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Weight points and tanks

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This commit is contained in:
JWocky 2016-11-08 07:38:48 -06:00
parent bb72d27122
commit 08b656bfbb
2 changed files with 126 additions and 100 deletions
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130
A320-200-IAE.xml
View file

@ -75,8 +75,8 @@ YAW MOI_________3950000______23089847_______24848934
<iyz unit="SLUG*FT2"> 0 </iyz>
<emptywt unit="LBS">80431</emptywt> <!-- #ref-1 page 67, WV016. 90927lbs - 5248x2 (engines)=80431lbs-->
<!-- #### PB: That makes no sense, the wohle aircraft is 1479.1339 inches long. 650inches eqauls to about 43.95% MAC with the Airbus limits according to the AMM between 45% and 49%
Also: The z-axis is -41.73 unches under the zero line of the plane while the pressure point is only -25,91 under the same line and slightly ahead, that causes the plane to behave quite unstable
<!-- #### PB: That makes no sense, the whole aircraft is 1479.1339 inches long. 650inches eqauls to about 43.95% MAC with the Airbus limits according to the AMM between 45% and 49%
Also: The z-axis is -41.73 inches under the zero line of the plane while the pressure point is only -25,91 under the same line and slightly ahead, that causes the plane to behave quite unstable
-->
<!-- location name="CG" unit="IN">
<! - -x> 642.122 </x- - >
@ -90,99 +90,77 @@ YAW MOI_________3950000______23089847_______24848934
<z> 0.00 </z>
</location>
<pointmass name="Crew">
<weight unit="LBS">400</weight> <!-- MAX: 600lbs-->
<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="PAX">
<weight unit="LBS">19750</weight> <!-- MAX: 39500 lbs ** looks too heavy. maybe low it and give a long cilinder shape. need to do some maths-->
<form shape="cylinder">
<radius unit="M"> 2.13 </radius>
<length unit="M"> 24.44 </length>
</form>
<pointmass name="Cabin Crew">
<weight unit="LBS">600</weight> <!-- MAX: 1320lbs, up to six flight-attendants-->
<location name="POINTMASS" unit="IN">
<x>705</x>
<x>696</x>
<y>0</y>
<z>0</z>
</location>
</pointmass>
<!-- NEW Pointmasses Start Weights for good CG -->
<pointmass name="Fwd Cargo">
<weight unit="LBS">3750</weight> <!-- #REF-3 page 19, MAX 3402 kilograms = 7500.12616 lbs -->
<form shape="cylinder">
<radius unit="M"> 1.24 </radius>
<length unit="M"> 4.95 </length>
</form>
<pointmass name="PAX 0A (60 seats)">
<weight unit="LBS">6600</weight> <!-- MAX: 13200lbs, 60 seats -->
<location name="POINTMASS" unit="IN">
<!-- #REF-1 page 88+98,
x= (door form nose(8.16m))-(door with(1.816m)/2)+(Cargo compartment lenght(4.953m)/2)
x= 9.7285 meters = 383.011811 in
-->
<x>383.01</x>
<x>450.1711</x>
<y>0</y>
<z>-59.05</z> <!-- Aprox lower deck 1.5 meters = 59.0551181 in -->
<z>0</z>
</location>
</pointmass>
<pointmass name="Aft Cargo">
<weight unit="LBS">0</weight> <!-- #REF-3 page 19, MAX 4536 kilograms = 10000.1682 lbs -->
<form shape="cylinder">
<radius unit="M"> 1.24 </radius>
<length unit="M"> 6.6 </length>
</form>
