Update overshoot tanks allowed during the first iterations (same as in landing gear)

Removed the error message for the first iterations also from the defueling function

weight_and_balance_analysis/src/tube_and_wing/standard/basic/methodbasic.py

@@ -179,7 +179,7 @@ def method_basic(paths_and_names, routing_dict, dict_ac_exchange, dict_mod_confi
     maximum_takeoff_mass.path_to_element = "./analysis/masses_cg_inertia/maximum_takeoff_mass"
     maximum_takeoff_mass.cg_mac = (
         design_mass_takeoff.center_of_gravity['x'] - x_leading_edge_mac) / mac * 100
-    maximum_takeoff_mass.print("Maximum takeoff mass")
+    maximum_takeoff_mass.print("Maximum Takeoff Mass")
 
     # Maximum payload + fuel up to MTOW
     mtow_max_payload_mass = calculate_mtow_max_payload(
@@ -315,10 +315,12 @@ def method_basic(paths_and_names, routing_dict, dict_ac_exchange, dict_mod_confi
 
     # Prepare defueling
     defueling_mass_per_tank = calculate_fuel_properties_defueling(
-        sorted_tanks_defueling, consumed_fuel, design_fuel_mass_takeoff_per_tank, runtime_output)
+        sorted_tanks_defueling, consumed_fuel, design_fuel_mass_takeoff_per_tank,
+        runtime_output, routing_dict, dict_ac_exchange)
 
     defueling_mass_per_tank_ferry = calculate_fuel_properties_defueling(
-        sorted_tanks_defueling, consumed_fuel, maximum_fuel_mass_per_tank, runtime_output)
+        sorted_tanks_defueling, consumed_fuel, maximum_fuel_mass_per_tank,
+        runtime_output, routing_dict, dict_ac_exchange)
 
     starting_mass = total_mass_cargo_back_front[-1]
     starting_cg = cg_positions_over_mac_cargo_front_back[-1] * \
@@ -1194,7 +1196,8 @@ def calculate_fuel_mass_properties(tanks, fuel_mass, routing_dict, dict_ac_excha
     return fuel_mass_properties, fuel_mass_per_tank
 
 
-def calculate_fuel_properties_defueling(tanks, fuel_to_remove, fuel_mass_per_tank, runtime_output):
+def calculate_fuel_properties_defueling(
+        tanks, fuel_to_remove, fuel_mass_per_tank, runtime_output, routing_dict, dict_ac_exchange):
 
     def map_fuel_mass_to_tanks(tanks, fuel_mass_per_tank, runtime_output):
 
@@ -1255,10 +1258,12 @@ def calculate_fuel_properties_defueling(tanks, fuel_to_remove, fuel_mass_per_tan
     total_fuel_available = sum(tank.filled_fuel_mass for tank in tanks)
 
     if fuel_to_remove > total_fuel_available:
-        runtime_output.critical(
-            "Fuel to remove exceeds the available fuel in all tanks!")
-        raise ValueError(
-            "Fuel to remove exceeds the available fuel in all tanks!")
+        if int(dict_ac_exchange['tool_level']) < int(routing_dict['tool_level']):
+            runtime_output.warning(
+                "Fuel to remove exceeds the available fuel in all tanks!")
+        else:
+            raise ValueError(
+                "Fuel to remove exceeds the available fuel in all tanks!")
 
     remaining_fuel_to_remove = fuel_to_remove
     defueled_mass_per_tank = []
@@ -1374,9 +1379,12 @@ def calculate_fuel_properties_defueling(tanks, fuel_to_remove, fuel_mass_per_tan
 
     # Check if we have defueled the correct amount
     if remaining_fuel_to_remove > 0:
-        runtime_output.critical(
-            "Not enough fuel in the tanks to complete defueling!")
-        raise ValueError("Not enough fuel in the tanks to complete defueling!")
+        if int(dict_ac_exchange['tool_level']) < int(routing_dict['tool_level']):
+            runtime_output.warning(
+                "Not enough fuel in the tanks to complete defueling!")
+        else:
+            raise ValueError(
+                "Not enough fuel in the tanks to complete defueling!")
 
     return defueled_mass_per_tank