descentGlideSlopeSizeNautics = 5.0
descentGlideSlope.buildSimulatedGlideSlope(descentGlideSlopeSizeNautics)
firstGlideSlopeWayPoint = descentGlideSlope.getVertex(v=0).getWeight()
aircraft.setTargetApproachWayPoint(firstGlideSlopeWayPoint)
aircraft.setArrivalRunwayTouchDownWayPoint(touchDownWayPoint)
distanceStillToFlyMeters = departureAirport.getDistanceMetersTo(
arrivalAirport)
print('distance still To Fly Meters= {0:.2f} meters'.format(
distanceStillToFlyMeters))
index = 0
while (endOfSimulation == False and not (aircraft.isLanding())):
endOfSimulation, deltaDistanceMeters, altitudeMeters = aircraft.fly(
elapsedTimeSeconds, deltaTimeSeconds, distanceStillToFlyMeters,
currentPosition)
distanceStillToFlyMeters = distanceStillToFlyMeters - deltaDistanceMeters
RateOfClimbDescentFeetMinute = (
(altitudeMeters - previousAltitudeMSLmeters) *
Meter2Feet) / (deltaTimeSeconds / 60.0)
previousAltitudeMSLmeters = altitudeMeters
#if math.fmod(elapsedTimeSecond)
#print 'rate of climb / descent= {0} feet/minute'.format(RateOfClimbDescentFeetMinute)
#print 'altitude= {0} feet'.format(altitudeMeters * Meter2Feet)
elapsedTimeSeconds += deltaTimeSeconds
bearingDegrees = currentPosition.getBearingDegreesTo(
firstGlideSlopeWayPoint)
newWayPoint = currentPosition.getWayPointAtDistanceBearing(
Name='pt-{0}'.format(index),
DistanceMeters=deltaDistanceMeters,
aircraft.setTargetCruiseFlightLevel(RequestedFlightLevel=310.0,
departureAirportAltitudeMSLmeters=0.0)
aircraft.setAircraftMassKilograms(massKilograms=64000.0)
aircraft.setTargetCruiseMach(cruiseMach=0.8)
tas = aircraft.getCurrentTrueAirSpeedMetersSecond()
previousAltitudeMSLmeters = 0.0
t0 = time.clock()
print('simulation start= {0} seconds'.format(t0))
print('=========== simulation start ==================')
endOfSimulation = False
while ((endOfSimulation == False)
and not (aircraft.isLandingConfiguration())):
endOfSimulation, deltaDistanceMeters, altitudeMeters = aircraft.fly(
elapsedTimeSeconds, deltaTimeSeconds, latitudeDegrees,
distanceStillToFlyMeters)
distanceStillToFlyMeters = distanceStillToFlyMeters - deltaDistanceMeters
RateOfClimbDescentFeetMinute = (
(altitudeMeters - previousAltitudeMSLmeters) *
Meter2Feet) / (deltaTimeSeconds / 60.0)
previousAltitudeMSLmeters = altitudeMeters
#if math.fmod(elapsedTimeSecond)
#print 'rate of climb / descent= {0} feet/minute'.format(RateOfClimbDescentFeetMinute)
#print 'altitude= {0} feet'.format(altitudeMeters * Meter2Feet)
elapsedTimeSeconds += deltaTimeSeconds
print('=========== create State Vector output file ==================')
print('simulation end - duration= {0} seconds'.format(time.clock() - t0))
aircraft.createStateVectorOutputFile()
print('=========== simulation end ==================')
