def test_turn_leg(self):
print('==================== Turn Leg ==================== ' +
time.strftime("%c"))
print('==================== aircraft found ==================== ' +
time.strftime("%c"))
self.aircraft.dump()
print('==================== Get Airport ==================== ' +
time.strftime("%c"))
airportsDB = AirportsDatabase()
assert airportsDB.read()
print(
'==================== Get Arrival Airport ==================== ' +
time.strftime("%c"))
Lisbonne = airportsDB.getAirportFromICAOCode('LPPT')
print(Lisbonne)
print('==================== find the run-ways ==================== ' +
time.strftime("%c"))
runWaysDatabase = RunWayDataBase()
if runWaysDatabase.read():
print('runways DB correctly read')
print('==================== take off run-way ==================== ' +
time.strftime("%c"))
arrivalRunway = runWaysDatabase.getFilteredRunWays(
airportICAOcode='LPPT', runwayName='')
print(arrivalRunway)
print('==================== Ground run ==================== ' +
time.strftime("%c"))
groundRun = GroundRunLeg(runway=arrivalRunway,
aircraft=self.aircraft,
airport=Lisbonne)
touchDownWayPoint = groundRun.computeTouchDownWayPoint()
print(touchDownWayPoint)
groundRun.buildDepartureGroundRun(deltaTimeSeconds=1.0,
elapsedTimeSeconds=0.0,
distanceStillToFlyMeters=0.0,
distanceToLastFixMeters=0.0)
print('==================== Climb Ramp ==================== ' +
time.strftime("%c"))
initialWayPoint = groundRun.getLastVertex().getWeight()
descentGlideSlope = DescentGlideSlope(runway=arrivalRunway,
aircraft=self.aircraft,
arrivalAirport=Lisbonne,
descentGlideSlopeDegrees=3.0)
''' if there is a fix nearer to 5 nautics of the touch-down then limit size of simulated glide slope '''
descentGlideSlope.buildSimulatedGlideSlope(
descentGlideSlopeSizeNautics=5.0)
descentGlideSlope.createKmlOutputFile()
firstGlideSlopeWayPoint = descentGlideSlope.getVertex(v=0).getWeight()
print('==================== Climb Ramp ==================== ' +
time.strftime("%c"))
initialWayPoint = groundRun.getLastVertex().getWeight()
print(' ================== turn leg start =============== ')
wayPointsDb = WayPointsDatabase()
assert (wayPointsDb.read())
Exona = wayPointsDb.getWayPoint('EXONA')
Rosal = wayPointsDb.getWayPoint('ROSAL')
print(Rosal.getBearingDegreesTo(Exona))
initialHeadingDegrees = arrivalRunway.getTrueHeadingDegrees()
lastTurnLeg = TurnLeg(initialWayPoint=firstGlideSlopeWayPoint,
finalWayPoint=Exona,
initialHeadingDegrees=initialHeadingDegrees,
aircraft=self.aircraft,
reverse=True)
deltaTimeSeconds = 1.0
lastTurnLeg.buildNewSimulatedArrivalTurnLeg(
deltaTimeSeconds=deltaTimeSeconds,
elapsedTimeSeconds=0.0,
distanceStillToFlyMeters=0.0,
simulatedAltitudeSeaLevelMeters=firstGlideSlopeWayPoint.
getAltitudeMeanSeaLevelMeters(),
flightPathAngleDegrees=3.0)
lastTurnLeg.createKmlOutputFile()
descentGlideSlope.addGraph(lastTurnLeg)
descentGlideSlope.createXlsxOutputFile()
descentGlideSlope.createKmlOutputFile()
print(' ================== turn leg end =============== ')
aircraft = BadaAircraft(aircraftIcaoCode,
acBd.getAircraftPerformanceFile(aircraftIcaoCode),
atmosphere,
earth)
aircraft.dump()
takeOffMassKilograms = 64000.0
aircraft.setAircraftMassKilograms(takeOffMassKilograms)
RequestedFlightLevel = 310.0
fieldElevationAboveSeaLevelMeters = 150.0
aircraft.setTargetCruiseFlightLevel(RequestedFlightLevel, fieldElevationAboveSeaLevelMeters)
tasMetersPerSecond = tasKnots * Knots2MetersPerSecond
aircraft.initStateVector(elapsedTimeSeconds = 0.0,
trueAirSpeedMetersSecond = tasMetersPerSecond,
altitudeMeanSeaLevelMeters = 3000.0 * Meter2Feet,
deltaDistanceFlownMeters = 0.0)
aircraft.setCruiseConfiguration(elapsedTimeSeconds = 0.0)
turnLeg = TurnLeg( initialWayPoint = departureAirport,
finalWayPoint = arrivalAirport,
initialHeadingDegrees = 215.0,
finalHeadingDegrees = 180.0,
aircraft = aircraft,
reverse = False)
distanceStillToFlyMeters = 700000.0
turnLeg.buildTurnLeg(elapsedTimeSeconds = 0.0, distanceStillToFlyMeters = distanceStillToFlyMeters)
turnLeg.createKmlOutputFile()
turnLeg.createXlsxOutputFile()
