fuel calculation

aircraft.csv

@@ -1,23 +1,23 @@
-Aircraft,Range_NauticalMiles,Range_km,Fuel_Consumption_kg/hr,Cruising Speed (kts),Speed_kmh,MaxFlightTime_hr,Max_Fuel_Capacity_kg
-Boeing 737-800,2935,5435.62,2530,455,842.66,6.45,16318.50
-Airbus A321-100,3000,5556,2885,493,913.04,6.09,17569.65
-Airbus A321-231,3200,5926.4,2740,493,913.04,6.49,17782.60
-Airbus A320,3300,6111.6,2430,468,866.74,7.05,17131.50
-Boeing 767-200,3900,7222.8,4500,470,870.44,8.3,37350.00
-Boeing 757-200,3915,7250.58,3320,470,870.44,8.33,27655.60
-Boeing 767-300,4020,7445.04,4800,470,870.44,8.55,41040.00
-Boeing 777-200,5240,9704.48,6080,490,907.48,10.69,64995.20
-Boeing 767-300ER,5980,11074.96,4940,490,907.48,12.2,60268.00
-Airbus A330-300,6350,11760.2,5700,490,907.48,12.96,73872.00
-Airbus A330-200,7250,13427,5590,490,907.48,14.8,82732.00
-Boeing 747-400,7260,13445.52,10230,488,903.78,14.88,152222.40
-Airbus A340-300,7300,13519.6,6500,488,903.78,14.96,97240.00
-Boeing 787-8,7355,13621.46,4900,447,827.84,16.45,80605.00
-Boeing 777-300ER,7370,13649.24,7500,447,827.84,16.49,123675.00
-Boeing 787-9,7530,13945.56,5600,447,827.84,16.85,94360.00
-Boeing 777-200ER,7725,14306.7,6630,470,870.44,16.44,108997.20
-Boeing 747-8,7730,14315.96,9600,470,870.44,16.45,157920.00
-Airbus A380,8000,14816,11000,470,870.44,17.02,187220.00
-Airbus A350-900,8100,15001.2,5800,470,870.44,17.23,99934.00
-Boeing 777-200LR,8555,15843.86,6800,488,903.78,17.53,119204.00
-Airbus A340-500,9000,16668,8000,488,903.78,18.44,147520.00
+Aircraft,Range_NauticalMiles,Range_km,Fuel_Consumption_kg/hr,Cruising Speed (kts),Speed_kmh,MaxFlightTime_hr,Max_Fuel_Capacity_kg
+Airbus A320,3300,6111.6,2430,468,866.74,7.05,17131.5
+Airbus A321-100,3000,5556,2885,493,913.04,6.09,17569.65
+Airbus A321-231,3200,5926.4,2740,493,913.04,6.49,17782.6
+Airbus A330-200,7250,13427,5590,490,907.48,14.8,82732
+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 A350-900,8100,15732,5800,470,870.44,17.23,165000
+Airbus A380,8000,14816,12280,470,870.44,17.35,256000
+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
+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 777-200,5240,9704.48,6080,490,907.48,10.69,64995.2
+Boeing 777-200ER,7725,14306.7,6630,470,870.44,16.44,108997.2
+Boeing 777-200LR,8555,15843.86,6800,488,903.78,17.53,119204
+Boeing 777-300ER,7370,13649.24,7700,447,827.84,16.49,127154.39
+Boeing 787-8,7355,13621.46,4900,447,827.84,16.45,80605
+Boeing 787-9,7530,13945.56,5600,447,827.84,17.45,12116

flight_distance.py

@@ -121,7 +121,7 @@ def calculate_distances(airport_identifiers):
 
     return distances
 
-def calculate_fuel_and_time(distance, cruising_speed, fuel_burn_rate, reserve_fuel_percentage, max_fuel_capacity):
+def calculate_fuel_and_time(distance, cruising_speed, fuel_burn_rate, reserve_fuel_percentage, max_fuel_capacity, climb_descent_fraction=0.02):
     """
     Calculate the total fuel required for a given distance including reserve fuel and flight time.
 
@@ -133,24 +133,20 @@ def calculate_fuel_and_time(distance, cruising_speed, fuel_burn_rate, reserve_fu
     :return: Total fuel required including reserve, and estimated flight time
     """
     # Phase speeds and times
-    climb_speed = 280  # km/h
-    climb_time = 15 / 60  # 15 minutes in hours
-    descent_speed = 250  # km/h
-    descent_time = 10 / 60  # 10 minutes in hours
-
-    # Calculate distances for each phase
-    climb_distance = climb_speed * climb_time
-    descent_distance = descent_speed * descent_time
-    cruise_distance = distance - (climb_distance + descent_distance)
+    climb_speed = cruising_speed*0.7
+    descent_speed = cruising_speed*0.6  # km/h
+    climb_descent_distance = distance * climb_descent_fraction
+    cruise_distance = distance - (2 * climb_descent_distance)  # Remaining distance for cruise
 
     # Adjust if cruise distance is negative (short flights)
     if cruise_distance < 0:
-        climb_time = climb_distance / climb_speed
-        descent_time = descent_distance / descent_speed
+        climb_time = climb_descent_distance / climb_speed
+        descent_time = climb_descent_distance / descent_speed
         cruise_distance = 0
 
     cruise_time = cruise_distance / cruising_speed
-
+    climb_time = climb_descent_distance / climb_speed
+    descent_time = climb_descent_distance / descent_speed
     # Total flight time
     total_flight_time = climb_time + cruise_time + descent_time
 

flight_route_ui.py

@@ -48,7 +48,7 @@ def check_route(airport_selections, aircraft_type):
     # Convert all dictionary keys to strings for JSON compatibility
     return {
         "Optimal Route": " -> ".join(optimal_route) + f" -> {optimal_route[0]}",
-        "Total Adjusted Distance/Cost": str(optimal_distance),  # Convert to string if necessary
+        "Total Round Trip Distance": str(optimal_distance),  # Convert to string if necessary
         "Can Fly Route": str(result)  # Convert to string if necessary
     }
 

main.py

@@ -27,7 +27,7 @@ optimal_route, optimal_distance = find_optimal_route(airport_identifiers, trip_d
 
 # Display the optimal route and the total adjusted distance/cost
 print("Optimal Route:", " -> ".join(optimal_route) + f" -> {optimal_route[0]}")
-print("Total Adjusted Distance/Cost:", optimal_distance)
+print("Total Adjusted Distance:", optimal_distance)
 
 aircraft_type = input("Enter the aircraft type: ")
 

weather.py

@@ -7,7 +7,7 @@ from functools import lru_cache
 API_KEY = '9811dd1481209c64fba6cb2c90f27140'
 
 # Interpolation function to get intermediate points between airports
-def get_intermediate_points(start, end, num_points=2):
+def get_intermediate_points(start, end, num_points=4):
     points = []
     lat_step = (end[0] - start[0]) / (num_points + 1)
     lon_step = (end[1] - start[1]) / (num_points + 1)