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- flight_height = int(input('Enter the height of the flight: '))
- km_to_travle = int(input('Enter the KM to travle: '))
- wind_cond = input('Wind Condition (H/C/T) : ')
- wind_cond = wind_cond.lower()
- fuel_percent = 0
- if wind_cond == 'h':
- fuel_percent = 0.05
- elif wind_cond == 'c':
- fuel_percent = 0.02
- else:
- fuel_percent = -0.04
- if flight_height < 10000 or flight_height > 35000:
- print('NO Fly Zone')
- else:
- fuel_comp = 0
- #t = s/v
- total_min = km_to_travle / (1000/100) # distance / velocity
- total_min += total_min * fuel_percent # time + (time * fuel_percent)
- # n = q.60+r
- time_hour = total_min//60
- # r = n - (q*60)
- time_min = total_min - (time_hour*60)
- if flight_height > 25000:
- fuel_comp = km_to_travle * (1000/1000)
- fuel_comp += fuel_comp * fuel_percent
- elif flight_height > 20000:
- fuel_comp = km_to_travle * (1500/1000)
- fuel_comp += fuel_comp * fuel_percent
- else:
- fuel_comp = km_to_travle * (2000/1000)
- fuel_comp += fuel_comp * fuel_percent
- print(f"AirPlane should carry {fuel_comp} liters of fuel.")
- print(f"Flight will be {int(time_hour)} hours and {int(time_min)} minutes long.")
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