def test_main_five(self):
airportsDb = AirportsDatabase()
assert (airportsDb.read())
print ' ============== g3 performance ==============='
t0 = time.clock()
g3 = Graph()
index = 0
for airport in airportsDb.getAirports():
print airport
g3.addVertex(airport)
index += 1
t1 = time.clock()
print 'number of airports= {0} - duration= {1} seconds'.format(
index, t1 - t0)
airport = airportsDb.getAirportFromICAOCode('LFPG')
t2 = time.clock()
g4 = Graph()
for i in range(0, 10000):
g4.addVertex(airport)
t3 = time.clock()
print 'number of addVertex = {0} - duration= {1:.8f} seconds'.format(
i, t3 - t2)
def test_class_one(self):
print '==================== Main start ==================== ' + time.strftime(
"%c")
t0 = time.clock()
print "time start= {0}".format(t0)
atmosphere = Atmosphere()
t1 = time.clock()
print "simulation time= {0} - simulation duration= {1:3.10f} seconds".format(
t1, (t1 - t0))
print '==================== load airports ==================== ' + time.strftime(
"%c")
airportsDB = AirportsDatabase()
assert airportsDB.read()
print '==================== air density at airports field elevation ==================== ' + time.strftime(
"%c")
for airport in airportsDB.getAirports():
print '=======================' + airport.getName(
) + '===================='
print 'field elevation= ' + str(
airport.getFieldElevationAboveSeaLevelMeters()) + ' meters'
altitudeMeters = airport.getFieldElevationAboveSeaLevelMeters()
print 'air density= ' + str(
atmosphere.getAirDensityKilogramsPerCubicMeters(
altitudeMeters)) + ' kg / meters ^^ 3'
def test_performance_graph_with_airport(self):
airportsDb = AirportsDatabase()
assert (airportsDb.read())
print(' ============== g3 performance ===============')
t0 = time.process_time()
g3 = Graph()
count = 0
for airport in airportsDb.getAirports():
print(airport)
g3.addVertex(airport)
count += 1
t1 = time.process_time()
print('number of airports= {0} - duration= {1} seconds'.format(
count, t1 - t0))
self.assertEqual(g3.getNumberOfVertices(), count)
g3.createXlsxOutputFile()
g3.createKmlOutputFile()
print(' ============== g4 performance ===============')
airport = airportsDb.getAirportFromICAOCode('LFPG')
t2 = time.process_time()
g4 = Graph()
for i in range(0, 10000):
g4.addVertex(airport)
t3 = time.process_time()
print('number of addVertex = {0} - duration= {1:.8f} seconds'.format(
i, t3 - t2))
def test_Vstall(self):
t0 = time.clock()
print("time start= ", t0)
atmosphere = Atmosphere()
earth = Earth()
print(
'==================== Stall Speed according to airport field elevation ==================== '
+ time.strftime("%c"))
acBd = BadaAircraftDatabase()
aircraftICAOcode = 'B743'
if acBd.read():
if (acBd.aircraftExists(aircraftICAOcode)
and acBd.aircraftPerformanceFileExists(
acBd.getAircraftPerformanceFile(aircraftICAOcode))):
print(
'==================== aircraft found ==================== '
+ time.strftime("%c"))
aircraft = BadaAircraft(
ICAOcode=aircraftICAOcode,
aircraftFullName=acBd.getAircraftFullName(
aircraftICAOcode),
badaPerformanceFilePath=acBd.getAircraftPerformanceFile(
aircraftICAOcode),
atmosphere=atmosphere,
earth=earth)
aircraft.dump()
print('==================== Airport database ==================== ' +
time.strftime("%c"))
airportsDB = AirportsDatabase()
assert airportsDB.read()
for airport in airportsDB.getAirports():
print('============' + airport.getName() + ' ============')
#print airport
aircraft = BadaAircraft(
ICAOcode=aircraftICAOcode,
aircraftFullName=acBd.getAircraftFullName(aircraftICAOcode),
badaPerformanceFilePath=acBd.getAircraftPerformanceFile(
aircraftICAOcode),
atmosphere=atmosphere,
earth=earth)
