update of config for propulsion design (2) - not final

design_evaluator/design_evaluator_conf_propulsion_design.xml

@@ -12,18 +12,24 @@
         </aircraft_design>
     </program_settings>
     <parameters Desc="parameters to be compared">
-            <something>
-                <sub_path ID="0" Name="MTOM">analysis/masses_cg_inertia/maximum_takeoff_mass/mass_properties/mass/value</sub_path>
-            </something>
-            <sub_path ID="1" Name="Position_x">component_design/propulsion/position/x/value</sub_path>
-            <sub_path ID="2" Name="Position_y">component_design/propulsion/position/y/value</sub_path>
-            <sub_path ID="3" Name="Position_z">component_design/propulsion/position/z/value</sub_path>
-            <sub_path ID="4" Name="Engine_mass">component_design/propulsion/mass_properties/mass/value</sub_path>
-            <sub_path ID="5" Name="Engine_inertia_xx">component_design/propulsion/inertia/j_xx/value</sub_path>
-            <sub_path ID="6" Name="Engine_inertia_yy">component_design/propulsion/inertia/j_yy/value</sub_path>
-            <sub_path ID="7" Name="Engine_inertia_zz">component_design/propulsion/inertia/j_zz/value</sub_path>
-            <sub_path ID="8" Name="Engine_inertia_xy">component_design/propulsion/inertia/j_xy/value</sub_path>
-            <sub_path ID="9" Name="Engine_inertia_xz">component_design/propulsion/inertia/j_xz/value</sub_path>
-            <sub_path ID="10" Name="Engine_inertia_yz">component_design/propulsion/inertia/j_yz/value</sub_path>
+            <sub_path ID="0" Name="Position_x">component_design/propulsion/position/x/value</sub_path>
+            <sub_path ID="1" Name="Position_y">component_design/propulsion/position/y/value</sub_path>
+            <sub_path ID="2" Name="Position_z">component_design/propulsion/position/z/value</sub_path>
+            <sub_path ID="3" Name="Engine_mass">component_design/propulsion/mass_properties/mass/value</sub_path>
+            <sub_path ID="4" Name="Engine_inertia_xx">component_design/propulsion/inertia/j_xx/value</sub_path>
+            <sub_path ID="5" Name="Engine_inertia_yy">component_design/propulsion/inertia/j_yy/value</sub_path>
+            <sub_path ID="6" Name="Engine_inertia_zz">component_design/propulsion/inertia/j_zz/value</sub_path>
+            <sub_path ID="7" Name="Engine_inertia_xy">component_design/propulsion/inertia/j_xy/value</sub_path>
+            <sub_path ID="8" Name="Engine_inertia_xz">component_design/propulsion/inertia/j_xz/value</sub_path>
+            <sub_path ID="9" Name="Engine_inertia_yz">component_design/propulsion/inertia/j_yz/value</sub_path>
+            <sub_path ID="10" Name="CoG_x">/component_design/propulsion/mass_properties/center_of_gravity/x/value</sub_path>
+            <sub_path ID="11" Name="CoG_y">/component_design/propulsion/mass_properties/center_of_gravity/y/value</sub_path>
+            <sub_path ID="12" Name="CoG_z">/component_design/propulsion/mass_properties/center_of_gravity/z/value</sub_path>
+            <sub_path ID="13" Name="Nacelle_0_position_x">component_design/propulsion/specific/propulsion/nacelle/position/x/value</sub_path>
+            <sub_path ID="14" Name="Nacelle_0_position_y">component_design/propulsion/specific/propulsion/nacelle/position/y/value</sub_path>
+            <sub_path ID="15" Name="Nacelle_0_position_z">component_design/propulsion/specific/propulsion/nacelle/position/z/value</sub_path>
+            <sub_path ID="16" Name="Pylon_0_position_x">component_design/propulsion/specific/propulsion/pylon/position/x/value</sub_path>
+            <sub_path ID="17" Name="Pylon_0_position_y">component_design/propulsion/specific/propulsion/pylon/position/y/value</sub_path>
+            <sub_path ID="18" Name="Pylon_0_position_z">component_design/propulsion/specific/propulsion/pylon/position/z/value</sub_path>
         </parameters>
 </config_file>
\ No newline at end of file