From fd7684484a233d0f0244a906ad7b7d794c14fb53 Mon Sep 17 00:00:00 2001 From: Joshua Davidson <joshuadavidson2000@gmail.com> Date: Thu, 29 Jun 2017 15:30:58 -0400 Subject: [PATCH] A3XX: Fix Pipe position, formatting --- A318-100-CFM.xml | 1096 ++++++++++++++++++++++----------------------- A319-100-CFM.xml | 1096 ++++++++++++++++++++++----------------------- A319-100-IAE.xml | 1096 ++++++++++++++++++++++----------------------- A320-100-CFM.xml | 1096 ++++++++++++++++++++++----------------------- A320-200-CFM.xml | 48 +- A320-200-IAE.xml | 1100 +++++++++++++++++++++++----------------------- A320neo-CFM.xml | 1096 ++++++++++++++++++++++----------------------- A321-200-CFM.xml | 1096 ++++++++++++++++++++++----------------------- A321-200-IAE.xml | 1096 ++++++++++++++++++++++----------------------- A321neo-CFM.xml | 1096 ++++++++++++++++++++++----------------------- 10 files changed, 4956 insertions(+), 4960 deletions(-) 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>