import pandas as pd from math import * def get_aircraft_details(aircraft_type): # Load the CSV file csv_file = r'aircraft.csv' # Replace with the actual path if needed df = pd.read_csv(csv_file) # Check if the aircraft type exists in the DataFrame if aircraft_type not in df['Aircraft'].values: return f"Aircraft type '{aircraft_type}' not found in the dataset." # Fetch the relevant details for the given aircraft type aircraft_details = df[df['Aircraft'] == aircraft_type][[ 'Range_km', 'Fuel_Consumption_kg/hr', 'Cruising Speed (kts)', 'Speed_kmh', 'MaxFlightTime_hr', 'Max_Fuel_Capacity_kg' ]] # Convert the result to a dictionary for easier reading details_dict = aircraft_details.to_dict(orient='records')[0] return details_dict def get_airport_lat_long(identifiers): """ Fetch latitude and longitude for a list of airport names or IATA codes. :param identifiers: List of airport names or IATA codes (minimum of 2) :return: Dictionary with airport identifiers as keys and (latitude, longitude) tuples as values """ if len(identifiers) < 2: return "Please provide at least two airport identifiers." # Load the CSV file csv_file = r'airport.csv' # Replace with the actual path if needed df = pd.read_csv(csv_file) # Efficiently filter rows where the 'Name' or 'IATA' matches any of the provided identifiers df_filtered = df[df['Airport_Name'].isin(identifiers) | df['IATA'].isin(identifiers)] # Extract relevant information and store in a dictionary lat_long_dict = {} for _, row in df_filtered.iterrows(): identifier = row['IATA'] if row['IATA'] in identifiers else row['Name'] lat_long_dict[identifier] = (row['Lat'], row['Long']) # Check if all identifiers were found not_found = [id for id in identifiers if id not in lat_long_dict] if not_found: return f"These identifiers were not found: {', '.join(not_found)}" return lat_long_dict def haversine_distance(lat1, lon1, lat2, lon2): """ Calculate the Haversine distance between two points on the Earth. """ R = 6371.0 # Radius of Earth in kilometers # Convert latitude and longitude from degrees to radians lat1, lon1, lat2, lon2 = map(radians, [lat1, lon1, lat2, lon2]) # Haversine formula dlat = lat2 - lat1 dlon = lon2 - lon1 a = sin(dlat / 2)**2 + cos(lat1) * cos(lat2) * sin(dlon / 2)**2 c = 2 * asin(sqrt(a)) distance = round(R * c,2) return distance def calculate_distances(airport_identifiers): """ Calculate the distance between multiple airports. :param airport_identifiers: List of airport names or IATA codes :return: Dictionary with airport pairs as keys and their distances in kilometers as values """ lat_long_dict = get_airport_lat_long(airport_identifiers) if isinstance(lat_long_dict, str): # Check if there was an error fetching airport data return lat_long_dict # Calculate the distance for each combination of airports distances = {} identifiers = list(lat_long_dict.keys()) for i in range(len(identifiers)): for j in range(i + 1, len(identifiers)): airport1 = identifiers[i] airport2 = identifiers[j] lat1, lon1 = lat_long_dict[airport1] lat2, lon2 = lat_long_dict[airport2] distance = haversine_distance(lat1, lon1, lat2, lon2) distances[(airport1, airport2)] = distance return distances # Example usage: # aircraft_type = input("Enter the aircraft type: ") # aircraft_specs = get_aircraft_details(aircraft_type) # print(aircraft_specs) # airport_list = ['SIN','CDG'] # print(get_airport_lat_long(airport_list)) # print(calculate_distances(airport_list)) # fuel_burn_rate = aircraft_specs['Fuel_Consumption_kg/hr'] # cruising_speed = aircraft_specs['Max_Fuel_Capacity_kg'] # max_fuel_capacity = aircraft_specs['Speed_kmh'] # reserve_fuel_percentage = 0.05 # 5% reserve # #Reserver Fuel calculation # reserve_fuel = reserve_fuel_percentage*max_fuel_capacity # #Flight Time # flight_time = trip_distance/cruising_speed # #Fuel needed for Trip # fuel_required = flight_time*fuel_burn_rate # total_fuel_with_reserve = fuel_required+reserve_fuel # if total_fuel_with_reserve>max_fuel_capacity: # print("Cant Fly without refuel") # else: # print(f"Total fuel required for the trip (including reserve): {round(total_fuel_with_reserve,2)} kg")