location>
+ </pointmass>
+ <pointmass name="PAX 0B (60 seats)">
+ <weight unit="LBS">6600</weight>
+ <!-- MAX: 13200lbs, 60 seats -->
+ <location name="POINTMASS" unit="IN">
+ <x>809.5669</x>
+ <y>0</y>
+ <z>0</z>
+ </location>
+ </pointmass>
+ <pointmass name="PAX 0C (54 seats)">
+ <weight unit="LBS">5940</weight>
+ <!-- MAX: 11880lbs, 54 seats -->
+ <location name="POINTMASS" unit="IN">
+ <x>1163.2729</x>
+ <y>0</y>
+ <z>0</z>
+ </location>
+ </pointmass>
+ <pointmass name="Cargo Hold 1">
+ <weight unit="LBS">2000</weight>
+ <!-- MAX: 7500.126lbs -->
+ <location name="POINTMASS" unit="IN">
+ <x>383.4792</x>
+ <y>0</y>
+ <z>-29.5</z>
+ <!-- 1.5m and now half of it for the center point of the load -->
+ </location>
+ </pointmass>
+ <!-- Cargo Hold 2 doesn't exist, that is the center tank -->
+ <pointmass name="Cargo Hold 3">
+ <weight unit="LBS">2000</weight>
+ <!-- MAX: 5384.414lbs -->
+ <location name="POINTMASS" unit="IN">
+ <x>849.1324</x>
+ <y>0</y>
+ <z>-29.5</z>
+ </location>
+ </pointmass>
+ <pointmass name="Cargo Hold 4">
+ <weight unit="LBS">1500</weight>
+ <!-- MAX: 4651.754lbs -->
+ <location name="POINTMASS" unit="IN">
+ <x>931.0653</x>
+ <y>0</y>
+ <z>-29.5</z>
+ </location>
+ </pointmass>
+ <pointmass name="Cargo Hold 5">
+ <weight unit="LBS">2000</weight>
+ <!-- MAX: 3300.320lbs -->
+ <location name="POINTMASS" unit="IN">
+ <x>1068.2634</x>
+ <y>0</y>
+ <z>0</z>
+ <!-- Cargo Hold #5 sits higher on the range of the cabin deck, it's only loadable with lifter -->
+ </location>
+ </pointmass>
- </mass_balance>
+ </mass_balance>
- <ground_reactions>
- <!-- REF-1 page 165 + 271 -->
- <contact type="BOGEY" name="NOSE_LG">
- <location unit="IN">
- <x> 197.6772 </x>
- <y> 0 </y>
- <z> -137.9617 </z>
- </location>
- <static_friction> 0.8 </static_friction>
- <dynamic_friction> 0.5 </dynamic_friction>
- <rolling_friction> 0.02 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 30935.5 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 16978.5 </damping_coeff>
- <max_steer unit="DEG"> 70 </max_steer>
- <!-- REF-1 page 133 -->
- <brake_group> NOSE </brake_group>
- <retractable>1</retractable>
- </contact>
- <contact type="BOGEY" name="LEFT_MLG">
- <location unit="IN">
- <!--<x> 699.9243 </x>-->
- <x> 695.3149 </x>
- <y> -149.4094 </y>
- <z> -150.4824 </z>
- </location>
- <!-- <static_friction> 0.5 </static_friction> WHAT??? less static than dinamyc friction?-->
- <static_friction> 0.8 </static_friction>
- <dynamic_friction> 0.5 </dynamic_friction>
- <rolling_friction> 0.02 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 59785 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 23957 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> LEFT </brake_group>
- <retractable>1</retractable>
- </contact>
- <contact type="BOGEY" name="RIGHT_MLG">
- <location unit="IN">
- <!-- <x> 697.3425 </x> It should be right left simetric
- <x> 699.9243 </x> -->
- <x> 695.3149 </x>
- <y> 149.4094 </y>
- <z> -150.4824 </z>
- </location>
- <!-- <static_friction> 0.5 </static_friction> WHAT??? less static than dinamyc friction?-->
- <static_friction> 0.8 </static_friction>
- <dynamic_friction> 0.5 </dynamic_friction>
- <rolling_friction> 0.02 </rolling_friction>
- <!--spring_coeff unit="LBS/FT"> 169785 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 33957 </damping_coeff-->
- <spring_coeff unit="LBS/FT"> 59785 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 23957 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> RIGHT </brake_group>
- <retractable>1</retractable>
- </contact>
+ <ground_reactions>
+ <!-- REF-1 page 165 + 271 -->
+ <contact type="BOGEY" name="NOSE_LG">
+ <location unit="IN">
+ <x> 197.6772 </x>
+ <y> 0 </y>
+ <z> -137.9617 </z>
+ </location>
+ <static_friction> 0.8 </static_friction>
+ <dynamic_friction> 0.5 </dynamic_friction>
+ <rolling_friction> 0.02 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 30935.5 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 16978.5 </damping_coeff>
+ <max_steer unit="DEG"> 70 </max_steer>
+ <!-- REF-1 page 133 -->
+ <brake_group> NOSE </brake_group>
+ <retractable>1</retractable>
+ </contact>
+ <contact type="BOGEY" name="LEFT_MLG">
+ <location unit="IN">
+ <!--<x> 699.9243 </x>-->
+ <x> 695.3149 </x>
+ <y> -149.4094 </y>
+ <z> -150.4824 </z>
+ </location>
+ <!-- <static_friction> 0.5 </static_friction> WHAT??? less static than dinamyc friction?-->
+ <static_friction> 0.8 </static_friction>
+ <dynamic_friction> 0.5 </dynamic_friction>
+ <rolling_friction> 0.02 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 59785 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 23957 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> LEFT </brake_group>
+ <retractable>1</retractable>
+ </contact>
+ <contact type="BOGEY" name="RIGHT_MLG">
+ <location unit="IN">
+ <!-- <x> 697.3425 </x> It should be right left simetric
+ <x> 699.9243 </x> -->
+ <x> 695.3149 </x>
+ <y> 149.4094 </y>
+ <z> -150.4824 </z>
+ </location>
+ <!-- <static_friction> 0.5 </static_friction> WHAT??? less static than dinamyc friction?-->
+ <static_friction> 0.8 </static_friction>
+ <dynamic_friction> 0.5 </dynamic_friction>
+ <rolling_friction> 0.02 </rolling_friction>
+ <!--spring_coeff unit="LBS/FT"> 169785 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 33957 </damping_coeff-->
+ <spring_coeff unit="LBS/FT"> 59785 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 23957 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> RIGHT </brake_group>
+ <retractable>1</retractable>
+ </contact>
- <contact type="STRUCTURE" name="NOSE_1">
- <location unit="IN">
- <x> 37.7953 </x>
- <y> 0 </y>
- <z> -38.1374 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="NOSE_2">
- <location unit="IN">
- <x> 128.1102 </x>
- <y> 0 </y>
- <z> -55.0271 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="CENTER_1">
- <location unit="IN">
- <x> 274.0157 </x>
- <y> 0 </y>
- <z> -60.0665 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="CENTER_2">
- <location unit="IN">
- <x> 930 </x>
- <y> 0 </y>
- <z> -60.0665 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
+ <contact type="STRUCTURE" name="NOSE_1">
+ <location unit="IN">
+ <x> 37.7953 </x>
+ <y> 0 </y>
+ <z> -38.1374 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="NOSE_2">
+ <location unit="IN">
+ <x> 128.1102 </x>
+ <y> 0 </y>
+ <z> -55.0271 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="CENTER_1">
+ <location unit="IN">
+ <x> 274.0157 </x>
+ <y> 0 </y>
+ <z> -60.0665 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="CENTER_2">
+ <location unit="IN">
+ <x> 930 </x>
+ <y> 0 </y>
+ <z> -60.0665 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
- <contact type="STRUCTURE" name="ENG_1">
- <location unit="IN">
- <x>589.735</x>
- <y>-226.575</y>
- <z>-95.567</z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="ENG_2">
- <location unit="IN">
- <x>589.735</x>
- <y>226.575</y>
- <z>-95.567</z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.5 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
+ <contact type="STRUCTURE" name="ENG_1">
+ <location unit="IN">
+ <x>589.735</x>
+ <y>-226.575</y>
+ <z>-95.567</z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="ENG_2">
+ <location unit="IN">
+ <x>589.735</x>
+ <y>226.575</y>
+ <z>-95.567</z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.5 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
- <contact type="STRUCTURE" name="TAIL_1">
- <location unit="IN">
- <x> 1097.9921 </x>
- <y> 0 </y>
- <z> -44.7722 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="TAIL_2">
- <location unit="IN">
- <x> 1225 </x>
- <y> 0 </y>
- <z> -18.8067 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="TAIL_3">
- <location unit="IN">
- <x> 1341.6142 </x>
- <y> 0 </y>
- <z> -10.2599 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="TAIL_4">
- <location unit="IN">
- <x> 1469.0945 </x>
- <y> 0 </y>
- <z> 47.4138 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 1 </dynamic_friction>
- <rolling_friction> 1 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="WING_TIP_1">
- <location unit="IN">
- <x> 838.8898 </x>
- <y> -667.5197 </y>
- <z> 35.7926 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="WING_TIP_2">
- <location unit="IN">
- <x> 838.8898 </x>
- <y> 667.5197 </y>
- <z> 35.7926 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 1 </dynamic_friction>
- <rolling_friction> 1 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- </ground_reactions>
+ <contact type="STRUCTURE" name="TAIL_1">
+ <location unit="IN">
+ <x> 1097.9921 </x>
+ <y> 0 </y>
+ <z> -44.7722 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="TAIL_2">
+ <location unit="IN">
+ <x> 1225 </x>
+ <y> 0 </y>
+ <z> -18.8067 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="TAIL_3">
+ <location unit="IN">
+ <x> 1341.6142 </x>
+ <y> 0 </y>
+ <z> -10.2599 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="TAIL_4">
+ <location unit="IN">
+ <x> 1469.0945 </x>
+ <y> 0 </y>
+ <z> 47.4138 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 1 </dynamic_friction>
+ <rolling_friction> 1 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="WING_TIP_1">
+ <location unit="IN">
+ <x> 838.8898 </x>
+ <y> -667.5197 </y>
+ <z> 35.7926 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="WING_TIP_2">
+ <location unit="IN">
+ <x> 838.8898 </x>
+ <y> 667.5197 </y>
+ <z> 35.7926 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 1 </dynamic_friction>
+ <rolling_friction> 1 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ </ground_reactions>
-<propulsion>
+ <propulsion>
- <engine file="leap1a26">
- <location unit="IN">
- <x> 620.0683 </x>
- <y> -226.575 </y>
- <z> -45.567 </z>
- </location>
- <orient unit="DEG">
- <roll> 0.0 </roll>
- <pitch> 2.2 </pitch>
- <yaw> 1 </yaw>
- </orient>
- <feed>7</feed>
- <thruster file="direct">
+ <engine file="leap1a26">
<location unit="IN">
- <x> 655.4820 </x>
- <y> -226.575 </y>
- <z> 0.000 </z>
+ <x> 620.0683 </x>
+ <y> -226.575 </y>
+ <z> -45.567 </z>
</location>
<orient unit="DEG">
- <roll> 0.0 </roll>
- <pitch> 2.2 </pitch>
- <yaw> 1 </yaw>
+ <roll> 0.0 </roll>
+ <pitch> 2.2 </pitch>
+ <yaw> 1 </yaw>
</orient>
- </thruster>
- </engine>
+ <feed>7</feed>
+ <thruster file="direct">
+ <location unit="IN">
+ <x> 655.4820 </x>
+ <y> -226.575 </y>
+ <z> 0.000 </z>
+ </location>
+ <orient unit="DEG">
+ <roll> 0.0 </roll>
+ <pitch> 2.2 </pitch>
+ <yaw> 1 </yaw>
+ </orient>
+ </thruster>
+ </engine>
- <engine file="leap1a26">
- <location unit="IN">
- <x> 620.0683 </x>
- <y> 226.575 </y>
- <z> -45.567 </z>
- </location>
- <orient unit="DEG">
- <roll> 0.0 </roll>
- <pitch> 2.2 </pitch>
- <yaw> -1 </yaw>
- </orient>
- <feed>8</feed>
- <thruster file="direct">
+ <engine file="leap1a26">
<location unit="IN">
- <x> 655.4820 </x>
- <y> 226.575 </y>
- <z> 0.000 </z>
+ <x> 620.0683 </x>
+ <y> 226.575 </y>
+ <z> -45.567 </z>
</location>
<orient unit="DEG">
- <roll> 0.0 </roll>
- <pitch> 2.2 </pitch>
- <yaw> -1 </yaw>
+ <roll> 0.0 </roll>
+ <pitch> 2.2 </pitch>
+ <yaw> -1 </yaw>
</orient>
- </thruster>
- </engine>
+ <feed>8</feed>
+ <thruster file="direct">
+ <location unit="IN">
+ <x> 655.4820 </x>
+ <y> 226.575 </y>
+ <z> 0.000 </z>
+ </location>
+ <orient unit="DEG">
+ <roll> 0.0 </roll>
+ <pitch> 2.2 </pitch>
+ <yaw> -1 </yaw>
+ </orient>
+ </thruster>
+ </engine>
- <tank type="FUEL"> <!-- Left Tank (Wing tip Ventilation Surge) 0 -->
- <location unit="IN">
- <x> 783.0709 </x>
- <y> -574.4148 </y>
- <z> 3.1080 </z>
- </location>
- <capacity unit="LBS"> 412 </capacity><!-- 1 percent of total capacity, needs 20C to be filled -->
- <contents unit="LBS"> 0 </contents>
-
- <priority>4</priority>
- <type>JET-A1</type>
- <temperature>50</temperature>
- </tank>
- <tank type="FUEL"> <!-- Left Tank (Outer) 1 -->
- <location unit="IN">
- <x> 739.5669 </x>
- <y> -457.4259 </y>
- <z> -8.0898 </z>
- </location>
