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AIRCRAFT_LENGTH['Airbus A220-100 (twin-jet)'] = 35
AIRCRAFT_LENGTH['Airbus A300F4-600 (twin-jet)'] = 54.08
AIRCRAFT_LENGTH['Airbus A319 (twin-jet)'] = 33.84
AIRCRAFT_LENGTH['Airbus A320 (twin-jet)'] = 37.57
AIRCRAFT_LENGTH['Airbus A320neo (twin-jet)'] = 37.57
AIRCRAFT_LENGTH['Airbus A321 (twin-jet)'] = 44.51
AIRCRAFT_LENGTH['Airbus A321neo (twin-jet)'] = 44.51
AIRCRAFT_LENGTH['Airbus A330-200 (twin-jet)'] = 58.82
AIRCRAFT_LENGTH['Airbus A330-300 (twin-jet)'] = 63.67
AIRCRAFT_LENGTH['Airbus A340-300 (quad-jet)'] = 63.69
AIRCRAFT_LENGTH['Airbus A350-1000 (twin-jet)'] = 73.79
AIRCRAFT_LENGTH['Airbus A350-900 (twin-jet)'] = 66.8
AIRCRAFT_LENGTH['Airbus A380-800 (quad-jet)'] = 72.72
AIRCRAFT_LENGTH['Antonov An-124 Ruslan (quad-jet)'] = 69.1
AIRCRAFT_LENGTH['Beechcraft Beechjet (twin-jet)'] = 14.76
AIRCRAFT_LENGTH['Beechcraft Bonanza (33) (piston-single)'] = 7.65
AIRCRAFT_LENGTH['Beechcraft Premier 1 (twin-jet)'] = 14.02
AIRCRAFT_LENGTH['Beechcraft Super King Air 200 (twin-turboprop)'] = 13.31
AIRCRAFT_LENGTH['Beechcraft Super King Air 350 (twin-turboprop)'] = 14.22
AIRCRAFT_LENGTH['Beechcraft King Air 90 (twin-turboprop)'] = 10.82

AIRCRAFT_LENGTH['Boeing 777-300 (twin-jet)'] = 33.4
AIRCRAFT_LENGTH['Boeing 737-400 (twin-jet)'] = 36.4
AIRCRAFT_LENGTH['Boeing 737-700 (twin-jet)'] = 33.63
AIRCRAFT_LENGTH['Boeing 737-800 (twin-jet)'] = 39.47
AIRCRAFT_LENGTH['Boeing 737-900 (twin-jet)'] = 42.11
AIRCRAFT_LENGTH['Boeing 747-100 (quad-jet)'] = 70.66
AIRCRAFT_LENGTH['Boeing 747-400 (quad-jet)'] = 70.66
AIRCRAFT_LENGTH['Boeing 747-8 (quad-jet)'] = 76.25
AIRCRAFT_LENGTH['Boeing 757-200 (twin-jet)'] = 47.3
AIRCRAFT_LENGTH['Boeing 757-300 (twin-jet)'] = 54.4
AIRCRAFT_LENGTH['Boeing 767-200 (twin-jet)'] = 48.51
AIRCRAFT_LENGTH['Boeing 767-300 (twin-jet)'] = 54.94
AIRCRAFT_LENGTH['Boeing 777 (twin-jet)'] = (63.73 + 73.86) / 2
AIRCRAFT_LENGTH['Boeing 777-200 (twin-jet)'] = 63.73
AIRCRAFT_LENGTH['Boeing 777-200LR/F (twin-jet)'] = 63.73
AIRCRAFT_LENGTH['Boeing 777-300ER (twin-jet)'] = 73.86
AIRCRAFT_LENGTH['Boeing 787-10 (twin-jet)'] = 68.28
AIRCRAFT_LENGTH['Boeing 787-8 (twin-jet)'] = 56.72
AIRCRAFT_LENGTH['Boeing 787-9 (twin-jet)'] = 62.81
AIRCRAFT_LENGTH['Bombardier Challenger 300 (twin-jet)'] = 20.92




