112 lines
5.2 KiB
Python
112 lines
5.2 KiB
Python
#!/usr/bin/env python
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import pytz
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from datetime import datetime, timedelta
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from aman.com import AircraftReport_pb2
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from aman.config.AirportSequencing import AirportSequencing
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from aman.formats.SctEseFormat import SctEseFormat
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from aman.sys.WeatherModel import WeatherModel
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from aman.types.PerformanceData import PerformanceData
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from aman.types.Waypoint import Waypoint
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class Inbound:
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def __init__(self, report : AircraftReport_pb2.AircraftReport, sequencingConfig : AirportSequencing, navData : SctEseFormat,
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performanceData : PerformanceData, weatherModel : WeatherModel):
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self.Report = report
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self.CurrentPosition = report.position
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self.ReportTime = datetime.strptime(report.reportTime + '+0000', '%Y%m%d%H%M%S%z').replace(tzinfo = pytz.UTC)
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# search performance data -> fallback to A320
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if self.Report.aircraft.type in performanceData.Aircrafts:
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self.PerformanceData = performanceData.Aircrafts[self.Report.aircraft.type]
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if None == self.PerformanceData:
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self.PerformanceData = performanceData.Aircrafts['A320']
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self.findArrivalRunway(sequencingConfig)
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self.findArrivalRoute(navData)
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duration = self.secondsUntilTouchdown(weatherModel)
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self.InitialArrivalTime = self.ReportTime + duration
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self.EstimatedArrivalTime = self.InitialArrivalTime
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self.EstimatedStarEntryTime = None
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def findArrivalRunway(self, sequencingConfig : AirportSequencing):
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self.PlannedRunway = None
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# find the nearest runway for an initial guess
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distance = 100000.0
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currentPosition = Waypoint('', self.Report.position.latitude, self.Report.position.longitude)
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for runway in sequencingConfig.ActiveArrivalRunways:
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candidateDistance = runway.Runway.Start.haversine(currentPosition)
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if distance > candidateDistance:
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self.PlannedRunway = runway
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distance = candidateDistance
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def findArrivalRoute(self, navData : SctEseFormat):
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self.PlannedStar = None
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if None == self.PlannedRunway:
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return
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for arrivalRunway in navData.ArrivalRoutes:
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if arrivalRunway == self.PlannedRunway.Runway.Name:
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stars = navData.ArrivalRoutes[arrivalRunway]
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for star in stars:
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if 0 != len(star.Route) and self.Report.initialApproachFix == star.Iaf.Name:
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self.PlannedStar = star
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return
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def secondsUntilTouchdown(self, weather : WeatherModel):
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if None == self.PlannedRunway or None == self.PlannedStar:
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return timedelta(seconds = 0)
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# calculate remaining trackmiles
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remainingDistanceNM = self.Report.distanceToIAF
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start = self.PlannedStar.Route[0]
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for i in range(1, len(self.PlannedStar.Route)):
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remainingDistanceNM += start.haversine(self.PlannedStar.Route[i]) * 0.539957
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start = self.PlannedStar.Route[i]
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# calculate descend profile
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flightTimeSeconds = 0
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currentHeading = Waypoint('', self.Report.position.latitude, self.Report.position.longitude).bearing(self.PlannedStar.Route[0])
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distanceToWaypoint = self.Report.distanceToIAF
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nextWaypointIndex = 0
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currentPosition = [ self.Report.dynamics.altitude, self.Report.dynamics.groundSpeed ]
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while 0 < currentPosition[0]:
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lastDistance = remainingDistanceNM
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# TODO integrate speed and altitude constraints
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# calculate the next position after 10 seconds
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if (currentPosition[0] / 1000 * 3) > remainingDistanceNM:
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oldGroundspeed = currentPosition[1]
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descendRate = (currentPosition[1] / 60) / 3 * 1000 / 6
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newAltitude = currentPosition[0] - descendRate
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if 0 > newAltitude:
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newAltitude = 0
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# get the planned IAS and calculate the new altitude and GS out of the predicted information
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# we assume that the aircraft only decelerates
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ias = self.PerformanceData.ias(newAltitude, remainingDistanceNM)
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currentPosition = [ newAltitude, min(weather.calculateGS(newAltitude, int(ias), currentHeading), currentPosition[1]) ]
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# use the average between last and current speed to estimate the remaining distance
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remainingDistanceNM -= (currentPosition[1] + oldGroundspeed) / 2 / 60 / 6
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else:
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remainingDistanceNM -= currentPosition[1] / 60 / 6
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flightTimeSeconds += 10
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if 0 > remainingDistanceNM:
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break
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# check if we follow a new waypoint pair
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distanceToWaypoint -= abs(lastDistance - remainingDistanceNM)
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if 0 >= distanceToWaypoint:
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nextWaypointIndex += 1
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if nextWaypointIndex < len(self.PlannedStar.Route):
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currentHeading = self.PlannedStar.Route[nextWaypointIndex - 1].bearing(self.PlannedStar.Route[nextWaypointIndex])
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return timedelta(seconds = flightTimeSeconds)
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