- <capacity unit="LBS"> 1520.00 </capacity><!-- correct by FCOM -->
- <contents unit="LBS"> 1520 </contents><!-- outer filled first than inner -->
- <standpipe unit="LBS">21</standpipe><!-- minimun fuel on pipes -->
- <priority>2</priority>
- <type>JET-A1</type>
- <temperature>50</temperature>
- </tank>
- <tank type="FUEL"> <!-- Left Tank (Inner) 2 -->
- <location unit="IN">
- <x> 652.5591 </x>
- <y> -236.2992 </y>
- <z> -33.9470 </z>
- </location>
- <capacity unit="LBS"> 11982 </capacity><!-- correct by FCOM -->
- <contents unit="LBS"> 4480 </contents>
- <standpipe unit="LBS">31</standpipe><!-- minimun fuel on pipes -->
- <priority>3</priority>
- <type>JET-A1</type>
- <temperature>50</temperature>
- </tank>
- <tank type="FUEL"> <!-- Center Tank 3 -->
- <location unit="IN">
- <x> 522.0473 </x>
- <y> 0 </y>
- <z> -47.0 </z>
- </location>
- <capacity unit="LBS"> 14281 </capacity><!-- correct by FCOM -->
- <contents unit="LBS"> 0 </contents> <!-- wing tanks filled first -->
- <standpipe unit="LBS">43</standpipe><!-- minimun fuel on pipes -->
- <priority>1</priority>
- <type>JET-A1</type>
- <temperature>50</temperature>
- </tank>
- <tank type="FUEL"> <!-- Right Tank (Inner) 4 -->
- <location unit="IN">
- <x> 652.5591 </x>
- <y> 236.2992 </y>
- <z> -33.9470 </z>
- </location>
- <capacity unit="LBS"> 11982 </capacity><!-- correct by FCOM -->
- <contents unit="LBS"> 4480 </contents>
- <standpipe unit="LBS">31</standpipe><!-- minimum fuel on pipes -->
- <priority>3</priority>
- <type>JET-A1</type>
- <temperature>50</temperature>
- </tank>
- <tank type="FUEL"> <!-- Right Tank (Outer) 5 -->
- <location unit="IN">
- <x> 739.5669 </x>
- <y> 457.4259 </y>
- <z> -8.0898 </z>
- </location>
- <capacity unit="LBS"> 1520 </capacity><!-- need review -->
- <contents unit="LBS"> 1520 </contents><!-- outer tank filled first than inner tank -->
- <standpipe unit="LBS">21</standpipe><!-- minimun fuel on pipes -->
- <priority>2</priority>
- <type>JET-A1</type>
- <temperature>50</temperature>
- </tank>
- <tank type="FUEL"> <!-- Right Tank (Wing tip Ventilation Surge) 6 -->
- <location unit="IN">
- <x> 783.0709 </x>
- <y> 574.4148 </y>
- <z> 3.1080 </z>
- </location>
- <capacity unit="LBS"> 412 </capacity><!-- 1 percent of total fuel capacity, needs 20C-->
- <contents unit="LBS"> 0 </contents>
- <priority>4</priority>
- <type>JET-A1</type>
- <temperature>50</temperature>
- </tank>
- <tank type="FUEL"> <!-- LEFT FUEL PIPES (Engine 1 feed from this) -->
- <location unit="IN">
- <x>589.735</x>
- <y>-226.575</y>
- <z>-45.567</z>
- </location>
- <capacity unit="LBS"> 100 </capacity><!-- need review -->
- <contents unit="LBS"> 0 </contents>
- <priority>1</priority>
- <type>JET-A1</type>
- </tank>
- <tank type="FUEL"> <!-- RIGHT FUEL PIPES (Engine 2 feed from this) -->
- <location unit="IN">
- <x>589.735</x>
- <y>226.575</y>
- <z>-45.567</z>
- </location>
- <capacity unit="LBS"> 100 </capacity><!-- need review -->
- <contents unit="LBS"> 0 </contents>
- <priority>1</priority>
- <type>JET-A1</type>
- </tank>
-</propulsion>
+ <tank type="FUEL"> <!-- Left Tank (Wing tip Ventilation Surge) 0 -->
+ <location unit="IN">
+ <x> 783.0709 </x>
+ <y> -574.4148 </y>
+ <z> 3.1080 </z>
+ </location>
+ <capacity unit="LBS"> 412 </capacity><!-- 1 percent of total capacity, needs 20C to be filled -->
+ <contents unit="LBS"> 0 </contents>
+
+ <priority>4</priority>
+ <type>JET-A1</type>
+ <temperature>50</temperature>
+ </tank>
+ <tank type="FUEL"> <!-- Left Tank (Outer) 1 -->
+ <location unit="IN">
+ <x> 739.5669 </x>
+ <y> -457.4259 </y>
+ <z> -8.0898 </z>
+ </location>
+ <capacity unit="LBS"> 1520.00 </capacity><!-- correct by FCOM -->
+ <contents unit="LBS"> 1520 </contents><!-- outer filled first than inner -->
+ <standpipe unit="LBS">21</standpipe><!-- minimun fuel on pipes -->
+ <priority>2</priority>
+ <type>JET-A1</type>
+ <temperature>50</temperature>
+ </tank>
+ <tank type="FUEL"> <!-- Left Tank (Inner) 2 -->
+ <location unit="IN">
+ <x> 652.5591 </x>
+ <y> -236.2992 </y>
+ <z> -33.9470 </z>
+ </location>
+ <capacity unit="LBS"> 11982 </capacity><!-- correct by FCOM -->
+ <contents unit="LBS"> 4480 </contents>
+ <standpipe unit="LBS">31</standpipe><!-- minimun fuel on pipes -->
+ <priority>3</priority>
+ <type>JET-A1</type>
+ <temperature>50</temperature>
+ </tank>
+ <tank type="FUEL"> <!-- Center Tank 3 -->
+ <location unit="IN">
+ <x> 522.0473 </x>
+ <y> 0 </y>
+ <z> -47.0 </z>
+ </location>
+ <capacity unit="LBS"> 14281 </capacity><!-- correct by FCOM -->
+ <contents unit="LBS"> 0 </contents> <!-- wing tanks filled first -->
+ <standpipe unit="LBS">43</standpipe><!-- minimun fuel on pipes -->
+ <priority>1</priority>
+ <type>JET-A1</type>
+ <temperature>50</temperature>
+ </tank>
+ <tank type="FUEL"> <!-- Right Tank (Inner) 4 -->
+ <location unit="IN">
+ <x> 652.5591 </x>
+ <y> 236.2992 </y>
+ <z> -33.9470 </z>
+ </location>
+ <capacity unit="LBS"> 11982 </capacity><!-- correct by FCOM -->
+ <contents unit="LBS"> 4480 </contents>
+ <standpipe unit="LBS">31</standpipe><!-- minimum fuel on pipes -->
+ <priority>3</priority>
+ <type>JET-A1</type>
+ <temperature>50</temperature>
+ </tank>
+ <tank type="FUEL"> <!-- Right Tank (Outer) 5 -->
+ <location unit="IN">
+ <x> 739.5669 </x>
+ <y> 457.4259 </y>
+ <z> -8.0898 </z>
+ </location>
+ <capacity unit="LBS"> 1520 </capacity><!-- need review -->
+ <contents unit="LBS"> 1520 </contents><!-- outer tank filled first than inner tank -->
+ <standpipe unit="LBS">21</standpipe><!-- minimun fuel on pipes -->
+ <priority>2</priority>
+ <type>JET-A1</type>
+ <temperature>50</temperature>
+ </tank>
+ <tank type="FUEL"> <!-- Right Tank (Wing tip Ventilation Surge) 6 -->
+ <location unit="IN">
+ <x> 783.0709 </x>
+ <y> 574.4148 </y>
+ <z> 3.1080 </z>
+ </location>
+ <capacity unit="LBS"> 412 </capacity><!-- 1 percent of total fuel capacity, needs 20C-->
+ <contents unit="LBS"> 0 </contents>
+ <priority>4</priority>
+ <type>JET-A1</type>
+ <temperature>50</temperature>
+ </tank>
+ <tank type="FUEL"> <!-- LEFT FUEL PIPES (Engine 1 feed from this) -->
+ <location unit="IN">
+ <x>589.735</x>
+ <y>0</y>
+ <z>-45.567</z>
+ </location>
+ <capacity unit="LBS"> 100 </capacity><!-- need review -->
+ <contents unit="LBS"> 0 </contents>
+ <priority>1</priority>
+ <type>JET-A1</type>
+ </tank>
+ <tank type="FUEL"> <!-- RIGHT FUEL PIPES (Engine 2 feed from this) -->
+ <location unit="IN">
+ <x>589.735</x>
+ <y>0</y>
+ <z>-45.567</z>
+ </location>
+ <capacity unit="LBS"> 100 </capacity><!-- need review -->
+ <contents unit="LBS"> 0 </contents>
+ <priority>1</priority>
+ <type>JET-A1</type>
+ </tank>
+ </propulsion>
-<system file="pushback" />
-<system file="fuel" />
-<system file="glass-effect1" />
-<system file="fmgc" />
-<system file="fcs" />
+ <system file="pushback" />
+ <system file="fuel" />
+ <system file="glass-effect1" />
+ <system file="fmgc" />
+ <system file="fcs" />
-<flight_control name="none"/>
+ <flight_control name="none"/>
-<aerodynamics file="Systems/a320-aerodynamics.xml" />
+ <aerodynamics file="Systems/a320-aerodynamics.xml" />
-<external_reactions>
- <force name="pushback" frame="BODY">
- <location unit="IN">
- <x>294</x>
- <y>0</y>
- <z>-149</z>
- </location>
- <direction>
- <x>1</x>
- <y>0</y>
- <z>0</z>
- </direction>
- </force>
-</external_reactions>
+ <external_reactions>
+ <force name="pushback" frame="BODY">
+ <location unit="IN">
+ <x>294</x>
+ <y>0</y>
+ <z>-149</z>
+ </location>
+ <direction>
+ <x>1</x>
+ <y>0</y>
+ <z>0</z>
+ </direction>
+ </force>
+ </external_reactions>
</fdm_config>
diff --git a/A321-200-CFM.xml b/A321-200-CFM.xml
index 2673fddd..f1e7ff04 100644
--- a/A321-200-CFM.xml
+++ b/A321-200-CFM.xml
@@ -4,585 +4,585 @@
xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance"
xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
-<fileheader>
- <author>Joshua Davidson (it0uchpods)</author>
- <version>Pre V1.0</version>
- <description>A3XX FDE</description>
-</fileheader>
+ <fileheader>
+ <author>Joshua Davidson (it0uchpods)</author>
+ <version>Pre V1.0</version>
+ <description>A3XX FDE</description>
+ </fileheader>
-<metrics>
- <wingarea unit="FT2"> 1319.79 </wingarea>
- <wingspan unit="FT" > 111.26 </wingspan>
- <wing_incidence> 1.03 </wing_incidence>
- <chord unit="FT" > 13.76 </chord>
- <htailarea unit="FT2"> 334.24 </htailarea>
- <htailarm unit="FT" > 57.88 </htailarm>
- <vtailarea unit="FT2"> 248.79 </vtailarea>
- <vtailarm unit="FT" > 57.33 </vtailarm>
+ <metrics>
+ <wingarea unit="FT2"> 1319.79 </wingarea>
+ <wingspan unit="FT" > 111.26 </wingspan>
+ <wing_incidence> 1.03 </wing_incidence>
+ <chord unit="FT" > 13.76 </chord>
+ <htailarea unit="FT2"> 334.24 </htailarea>
+ <htailarm unit="FT" > 57.88 </htailarm>
+ <vtailarea unit="FT2"> 248.79 </vtailarea>
+ <vtailarm unit="FT" > 57.33 </vtailarm>
- <location name="AERORP" unit="IN">
- <x> 700.00 </x>
- <y> 0 </y>
- <z> 0.00 </z>
- </location>
+ <location name="AERORP" unit="IN">
+ <x> 700.00 </x>
+ <y> 0 </y>
+ <z> 0.00 </z>
+ </location>
- <location name="EYEPOINT" unit="IN">
- <x> 80 </x>
- <y> -30 </y>
- <z> 70 </z>
- </location>
+ <location name="EYEPOINT" unit="IN">
+ <x> 80 </x>
+ <y> -30 </y>
+ <z> 70 </z>
+ </location>
- <location name="VRP" unit="IN">
- <x> 661.1 </x>
- <y> 0 </y>
- <z> -37 </z>
- </location>
+ <location name="VRP" unit="IN">
+ <x> 661.1 </x>
+ <y> 0 </y>
+ <z> -37 </z>
+ </location>
- </metrics>
+ </metrics>
- <mass_balance>
- <ixx unit="SLUG*FT2"> 611903</ixx>
- <iyy unit="SLUG*FT2">1735389</iyy>
- <izz unit="SLUG*FT2">2301293</izz>
+ <mass_balance>
+ <ixx unit="SLUG*FT2"> 611903</ixx>
+ <iyy unit="SLUG*FT2">1735389</iyy>
+ <izz unit="SLUG*FT2">2301293</izz>
- <ixy unit="SLUG*FT2">0</ixy>
- <ixz unit="SLUG*FT2">0</ixz>
- <iyz unit="SLUG*FT2">0</iyz>
- <emptywt unit="LBS">80431</emptywt>
+ <ixy unit="SLUG*FT2">0</ixy>
+ <ixz unit="SLUG*FT2">0</ixz>
+ <iyz unit="SLUG*FT2">0</iyz>
+ <emptywt unit="LBS">80431</emptywt>
- <location name="CG" unit="IN">
- <x> 652.00 </x>
- <y> 0 </y>
- <z> 0.00 </z>
- </location>
+ <location name="CG" unit="IN">
+ <x> 652.00 </x>
+ <y> 0 </y>
+ <z> 0.00 </z>
+ </location>
- <pointmass name="Cockpit Crew">
- <weight unit="LBS">400</weight>
- <!-- MAX: 400lbs, two pilots-->
- <location name="POINTMASS" unit="IN">
- <x>200</x>
- <y>0</y>
- <z>0</z>
- </location>
- </pointmass>
- <pointmass name="Engine 1">
- <weight unit="LBS">5200.7</weight>
- <location name="POINTMASS" unit="IN">
- <x>530.86</x>
- <y>-5.755</y>
- <z>-78.56019</z>
- </location>
- </pointmass>
- <pointmass name="Engine 2">
- <weight unit="LBS">5200.7</weight>
- <location name="POINTMASS" unit="IN">
- <x>530.86</x>
- <y>5.755</y>
- <z>-78.56019</z>
- </location>
- </pointmass>
- <pointmass name="PAX 0A (60 seats)">
- <weight unit="LBS">6600</weight>
- <!-- MAX: 13200lbs, 60 seats -->
- <location name="POINTMASS" unit="IN">
- <x>470.1711</x>
- <y>0</y>
- <z>0</z>
- </location>
- </pointmass>
- <pointmass name="PAX 0B (60 seats)">
- <weight unit="LBS">6600</weight>
- <!-- MAX: 13200lbs, 60 seats -->
- <location name="POINTMASS" unit="IN">
- <x>809.5669</x>
- <y>0</y>
- <z>0</z>
- </location>
- </pointmass>
- <pointmass name="PAX 0C (54 seats)">
- <weight unit="LBS">5940</weight>
- <!-- MAX: 11880lbs, 54 seats -->
- <location name="POINTMASS" unit="IN">
- <x>1163.2729</x>
- <y>0</y>
- <z>0</z>
- </location>
- </pointmass>
- <pointmass name="Cargo Hold 1">
- <weight unit="LBS">2000</weight>
- <!-- MAX: 7500.126lbs -->
- <location name="POINTMASS" unit="IN">
- <x>383.4792</x>
- <y>0</y>
- <z>-29.5</z>
- <!-- 1.5m and now half of it for the center point of the load -->
- </location>
- </pointmass>
- <!-- Cargo Hold 2 doesn't exist, that is the center tank -->
- <pointmass name="Cargo Hold 3">
- <weight unit="LBS">2000</weight>
- <!-- MAX: 5384.414lbs -->
- <location name="POINTMASS" unit="IN">
- <x>849.1324</x>
- <y>0</y>
- <z>-29.5</z>
- </location>
- </pointmass>
- <pointmass name="Cargo Hold 4">
- <weight unit="LBS">1500</weight>
