Sim: Fix weights to proper locations, Aero: Adjust drag
This commit is contained in:
Joshua Davidson
parent
93bd21099a
commit
0e7dd5b62f
4 changed files with 66 additions and 21 deletions
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@ -446,22 +446,40 @@
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<max-lb type="double">440</max-lb>
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<max-lb type="double">440</max-lb>
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</weight>
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</weight>
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<weight n="1">
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<weight n="1">
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<name>Passengers</name>
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<name>Forward Cabin</name>
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<weight-lb alias="/fdm/jsbsim/inertia/pointmass-weight-lbs[1]"/>
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<weight-lb alias="/fdm/jsbsim/inertia/pointmass-weight-lbs[1]"/>
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<min-lb type="double">0</min-lb>
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<min-lb type="double">0</min-lb>
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<max-lb type="double">24360</max-lb>
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<max-lb type="double">4649</max-lb>
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</weight>
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</weight>
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<weight n="2">
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<weight n="2">
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<name>Forward Cargo</name>
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<name>Center Cabin</name>
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<weight-lb alias="/fdm/jsbsim/inertia/pointmass-weight-lbs[2]"/>
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<weight-lb alias="/fdm/jsbsim/inertia/pointmass-weight-lbs[2]"/>
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<min-lb type="double">0</min-lb>
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<min-lb type="double">0</min-lb>
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<max-lb type="double">9400</max-lb>
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<max-lb type="double">13949</max-lb>
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</weight>
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</weight>
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<weight n="3">
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<weight n="3">
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<name>Aft Cargo</name>
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<name>Aft Cabin</name>
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<weight-lb alias="/fdm/jsbsim/inertia/pointmass-weight-lbs[3]"/>
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<weight-lb alias="/fdm/jsbsim/inertia/pointmass-weight-lbs[3]"/>
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<min-lb type="double">0</min-lb>
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<min-lb type="double">0</min-lb>
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<max-lb type="double">9400</max-lb>
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<max-lb type="double">10462</max-lb>
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</weight>
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<weight n="4">
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<name>Forward Cargo</name>
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<weight-lb alias="/fdm/jsbsim/inertia/pointmass-weight-lbs[4]"/>
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<min-lb type="double">0</min-lb>
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<max-lb type="double">5000</max-lb>
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</weight>
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<weight n="5">
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<name>Aft Cargo</name>
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<weight-lb alias="/fdm/jsbsim/inertia/pointmass-weight-lbs[5]"/>
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<min-lb type="double">0</min-lb>
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<max-lb type="double">6662</max-lb>
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</weight>
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<weight n="6">
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<name>Aft Bulk Cargo</name>
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<weight-lb alias="/fdm/jsbsim/inertia/pointmass-weight-lbs[6]"/>
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<min-lb type="double">0</min-lb>
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<max-lb type="double">3285</max-lb>
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</weight>
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</weight>
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</payload>
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</payload>
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@ -181,9 +181,9 @@
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<independentVar lookup="row">aero/alpha-rad</independentVar>
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<independentVar lookup="row">aero/alpha-rad</independentVar>
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<tableData>
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<tableData>
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-1.57 1.3083
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-1.57 1.3083
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-0.20 0.0331
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-0.20 0.0301
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0.00 0.0000
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0.00 0.0000
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0.20 0.0331
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0.20 0.0301
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1.57 1.3083
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1.57 1.3083
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</tableData>
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</tableData>
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</table>
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</table>
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@ -210,7 +210,7 @@
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<tableData>
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<tableData>
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0.00 0.000
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0.00 0.000
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0.20 0.000
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0.20 0.000
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0.79 0.002
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0.82 0.002
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1.10 0.023
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1.10 0.023
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1.80 0.015
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1.80 0.015
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</tableData>
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</tableData>
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@ -20,38 +20,65 @@
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</location>
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</location>
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<pointmass name="Crew">
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<pointmass name="Crew">
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<weight unit="LBS">380</weight>
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<weight unit="LBS">320</weight>
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<location name="POINTMASS" unit="M">
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<location name="POINTMASS" unit="M">
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<x> 5.29845 </x>
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<x> 5.29845 </x>
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<y> 0 </y>
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<y> 0 </y>
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<z> -0.66384 </z>
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<z> 0.5 </z>
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</location>
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</location>
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</pointmass>
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</pointmass>
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<pointmass name="PAX">
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<pointmass name="Forward Cabin">
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<weight unit="LBS">23000</weight>
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<weight unit="LBS">3722</weight>
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<location name="POINTMASS" unit="M">
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<location name="POINTMASS" unit="M">
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<x> 18.8231 </x>
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<x> 10 </x>
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<y> 0 </y>
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<y> 0 </y>
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<z> 0.19249 </z>
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<z> 0.5 </z>
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</location>
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</pointmass>
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<pointmass name="Center Cabin">
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<weight unit="LBS">11361</weight>
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<location name="POINTMASS" unit="M">
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<x> 16.5 </x>
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<y> 0 </y>
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<z> 0.5 </z>
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</location>
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</pointmass>
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<pointmass name="Aft Cabin">
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<weight unit="LBS">8422</weight>
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<location name="POINTMASS" unit="M">
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<x> 26 </x>
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<y> 0 </y>
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<z> 0.5 </z>
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</location>
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</location>
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</pointmass>
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</pointmass>
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<pointmass name="Fwd Cargo">
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<pointmass name="Fwd Cargo">
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<weight unit="LBS">3000</weight>
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<weight unit="LBS">3000</weight>
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<location name="POINTMASS" unit="M">
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<location name="POINTMASS" unit="M">
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<x> 13.0849 </x>
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<x> 14.0 </x>
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<y> 0 </y>
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<y> 0 </y>
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<z> -1.18112 </z>
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<z> -1.1 </z>
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</location>
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</location>
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</pointmass>
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</pointmass>
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<pointmass name="Aft Cargo">
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<pointmass name="Aft Cargo">
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<weight unit="LBS">3000</weight>
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<weight unit="LBS">3000</weight>
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<location name="POINTMASS" unit="M">
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<location name="POINTMASS" unit="M">
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<x> 24.5565 </x>
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<x> 24.0 </x>
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<y> 0 </y>
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<y> 0 </y>
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<z> -1.18112 </z>
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<z> -1.1 </z>
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</location>
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</pointmass>
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<pointmass name="Aft Bulk Cargo">
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<weight unit="LBS">0</weight>
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<location name="POINTMASS" unit="M">
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<x> 29.0 </x>
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<y> 0 </y>
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<z> -1.1 </z>
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</location>
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</location>
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</pointmass>
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</pointmass>
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</mass_balance>
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</mass_balance>
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@ -1 +1 @@
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4753
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4754
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