<pointmass name="PAX 0B (60 seats)">
<weight unit="LBS">6600</weight> <!-- MAX: 13200lbs, 60 seats -->
<location name="POINTMASS" unit="IN">
<!-- #REF-1 page 88+98,
x= (door form nose(22.69m))-(door with(1.816m)/2)
x= 21.78200 meters = 857.559055 in
-->
<x>857.55</x>
<x>739.5669</x>
<y>0</y>
<z>-59.05</z> <!-- Aprox lower deck 1.5 meters = 59.0551181 in -->
<z>0</z>
</location>
</pointmass>
<pointmass name="Rear Bulk Cargo">
<weight unit="LBS">0</weight> <!-- #REF-3 page 19, MAX 1497 kilograms = 3300.32006 lbs -->
<form shape="cylinder">
<radius unit="M"> 1.24 </radius>
<length unit="M"> 2 </length>
</form>
<pointmass name="PAX 0C (54 seats)">
<weight unit="LBS">5940</weight> <!-- MAX: 11880lbs, 54 seats -->
<location name="POINTMASS" unit="IN">
<!-- #REF-1 page 88+102,
x= (door form nose(22.69m))+(door with(1.816m)/2)+( Dist. between rear doors(2.19))+(Aprox to compartment center (2m))
x= 27.78800 meters = 1 094.01575 in
-->
<x>1094</x>
<x>1093.2729</x>
<y>0</y>
<z>-39.37</z> <!-- Aprox bulk lower deck 1 meter = 39.3700787 in -->
<z>0</z>
</location>
</pointmass>
<pointmass name="Engine1">
<weight unit="LBS">5248</weight>
<form shape="cylinder">
<radius unit="M"> 1.31 </radius>
<length unit="M"> 5 </length>
</form>
<pointmass name="Cargo Hold 1">
<weight unit="LBS">2000</weight> <!-- MAX: 7500.126lbs -->
<location name="POINTMASS" unit="IN">
<x>589.735</x>
<y>-226.575</y>
<z>-45.567</z>
<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>
<pointmass name="Engine2">
<weight unit="LBS">5248</weight>
<form shape="cylinder">
<radius unit="M"> 1.31 </radius>
<length unit="M"> 5 </length>
</form>
<!-- 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>589.735</x>
<y>226.575</y>
<z>-45.567</z>
<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>
@ -430,6 +408,7 @@ YAW MOI_________3950000______23089847_______24848934
</ground_reactions>
<propulsion>
<engine file="v2527_a5">
<location unit="IN">
<x> 589.735 </x>
@ -457,6 +436,7 @@ YAW MOI_________3950000______23089847_______24848934
</orient>
</thruster>
</engine>
<engine file="v2527_a5">
<location unit="IN">
<x> 589.735 </x>
@ -488,7 +468,7 @@ YAW MOI_________3950000______23089847_______24848934
<tank type="FUEL"> <!-- Left Tank (Wing tip Ventilation Surge) 0 -->
<location unit="IN">
<x> 788.4322 </x>
<x> 783.0709 </x>
<y> -574.4148 </y>
<z> 3.1080 </z>
</location>
@ -501,7 +481,7 @@ YAW MOI_________3950000______23089847_______24848934
</tank>
<tank type="FUEL"> <!-- Left Tank (Outer) 1 -->
<location unit="IN">
<x> 737.4190 </x>
<x> 739.5669 </x>
<y> -457.4259 </y>
<z> -8.0898 </z>
</location>
@ -514,7 +494,7 @@ YAW MOI_________3950000______23089847_______24848934
</tank>
<tank type="FUEL"> <!-- Left Tank (Inner) 2 -->
<location unit="IN">
<x> 630.6588 </x>
<x> 652.5591 </x>
<y> -236.2992 </y>
<z> -33.9470 </z>
</location>
@ -527,7 +507,7 @@ YAW MOI_________3950000______23089847_______24848934
</tank>
<tank type="FUEL"> <!-- Center Tank 3 -->
<location unit="IN">
<x> 580.9955 </x>
<x> 522.0473 </x>
<y> 0 </y>