- <!-- MAX: 4651.754lbs -->
- <location name="POINTMASS" unit="IN">
- <x>931.0653</x>
- <y>0</y>
- <z>-29.5</z>
- </location>
- </pointmass>
- <pointmass name="Cargo Hold 5">
- <weight unit="LBS">2000</weight>
- <!-- MAX: 3300.320lbs -->
- <location name="POINTMASS" unit="IN">
- <x>1068.2634</x>
- <y>0</y>
- <z>0</z>
- <!-- Cargo Hold #5 sits higher on the range of the cabin deck, it's only loadable with lifter -->
- </location>
- </pointmass>
+ <pointmass name="Cockpit Crew">
+ <weight unit="LBS">400</weight>
+ <!-- MAX: 400lbs, two pilots-->
+ <location name="POINTMASS" unit="IN">
+ <x>200</x>
+ <y>0</y>
+ <z>0</z>
+ </location>
+ </pointmass>
+ <pointmass name="Engine 1">
+ <weight unit="LBS">5200.7</weight>
+ <location name="POINTMASS" unit="IN">
+ <x>530.86</x>
+ <y>-5.755</y>
+ <z>-78.56019</z>
+ </location>
+ </pointmass>
+ <pointmass name="Engine 2">
+ <weight unit="LBS">5200.7</weight>
+ <location name="POINTMASS" unit="IN">
+ <x>530.86</x>
+ <y>5.755</y>
+ <z>-78.56019</z>
+ </location>
+ </pointmass>
+ <pointmass name="PAX 0A (60 seats)">
+ <weight unit="LBS">6600</weight>
+ <!-- MAX: 13200lbs, 60 seats -->
+ <location name="POINTMASS" unit="IN">
+ <x>470.1711</x>
+ <y>0</y>
+ <z>0</z>
+ </location>
+ </pointmass>
+ <pointmass name="PAX 0B (60 seats)">
+ <weight unit="LBS">6600</weight>
+ <!-- MAX: 13200lbs, 60 seats -->
+ <location name="POINTMASS" unit="IN">
+ <x>809.5669</x>
+ <y>0</y>
+ <z>0</z>
+ </location>
+ </pointmass>
+ <pointmass name="PAX 0C (54 seats)">
+ <weight unit="LBS">5940</weight>
+ <!-- MAX: 11880lbs, 54 seats -->
+ <location name="POINTMASS" unit="IN">
+ <x>1163.2729</x>
+ <y>0</y>
+ <z>0</z>
+ </location>
+ </pointmass>
+ <pointmass name="Cargo Hold 1">
+ <weight unit="LBS">2000</weight>
+ <!-- MAX: 7500.126lbs -->
+ <location name="POINTMASS" unit="IN">
+ <x>383.4792</x>
+ <y>0</y>
+ <z>-29.5</z>
+ <!-- 1.5m and now half of it for the center point of the load -->
+ </location>
+ </pointmass>
+ <!-- Cargo Hold 2 doesn't exist, that is the center tank -->
+ <pointmass name="Cargo Hold 3">
+ <weight unit="LBS">2000</weight>
+ <!-- MAX: 5384.414lbs -->
+ <location name="POINTMASS" unit="IN">
+ <x>849.1324</x>
+ <y>0</y>
+ <z>-29.5</z>
+ </location>
+ </pointmass>
+ <pointmass name="Cargo Hold 4">
+ <weight unit="LBS">1500</weight>
+ <!-- MAX: 4651.754lbs -->
+ <location name="POINTMASS" unit="IN">
+ <x>931.0653</x>
+ <y>0</y>
+ <z>-29.5</z>
+ </location>
+ </pointmass>
+ <pointmass name="Cargo Hold 5">
+ <weight unit="LBS">2000</weight>
+ <!-- MAX: 3300.320lbs -->
+ <location name="POINTMASS" unit="IN">
+ <x>1068.2634</x>
+ <y>0</y>
+ <z>0</z>
+ <!-- Cargo Hold #5 sits higher on the range of the cabin deck, it's only loadable with lifter -->
+ </location>
+ </pointmass>
- </mass_balance>
+ </mass_balance>
- <ground_reactions>
- <!-- REF-1 page 165 + 271 -->
- <contact type="BOGEY" name="NOSE_LG">
- <location unit="IN">
- <x> 197.6772 </x>
- <y> 0 </y>
- <z> -137.9617 </z>
- </location>
- <static_friction> 0.8 </static_friction>
- <dynamic_friction> 0.5 </dynamic_friction>
- <rolling_friction> 0.02 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 30935.5 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 16978.5 </damping_coeff>
- <max_steer unit="DEG"> 70 </max_steer>
- <!-- REF-1 page 133 -->
- <brake_group> NOSE </brake_group>
- <retractable>1</retractable>
- </contact>
- <contact type="BOGEY" name="LEFT_MLG">
- <location unit="IN">
- <!--<x> 699.9243 </x>-->
- <x> 695.3149 </x>
- <y> -149.4094 </y>
- <z> -150.4824 </z>
- </location>
- <!-- <static_friction> 0.5 </static_friction> WHAT??? less static than dinamyc friction?-->
- <static_friction> 0.8 </static_friction>
- <dynamic_friction> 0.5 </dynamic_friction>
- <rolling_friction> 0.02 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 59785 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 23957 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> LEFT </brake_group>
- <retractable>1</retractable>
- </contact>
- <contact type="BOGEY" name="RIGHT_MLG">
- <location unit="IN">
- <!-- <x> 697.3425 </x> It should be right left simetric
- <x> 699.9243 </x> -->
- <x> 695.3149 </x>
- <y> 149.4094 </y>
- <z> -150.4824 </z>
- </location>
- <!-- <static_friction> 0.5 </static_friction> WHAT??? less static than dinamyc friction?-->
- <static_friction> 0.8 </static_friction>
- <dynamic_friction> 0.5 </dynamic_friction>
- <rolling_friction> 0.02 </rolling_friction>
- <!--spring_coeff unit="LBS/FT"> 169785 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 33957 </damping_coeff-->
- <spring_coeff unit="LBS/FT"> 59785 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 23957 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> RIGHT </brake_group>
- <retractable>1</retractable>
- </contact>
+ <ground_reactions>
+ <!-- REF-1 page 165 + 271 -->
+ <contact type="BOGEY" name="NOSE_LG">
+ <location unit="IN">
+ <x> 197.6772 </x>
+ <y> 0 </y>
+ <z> -137.9617 </z>
+ </location>
+ <static_friction> 0.8 </static_friction>
+ <dynamic_friction> 0.5 </dynamic_friction>
+ <rolling_friction> 0.02 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 30935.5 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 16978.5 </damping_coeff>
+ <max_steer unit="DEG"> 70 </max_steer>
+ <!-- REF-1 page 133 -->
+ <brake_group> NOSE </brake_group>
+ <retractable>1</retractable>
+ </contact>
+ <contact type="BOGEY" name="LEFT_MLG">
+ <location unit="IN">
+ <!--<x> 699.9243 </x>-->
+ <x> 695.3149 </x>
+ <y> -149.4094 </y>
+ <z> -150.4824 </z>
+ </location>
+ <!-- <static_friction> 0.5 </static_friction> WHAT??? less static than dinamyc friction?-->
+ <static_friction> 0.8 </static_friction>
+ <dynamic_friction> 0.5 </dynamic_friction>
+ <rolling_friction> 0.02 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 59785 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 23957 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> LEFT </brake_group>
+ <retractable>1</retractable>
+ </contact>
+ <contact type="BOGEY" name="RIGHT_MLG">
+ <location unit="IN">
+ <!-- <x> 697.3425 </x> It should be right left simetric
+ <x> 699.9243 </x> -->
+ <x> 695.3149 </x>
+ <y> 149.4094 </y>
+ <z> -150.4824 </z>
+ </location>
+ <!-- <static_friction> 0.5 </static_friction> WHAT??? less static than dinamyc friction?-->
+ <static_friction> 0.8 </static_friction>
+ <dynamic_friction> 0.5 </dynamic_friction>
+ <rolling_friction> 0.02 </rolling_friction>
+ <!--spring_coeff unit="LBS/FT"> 169785 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 33957 </damping_coeff-->
+ <spring_coeff unit="LBS/FT"> 59785 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 23957 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> RIGHT </brake_group>
+ <retractable>1</retractable>
+ </contact>
- <contact type="STRUCTURE" name="NOSE_1">
- <location unit="IN">
- <x> 37.7953 </x>
- <y> 0 </y>
- <z> -38.1374 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="NOSE_2">
- <location unit="IN">
- <x> 128.1102 </x>
- <y> 0 </y>
- <z> -55.0271 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="CENTER_1">
- <location unit="IN">
- <x> 274.0157 </x>
- <y> 0 </y>
- <z> -60.0665 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="CENTER_2">
- <location unit="IN">
- <x> 930 </x>
- <y> 0 </y>
- <z> -60.0665 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
+ <contact type="STRUCTURE" name="NOSE_1">
+ <location unit="IN">
+ <x> 37.7953 </x>
+ <y> 0 </y>
+ <z> -38.1374 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="NOSE_2">
+ <location unit="IN">
+ <x> 128.1102 </x>
+ <y> 0 </y>
+ <z> -55.0271 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="CENTER_1">
+ <location unit="IN">
+ <x> 274.0157 </x>
+ <y> 0 </y>
+ <z> -60.0665 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="CENTER_2">
+ <location unit="IN">
+ <x> 930 </x>
+ <y> 0 </y>
+ <z> -60.0665 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
- <contact type="STRUCTURE" name="ENG_1">
- <location unit="IN">
- <x>589.735</x>
- <y>-226.575</y>
- <z>-95.567</z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="ENG_2">
- <location unit="IN">
- <x>589.735</x>
- <y>226.575</y>
- <z>-95.567</z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.5 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
+ <contact type="STRUCTURE" name="ENG_1">
+ <location unit="IN">
+ <x>589.735</x>
+ <y>-226.575</y>
+ <z>-95.567</z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="ENG_2">
+ <location unit="IN">
+ <x>589.735</x>
+ <y>226.575</y>
+ <z>-95.567</z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.5 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
- <contact type="STRUCTURE" name="TAIL_1">
- <location unit="IN">
- <x> 1097.9921 </x>
- <y> 0 </y>
- <z> -44.7722 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="TAIL_2">
- <location unit="IN">
- <x> 1225 </x>
- <y> 0 </y>
- <z> -18.8067 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="TAIL_3">
- <location unit="IN">
- <x> 1341.6142 </x>
- <y> 0 </y>
- <z> -10.2599 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="TAIL_4">
- <location unit="IN">
- <x> 1469.0945 </x>
- <y> 0 </y>
- <z> 47.4138 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 1 </dynamic_friction>
- <rolling_friction> 1 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="WING_TIP_1">
- <location unit="IN">
- <x> 838.8898 </x>
- <y> -667.5197 </y>
- <z> 35.7926 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="WING_TIP_2">
- <location unit="IN">
- <x> 838.8898 </x>
- <y> 667.5197 </y>
- <z> 35.7926 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 1 </dynamic_friction>
- <rolling_friction> 1 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- </ground_reactions>
+ <contact type="STRUCTURE" name="TAIL_1">
+ <location unit="IN">
+ <x> 1097.9921 </x>
+ <y> 0 </y>
+ <z> -44.7722 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="TAIL_2">
+ <location unit="IN">
+ <x> 1225 </x>
+ <y> 0 </y>
+ <z> -18.8067 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="TAIL_3">
+ <location unit="IN">
+ <x> 1341.6142 </x>
+ <y> 0 </y>
+ <z> -10.2599 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="TAIL_4">
+ <location unit="IN">
+ <x> 1469.0945 </x>
+ <y> 0 </y>
+ <z> 47.4138 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 1 </dynamic_friction>
+ <rolling_friction> 1 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="WING_TIP_1">
+ <location unit="IN">
+ <x> 838.8898 </x>
+ <y> -667.5197 </y>
+ <z> 35.7926 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="WING_TIP_2">
+ <location unit="IN">
+ <x> 838.8898 </x>
+ <y> 667.5197 </y>
+ <z> 35.7926 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 1 </dynamic_friction>
+ <rolling_friction> 1 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ </ground_reactions>
-<propulsion>
+ <propulsion>
- <engine file="cfm56_5b3">
- <location unit="IN">
- <x> 620.0683 </x>
- <y> -226.575 </y>
- <z> -45.567 </z>
- </location>
- <orient unit="DEG">
- <roll> 0.0 </roll>
- <pitch> 2.2 </pitch>
- <yaw> 1 </yaw>
- </orient>
- <feed>7</feed>
- <thruster file="direct">
+ <engine file="cfm56_5b3">
<location unit="IN">
- <x> 655.4820 </x>
- <y> -226.575 </y>
- <z> 0.000 </z>
+ <x> 620.0683 </x>
+ <y> -226.575 </y>
+ <z> -45.567 </z>
</location>
<orient unit="DEG">
- <roll> 0.0 </roll>
- <pitch> 2.2 </pitch>
- <yaw> 1 </yaw>
+ <roll> 0.0 </roll>
+ <pitch> 2.2 </pitch>
+ <yaw> 1 </yaw>
</orient>
- </thruster>
- </engine>
+ <feed>7</feed>
+ <thruster file="direct">
+ <location unit="IN">
+ <x> 655.4820 </x>
+ <y> -226.575 </y>
+ <z> 0.000 </z>
+ </location>
+ <orient unit="DEG">
+ <roll> 0.0 </roll>
+ <pitch> 2.2 </pitch>
+ <yaw> 1 </yaw>
+ </orient>
+ </thruster>
+ </engine>
- <engine file="cfm56_5b3">
- <location unit="IN">
- <x> 620.0683 </x>
- <y> 226.575 </y>
- <z> -45.567 </z>
- </location>
- <orient unit="DEG">
- <roll> 0.0 </roll>
- <pitch> 2.2 </pitch>
- <yaw> -1 </yaw>
- </orient>
