fuel calculation corrections

aircraft.csv

@@ -7,7 +7,7 @@ Airbus A330-300,6350,11760.2,5700,490,907.48,12.96,73872
 Airbus A340-300,7300,13519.6,6500,488,903.78,14.96,97240
 Airbus A340-500,9000,16668,8000,488,903.78,18.44,147520
 Airbus A350-900,8100,15732,5800,470,903,17.23,165000
-Airbus A380,8000,14816,12280,470,903,17.35,256000
+Airbus A380-800,8000,14816,12280,470,903,17.35,256000
 Boeing 737-800,2935,5435.62,2530,455,842.66,6.45,16318.5
 Boeing 747-400,7260,13445.52,10230,488,903.78,14.88,152222.4
 Boeing 747-8,7730,14315.96,9600,470,870.44,16.45,157920
@@ -15,9 +15,9 @@ Boeing 757-200,3915,7250.58,3320,470,870.44,8.33,27655.6
 Boeing 767-200,3900,7222.8,4500,470,870.44,8.3,37350
 Boeing 767-300,4020,7445.04,4800,470,870.44,8.55,41040
 Boeing 767-300ER,5980,11074.96,4940,490,907.48,12.2,60268
-Boeing 777-200,5240,9704.48,6080,490,907.48,10.69,93872
+Boeing 777-200,5240,9704.48,6080,490,907.48,10.69,136936
 Boeing 777-200ER,7725,14306.7,6630,470,870.44,16.44,136936
 Boeing 777-200LR,8555,15843.86,6800,488,903.78,17.53,145024
 Boeing 777-300ER,7370,13649.24,7700,447,827.84,16.49,145024
-Boeing 787-8,7355,13621.46,4900,447,827.84,16.45,101343
-Boeing 787-9,7530,13945.56,5600,447,827.84,17.45,101522
+Boeing 787-8,7355,13621.46,4900,447,903,16.45,101343
+Boeing 787-9,7530,13945.56,5600,447,903,17.45,101522

flight_distance.py

@@ -134,7 +134,7 @@ def calculate_fuel_and_time(distance, cruising_speed, fuel_burn_rate, reserve_fu
     """
     # Phase speeds and times
     climb_speed = cruising_speed*0.3 # km/h
-    descent_speed = cruising_speed*0.2  # km/h
+    descent_speed = cruising_speed*0.3  # km/h
     climb_descent_distance = round(distance * climb_descent_fraction,2)
     cruise_distance = round(distance - (2 * climb_descent_distance),2)  # Remaining distance for cruise
 
@@ -148,12 +148,13 @@ def calculate_fuel_and_time(distance, cruising_speed, fuel_burn_rate, reserve_fu
     climb_time = round(climb_descent_distance / climb_speed,2)
     descent_time = round(climb_descent_distance / descent_speed,2)
     # Total flight time
-    print(climb_descent_distance,climb_time,cruise_distance, cruise_time,descent_time)
+    # print(climb_descent_distance,climb_time,cruise_distance, cruise_time,descent_time)
     total_flight_time = climb_time + cruise_time + descent_time
 
     # Fuel calculations
     fuel_required = total_flight_time * fuel_burn_rate
     reserve_fuel = reserve_fuel_percentage * max_fuel_capacity
+    # print(fuel_burn_rate, fuel_required, reserve_fuel)
     total_fuel_with_reserve = fuel_required + reserve_fuel
 
     return total_fuel_with_reserve, total_flight_time