<z> -47.0 </z>
</location>
@ -540,7 +520,7 @@ YAW MOI_________3950000______23089847_______24848934
</tank>
<tank type="FUEL"> <!-- Right Tank (Inner) 4 -->
<location unit="IN">
<x> 630.6588 </x>
<x> 652.5591 </x>
<y> 236.2992 </y>
<z> -33.9470 </z>
</location>
@ -553,7 +533,7 @@ YAW MOI_________3950000______23089847_______24848934
</tank>
<tank type="FUEL"> <!-- Right Tank (Outer) 5 -->
<location unit="IN">
<x> 737.4190 </x>
<x> 739.5669 </x>
<y> 457.4259 </y>
<z> -8.0898 </z>
</location>
@ -566,7 +546,7 @@ YAW MOI_________3950000______23089847_______24848934
</tank>
<tank type="FUEL"> <!-- Right Tank (Wing tip Ventilation Surge) 6 -->
<location unit="IN">
<x> 788.4322 </x>
<x> 783.0709 </x>
<y> 574.4148 </y>
<z> 3.1080 </z>
</location>

72
A320-main.xml
View file

@ -158,6 +158,65 @@
</fuel>
</consumables>
<payload>
<weight n="0">
<name>Cockpit Crew</name>
<weight-lb alias="/fdm/jsbsim/inertia/pointmass-weight-lbs[0]" />
<min-lb type="double">200</min-lb>
<max-lb type="double">440</max-lb>
</weight>
<weight n="1">
<name>Cabin Crew</name>
<weight-lb alias="/fdm/jsbsim/inertia/pointmass-weight-lbs[1]" />
<min-lb type="double">300</min-lb>
<max-lb type="double">1320</max-lb>
</weight>
<weight n="2">
<name>PAX 0A (60 seats)</name>
<weight-lb alias="/fdm/jsbsim/inertia/pointmass-weight-lbs[2]" />
<min-lb type="double">300</min-lb>
<max-lb type="double">13200</max-lb>
</weight>
<weight n="3">
<name>PAX 0B (60 seats)</name>
<weight-lb alias="/fdm/jsbsim/inertia/pointmass-weight-lbs[3]" />
<min-lb type="double">300</min-lb>
<max-lb type="double">13200</max-lb>
</weight>
<weight n="4">
<name>PAX 0C (54 seats)</name>
<weight-lb alias="/fdm/jsbsim/inertia/pointmass-weight-lbs[4]" />
<min-lb type="double">300</min-lb>
<max-lb type="double">11880</max-lb>
</weight>
<weight n="5">
<name>Cargo Hold 1</name>
<weight-lb alias="/fdm/jsbsim/inertia/pointmass-weight-lbs[5]" />
<min-lb type="double">0</min-lb>
<max-lb type="double">7500.126</max-lb>
</weight>
<weight n="6">
<name>Cargo Hold 3</name>
<weight-lb alias="/fdm/jsbsim/inertia/pointmass-weight-lbs[6]" />
<min-lb type="double">0</min-lb>
<max-lb type="double">5384.414</max-lb>
</weight>
<weight n="7">
<name>Cargo Hold 4</name>
<weight-lb alias="/fdm/jsbsim/inertia/pointmass-weight-lbs[7]" />
<min-lb type="double">0</min-lb>
<max-lb type="double">4651.754</max-lb>
</weight>
<weight n="8">
<name>Cargo Hold 5</name>
<weight-lb alias="/fdm/jsbsim/inertia/pointmass-weight-lbs[8]" />
<min-lb type="double">0</min-lb>
<max-lb type="double">3300.320</max-lb>
</weight>
</payload>
<it-autoflight>
<settings>
<altitude-dial-mode>0</altitude-dial-mode>
@ -188,19 +247,6 @@
</settings>
</it-autoflight>
<payload>
<weight n="0">
<name>Crew</name>
<weight-lb alias="/fdm/jsbsim/inertia/pointmass-weight-lbs[0]" />
<min-lb type="double">120</min-lb>
<max-lb type="double">600</max-lb>
</weight>
<weight n="1">
<name>PAX</name>
<weight-lb alias="/fdm/jsbsim/inertia/pointmass-weight-lbs[1]" />
</weight>
</payload>
<autopilot>
<autobrake>
<config>