- <feed>8</feed>
- <thruster file="direct">
+ <engine file="cfm56_5b3">
<location unit="IN">
- <x> 655.4820 </x>
- <y> 226.575 </y>
- <z> 0.000 </z>
+ <x> 620.0683 </x>
+ <y> 226.575 </y>
+ <z> -45.567 </z>
</location>
<orient unit="DEG">
- <roll> 0.0 </roll>
- <pitch> 2.2 </pitch>
- <yaw> -1 </yaw>
+ <roll> 0.0 </roll>
+ <pitch> 2.2 </pitch>
+ <yaw> -1 </yaw>
</orient>
- </thruster>
- </engine>
+ <feed>8</feed>
+ <thruster file="direct">
+ <location unit="IN">
+ <x> 655.4820 </x>
+ <y> 226.575 </y>
+ <z> 0.000 </z>
+ </location>
+ <orient unit="DEG">
+ <roll> 0.0 </roll>
+ <pitch> 2.2 </pitch>
+ <yaw> -1 </yaw>
+ </orient>
+ </thruster>
+ </engine>
- <tank type="FUEL"> <!-- Left Tank (Wing tip Ventilation Surge) 0 -->
- <location unit="IN">
- <x> 783.0709 </x>
- <y> -574.4148 </y>
- <z> 3.1080 </z>
- </location>
- <capacity unit="LBS"> 412 </capacity><!-- 1 percent of total capacity, needs 20C to be filled -->
- <contents unit="LBS"> 0 </contents>
-
- <priority>4</priority>
- <type>JET-A1</type>
- <temperature>50</temperature>
- </tank>
- <tank type="FUEL"> <!-- Left Tank (Outer) 1 -->
- <location unit="IN">
- <x> 739.5669 </x>
- <y> -457.4259 </y>
- <z> -8.0898 </z>
- </location>
- <capacity unit="LBS"> 1520.00 </capacity><!-- correct by FCOM -->
- <contents unit="LBS"> 1520 </contents><!-- outer filled first than inner -->
- <standpipe unit="LBS">21</standpipe><!-- minimun fuel on pipes -->
- <priority>2</priority>
- <type>JET-A1</type>
- <temperature>50</temperature>
- </tank>
- <tank type="FUEL"> <!-- Left Tank (Inner) 2 -->
- <location unit="IN">
- <x> 652.5591 </x>
- <y> -236.2992 </y>
- <z> -33.9470 </z>
- </location>
- <capacity unit="LBS"> 11982 </capacity><!-- correct by FCOM -->
- <contents unit="LBS"> 4480 </contents>
- <standpipe unit="LBS">31</standpipe><!-- minimun fuel on pipes -->
- <priority>3</priority>
- <type>JET-A1</type>
- <temperature>50</temperature>
- </tank>
- <tank type="FUEL"> <!-- Center Tank 3 -->
- <location unit="IN">
- <x> 522.0473 </x>
- <y> 0 </y>
- <z> -47.0 </z>
- </location>
- <capacity unit="LBS"> 14281 </capacity><!-- correct by FCOM -->
- <contents unit="LBS"> 0 </contents> <!-- wing tanks filled first -->
- <standpipe unit="LBS">43</standpipe><!-- minimun fuel on pipes -->
- <priority>1</priority>
- <type>JET-A1</type>
- <temperature>50</temperature>
- </tank>
- <tank type="FUEL"> <!-- Right Tank (Inner) 4 -->
- <location unit="IN">
- <x> 652.5591 </x>
- <y> 236.2992 </y>
- <z> -33.9470 </z>
- </location>
- <capacity unit="LBS"> 11982 </capacity><!-- correct by FCOM -->
- <contents unit="LBS"> 4480 </contents>
- <standpipe unit="LBS">31</standpipe><!-- minimum fuel on pipes -->
- <priority>3</priority>
- <type>JET-A1</type>
- <temperature>50</temperature>
- </tank>
- <tank type="FUEL"> <!-- Right Tank (Outer) 5 -->
- <location unit="IN">
- <x> 739.5669 </x>
- <y> 457.4259 </y>
- <z> -8.0898 </z>
- </location>
- <capacity unit="LBS"> 1520 </capacity><!-- need review -->
- <contents unit="LBS"> 1520 </contents><!-- outer tank filled first than inner tank -->
- <standpipe unit="LBS">21</standpipe><!-- minimun fuel on pipes -->
- <priority>2</priority>
- <type>JET-A1</type>
- <temperature>50</temperature>
- </tank>
- <tank type="FUEL"> <!-- Right Tank (Wing tip Ventilation Surge) 6 -->
- <location unit="IN">
- <x> 783.0709 </x>
- <y> 574.4148 </y>
- <z> 3.1080 </z>
- </location>
- <capacity unit="LBS"> 412 </capacity><!-- 1 percent of total fuel capacity, needs 20C-->
- <contents unit="LBS"> 0 </contents>
- <priority>4</priority>
- <type>JET-A1</type>
- <temperature>50</temperature>
- </tank>
- <tank type="FUEL"> <!-- LEFT FUEL PIPES (Engine 1 feed from this) -->
- <location unit="IN">
- <x>589.735</x>
- <y>-226.575</y>
- <z>-45.567</z>
- </location>
- <capacity unit="LBS"> 100 </capacity><!-- need review -->
- <contents unit="LBS"> 0 </contents>
- <priority>1</priority>
- <type>JET-A1</type>
- </tank>
- <tank type="FUEL"> <!-- RIGHT FUEL PIPES (Engine 2 feed from this) -->
- <location unit="IN">
- <x>589.735</x>
- <y>226.575</y>
- <z>-45.567</z>
- </location>
- <capacity unit="LBS"> 100 </capacity><!-- need review -->
- <contents unit="LBS"> 0 </contents>
- <priority>1</priority>
- <type>JET-A1</type>
- </tank>
-</propulsion>
+ <tank type="FUEL"> <!-- Left Tank (Wing tip Ventilation Surge) 0 -->
+ <location unit="IN">
+ <x> 783.0709 </x>
+ <y> -574.4148 </y>
+ <z> 3.1080 </z>
+ </location>
+ <capacity unit="LBS"> 412 </capacity><!-- 1 percent of total capacity, needs 20C to be filled -->
+ <contents unit="LBS"> 0 </contents>
+
+ <priority>4</priority>
+ <type>JET-A1</type>
+ <temperature>50</temperature>
+ </tank>
+ <tank type="FUEL"> <!-- Left Tank (Outer) 1 -->
+ <location unit="IN">
+ <x> 739.5669 </x>
+ <y> -457.4259 </y>
+ <z> -8.0898 </z>
+ </location>
+ <capacity unit="LBS"> 1520.00 </capacity><!-- correct by FCOM -->
+ <contents unit="LBS"> 1520 </contents><!-- outer filled first than inner -->
+ <standpipe unit="LBS">21</standpipe><!-- minimun fuel on pipes -->
+ <priority>2</priority>
+ <type>JET-A1</type>
+ <temperature>50</temperature>
+ </tank>
+ <tank type="FUEL"> <!-- Left Tank (Inner) 2 -->
+ <location unit="IN">
+ <x> 652.5591 </x>
+ <y> -236.2992 </y>
+ <z> -33.9470 </z>
+ </location>
+ <capacity unit="LBS"> 11982 </capacity><!-- correct by FCOM -->
+ <contents unit="LBS"> 4480 </contents>
+ <standpipe unit="LBS">31</standpipe><!-- minimun fuel on pipes -->
+ <priority>3</priority>
+ <type>JET-A1</type>
+ <temperature>50</temperature>
+ </tank>
+ <tank type="FUEL"> <!-- Center Tank 3 -->
+ <location unit="IN">
+ <x> 522.0473 </x>
+ <y> 0 </y>
+ <z> -47.0 </z>
+ </location>
+ <capacity unit="LBS"> 14281 </capacity><!-- correct by FCOM -->
+ <contents unit="LBS"> 0 </contents> <!-- wing tanks filled first -->
+ <standpipe unit="LBS">43</standpipe><!-- minimun fuel on pipes -->
+ <priority>1</priority>
+ <type>JET-A1</type>
+ <temperature>50</temperature>
+ </tank>
+ <tank type="FUEL"> <!-- Right Tank (Inner) 4 -->
+ <location unit="IN">
+ <x> 652.5591 </x>
+ <y> 236.2992 </y>
+ <z> -33.9470 </z>
+ </location>
+ <capacity unit="LBS"> 11982 </capacity><!-- correct by FCOM -->
+ <contents unit="LBS"> 4480 </contents>
+ <standpipe unit="LBS">31</standpipe><!-- minimum fuel on pipes -->
+ <priority>3</priority>
+ <type>JET-A1</type>
+ <temperature>50</temperature>
+ </tank>
+ <tank type="FUEL"> <!-- Right Tank (Outer) 5 -->
+ <location unit="IN">
+ <x> 739.5669 </x>
+ <y> 457.4259 </y>
+ <z> -8.0898 </z>
+ </location>
+ <capacity unit="LBS"> 1520 </capacity><!-- need review -->
+ <contents unit="LBS"> 1520 </contents><!-- outer tank filled first than inner tank -->
+ <standpipe unit="LBS">21</standpipe><!-- minimun fuel on pipes -->
+ <priority>2</priority>
+ <type>JET-A1</type>
+ <temperature>50</temperature>
+ </tank>
+ <tank type="FUEL"> <!-- Right Tank (Wing tip Ventilation Surge) 6 -->
+ <location unit="IN">
+ <x> 783.0709 </x>
+ <y> 574.4148 </y>
+ <z> 3.1080 </z>
+ </location>
+ <capacity unit="LBS"> 412 </capacity><!-- 1 percent of total fuel capacity, needs 20C-->
+ <contents unit="LBS"> 0 </contents>
+ <priority>4</priority>
+ <type>JET-A1</type>
+ <temperature>50</temperature>
+ </tank>
+ <tank type="FUEL"> <!-- LEFT FUEL PIPES (Engine 1 feed from this) -->
+ <location unit="IN">
+ <x>589.735</x>
+ <y>0</y>
+ <z>-45.567</z>
+ </location>
+ <capacity unit="LBS"> 100 </capacity><!-- need review -->
+ <contents unit="LBS"> 0 </contents>
+ <priority>1</priority>
+ <type>JET-A1</type>
+ </tank>
+ <tank type="FUEL"> <!-- RIGHT FUEL PIPES (Engine 2 feed from this) -->
+ <location unit="IN">
+ <x>589.735</x>
+ <y>0</y>
+ <z>-45.567</z>
+ </location>
+ <capacity unit="LBS"> 100 </capacity><!-- need review -->
+ <contents unit="LBS"> 0 </contents>
+ <priority>1</priority>
+ <type>JET-A1</type>
+ </tank>
+ </propulsion>
-<system file="pushback" />
-<system file="fuel" />
-<system file="glass-effect1" />
-<system file="fmgc" />
-<system file="fcs" />
+ <system file="pushback" />
+ <system file="fuel" />
+ <system file="glass-effect1" />
+ <system file="fmgc" />
+ <system file="fcs" />
-<flight_control name="none"/>
+ <flight_control name="none"/>
-<aerodynamics file="Systems/a321-aerodynamics.xml" />
+ <aerodynamics file="Systems/a321-aerodynamics.xml" />
-<external_reactions>
- <force name="pushback" frame="BODY">
- <location unit="IN">
- <x>294</x>
- <y>0</y>
- <z>-149</z>
- </location>
- <direction>
- <x>1</x>
- <y>0</y>
- <z>0</z>
- </direction>
- </force>
-</external_reactions>
+ <external_reactions>
+ <force name="pushback" frame="BODY">
+ <location unit="IN">
+ <x>294</x>
+ <y>0</y>
+ <z>-149</z>
+ </location>
+ <direction>
+ <x>1</x>
+ <y>0</y>
+ <z>0</z>
+ </direction>
+ </force>
+ </external_reactions>
</fdm_config>
diff --git a/A321-200-IAE.xml b/A321-200-IAE.xml
index f5f28233..2678a452 100644
--- a/A321-200-IAE.xml
+++ b/A321-200-IAE.xml
@@ -4,585 +4,585 @@
xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance"
xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
-<fileheader>
- <author>Joshua Davidson (it0uchpods)</author>
- <version>Pre V1.0</version>
- <description>A3XX FDE</description>
-</fileheader>
+ <fileheader>
+ <author>Joshua Davidson (it0uchpods)</author>
+ <version>Pre V1.0</version>
+ <description>A3XX FDE</description>
+ </fileheader>
-<metrics>
- <wingarea unit="FT2"> 1319.79 </wingarea>
- <wingspan unit="FT" > 111.26 </wingspan>
- <wing_incidence> 1.03 </wing_incidence>
- <chord unit="FT" > 13.76 </chord>
- <htailarea unit="FT2"> 334.24 </htailarea>
- <htailarm unit="FT" > 57.88 </htailarm>
- <vtailarea unit="FT2"> 248.79 </vtailarea>
- <vtailarm unit="FT" > 57.33 </vtailarm>
+ <metrics>
+ <wingarea unit="FT2"> 1319.79 </wingarea>
+ <wingspan unit="FT" > 111.26 </wingspan>
+ <wing_incidence> 1.03 </wing_incidence>
+ <chord unit="FT" > 13.76 </chord>
+ <htailarea unit="FT2"> 334.24 </htailarea>
+ <htailarm unit="FT" > 57.88 </htailarm>
+ <vtailarea unit="FT2"> 248.79 </vtailarea>
+ <vtailarm unit="FT" > 57.33 </vtailarm>
- <location name="AERORP" unit="IN">
- <x> 700.00 </x>
- <y> 0 </y>
- <z> 0.00 </z>
- </location>
+ <location name="AERORP" unit="IN">
+ <x> 700.00 </x>
+ <y> 0 </y>
+ <z> 0.00 </z>
+ </location>
- <location name="EYEPOINT" unit="IN">
- <x> 80 </x>
- <y> -30 </y>
- <z> 70 </z>
- </location>
+ <location name="EYEPOINT" unit="IN">
+ <x> 80 </x>
+ <y> -30 </y>
+ <z> 70 </z>
+ </location>
- <location name="VRP" unit="IN">
- <x> 661.1 </x>
- <y> 0 </y>
- <z> -37 </z>
- </location>
+ <location name="VRP" unit="IN">
+ <x> 661.1 </x>
+ <y> 0 </y>
+ <z> -37 </z>
+ </location>
- </metrics>
+ </metrics>
- <mass_balance>
- <ixx unit="SLUG*FT2"> 611903</ixx>
- <iyy unit="SLUG*FT2">1735389</iyy>
- <izz unit="SLUG*FT2">2301293</izz>
+ <mass_balance>
+ <ixx unit="SLUG*FT2"> 611903</ixx>
+ <iyy unit="SLUG*FT2">1735389</iyy>
+ <izz unit="SLUG*FT2">2301293</izz>
- <ixy unit="SLUG*FT2">0</ixy>
- <ixz unit="SLUG*FT2">0</ixz>
- <iyz unit="SLUG*FT2">0</iyz>
- <emptywt unit="LBS">80431</emptywt>
+ <ixy unit="SLUG*FT2">0</ixy>
+ <ixz unit="SLUG*FT2">0</ixz>
+ <iyz unit="SLUG*FT2">0</iyz>
+ <emptywt unit="LBS">80431</emptywt>
- <location name="CG" unit="IN">
- <x> 652.00 </x>
- <y> 0 </y>
- <z> 0.00 </z>
- </location>
+ <location name="CG" unit="IN">
+ <x> 652.00 </x>
+ <y> 0 </y>
+ <z> 0.00 </z>
+ </location>
- <pointmass name="Cockpit Crew">
- <weight unit="LBS">400</weight>
- <!-- MAX: 400lbs, two pilots-->
- <location name="POINTMASS" unit="IN">
- <x>200</x>
- <y>0</y>
- <z>0</z>
- </location>
- </pointmass>
- <pointmass name="Engine 1">
- <weight unit="LBS">5200.7</weight>
- <location name="POINTMASS" unit="IN">
- <x>530.86</x>
- <y>-5.755</y>
- <z>-78.56019</z>
- </location>
- </pointmass>
- <pointmass name="Engine 2">
- <weight unit="LBS">5200.7</weight>
- <location name="POINTMASS" unit="IN">
- <x>530.86</x>
- <y>5.755</y>
- <z>-78.56019</z>
- </location>
- </pointmass>
- <pointmass name="PAX 0A (60 seats)">