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AIRCRAFT_LENGTH['Cessna Citation Excel/XLS (twin-jet)'] = 16.0
AIRCRAFT_LENGTH['Cessna Citation II (twin-jet)'] = 14.54
AIRCRAFT_LENGTH['Cessna Citation Latitude (twin-jet)'] = 18.97
AIRCRAFT_LENGTH['Cessna Citation Longitude (twin-jet)'] = 22.3
AIRCRAFT_LENGTH['Cessna Citation Sovereign (twin-jet)'] = 19.35
AIRCRAFT_LENGTH['Cessna Citation V (twin-jet)'] = 14.91
AIRCRAFT_LENGTH['Cessna Citation X (twin-jet)'] = 22.04
AIRCRAFT_LENGTH['Cessna Citation Mustang (twin-jet)'] = 12.37
AIRCRAFT_LENGTH['Cessna Conquest 2 (twin-turboprop)'] = 11.89
AIRCRAFT_LENGTH['Cessna Skyhawk (piston-single)'] = 8.28
AIRCRAFT_LENGTH['Cessna Skylane (piston-single)'] = 8.84
AIRCRAFT_LENGTH['Cessna T206 Turbo Stationair (piston-single)'] = 8.61
AIRCRAFT_LENGTH['Cirrus SR-22 (piston-single)'] = 7.92
AIRCRAFT_LENGTH['Dassault Falcon 900 (tri-jet)'] = 20.21
AIRCRAFT_LENGTH['Dassault Falcon 2000 (twin-jet)'] = 20.23
AIRCRAFT_LENGTH['Embraer 170/175 (twin-jet)'] = (29.90 + 31.68) / 2
AIRCRAFT_LENGTH['Embraer Phenom 300 (twin-jet)'] = 15.9
AIRCRAFT_LENGTH['Embraer ERJ-135 (twin-jet)'] = 26.33
AIRCRAFT_LENGTH['Embraer ERJ-145 (twin-jet)'] = 29.87
AIRCRAFT_LENGTH['Embraer Legacy 450 (twin-jet)'] = 19.69

AIRCRAFT_LENGTH['EMBRAER 175 (long wing) (twin-jet)'] = 31.68
AIRCRAFT_LENGTH['Eurocopter EC-635 (twin-turboshaft)'] = 10.21
AIRCRAFT_LENGTH['IAI Gulfstream G280 (twin-jet)'] = 20.3
AIRCRAFT_LENGTH['Gulfstream Aerospace Gulfstream G550 (twin-jet)'] = 29.39

AIRCRAFT_LENGTH['Gulfstream Aerospace Gulfstream IV (twin-jet)'] = 26.92
AIRCRAFT_LENGTH['Learjet 35 (twin-jet)'] = 14.83
AIRCRAFT_LENGTH['Learjet 45 (twin-jet)'] = 17.68
AIRCRAFT_LENGTH['McDonnell Douglas MD-11 (tri-jet)'] = 61.6
AIRCRAFT_LENGTH['Pilatus PC-12 (single-turboprop)'] = 14.4

AIRCRAFT_LENGTH['Rockwell Turbo Commander 690 (twin-turboprop)'] = 11.22


def Log(message, file=None, rolling=None):
  """Write a message to a logfile along with a timestamp.

  Args:
    message: string message to write
    file: string representing file name and, if needed, path to the
      file to write to
    rolling: name of file that will keep only the last n files of file
  """
  # can't define as a default parameter because LOGFILE name is potentially
  # modified based on SIMULATION flag
  if not file:
    file = LOGFILE

  # special case: for the main logfile, we always keep a rolling log
  if not rolling and file == LOGFILE:
    rolling = ROLLING_LOGFILE




