landing_gear_design: - bug fix of maximum nose gear position error

Description

• bug fix in estimation of initial main gear position - -> now the max nose gear position error should only occurred for fuselage lengths above 50 meter

Related Issue(s)

-no related issues

Other Changes

• no other changes

Screenshots/Logs

Attach screenshots or log outputs if applicable.

Testing Instructions

1. run the tlar test for different passenger class distribution

Developer Checklist

• Code has been tested locally and/or in pipeline.
• (if applicable) documentation updated.
• (if applicable) impact of new dependencies reviewed and included in project.
• Merge conflicts resolved with the target branch.

Additional Notes

• code change tested by @AndiGob locally -> no errors occurred

landing_gear_design/src/wing_mounted/empirical/landing_gear_design_tu_berlin/general/call_functions/_00_estimatepositions.py

@@ -87,10 +87,8 @@ def estimate_positions(dict_ac_exchange, dict_mod_config, landing_gear_descripti
             not ('main_gear_x_position' in landing_gear_positions):
         _, landing_gear_position_value = \
             next(reversed(list(dict_ac_exchange['landing_gear_positions_in_x_direction'].items())), (None, None))
-        _, wing_reference_point_value = \
-            next(reversed(list(dict_ac_exchange['wing_section_position_in_x'].items())), (None, None))
-        _, wing_chord_length_value = \
-            next(reversed(list(dict_ac_exchange['wing_chord_length_on_section'].items())), (None, None))
+        wing_reference_point_value = next(iter(dict_ac_exchange['wing_section_position_in_x'].values()))
+        wing_chord_length_value = next(iter(dict_ac_exchange['wing_chord_length_on_section'].values()))
         # Check if the main gear position and the wing center reference point
         #  and the o most aft CoG position in x direction are None.
         #   -> if true: -> Check which kind of fuselage type is selected and set type specific start values.