- <weight unit="LBS">6600</weight>
- <!-- MAX: 13200lbs, 60 seats -->
- <location name="POINTMASS" unit="IN">
- <x>470.1711</x>
- <y>0</y>
- <z>0</z>
- </location>
- </pointmass>
- <pointmass name="PAX 0B (60 seats)">
- <weight unit="LBS">6600</weight>
- <!-- MAX: 13200lbs, 60 seats -->
- <location name="POINTMASS" unit="IN">
- <x>809.5669</x>
- <y>0</y>
- <z>0</z>
- </location>
- </pointmass>
- <pointmass name="PAX 0C (54 seats)">
- <weight unit="LBS">5940</weight>
- <!-- MAX: 11880lbs, 54 seats -->
- <location name="POINTMASS" unit="IN">
- <x>1163.2729</x>
- <y>0</y>
- <z>0</z>
- </location>
- </pointmass>
- <pointmass name="Cargo Hold 1">
- <weight unit="LBS">2000</weight>
- <!-- MAX: 7500.126lbs -->
- <location name="POINTMASS" unit="IN">
- <x>383.4792</x>
- <y>0</y>
- <z>-29.5</z>
- <!-- 1.5m and now half of it for the center point of the load -->
- </location>
- </pointmass>
- <!-- Cargo Hold 2 doesn't exist, that is the center tank -->
- <pointmass name="Cargo Hold 3">
- <weight unit="LBS">2000</weight>
- <!-- MAX: 5384.414lbs -->
- <location name="POINTMASS" unit="IN">
- <x>849.1324</x>
- <y>0</y>
- <z>-29.5</z>
- </location>
- </pointmass>
- <pointmass name="Cargo Hold 4">
- <weight unit="LBS">1500</weight>
- <!-- MAX: 4651.754lbs -->
- <location name="POINTMASS" unit="IN">
- <x>931.0653</x>
- <y>0</y>
- <z>-29.5</z>
- </location>
- </pointmass>
- <pointmass name="Cargo Hold 5">
- <weight unit="LBS">2000</weight>
- <!-- MAX: 3300.320lbs -->
- <location name="POINTMASS" unit="IN">
- <x>1068.2634</x>
- <y>0</y>
- <z>0</z>
- <!-- Cargo Hold #5 sits higher on the range of the cabin deck, it's only loadable with lifter -->
- </location>
- </pointmass>
+ <pointmass name="Cockpit Crew">
+ <weight unit="LBS">400</weight>
+ <!-- MAX: 400lbs, two pilots-->
+ <location name="POINTMASS" unit="IN">
+ <x>200</x>
+ <y>0</y>
+ <z>0</z>
+ </location>
+ </pointmass>
+ <pointmass name="Engine 1">
+ <weight unit="LBS">5200.7</weight>
+ <location name="POINTMASS" unit="IN">
+ <x>530.86</x>
+ <y>-5.755</y>
+ <z>-78.56019</z>
+ </location>
+ </pointmass>
+ <pointmass name="Engine 2">
+ <weight unit="LBS">5200.7</weight>
+ <location name="POINTMASS" unit="IN">
+ <x>530.86</x>
+ <y>5.755</y>
+ <z>-78.56019</z>
+ </location>
+ </pointmass>
+ <pointmass name="PAX 0A (60 seats)">
+ <weight unit="LBS">6600</weight>
+ <!-- MAX: 13200lbs, 60 seats -->
+ <location name="POINTMASS" unit="IN">
+ <x>470.1711</x>
+ <y>0</y>
+ <z>0</z>
+ </location>
+ </pointmass>
+ <pointmass name="PAX 0B (60 seats)">
+ <weight unit="LBS">6600</weight>
+ <!-- MAX: 13200lbs, 60 seats -->
+ <location name="POINTMASS" unit="IN">
+ <x>809.5669</x>
+ <y>0</y>
+ <z>0</z>
+ </location>
+ </pointmass>
+ <pointmass name="PAX 0C (54 seats)">
+ <weight unit="LBS">5940</weight>
+ <!-- MAX: 11880lbs, 54 seats -->
+ <location name="POINTMASS" unit="IN">
+ <x>1163.2729</x>
+ <y>0</y>
+ <z>0</z>
+ </location>
+ </pointmass>
+ <pointmass name="Cargo Hold 1">
+ <weight unit="LBS">2000</weight>
+ <!-- MAX: 7500.126lbs -->
+ <location name="POINTMASS" unit="IN">
+ <x>383.4792</x>
+ <y>0</y>
+ <z>-29.5</z>
+ <!-- 1.5m and now half of it for the center point of the load -->
+ </location>
+ </pointmass>
+ <!-- Cargo Hold 2 doesn't exist, that is the center tank -->
+ <pointmass name="Cargo Hold 3">
+ <weight unit="LBS">2000</weight>
+ <!-- MAX: 5384.414lbs -->
+ <location name="POINTMASS" unit="IN">
+ <x>849.1324</x>
+ <y>0</y>
+ <z>-29.5</z>
+ </location>
+ </pointmass>
+ <pointmass name="Cargo Hold 4">
+ <weight unit="LBS">1500</weight>
+ <!-- MAX: 4651.754lbs -->
+ <location name="POINTMASS" unit="IN">
+ <x>931.0653</x>
+ <y>0</y>
+ <z>-29.5</z>
+ </location>
+ </pointmass>
+ <pointmass name="Cargo Hold 5">
+ <weight unit="LBS">2000</weight>
+ <!-- MAX: 3300.320lbs -->
+ <location name="POINTMASS" unit="IN">
+ <x>1068.2634</x>
+ <y>0</y>
+ <z>0</z>
+ <!-- Cargo Hold #5 sits higher on the range of the cabin deck, it's only loadable with lifter -->
+ </location>
+ </pointmass>
- </mass_balance>
+ </mass_balance>
- <ground_reactions>
- <!-- REF-1 page 165 + 271 -->
- <contact type="BOGEY" name="NOSE_LG">
- <location unit="IN">
- <x> 197.6772 </x>
- <y> 0 </y>
- <z> -137.9617 </z>
- </location>
- <static_friction> 0.8 </static_friction>
- <dynamic_friction> 0.5 </dynamic_friction>
- <rolling_friction> 0.02 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 30935.5 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 16978.5 </damping_coeff>
- <max_steer unit="DEG"> 70 </max_steer>
- <!-- REF-1 page 133 -->
- <brake_group> NOSE </brake_group>
- <retractable>1</retractable>
- </contact>
- <contact type="BOGEY" name="LEFT_MLG">
- <location unit="IN">
- <!--<x> 699.9243 </x>-->
- <x> 695.3149 </x>
- <y> -149.4094 </y>
- <z> -150.4824 </z>
- </location>
- <!-- <static_friction> 0.5 </static_friction> WHAT??? less static than dinamyc friction?-->
- <static_friction> 0.8 </static_friction>
- <dynamic_friction> 0.5 </dynamic_friction>
- <rolling_friction> 0.02 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 59785 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 23957 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> LEFT </brake_group>
- <retractable>1</retractable>
- </contact>
- <contact type="BOGEY" name="RIGHT_MLG">
- <location unit="IN">
- <!-- <x> 697.3425 </x> It should be right left simetric
- <x> 699.9243 </x> -->
- <x> 695.3149 </x>
- <y> 149.4094 </y>
- <z> -150.4824 </z>
- </location>
- <!-- <static_friction> 0.5 </static_friction> WHAT??? less static than dinamyc friction?-->
- <static_friction> 0.8 </static_friction>
- <dynamic_friction> 0.5 </dynamic_friction>
- <rolling_friction> 0.02 </rolling_friction>
- <!--spring_coeff unit="LBS/FT"> 169785 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 33957 </damping_coeff-->
- <spring_coeff unit="LBS/FT"> 59785 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 23957 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> RIGHT </brake_group>
- <retractable>1</retractable>
- </contact>
+ <ground_reactions>
+ <!-- REF-1 page 165 + 271 -->
+ <contact type="BOGEY" name="NOSE_LG">
+ <location unit="IN">
+ <x> 197.6772 </x>
+ <y> 0 </y>
+ <z> -137.9617 </z>
+ </location>
+ <static_friction> 0.8 </static_friction>
+ <dynamic_friction> 0.5 </dynamic_friction>
+ <rolling_friction> 0.02 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 30935.5 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 16978.5 </damping_coeff>
+ <max_steer unit="DEG"> 70 </max_steer>
+ <!-- REF-1 page 133 -->
+ <brake_group> NOSE </brake_group>
+ <retractable>1</retractable>
+ </contact>
+ <contact type="BOGEY" name="LEFT_MLG">
+ <location unit="IN">
+ <!--<x> 699.9243 </x>-->
+ <x> 695.3149 </x>
+ <y> -149.4094 </y>
+ <z> -150.4824 </z>
+ </location>
+ <!-- <static_friction> 0.5 </static_friction> WHAT??? less static than dinamyc friction?-->
+ <static_friction> 0.8 </static_friction>
+ <dynamic_friction> 0.5 </dynamic_friction>
+ <rolling_friction> 0.02 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 59785 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 23957 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> LEFT </brake_group>
+ <retractable>1</retractable>
+ </contact>
+ <contact type="BOGEY" name="RIGHT_MLG">
+ <location unit="IN">
+ <!-- <x> 697.3425 </x> It should be right left simetric
+ <x> 699.9243 </x> -->
+ <x> 695.3149 </x>
+ <y> 149.4094 </y>
+ <z> -150.4824 </z>
+ </location>
+ <!-- <static_friction> 0.5 </static_friction> WHAT??? less static than dinamyc friction?-->
+ <static_friction> 0.8 </static_friction>
+ <dynamic_friction> 0.5 </dynamic_friction>
+ <rolling_friction> 0.02 </rolling_friction>
+ <!--spring_coeff unit="LBS/FT"> 169785 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 33957 </damping_coeff-->
+ <spring_coeff unit="LBS/FT"> 59785 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 23957 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> RIGHT </brake_group>
+ <retractable>1</retractable>
+ </contact>
- <contact type="STRUCTURE" name="NOSE_1">
- <location unit="IN">
- <x> 37.7953 </x>
- <y> 0 </y>
- <z> -38.1374 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="NOSE_2">
- <location unit="IN">
- <x> 128.1102 </x>
- <y> 0 </y>
- <z> -55.0271 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="CENTER_1">
- <location unit="IN">
- <x> 274.0157 </x>
- <y> 0 </y>
- <z> -60.0665 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="CENTER_2">
- <location unit="IN">
- <x> 930 </x>
- <y> 0 </y>
- <z> -60.0665 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
+ <contact type="STRUCTURE" name="NOSE_1">
+ <location unit="IN">
+ <x> 37.7953 </x>
+ <y> 0 </y>
+ <z> -38.1374 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="NOSE_2">
+ <location unit="IN">
+ <x> 128.1102 </x>
+ <y> 0 </y>
+ <z> -55.0271 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="CENTER_1">
+ <location unit="IN">
+ <x> 274.0157 </x>
+ <y> 0 </y>
+ <z> -60.0665 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="CENTER_2">
+ <location unit="IN">
+ <x> 930 </x>
+ <y> 0 </y>
+ <z> -60.0665 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
- <contact type="STRUCTURE" name="ENG_1">
- <location unit="IN">
- <x>589.735</x>
- <y>-226.575</y>
- <z>-95.567</z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="ENG_2">
- <location unit="IN">
- <x>589.735</x>
- <y>226.575</y>
- <z>-95.567</z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.5 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
+ <contact type="STRUCTURE" name="ENG_1">
+ <location unit="IN">
+ <x>589.735</x>
+ <y>-226.575</y>
+ <z>-95.567</z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="ENG_2">
+ <location unit="IN">
+ <x>589.735</x>
+ <y>226.575</y>
+ <z>-95.567</z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.5 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
- <contact type="STRUCTURE" name="TAIL_1">
- <location unit="IN">
- <x> 1097.9921 </x>
- <y> 0 </y>
- <z> -44.7722 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="TAIL_2">
- <location unit="IN">
- <x> 1225 </x>
- <y> 0 </y>
- <z> -18.8067 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="TAIL_3">
- <location unit="IN">
- <x> 1341.6142 </x>
- <y> 0 </y>
- <z> -10.2599 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="TAIL_4">
- <location unit="IN">
- <x> 1469.0945 </x>
- <y> 0 </y>
- <z> 47.4138 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 1 </dynamic_friction>
- <rolling_friction> 1 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="WING_TIP_1">
- <location unit="IN">
- <x> 838.8898 </x>
- <y> -667.5197 </y>
- <z> 35.7926 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="WING_TIP_2">
- <location unit="IN">
- <x> 838.8898 </x>
- <y> 667.5197 </y>
- <z> 35.7926 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 1 </dynamic_friction>
- <rolling_friction> 1 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- </ground_reactions>
+ <contact type="STRUCTURE" name="TAIL_1">
+ <location unit="IN">
+ <x> 1097.9921 </x>
+ <y> 0 </y>
+ <z> -44.7722 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="TAIL_2">
+ <location unit="IN">
+ <x> 1225 </x>
+ <y> 0 </y>
+ <z> -18.8067 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="TAIL_3">
+ <location unit="IN">
+ <x> 1341.6142 </x>
+ <y> 0 </y>
+ <z> -10.2599 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="TAIL_4">
+ <location unit="IN">
+ <x> 1469.0945 </x>
+ <y> 0 </y>
+ <z> 47.4138 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 1 </dynamic_friction>
+ <rolling_friction> 1 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="WING_TIP_1">
+ <location unit="IN">
+ <x> 838.8898 </x>
+ <y> -667.5197 </y>
+ <z> 35.7926 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="WING_TIP_2">
+ <location unit="IN">
+ <x> 838.8898 </x>
+ <y> 667.5197 </y>
+ <z> 35.7926 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 1 </dynamic_friction>