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AIRCRAFT_LENGTH['Airbus A220-100 (twin-jet)'] = 35
AIRCRAFT_LENGTH['Airbus A300F4-600 (twin-jet)'] = 54.08
AIRCRAFT_LENGTH['Airbus A319 (twin-jet)'] = 33.84
AIRCRAFT_LENGTH['Airbus A320 (twin-jet)'] = 37.57
AIRCRAFT_LENGTH['Airbus A320neo (twin-jet)'] = 37.57
AIRCRAFT_LENGTH['Airbus A321 (twin-jet)'] = 44.51
AIRCRAFT_LENGTH['Airbus A321neo (twin-jet)'] = 44.51
AIRCRAFT_LENGTH['Airbus A330-200 (twin-jet)'] = 58.82
AIRCRAFT_LENGTH['Airbus A330-300 (twin-jet)'] = 63.67
AIRCRAFT_LENGTH['Airbus A340-300 (quad-jet)'] = 63.69
AIRCRAFT_LENGTH['Airbus A350-1000 (twin-jet)'] = 73.79
AIRCRAFT_LENGTH['Airbus A350-900 (twin-jet)'] = 66.8
AIRCRAFT_LENGTH['Airbus A380-800 (quad-jet)'] = 72.72
AIRCRAFT_LENGTH['Antonov An-124 Ruslan (quad-jet)'] = 69.1
AIRCRAFT_LENGTH['Beechcraft Beechjet (twin-jet)'] = 14.76
AIRCRAFT_LENGTH['Beechcraft Bonanza (33) (piston-single)'] = 7.65
AIRCRAFT_LENGTH['Beechcraft Premier 1 (twin-jet)'] = 14.02
AIRCRAFT_LENGTH['Beechcraft Super King Air 200 (twin-turboprop)'] = 13.31
AIRCRAFT_LENGTH['Beechcraft Super King Air 350 (twin-turboprop)'] = 14.22
AIRCRAFT_LENGTH['Beechcraft King Air 90 (twin-turboprop)'] = 10.82
AIRCRAFT_LENGTH['Beechcraft King Air F90 (twin-turboprop)'] = 12.14
AIRCRAFT_LENGTH['Boeing 777-300 (twin-jet)'] = 33.4
AIRCRAFT_LENGTH['Boeing 737-400 (twin-jet)'] = 36.4
AIRCRAFT_LENGTH['Boeing 737-700 (twin-jet)'] = 33.63
AIRCRAFT_LENGTH['Boeing 737-800 (twin-jet)'] = 39.47
AIRCRAFT_LENGTH['Boeing 737-900 (twin-jet)'] = 42.11
AIRCRAFT_LENGTH['Boeing 747-100 (quad-jet)'] = 70.66
AIRCRAFT_LENGTH['Boeing 747-400 (quad-jet)'] = 70.66
AIRCRAFT_LENGTH['Boeing 747-8 (quad-jet)'] = 76.25
AIRCRAFT_LENGTH['Boeing 757-200 (twin-jet)'] = 47.3
AIRCRAFT_LENGTH['Boeing 757-300 (twin-jet)'] = 54.4
AIRCRAFT_LENGTH['Boeing 767-200 (twin-jet)'] = 48.51
AIRCRAFT_LENGTH['Boeing 767-300 (twin-jet)'] = 54.94
AIRCRAFT_LENGTH['Boeing 777 (twin-jet)'] = (63.73 + 73.86) / 2
AIRCRAFT_LENGTH['Boeing 777-200 (twin-jet)'] = 63.73
AIRCRAFT_LENGTH['Boeing 777-200LR/F (twin-jet)'] = 63.73
AIRCRAFT_LENGTH['Boeing 777-300ER (twin-jet)'] = 73.86
AIRCRAFT_LENGTH['Boeing 787-10 (twin-jet)'] = 68.28
AIRCRAFT_LENGTH['Boeing 787-8 (twin-jet)'] = 56.72
AIRCRAFT_LENGTH['Boeing 787-9 (twin-jet)'] = 62.81
AIRCRAFT_LENGTH['Bombardier Challenger 300 (twin-jet)'] = 20.92