print('airport field elevation= {0:.2f} meters'.format(
airport.getFieldElevationAboveSeaLevelMeters()))
CAS = aircraft.computeStallSpeedCasKnots()
print('V stall Calibrated AirSpeed= {0:.2f} knots'.format(CAS))
TAS = cas2tas(
cas=CAS,
altitude=airport.getFieldElevationAboveSeaLevelMeters(),
temp='std',
speed_units='kt',
alt_units='m',
temp_units=default_temp_units,
)
print('V stall True AirSpeed= {0:.2f} knots'.format(TAS))
def test_Vstall(self):
t0 = time.clock()
print "time start= ", t0
atmosphere = Atmosphere()
earth = Earth()
print '==================== Stall Speed according to airport field elevation ==================== '+ time.strftime("%c")
acBd = BadaAircraftDatabase()
aircraftICAOcode = 'B743'
if acBd.read():
if ( acBd.aircraftExists(aircraftICAOcode)
and acBd.aircraftPerformanceFileExists(acBd.getAircraftPerformanceFile(aircraftICAOcode))):
print '==================== aircraft found ==================== '+ time.strftime("%c")
aircraft = BadaAircraft(ICAOcode = aircraftICAOcode,
aircraftFullName = acBd.getAircraftFullName(aircraftICAOcode),
badaPerformanceFilePath = acBd.getAircraftPerformanceFile(aircraftICAOcode),
atmosphere = atmosphere,
earth = earth)
aircraft.dump()
print '==================== Airport database ==================== '+ time.strftime("%c")
airportsDB = AirportsDatabase()
assert airportsDB.read()
for airport in airportsDB.getAirports():
print '============' + airport.getName() + ' ============'
#print airport
aircraft = BadaAircraft(ICAOcode = aircraftICAOcode,
aircraftFullName = acBd.getAircraftFullName(aircraftICAOcode),
badaPerformanceFilePath = acBd.getAircraftPerformanceFile(aircraftICAOcode),
atmosphere = atmosphere,
earth = earth)
print 'airport field elevation= {0:.2f} meters'.format( airport.getFieldElevationAboveSeaLevelMeters())
CAS = aircraft.computeStallSpeedCasKnots()
print 'V stall Calibrated AirSpeed= {0:.2f} knots'.format(CAS)
TAS = cas2tas(cas = CAS ,
altitude = airport.getFieldElevationAboveSeaLevelMeters(),
temp = 'std',
speed_units = 'kt',
alt_units = 'm',
temp_units=default_temp_units,
)
print 'V stall True AirSpeed= {0:.2f} knots'.format(TAS)
def test_class_one(self):
print '==================== Main start ==================== '+ time.strftime("%c")
t0 = time.clock()
print "time start= {0}".format( t0)
atmosphere = Atmosphere()
t1 = time.clock()
print "simulation time= {0} - simulation duration= {1:3.10f} seconds".format(t1 , (t1-t0))
print '==================== load airports ==================== '+ time.strftime("%c")
airportsDB = AirportsDatabase()
assert airportsDB.read()
print '==================== air density at airports field elevation ==================== '+ time.strftime("%c")
for airport in airportsDB.getAirports():
print '=======================' + airport.getName() + '===================='
print 'field elevation= ' + str(airport.getFieldElevationAboveSeaLevelMeters()) + ' meters'
altitudeMeters = airport.getFieldElevationAboveSeaLevelMeters()
print 'air density= ' + str(atmosphere.getAirDensityKilogramsPerCubicMeters(altitudeMeters)) + ' kg / meters ^^ 3'
def test_main_five(self):
airportsDb = AirportsDatabase()
assert (airportsDb.read())
print ' ============== g3 performance ==============='
t0 = time.clock()
g3 = Graph()
index = 0
for airport in airportsDb.getAirports():
print airport
g3.addVertex(airport)
index += 1
t1 = time.clock()
print 'number of airports= {0} - duration= {1} seconds'.format(index, t1-t0)
airport = airportsDb.getAirportFromICAOCode('LFPG')
t2= time.clock()
g4 = Graph()
for i in range (0,10000):
g4.addVertex(airport)
t3 = time.clock()
print 'number of addVertex = {0} - duration= {1:.8f} seconds'.format(i , t3-t2)