+ <rolling_friction> 1 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ </ground_reactions>
-<propulsion>
+ <propulsion>
- <engine file="v2533_a5">
- <location unit="IN">
- <x> 620.0683 </x>
- <y> -226.575 </y>
- <z> -45.567 </z>
- </location>
- <orient unit="DEG">
- <roll> 0.0 </roll>
- <pitch> 2.2 </pitch>
- <yaw> 1 </yaw>
- </orient>
- <feed>7</feed>
- <thruster file="direct">
+ <engine file="v2533_a5">
<location unit="IN">
- <x> 655.4820 </x>
- <y> -226.575 </y>
- <z> 0.000 </z>
+ <x> 620.0683 </x>
+ <y> -226.575 </y>
+ <z> -45.567 </z>
</location>
<orient unit="DEG">
- <roll> 0.0 </roll>
- <pitch> 2.2 </pitch>
- <yaw> 1 </yaw>
+ <roll> 0.0 </roll>
+ <pitch> 2.2 </pitch>
+ <yaw> 1 </yaw>
</orient>
- </thruster>
- </engine>
+ <feed>7</feed>
+ <thruster file="direct">
+ <location unit="IN">
+ <x> 655.4820 </x>
+ <y> -226.575 </y>
+ <z> 0.000 </z>
+ </location>
+ <orient unit="DEG">
+ <roll> 0.0 </roll>
+ <pitch> 2.2 </pitch>
+ <yaw> 1 </yaw>
+ </orient>
+ </thruster>
+ </engine>
- <engine file="v2533_a5">
- <location unit="IN">
- <x> 620.0683 </x>
- <y> 226.575 </y>
- <z> -45.567 </z>
- </location>
- <orient unit="DEG">
- <roll> 0.0 </roll>
- <pitch> 2.2 </pitch>
- <yaw> -1 </yaw>
- </orient>
- <feed>8</feed>
- <thruster file="direct">
+ <engine file="v2533_a5">
<location unit="IN">
- <x> 655.4820 </x>
- <y> 226.575 </y>
- <z> 0.000 </z>
+ <x> 620.0683 </x>
+ <y> 226.575 </y>
+ <z> -45.567 </z>
</location>
<orient unit="DEG">
- <roll> 0.0 </roll>
- <pitch> 2.2 </pitch>
- <yaw> -1 </yaw>
+ <roll> 0.0 </roll>
+ <pitch> 2.2 </pitch>
+ <yaw> -1 </yaw>
</orient>
- </thruster>
- </engine>
+ <feed>8</feed>
+ <thruster file="direct">
+ <location unit="IN">
+ <x> 655.4820 </x>
+ <y> 226.575 </y>
+ <z> 0.000 </z>
+ </location>
+ <orient unit="DEG">
+ <roll> 0.0 </roll>
+ <pitch> 2.2 </pitch>
+ <yaw> -1 </yaw>
+ </orient>
+ </thruster>
+ </engine>
- <tank type="FUEL"> <!-- Left Tank (Wing tip Ventilation Surge) 0 -->
- <location unit="IN">
- <x> 783.0709 </x>
- <y> -574.4148 </y>
- <z> 3.1080 </z>
- </location>
- <capacity unit="LBS"> 412 </capacity><!-- 1 percent of total capacity, needs 20C to be filled -->
- <contents unit="LBS"> 0 </contents>
-
- <priority>4</priority>
- <type>JET-A1</type>
- <temperature>50</temperature>
- </tank>
- <tank type="FUEL"> <!-- Left Tank (Outer) 1 -->
- <location unit="IN">
- <x> 739.5669 </x>
- <y> -457.4259 </y>
- <z> -8.0898 </z>
- </location>
- <capacity unit="LBS"> 1520.00 </capacity><!-- correct by FCOM -->
- <contents unit="LBS"> 1520 </contents><!-- outer filled first than inner -->
- <standpipe unit="LBS">21</standpipe><!-- minimun fuel on pipes -->
- <priority>2</priority>
- <type>JET-A1</type>
- <temperature>50</temperature>
- </tank>
- <tank type="FUEL"> <!-- Left Tank (Inner) 2 -->
- <location unit="IN">
- <x> 652.5591 </x>
- <y> -236.2992 </y>
- <z> -33.9470 </z>
- </location>
- <capacity unit="LBS"> 11982 </capacity><!-- correct by FCOM -->
- <contents unit="LBS"> 4480 </contents>
- <standpipe unit="LBS">31</standpipe><!-- minimun fuel on pipes -->
- <priority>3</priority>
- <type>JET-A1</type>
- <temperature>50</temperature>
- </tank>
- <tank type="FUEL"> <!-- Center Tank 3 -->
- <location unit="IN">
- <x> 522.0473 </x>
- <y> 0 </y>
- <z> -47.0 </z>
- </location>
- <capacity unit="LBS"> 14281 </capacity><!-- correct by FCOM -->
- <contents unit="LBS"> 0 </contents> <!-- wing tanks filled first -->
- <standpipe unit="LBS">43</standpipe><!-- minimun fuel on pipes -->
- <priority>1</priority>
- <type>JET-A1</type>
- <temperature>50</temperature>
- </tank>
- <tank type="FUEL"> <!-- Right Tank (Inner) 4 -->
- <location unit="IN">
- <x> 652.5591 </x>
- <y> 236.2992 </y>
- <z> -33.9470 </z>
- </location>
- <capacity unit="LBS"> 11982 </capacity><!-- correct by FCOM -->
- <contents unit="LBS"> 4480 </contents>
- <standpipe unit="LBS">31</standpipe><!-- minimum fuel on pipes -->
- <priority>3</priority>
- <type>JET-A1</type>
- <temperature>50</temperature>
- </tank>
- <tank type="FUEL"> <!-- Right Tank (Outer) 5 -->
- <location unit="IN">
- <x> 739.5669 </x>
- <y> 457.4259 </y>
- <z> -8.0898 </z>
- </location>
- <capacity unit="LBS"> 1520 </capacity><!-- need review -->
- <contents unit="LBS"> 1520 </contents><!-- outer tank filled first than inner tank -->
- <standpipe unit="LBS">21</standpipe><!-- minimun fuel on pipes -->
- <priority>2</priority>
- <type>JET-A1</type>
- <temperature>50</temperature>
- </tank>
- <tank type="FUEL"> <!-- Right Tank (Wing tip Ventilation Surge) 6 -->
- <location unit="IN">
- <x> 783.0709 </x>
- <y> 574.4148 </y>
- <z> 3.1080 </z>
- </location>
- <capacity unit="LBS"> 412 </capacity><!-- 1 percent of total fuel capacity, needs 20C-->
- <contents unit="LBS"> 0 </contents>
- <priority>4</priority>
- <type>JET-A1</type>
- <temperature>50</temperature>
- </tank>
- <tank type="FUEL"> <!-- LEFT FUEL PIPES (Engine 1 feed from this) -->
- <location unit="IN">
- <x>589.735</x>
- <y>-226.575</y>
- <z>-45.567</z>
- </location>
- <capacity unit="LBS"> 100 </capacity><!-- need review -->
- <contents unit="LBS"> 0 </contents>
- <priority>1</priority>
- <type>JET-A1</type>
- </tank>
- <tank type="FUEL"> <!-- RIGHT FUEL PIPES (Engine 2 feed from this) -->
- <location unit="IN">
- <x>589.735</x>
- <y>226.575</y>
- <z>-45.567</z>
- </location>
- <capacity unit="LBS"> 100 </capacity><!-- need review -->
- <contents unit="LBS"> 0 </contents>
- <priority>1</priority>
- <type>JET-A1</type>
- </tank>
-</propulsion>
+ <tank type="FUEL"> <!-- Left Tank (Wing tip Ventilation Surge) 0 -->
+ <location unit="IN">
+ <x> 783.0709 </x>
+ <y> -574.4148 </y>
+ <z> 3.1080 </z>
+ </location>
+ <capacity unit="LBS"> 412 </capacity><!-- 1 percent of total capacity, needs 20C to be filled -->
+ <contents unit="LBS"> 0 </contents>
+
+ <priority>4</priority>
+ <type>JET-A1</type>
+ <temperature>50</temperature>
+ </tank>
+ <tank type="FUEL"> <!-- Left Tank (Outer) 1 -->
+ <location unit="IN">
+ <x> 739.5669 </x>
+ <y> -457.4259 </y>
+ <z> -8.0898 </z>
+ </location>
+ <capacity unit="LBS"> 1520.00 </capacity><!-- correct by FCOM -->
+ <contents unit="LBS"> 1520 </contents><!-- outer filled first than inner -->
+ <standpipe unit="LBS">21</standpipe><!-- minimun fuel on pipes -->
+ <priority>2</priority>
+ <type>JET-A1</type>
+ <temperature>50</temperature>
+ </tank>
+ <tank type="FUEL"> <!-- Left Tank (Inner) 2 -->
+ <location unit="IN">
+ <x> 652.5591 </x>
+ <y> -236.2992 </y>
+ <z> -33.9470 </z>
+ </location>
+ <capacity unit="LBS"> 11982 </capacity><!-- correct by FCOM -->
+ <contents unit="LBS"> 4480 </contents>
+ <standpipe unit="LBS">31</standpipe><!-- minimun fuel on pipes -->
+ <priority>3</priority>
+ <type>JET-A1</type>
+ <temperature>50</temperature>
+ </tank>
+ <tank type="FUEL"> <!-- Center Tank 3 -->
+ <location unit="IN">
+ <x> 522.0473 </x>
+ <y> 0 </y>
+ <z> -47.0 </z>
+ </location>
+ <capacity unit="LBS"> 14281 </capacity><!-- correct by FCOM -->
+ <contents unit="LBS"> 0 </contents> <!-- wing tanks filled first -->
+ <standpipe unit="LBS">43</standpipe><!-- minimun fuel on pipes -->
+ <priority>1</priority>
+ <type>JET-A1</type>
+ <temperature>50</temperature>
+ </tank>
+ <tank type="FUEL"> <!-- Right Tank (Inner) 4 -->
+ <location unit="IN">
+ <x> 652.5591 </x>
+ <y> 236.2992 </y>
+ <z> -33.9470 </z>
+ </location>
+ <capacity unit="LBS"> 11982 </capacity><!-- correct by FCOM -->
+ <contents unit="LBS"> 4480 </contents>
+ <standpipe unit="LBS">31</standpipe><!-- minimum fuel on pipes -->
+ <priority>3</priority>
+ <type>JET-A1</type>
+ <temperature>50</temperature>
+ </tank>
+ <tank type="FUEL"> <!-- Right Tank (Outer) 5 -->
+ <location unit="IN">
+ <x> 739.5669 </x>
+ <y> 457.4259 </y>
+ <z> -8.0898 </z>
+ </location>
+ <capacity unit="LBS"> 1520 </capacity><!-- need review -->
+ <contents unit="LBS"> 1520 </contents><!-- outer tank filled first than inner tank -->
+ <standpipe unit="LBS">21</standpipe><!-- minimun fuel on pipes -->
+ <priority>2</priority>
+ <type>JET-A1</type>
+ <temperature>50</temperature>
+ </tank>
+ <tank type="FUEL"> <!-- Right Tank (Wing tip Ventilation Surge) 6 -->
+ <location unit="IN">
+ <x> 783.0709 </x>
+ <y> 574.4148 </y>
+ <z> 3.1080 </z>
+ </location>
+ <capacity unit="LBS"> 412 </capacity><!-- 1 percent of total fuel capacity, needs 20C-->
+ <contents unit="LBS"> 0 </contents>
+ <priority>4</priority>
+ <type>JET-A1</type>
+ <temperature>50</temperature>
+ </tank>
+ <tank type="FUEL"> <!-- LEFT FUEL PIPES (Engine 1 feed from this) -->
+ <location unit="IN">
+ <x>589.735</x>
+ <y>0</y>
+ <z>-45.567</z>
+ </location>
+ <capacity unit="LBS"> 100 </capacity><!-- need review -->
+ <contents unit="LBS"> 0 </contents>
+ <priority>1</priority>
+ <type>JET-A1</type>
+ </tank>
+ <tank type="FUEL"> <!-- RIGHT FUEL PIPES (Engine 2 feed from this) -->
+ <location unit="IN">
+ <x>589.735</x>
+ <y>0</y>
+ <z>-45.567</z>
+ </location>
+ <capacity unit="LBS"> 100 </capacity><!-- need review -->
+ <contents unit="LBS"> 0 </contents>
+ <priority>1</priority>
+ <type>JET-A1</type>
+ </tank>
+ </propulsion>
-<system file="pushback" />
-<system file="fuel" />
-<system file="glass-effect1" />
-<system file="fmgc" />
-<system file="fcs" />
+ <system file="pushback" />
+ <system file="fuel" />
+ <system file="glass-effect1" />
+ <system file="fmgc" />
+ <system file="fcs" />
-<flight_control name="none" />
+ <flight_control name="none" />
-<aerodynamics file="Systems/a321-aerodynamics.xml" />
+ <aerodynamics file="Systems/a321-aerodynamics.xml" />
-<external_reactions>
- <force name="pushback" frame="BODY">
- <location unit="IN">
- <x>294</x>
- <y>0</y>
- <z>-149</z>
- </location>
- <direction>
- <x>1</x>
- <y>0</y>
- <z>0</z>
- </direction>
- </force>
-</external_reactions>
+ <external_reactions>
+ <force name="pushback" frame="BODY">
+ <location unit="IN">
+ <x>294</x>
+ <y>0</y>
+ <z>-149</z>
+ </location>
+ <direction>
+ <x>1</x>
+ <y>0</y>
+ <z>0</z>
+ </direction>
+ </force>
+ </external_reactions>
</fdm_config>
diff --git a/A321neo-CFM.xml b/A321neo-CFM.xml
index 4231d94e..b35b5f46 100644
--- a/A321neo-CFM.xml
+++ b/A321neo-CFM.xml
@@ -4,585 +4,585 @@
xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance"
xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
-<fileheader>
- <author>Joshua Davidson (it0uchpods)</author>
- <version>Pre V1.0</version>
- <description>A3XX FDE</description>
-</fileheader>
+ <fileheader>
+ <author>Joshua Davidson (it0uchpods)</author>
+ <version>Pre V1.0</version>
+ <description>A3XX FDE</description>
+ </fileheader>
-<metrics>
- <wingarea unit="FT2"> 1319.79 </wingarea>
- <wingspan unit="FT" > 111.26 </wingspan>
- <wing_incidence> 1.03 </wing_incidence>
- <chord unit="FT" > 13.76 </chord>
- <htailarea unit="FT2"> 334.24 </htailarea>
- <htailarm unit="FT" > 57.88 </htailarm>
- <vtailarea unit="FT2"> 248.79 </vtailarea>
- <vtailarm unit="FT" > 57.33 </vtailarm>
+ <metrics>
+ <wingarea unit="FT2"> 1319.79 </wingarea>
+ <wingspan unit="FT" > 111.26 </wingspan>
+ <wing_incidence> 1.03 </wing_incidence>
+ <chord unit="FT" > 13.76 </chord>
+ <htailarea unit="FT2"> 334.24 </htailarea>
+ <htailarm unit="FT" > 57.88 </htailarm>
+ <vtailarea unit="FT2"> 248.79 </vtailarea>
+ <vtailarm unit="FT" > 57.33 </vtailarm>
- <location name="AERORP" unit="IN">
- <x> 700.00 </x>
- <y> 0 </y>
- <z> 0.00 </z>
- </location>
+ <location name="AERORP" unit="IN">
+ <x> 700.00 </x>
+ <y> 0 </y>
+ <z> 0.00 </z>
+ </location>
- <location name="EYEPOINT" unit="IN">
- <x> 80 </x>
- <y> -30 </y>
- <z> 70 </z>
- </location>
+ <location name="EYEPOINT" unit="IN">
+ <x> 80 </x>
+ <y> -30 </y>
+ <z> 70 </z>
+ </location>
- <location name="VRP" unit="IN">
- <x> 661.1 </x>
- <y> 0 </y>
- <z> -37 </z>
- </location>
+ <location name="VRP" unit="IN">
+ <x> 661.1 </x>
+ <y> 0 </y>
+ <z> -37 </z>
+ </location>
- </metrics>
+ </metrics>
- <mass_balance>
- <ixx unit="SLUG*FT2"> 611903</ixx>
- <iyy unit="SLUG*FT2">1735389</iyy>