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AIRCRAFT_LENGTH['Cessna Citation Excel/XLS (twin-jet)'] = 16.0
AIRCRAFT_LENGTH['Cessna Citation II (twin-jet)'] = 14.54
AIRCRAFT_LENGTH['Cessna Citation Latitude (twin-jet)'] = 18.97
AIRCRAFT_LENGTH['Cessna Citation Longitude (twin-jet)'] = 22.3
AIRCRAFT_LENGTH['Cessna Citation Sovereign (twin-jet)'] = 19.35
AIRCRAFT_LENGTH['Cessna Citation V (twin-jet)'] = 14.91
AIRCRAFT_LENGTH['Cessna Citation X (twin-jet)'] = 22.04
AIRCRAFT_LENGTH['Cessna Citation Mustang (twin-jet)'] = 12.37
AIRCRAFT_LENGTH['Cessna Conquest 2 (twin-turboprop)'] = 11.89
AIRCRAFT_LENGTH['Cessna Skyhawk (piston-single)'] = 8.28
AIRCRAFT_LENGTH['Cessna Skylane (piston-single)'] = 8.84
AIRCRAFT_LENGTH['Cessna T206 Turbo Stationair (piston-single)'] = 8.61
AIRCRAFT_LENGTH['Cirrus SR-22 (piston-single)'] = 7.92
AIRCRAFT_LENGTH['Dassault Falcon 900 (tri-jet)'] = 20.21
AIRCRAFT_LENGTH['Dassault Falcon 2000 (twin-jet)'] = 20.23
AIRCRAFT_LENGTH['Embraer 170/175 (twin-jet)'] = (29.90 + 31.68) / 2
AIRCRAFT_LENGTH['Embraer Phenom 300 (twin-jet)'] = 15.9
AIRCRAFT_LENGTH['Embraer ERJ-135 (twin-jet)'] = 26.33
AIRCRAFT_LENGTH['Embraer ERJ-145 (twin-jet)'] = 29.87
AIRCRAFT_LENGTH['Embraer Legacy 450 (twin-jet)'] = 19.69
AIRCRAFT_LENGTH['Embraer Legacy 550 (twin-jet)'] = 20.74
AIRCRAFT_LENGTH['EMBRAER 175 (long wing) (twin-jet)'] = 31.68
AIRCRAFT_LENGTH['Eurocopter EC-635 (twin-turboshaft)'] = 10.21
AIRCRAFT_LENGTH['IAI Gulfstream G280 (twin-jet)'] = 20.3
AIRCRAFT_LENGTH['Gulfstream Aerospace Gulfstream G550 (twin-jet)'] = 29.39
AIRCRAFT_LENGTH['Gulfstream Aerospace Gulfstream 3 (twin-jet)'] = 25.32
AIRCRAFT_LENGTH['Gulfstream Aerospace Gulfstream IV (twin-jet)'] = 26.92
AIRCRAFT_LENGTH['Learjet 35 (twin-jet)'] = 14.83
AIRCRAFT_LENGTH['Learjet 45 (twin-jet)'] = 17.68
AIRCRAFT_LENGTH['McDonnell Douglas MD-11 (tri-jet)'] = 61.6
AIRCRAFT_LENGTH['Pilatus PC-12 (single-turboprop)'] = 14.4
AIRCRAFT_LENGTH['Raytheon Hawker 800XP (twin-jet)'] = 15.60
AIRCRAFT_LENGTH['Rockwell Turbo Commander 690 (twin-turboprop)'] = 11.22


def Log(message, file=None, rolling=None):
  """Write a message to a logfile along with a timestamp.

  Args:
    message: string message to write
    file: string representing file name and, if needed, path to the
      file to write to
    rolling: name of file that will keep only the last n files of file
  """
  # can't define as a default parameter because LOGFILE name is potentially
  # modified based on SIMULATION flag
  if not file:
    file = LOGFILE

  # special case: for the main logfile, we always keep a rolling log
  if not rolling and file == LOGFILE:
    rolling = ROLLING_LOGFILE




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