import pandas as pd from math import radians, sin, cos, sqrt, asin import time ### Modular Flight Calculation Functions ### def get_aircraft_details(aircraft_type): """ Fetch aircraft details based on the given aircraft type. """ csv_file = 'aircraft.csv' df = pd.read_csv(csv_file) if aircraft_type not in df['Aircraft'].values: return f"Aircraft type '{aircraft_type}' not found in the dataset." aircraft_details = df[df['Aircraft'] == aircraft_type][[ 'Range_km', 'Fuel_Consumption_kg/hr', 'Cruising Speed (kts)', 'Speed_kmh', 'MaxFlightTime_hr', 'Max_Fuel_Capacity_kg']] return aircraft_details.to_dict(orient='records')[0] def get_airport_lat_long(identifiers): """ Get latitude and longitude for a list of airport identifiers (IATA codes). """ csv_file = 'airport.csv' start_time = time.time() df = pd.read_csv(csv_file) read_time = time.time() - start_time print(f"CSV file read in {read_time:.4f} seconds") df_filtered = df[df['Airport_Name'].isin(identifiers) | df['IATA'].isin(identifiers)] lat_long_dict = {row['IATA']: (row['Lat'], row['Long']) for _, row in df_filtered.iterrows()} return lat_long_dict def haversine_distance(lat1, lon1, lat2, lon2): """ Calculate the Haversine distance between two points on Earth (in kilometers). """ R = 6371.0 # Earth radius in kilometers lat1, lon1, lat2, lon2 = map(radians, [lat1, lon1, lat2, lon2]) dlat, dlon = lat2 - lat1, lon2 - lon1 a = sin(dlat / 2)**2 + cos(lat1) * cos(lat2) * sin(dlon / 2)**2 return round(R * 2 * asin(sqrt(a)), 2) def calculate_distances(airport_identifiers): """ Calculate the distance between each pair of airports. """ lat_long_dict = get_airport_lat_long(airport_identifiers) distances = {} for i in range(len(airport_identifiers)): for j in range(i + 1, len(airport_identifiers)): airport1, airport2 = airport_identifiers[i], airport_identifiers[j] lat1, lon1 = lat_long_dict[airport1] lat2, lon2 = lat_long_dict[airport2] distances[(airport1, airport2)] = haversine_distance(lat1, lon1, lat2, lon2) return distances def calculate_fuel_and_time_for_segment(segment_distance, aircraft_specs): """ Calculate the fuel and time required for a single flight segment. """ cruising_speed = aircraft_specs['Speed_kmh'] fuel_burn_rate = aircraft_specs['Fuel_Consumption_kg/hr'] max_fuel_capacity = aircraft_specs['Max_Fuel_Capacity_kg'] reserve_fuel_percentage = 0.05 # 5% reserve fuel climb_speed, descent_speed = 300, 350 climb_time, descent_time = 15 / 60, 10 / 60 # in hours climb_distance = climb_speed * climb_time descent_distance = descent_speed * descent_time # Calculate cruise distance cruise_distance = segment_distance - (climb_distance + descent_distance) cruise_distance = max(0, cruise_distance) # Ensure cruise distance is not negative # Calculate flight time for each phase cruise_time = cruise_distance / cruising_speed total_flight_time = climb_time + cruise_time + descent_time # Calculate fuel required fuel_required = total_flight_time * fuel_burn_rate reserve_fuel = reserve_fuel_percentage * max_fuel_capacity total_fuel_with_reserve = fuel_required + reserve_fuel return total_fuel_with_reserve, total_flight_time