- <izz unit="SLUG*FT2">2301293</izz>
+ <mass_balance>
+ <ixx unit="SLUG*FT2"> 611903</ixx>
+ <iyy unit="SLUG*FT2">1735389</iyy>
+ <izz unit="SLUG*FT2">2301293</izz>
- <ixy unit="SLUG*FT2">0</ixy>
- <ixz unit="SLUG*FT2">0</ixz>
- <iyz unit="SLUG*FT2">0</iyz>
- <emptywt unit="LBS">80431</emptywt>
+ <ixy unit="SLUG*FT2">0</ixy>
+ <ixz unit="SLUG*FT2">0</ixz>
+ <iyz unit="SLUG*FT2">0</iyz>
+ <emptywt unit="LBS">80431</emptywt>
- <location name="CG" unit="IN">
- <x> 652.00 </x>
- <y> 0 </y>
- <z> 0.00 </z>
- </location>
+ <location name="CG" unit="IN">
+ <x> 652.00 </x>
+ <y> 0 </y>
+ <z> 0.00 </z>
+ </location>
- <pointmass name="Cockpit Crew">
- <weight unit="LBS">400</weight>
- <!-- MAX: 400lbs, two pilots-->
- <location name="POINTMASS" unit="IN">
- <x>200</x>
- <y>0</y>
- <z>0</z>
- </location>
- </pointmass>
- <pointmass name="Engine 1">
- <weight unit="LBS">5200.7</weight>
- <location name="POINTMASS" unit="IN">
- <x>530.86</x>
- <y>-5.755</y>
- <z>-78.56019</z>
- </location>
- </pointmass>
- <pointmass name="Engine 2">
- <weight unit="LBS">5200.7</weight>
- <location name="POINTMASS" unit="IN">
- <x>530.86</x>
- <y>5.755</y>
- <z>-78.56019</z>
- </location>
- </pointmass>
- <pointmass name="PAX 0A (60 seats)">
- <weight unit="LBS">6600</weight>
- <!-- MAX: 13200lbs, 60 seats -->
- <location name="POINTMASS" unit="IN">
- <x>470.1711</x>
- <y>0</y>
- <z>0</z>
- </location>
- </pointmass>
- <pointmass name="PAX 0B (60 seats)">
- <weight unit="LBS">6600</weight>
- <!-- MAX: 13200lbs, 60 seats -->
- <location name="POINTMASS" unit="IN">
- <x>809.5669</x>
- <y>0</y>
- <z>0</z>
- </location>
- </pointmass>
- <pointmass name="PAX 0C (54 seats)">
- <weight unit="LBS">5940</weight>
- <!-- MAX: 11880lbs, 54 seats -->
- <location name="POINTMASS" unit="IN">
- <x>1163.2729</x>
- <y>0</y>
- <z>0</z>
- </location>
- </pointmass>
- <pointmass name="Cargo Hold 1">
- <weight unit="LBS">2000</weight>
- <!-- MAX: 7500.126lbs -->
- <location name="POINTMASS" unit="IN">
- <x>383.4792</x>
- <y>0</y>
- <z>-29.5</z>
- <!-- 1.5m and now half of it for the center point of the load -->
- </location>
- </pointmass>
- <!-- Cargo Hold 2 doesn't exist, that is the center tank -->
- <pointmass name="Cargo Hold 3">
- <weight unit="LBS">2000</weight>
- <!-- MAX: 5384.414lbs -->
- <location name="POINTMASS" unit="IN">
- <x>849.1324</x>
- <y>0</y>
- <z>-29.5</z>
- </location>
- </pointmass>
- <pointmass name="Cargo Hold 4">
- <weight unit="LBS">1500</weight>
- <!-- MAX: 4651.754lbs -->
- <location name="POINTMASS" unit="IN">
- <x>931.0653</x>
- <y>0</y>
- <z>-29.5</z>
- </location>
- </pointmass>
- <pointmass name="Cargo Hold 5">
- <weight unit="LBS">2000</weight>
- <!-- MAX: 3300.320lbs -->
- <location name="POINTMASS" unit="IN">
- <x>1068.2634</x>
- <y>0</y>
- <z>0</z>
- <!-- Cargo Hold #5 sits higher on the range of the cabin deck, it's only loadable with lifter -->
- </location>
- </pointmass>
+ <pointmass name="Cockpit Crew">
+ <weight unit="LBS">400</weight>
+ <!-- MAX: 400lbs, two pilots-->
+ <location name="POINTMASS" unit="IN">
+ <x>200</x>
+ <y>0</y>
+ <z>0</z>
+ </location>
+ </pointmass>
+ <pointmass name="Engine 1">
+ <weight unit="LBS">5200.7</weight>
+ <location name="POINTMASS" unit="IN">
+ <x>530.86</x>
+ <y>-5.755</y>
+ <z>-78.56019</z>
+ </location>
+ </pointmass>
+ <pointmass name="Engine 2">
+ <weight unit="LBS">5200.7</weight>
+ <location name="POINTMASS" unit="IN">
+ <x>530.86</x>
+ <y>5.755</y>
+ <z>-78.56019</z>
+ </location>
+ </pointmass>
+ <pointmass name="PAX 0A (60 seats)">
+ <weight unit="LBS">6600</weight>
+ <!-- MAX: 13200lbs, 60 seats -->
+ <location name="POINTMASS" unit="IN">
+ <x>470.1711</x>
+ <y>0</y>
+ <z>0</z>
+ </location>
+ </pointmass>
+ <pointmass name="PAX 0B (60 seats)">
+ <weight unit="LBS">6600</weight>
+ <!-- MAX: 13200lbs, 60 seats -->
+ <location name="POINTMASS" unit="IN">
+ <x>809.5669</x>
+ <y>0</y>
+ <z>0</z>
+ </location>
+ </pointmass>
+ <pointmass name="PAX 0C (54 seats)">
+ <weight unit="LBS">5940</weight>
+ <!-- MAX: 11880lbs, 54 seats -->
+ <location name="POINTMASS" unit="IN">
+ <x>1163.2729</x>
+ <y>0</y>
+ <z>0</z>
+ </location>
+ </pointmass>
+ <pointmass name="Cargo Hold 1">
+ <weight unit="LBS">2000</weight>
+ <!-- MAX: 7500.126lbs -->
+ <location name="POINTMASS" unit="IN">
+ <x>383.4792</x>
+ <y>0</y>
+ <z>-29.5</z>
+ <!-- 1.5m and now half of it for the center point of the load -->
+ </location>
+ </pointmass>
+ <!-- Cargo Hold 2 doesn't exist, that is the center tank -->
+ <pointmass name="Cargo Hold 3">
+ <weight unit="LBS">2000</weight>
+ <!-- MAX: 5384.414lbs -->
+ <location name="POINTMASS" unit="IN">
+ <x>849.1324</x>
+ <y>0</y>
+ <z>-29.5</z>
+ </location>
+ </pointmass>
+ <pointmass name="Cargo Hold 4">
+ <weight unit="LBS">1500</weight>
+ <!-- MAX: 4651.754lbs -->
+ <location name="POINTMASS" unit="IN">
+ <x>931.0653</x>
+ <y>0</y>
+ <z>-29.5</z>
+ </location>
+ </pointmass>
+ <pointmass name="Cargo Hold 5">
+ <weight unit="LBS">2000</weight>
+ <!-- MAX: 3300.320lbs -->
+ <location name="POINTMASS" unit="IN">
+ <x>1068.2634</x>
+ <y>0</y>
+ <z>0</z>
+ <!-- Cargo Hold #5 sits higher on the range of the cabin deck, it's only loadable with lifter -->
+ </location>
+ </pointmass>
- </mass_balance>
+ </mass_balance>
- <ground_reactions>
- <!-- REF-1 page 165 + 271 -->
- <contact type="BOGEY" name="NOSE_LG">
- <location unit="IN">
- <x> 197.6772 </x>
- <y> 0 </y>
- <z> -137.9617 </z>
- </location>
- <static_friction> 0.8 </static_friction>
- <dynamic_friction> 0.5 </dynamic_friction>
- <rolling_friction> 0.02 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 30935.5 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 16978.5 </damping_coeff>
- <max_steer unit="DEG"> 70 </max_steer>
- <!-- REF-1 page 133 -->
- <brake_group> NOSE </brake_group>
- <retractable>1</retractable>
- </contact>
- <contact type="BOGEY" name="LEFT_MLG">
- <location unit="IN">
- <!--<x> 699.9243 </x>-->
- <x> 695.3149 </x>
- <y> -149.4094 </y>
- <z> -150.4824 </z>
- </location>
- <!-- <static_friction> 0.5 </static_friction> WHAT??? less static than dinamyc friction?-->
- <static_friction> 0.8 </static_friction>
- <dynamic_friction> 0.5 </dynamic_friction>
- <rolling_friction> 0.02 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 59785 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 23957 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> LEFT </brake_group>
- <retractable>1</retractable>
- </contact>
- <contact type="BOGEY" name="RIGHT_MLG">
- <location unit="IN">
- <!-- <x> 697.3425 </x> It should be right left simetric
- <x> 699.9243 </x> -->
- <x> 695.3149 </x>
- <y> 149.4094 </y>
- <z> -150.4824 </z>
- </location>
- <!-- <static_friction> 0.5 </static_friction> WHAT??? less static than dinamyc friction?-->
- <static_friction> 0.8 </static_friction>
- <dynamic_friction> 0.5 </dynamic_friction>
- <rolling_friction> 0.02 </rolling_friction>
- <!--spring_coeff unit="LBS/FT"> 169785 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 33957 </damping_coeff-->
- <spring_coeff unit="LBS/FT"> 59785 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 23957 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> RIGHT </brake_group>
- <retractable>1</retractable>
- </contact>
+ <ground_reactions>
+ <!-- REF-1 page 165 + 271 -->
+ <contact type="BOGEY" name="NOSE_LG">
+ <location unit="IN">
+ <x> 197.6772 </x>
+ <y> 0 </y>
+ <z> -137.9617 </z>
+ </location>
+ <static_friction> 0.8 </static_friction>
+ <dynamic_friction> 0.5 </dynamic_friction>
+ <rolling_friction> 0.02 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 30935.5 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 16978.5 </damping_coeff>
+ <max_steer unit="DEG"> 70 </max_steer>
+ <!-- REF-1 page 133 -->
+ <brake_group> NOSE </brake_group>
+ <retractable>1</retractable>
+ </contact>
+ <contact type="BOGEY" name="LEFT_MLG">
+ <location unit="IN">
+ <!--<x> 699.9243 </x>-->
+ <x> 695.3149 </x>
+ <y> -149.4094 </y>
+ <z> -150.4824 </z>
+ </location>
+ <!-- <static_friction> 0.5 </static_friction> WHAT??? less static than dinamyc friction?-->
+ <static_friction> 0.8 </static_friction>
+ <dynamic_friction> 0.5 </dynamic_friction>
+ <rolling_friction> 0.02 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 59785 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 23957 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> LEFT </brake_group>
+ <retractable>1</retractable>
+ </contact>
+ <contact type="BOGEY" name="RIGHT_MLG">
+ <location unit="IN">
+ <!-- <x> 697.3425 </x> It should be right left simetric
+ <x> 699.9243 </x> -->
+ <x> 695.3149 </x>
+ <y> 149.4094 </y>
+ <z> -150.4824 </z>
+ </location>
+ <!-- <static_friction> 0.5 </static_friction> WHAT??? less static than dinamyc friction?-->
+ <static_friction> 0.8 </static_friction>
+ <dynamic_friction> 0.5 </dynamic_friction>
+ <rolling_friction> 0.02 </rolling_friction>
+ <!--spring_coeff unit="LBS/FT"> 169785 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 33957 </damping_coeff-->
+ <spring_coeff unit="LBS/FT"> 59785 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 23957 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> RIGHT </brake_group>
+ <retractable>1</retractable>
+ </contact>
- <contact type="STRUCTURE" name="NOSE_1">
- <location unit="IN">
- <x> 37.7953 </x>
- <y> 0 </y>
- <z> -38.1374 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="NOSE_2">
- <location unit="IN">
- <x> 128.1102 </x>
- <y> 0 </y>
- <z> -55.0271 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="CENTER_1">
- <location unit="IN">
- <x> 274.0157 </x>
- <y> 0 </y>
- <z> -60.0665 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="CENTER_2">
- <location unit="IN">
- <x> 930 </x>
- <y> 0 </y>
- <z> -60.0665 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
+ <contact type="STRUCTURE" name="NOSE_1">
+ <location unit="IN">
+ <x> 37.7953 </x>
+ <y> 0 </y>
+ <z> -38.1374 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="NOSE_2">
+ <location unit="IN">
+ <x> 128.1102 </x>
+ <y> 0 </y>
+ <z> -55.0271 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="CENTER_1">
+ <location unit="IN">
+ <x> 274.0157 </x>
+ <y> 0 </y>
+ <z> -60.0665 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="CENTER_2">
+ <location unit="IN">
+ <x> 930 </x>
+ <y> 0 </y>
+ <z> -60.0665 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
- <contact type="STRUCTURE" name="ENG_1">
- <location unit="IN">
- <x>589.735</x>
- <y>-226.575</y>
- <z>-95.567</z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="ENG_2">
- <location unit="IN">
- <x>589.735</x>
- <y>226.575</y>
- <z>-95.567</z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.5 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
+ <contact type="STRUCTURE" name="ENG_1">
+ <location unit="IN">
+ <x>589.735</x>
+ <y>-226.575</y>
+ <z>-95.567</z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="ENG_2">
+ <location unit="IN">
+ <x>589.735</x>
+ <y>226.575</y>
+ <z>-95.567</z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.5 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
- <contact type="STRUCTURE" name="TAIL_1">
- <location unit="IN">
- <x> 1097.9921 </x>
- <y> 0 </y>
- <z> -44.7722 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="TAIL_2">
- <location unit="IN">
- <x> 1225 </x>
- <y> 0 </y>
- <z> -18.8067 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="TAIL_3">
- <location unit="IN">
- <x> 1341.6142 </x>
- <y> 0 </y>
- <z> -10.2599 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="TAIL_4">
- <location unit="IN">
- <x> 1469.0945 </x>
- <y> 0 </y>
- <z> 47.4138 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 1 </dynamic_friction>
- <rolling_friction> 1 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="WING_TIP_1">
- <location unit="IN">
- <x> 838.8898 </x>
- <y> -667.5197 </y>
- <z> 35.7926 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 0.4 </dynamic_friction>
- <rolling_friction> 0.4 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- <contact type="STRUCTURE" name="WING_TIP_2">
- <location unit="IN">
- <x> 838.8898 </x>
- <y> 667.5197 </y>
- <z> 35.7926 </z>
- </location>
- <static_friction> 1.0 </static_friction>
- <dynamic_friction> 1 </dynamic_friction>
- <rolling_friction> 1 </rolling_friction>
- <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
- <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
- <max_steer unit="DEG"> 0.0 </max_steer>
- <brake_group> NONE </brake_group>
- <retractable>0</retractable>
- </contact>
- </ground_reactions>
+ <contact type="STRUCTURE" name="TAIL_1">
+ <location unit="IN">
+ <x> 1097.9921 </x>
+ <y> 0 </y>
+ <z> -44.7722 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="TAIL_2">
+ <location unit="IN">
+ <x> 1225 </x>
+ <y> 0 </y>
+ <z> -18.8067 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="TAIL_3">
+ <location unit="IN">
+ <x> 1341.6142 </x>
+ <y> 0 </y>
+ <z> -10.2599 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="TAIL_4">
+ <location unit="IN">
+ <x> 1469.0945 </x>
+ <y> 0 </y>
+ <z> 47.4138 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 1 </dynamic_friction>
+ <rolling_friction> 1 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="WING_TIP_1">
+ <location unit="IN">
+ <x> 838.8898 </x>
+ <y> -667.5197 </y>
+ <z> 35.7926 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 0.4 </dynamic_friction>
+ <rolling_friction> 0.4 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ <contact type="STRUCTURE" name="WING_TIP_2">
+ <location unit="IN">
+ <x> 838.8898 </x>
+ <y> 667.5197 </y>
+ <z> 35.7926 </z>
+ </location>
+ <static_friction> 1.0 </static_friction>
+ <dynamic_friction> 1 </dynamic_friction>
+ <rolling_friction> 1 </rolling_friction>
+ <spring_coeff unit="LBS/FT"> 50000 </spring_coeff>
+ <damping_coeff unit="LBS/FT/SEC"> 50000 </damping_coeff>
+ <max_steer unit="DEG"> 0.0 </max_steer>
+ <brake_group> NONE </brake_group>
+ <retractable>0</retractable>
+ </contact>
+ </ground_reactions>
-<propulsion>
+ <propulsion>
- <engine file="leap1a32">
- <location unit="IN">
- <x> 620.0683 </x>
- <y> -226.575 </y>
- <z> -45.567 </z>
- </location>
- <orient unit="DEG">
- <roll> 0.0 </roll>
- <pitch> 2.2 </pitch>
- <yaw> 1 </yaw>
- </orient>
- <feed>7</feed>
- <thruster file="direct">
+ <engine file="leap1a32">
<location unit="IN">
- <x> 655.4820 </x>
- <y> -226.575 </y>
- <z> 0.000 </z>
+ <x> 620.0683 </x>
+ <y> -226.575 </y>
+ <z> -45.567 </z>
</location>
<orient unit="DEG">
- <roll> 0.0 </roll>
- <pitch> 2.2 </pitch>
- <yaw> 1 </yaw>
+ <roll> 0.0 </roll>
+ <pitch> 2.2 </pitch>
+ <yaw> 1 </yaw>
</orient>
- </thruster>
- </engine>
+ <feed>7</feed>
+ <thruster file="direct">
+ <location unit="IN">
+ <x> 655.4820 </x>
+ <y> -226.575 </y>
+ <z> 0.000 </z>
+ </location>
+ <orient unit="DEG">
+ <roll> 0.0 </roll>
+ <pitch> 2.2 </pitch>
+ <yaw> 1 </yaw>
+ </orient>
+ </thruster>
+ </engine>
- <engine file="leap1a32">
- <location unit="IN">
- <x> 620.0683 </x>
- <y> 226.575 </y>
- <z> -45.567 </z>
- </location>
- <orient unit="DEG">
- <roll> 0.0 </roll>
- <pitch> 2.2 </pitch>
- <yaw> -1 </yaw>
- </orient>
- <feed>8</feed>
- <thruster file="direct">
+ <engine file="leap1a32">
<location unit="IN">
- <x> 655.4820 </x>
- <y> 226.575 </y>
- <z> 0.000 </z>
+ <x> 620.0683 </x>
+ <y> 226.575 </y>
+ <z> -45.567 </z>
</location>
<orient unit="DEG">
- <roll> 0.0 </roll>
- <pitch> 2.2 </pitch>
- <yaw> -1 </yaw>
+ <roll> 0.0 </roll>
+ <pitch> 2.2 </pitch>
+ <yaw> -1 </yaw>
</orient>
- </thruster>
- </engine>
+ <feed>8</feed>
+ <thruster file="direct">
+ <location unit="IN">
+ <x> 655.4820 </x>
+ <y> 226.575 </y>
+ <z> 0.000 </z>
+ </location>
+ <orient unit="DEG">
+ <roll> 0.0 </roll>
+ <pitch> 2.2 </pitch>
+ <yaw> -1 </yaw>
+ </orient>
+ </thruster>
+ </engine>
- <tank type="FUEL"> <!-- Left Tank (Wing tip Ventilation Surge) 0 -->
- <location unit="IN">
- <x> 783.0709 </x>
- <y> -574.4148 </y>
- <z> 3.1080 </z>
- </location>
- <capacity unit="LBS"> 412 </capacity><!-- 1 percent of total capacity, needs 20C to be filled -->
- <contents unit="LBS"> 0 </contents>
-
- <priority>4</priority>
- <type>JET-A1</type>
- <temperature>50</temperature>
- </tank>
- <tank type="FUEL"> <!-- Left Tank (Outer) 1 -->
- <location unit="IN">
- <x> 739.5669 </x>
- <y> -457.4259 </y>
- <z> -8.0898 </z>
- </location>
- <capacity unit="LBS"> 1520.00 </capacity><!-- correct by FCOM -->
- <contents unit="LBS"> 1520 </contents><!-- outer filled first than inner -->
- <standpipe unit="LBS">21</standpipe><!-- minimun fuel on pipes -->
- <priority>2</priority>
- <type>JET-A1</type>
- <temperature>50</temperature>
- </tank>
- <tank type="FUEL"> <!-- Left Tank (Inner) 2 -->
- <location unit="IN">
- <x> 652.5591 </x>
- <y> -236.2992 </y>
- <z> -33.9470 </z>
- </location>
- <capacity unit="LBS"> 11982 </capacity><!-- correct by FCOM -->
- <contents unit="LBS"> 4480 </contents>
- <standpipe unit="LBS">31</standpipe><!-- minimun fuel on pipes -->
- <priority>3</priority>
- <type>JET-A1</type>
- <temperature>50</temperature>
- </tank>
- <tank type="FUEL"> <!-- Center Tank 3 -->
- <location unit="IN">
- <x> 522.0473 </x>
- <y> 0 </y>
- <z> -47.0 </z>
- </location>
- <capacity unit="LBS"> 14281 </capacity><!-- correct by FCOM -->
- <contents unit="LBS"> 0 </contents> <!-- wing tanks filled first -->
- <standpipe unit="LBS">43</standpipe><!-- minimun fuel on pipes -->
- <priority>1</priority>
- <type>JET-A1</type>
- <temperature>50</temperature>
- </tank>
- <tank type="FUEL"> <!-- Right Tank (Inner) 4 -->
- <location unit="IN">
- <x> 652.5591 </x>
- <y> 236.2992 </y>
- <z> -33.9470 </z>
- </location>
- <capacity unit="LBS"> 11982 </capacity><!-- correct by FCOM -->
- <contents unit="LBS"> 4480 </contents>
- <standpipe unit="LBS">31</standpipe><!-- minimum fuel on pipes -->
- <priority>3</priority>
- <type>JET-A1</type>
- <temperature>50</temperature>
- </tank>
- <tank type="FUEL"> <!-- Right Tank (Outer) 5 -->
- <location unit="IN">
- <x> 739.5669 </x>
- <y> 457.4259 </y>
- <z> -8.0898 </z>
- </location>
- <capacity unit="LBS"> 1520 </capacity><!-- need review -->
- <contents unit="LBS"> 1520 </contents><!-- outer tank filled first than inner tank -->
- <standpipe unit="LBS">21</standpipe><!-- minimun fuel on pipes -->
- <priority>2</priority>
- <type>JET-A1</type>
- <temperature>50</temperature>
- </tank>
- <tank type="FUEL"> <!-- Right Tank (Wing tip Ventilation Surge) 6 -->
- <location unit="IN">
- <x> 783.0709 </x>
- <y> 574.4148 </y>
- <z> 3.1080 </z>
- </location>
- <capacity unit="LBS"> 412 </capacity><!-- 1 percent of total fuel capacity, needs 20C-->
- <contents unit="LBS"> 0 </contents>
- <priority>4</priority>
- <type>JET-A1</type>
- <temperature>50</temperature>
- </tank>
- <tank type="FUEL"> <!-- LEFT FUEL PIPES (Engine 1 feed from this) -->
- <location unit="IN">
- <x>589.735</x>
- <y>-226.575</y>
- <z>-45.567</z>
- </location>
- <capacity unit="LBS"> 100 </capacity><!-- need review -->
- <contents unit="LBS"> 0 </contents>
- <priority>1</priority>
- <type>JET-A1</type>
- </tank>
- <tank type="FUEL"> <!-- RIGHT FUEL PIPES (Engine 2 feed from this) -->
- <location unit="IN">
- <x>589.735</x>
- <y>226.575</y>
- <z>-45.567</z>
- </location>
- <capacity unit="LBS"> 100 </capacity><!-- need review -->
- <contents unit="LBS"> 0 </contents>
- <priority>1</priority>
- <type>JET-A1</type>
- </tank>
-</propulsion>
+ <tank type="FUEL"> <!-- Left Tank (Wing tip Ventilation Surge) 0 -->
+ <location unit="IN">
+ <x> 783.0709 </x>
+ <y> -574.4148 </y>
+ <z> 3.1080 </z>
+ </location>
+ <capacity unit="LBS"> 412 </capacity><!-- 1 percent of total capacity, needs 20C to be filled -->
+ <contents unit="LBS"> 0 </contents>
+
+ <priority>4</priority>
+ <type>JET-A1</type>
+ <temperature>50</temperature>
+ </tank>
+ <tank type="FUEL"> <!-- Left Tank (Outer) 1 -->
+ <location unit="IN">
+ <x> 739.5669 </x>
+ <y> -457.4259 </y>
+ <z> -8.0898 </z>
+ </location>
+ <capacity unit="LBS"> 1520.00 </capacity><!-- correct by FCOM -->
+ <contents unit="LBS"> 1520 </contents><!-- outer filled first than inner -->
+ <standpipe unit="LBS">21</standpipe><!-- minimun fuel on pipes -->
+ <priority>2</priority>
+ <type>JET-A1</type>
+ <temperature>50</temperature>
+ </tank>
+ <tank type="FUEL"> <!-- Left Tank (Inner) 2 -->
+ <location unit="IN">
+ <x> 652.5591 </x>
+ <y> -236.2992 </y>
+ <z> -33.9470 </z>
+ </location>
+ <capacity unit="LBS"> 11982 </capacity><!-- correct by FCOM -->
+ <contents unit="LBS"> 4480 </contents>
+ <standpipe unit="LBS">31</standpipe><!-- minimun fuel on pipes -->
+ <priority>3</priority>
+ <type>JET-A1</type>
+ <temperature>50</temperature>
+ </tank>
+ <tank type="FUEL"> <!-- Center Tank 3 -->
+ <location unit="IN">
+ <x> 522.0473 </x>
+ <y> 0 </y>
+ <z> -47.0 </z>
+ </location>
+ <capacity unit="LBS"> 14281 </capacity><!-- correct by FCOM -->
+ <contents unit="LBS"> 0 </contents> <!-- wing tanks filled first -->
+ <standpipe unit="LBS">43</standpipe><!-- minimun fuel on pipes -->
+ <priority>1</priority>
+ <type>JET-A1</type>
+ <temperature>50</temperature>
+ </tank>
+ <tank type="FUEL"> <!-- Right Tank (Inner) 4 -->
+ <location unit="IN">
+ <x> 652.5591 </x>
+ <y> 236.2992 </y>
+ <z> -33.9470 </z>
+ </location>
+ <capacity unit="LBS"> 11982 </capacity><!-- correct by FCOM -->
+ <contents unit="LBS"> 4480 </contents>
+ <standpipe unit="LBS">31</standpipe><!-- minimum fuel on pipes -->
+ <priority>3</priority>
+ <type>JET-A1</type>
+ <temperature>50</temperature>
+ </tank>
+ <tank type="FUEL"> <!-- Right Tank (Outer) 5 -->
+ <location unit="IN">
+ <x> 739.5669 </x>
+ <y> 457.4259 </y>
+ <z> -8.0898 </z>
+ </location>
+ <capacity unit="LBS"> 1520 </capacity><!-- need review -->
+ <contents unit="LBS"> 1520 </contents><!-- outer tank filled first than inner tank -->
+ <standpipe unit="LBS">21</standpipe><!-- minimun fuel on pipes -->
+ <priority>2</priority>
+ <type>JET-A1</type>
+ <temperature>50</temperature>
+ </tank>
+ <tank type="FUEL"> <!-- Right Tank (Wing tip Ventilation Surge) 6 -->
+ <location unit="IN">
+ <x> 783.0709 </x>
+ <y> 574.4148 </y>
+ <z> 3.1080 </z>
+ </location>
+ <capacity unit="LBS"> 412 </capacity><!-- 1 percent of total fuel capacity, needs 20C-->
+ <contents unit="LBS"> 0 </contents>
+ <priority>4</priority>
+ <type>JET-A1</type>
+ <temperature>50</temperature>
+ </tank>
+ <tank type="FUEL"> <!-- LEFT FUEL PIPES (Engine 1 feed from this) -->
+ <location unit="IN">
+ <x>589.735</x>
+ <y>0</y>
+ <z>-45.567</z>
+ </location>
+ <capacity unit="LBS"> 100 </capacity><!-- need review -->
+ <contents unit="LBS"> 0 </contents>
+ <priority>1</priority>
+ <type>JET-A1</type>
+ </tank>
+ <tank type="FUEL"> <!-- RIGHT FUEL PIPES (Engine 2 feed from this) -->
+ <location unit="IN">
+ <x>589.735</x>
+ <y>0</y>
+ <z>-45.567</z>
+ </location>
+ <capacity unit="LBS"> 100 </capacity><!-- need review -->
+ <contents unit="LBS"> 0 </contents>
+ <priority>1</priority>
+ <type>JET-A1</type>
+ </tank>
+ </propulsion>
-<system file="pushback" />
-<system file="fuel" />
-<system file="glass-effect1" />
-<system file="fmgc" />
-<system file="fcs" />
+ <system file="pushback" />
+ <system file="fuel" />
+ <system file="glass-effect1" />
+ <system file="fmgc" />
+ <system file="fcs" />
-<flight_control name="none"/>
+ <flight_control name="none"/>
-<aerodynamics file="Systems/a321-aerodynamics.xml" />
+ <aerodynamics file="Systems/a321-aerodynamics.xml" />
-<external_reactions>
- <force name="pushback" frame="BODY">
- <location unit="IN">
- <x>294</x>
- <y>0</y>
- <z>-149</z>
- </location>
- <direction>
- <x>1</x>
- <y>0</y>
- <z>0</z>
- </direction>
- </force>
-</external_reactions>
+ <external_reactions>
+ <force name="pushback" frame="BODY">
+ <location unit="IN">
+ <x>294</x>
+ <y>0</y>
+ <z>-149</z>
+ </location>
+ <direction>
+ <x>1</x>
+ <y>0</y>
+ <z>0</z>
+ </direction>
+ </force>
+ </external_reactions>
</fdm_config>