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- #!/usr/bin/env python
- import pytz
- import sys
- from datetime import datetime, timedelta
- from aman.com import AircraftReport_pb2
- from aman.config.AirportSequencing import AirportSequencing
- from aman.formats.SctEseFormat import SctEseFormat
- from aman.sys.WeatherModel import WeatherModel
- from aman.types.PerformanceData import PerformanceData
- from aman.types.ArrivalRoute import ArrivalRoute
- from aman.types.ArrivalTime import ArrivalTime
- from aman.types.Runway import Runway
- from aman.types.Waypoint import Waypoint
- class Inbound:
- def findArrivalRoute(self, runway : Runway, navData : SctEseFormat):
- for arrivalRunway in navData.ArrivalRoutes:
- if arrivalRunway == runway.Name:
- stars = navData.ArrivalRoutes[arrivalRunway]
- for star in stars:
- if 0 != len(star.Route) and self.Report.initialApproachFix == star.Iaf.Name:
- return star
- return None
- def __init__(self, report : AircraftReport_pb2.AircraftReport, sequencingConfig : AirportSequencing, navData : SctEseFormat,
- performanceData : PerformanceData, weatherModel : WeatherModel):
- self.Report = report
- self.Callsign = report.aircraft.callsign
- self.CurrentPosition = report.position
- self.ReportTime = datetime.strptime(report.reportTime + '+0000', '%Y%m%d%H%M%S%z').replace(tzinfo = pytz.UTC)
- self.InitialArrivalTime = None
- self.EarliestArrivalTime = None
- self.PlannedArrivalTime = None
- self.EstimatedStarEntryTime = None
- self.PlannedRunway = None
- self.PlannedStar = None
- self.ArrivalCandidates = {}
- self.WTC = None
- # analyze the WTC
- wtc = report.aircraft.wtc.upper()
- if 'L' == wtc or 'M' == wtc or 'H' == wtc or 'J' == wtc:
- self.WTC = wtc
- # search performance data -> fallback to A320
- if self.Report.aircraft.type in performanceData.Aircrafts:
- self.PerformanceData = performanceData.Aircrafts[self.Report.aircraft.type]
- if None == self.PerformanceData:
- self.PerformanceData = performanceData.Aircrafts['A320']
- # calculate the timings for the different arrival runways
- for identifier in sequencingConfig.ActiveArrivalRunways:
- star = self.findArrivalRoute(identifier.Runway, navData)
- if None != star:
- flightTime, flightTimeUntilIaf, trackmiles = self.arrivalEstimation(identifier.Runway, star, weatherModel)
- avgSpeed = trackmiles / (float(flightTime.seconds) / 3600.0)
- ttg = flightTime - timedelta(minutes = (trackmiles / (avgSpeed * 1.1)) * 60)
- ttl = timedelta(minutes = (trackmiles / (avgSpeed * 0.9)) * 60) - flightTime
- ita = self.ReportTime + flightTime
- earliest = ita - ttg
- latest = ita + ttl
- self.ArrivalCandidates[identifier.Runway.Name] = ArrivalTime(ttg = ttg, star = star, ita = ita, earliest = earliest,
- entry = flightTimeUntilIaf, touchdown = flightTime,
- ttl = ttl, latest = latest)
- # calculate the first values for later plannings
- for candidate in self.ArrivalCandidates:
- if None == self.EarliestArrivalTime or self.ArrivalCandidates[candidate].EarliestArrivalTime < self.EarliestArrivalTime:
- self.InitialArrivalTime = self.ArrivalCandidates[candidate].InitialArrivalTime
- self.EarliestArrivalTime = self.ArrivalCandidates[candidate].EarliestArrivalTime
- self.EstimatedStarEntryTime = self.ReportTime + self.ArrivalCandidates[candidate].FlightTimeUntilIaf
- self.PlannedStar = self.ArrivalCandidates[candidate].Star
- if None != self.PlannedStar:
- for runway in navData.Runways[self.Report.destination.upper()]:
- if runway.Name == self.PlannedStar.Runway:
- self.PlannedRunway = runway
- break
- def arrivalEstimation(self, runway : Runway, star : ArrivalRoute, weather : WeatherModel):
- # calculate remaining trackmiles
- trackmiles = self.Report.distanceToIAF
- start = star.Route[0]
- turnIndices = [ -1, -1 ]
- constraints = []
- for i in range(0, len(star.Route)):
- # identified the base turn
- if True == star.Route[i].BaseTurn:
- turnIndices[0] = i
- # identified the final turn
- elif -1 != turnIndices[0] and True == star.Route[i].FinalTurn:
- turnIndices[1] = i
- # skip waypoints until the final turn point is found
- elif -1 != turnIndices[0] and -1 == turnIndices[1]:
- continue
- trackmiles += start.haversine(star.Route[i]) * 0.539957
- # check if a new constraint is defined
- altitude = -1
- speed = -1
- if None != star.Route[i].Altitude:
- altitude = star.Route[i].Altitude
- if None != star.Route[i].Speed:
- speed = star.Route[i].Speed
- if -1 != altitude or -1 != speed:
- constraints.append([ trackmiles, altitude, speed ])
- start = star.Route[i]
- # add the remaining distance from the last waypoint to the runway threshold
- trackmiles += start.haversine(runway.Start)
- if turnIndices[0] > turnIndices[1] or (-1 == turnIndices[1] and -1 != turnIndices[0]):
- sys.stderr.write('Invalid constraint definition found for ' + star.Name)
- sys.exit(-1)
- # calculate descend profile
- currentHeading = Waypoint(latitude = self.Report.position.latitude, longitude = self.Report.position.longitude).bearing(star.Route[0])
- currentIAS = self.PerformanceData.ias(self.Report.dynamics.altitude, trackmiles)
- currentPosition = [ self.Report.dynamics.altitude, self.Report.dynamics.groundSpeed ]
- distanceToWaypoint = self.Report.distanceToIAF
- flightTimeUntilIafSeconds = 0
- flightTimeSeconds = 0
- nextWaypointIndex = 0
- flownDistance = 0.0
- while True:
- # check if a constraint cleanup is needed and if a speed-update is needed
- if 0 != len(constraints) and flownDistance >= constraints[0][0]:
- if -1 != constraints[0][2]:
- currentIAS = min(constraints[0][2], self.PerformanceData.ias(self.Report.dynamics.altitude, trackmiles - flownDistance))
- currentPosition[1] = min(weather.calculateGS(currentPosition[0], currentIAS, currentHeading), currentPosition[1])
- constraints.pop(0)
- # search next altitude constraint
- altitudeDistance = 0
- nextAltitude = 0
- for constraint in constraints:
- if -1 != constraint[1]:
- altitudeDistance = constraint[0]
- nextAltitude = constraint[1]
- break
- # check if update of altitude and speed is needed on 3° glide
- if currentPosition[0] > nextAltitude and ((currentPosition[0] - nextAltitude) / 1000 * 3) > (altitudeDistance - flownDistance):
- oldGroundspeed = currentPosition[1]
- descendRate = (currentPosition[1] / 60) / 3 * 1000 / 6
- newAltitude = currentPosition[0] - descendRate
- if 0 > newAltitude:
- newAltitude = 0
- currentPosition = [ newAltitude, min(weather.calculateGS(newAltitude, currentIAS, currentHeading), currentPosition[1]) ]
- distance = (currentPosition[1] + oldGroundspeed) / 2 / 60 / 6
- else:
- distance = currentPosition[1] / 60 / 6
- # update the statistics
- distanceToWaypoint -= distance
- flownDistance += distance
- newIAS = min(currentIAS, self.PerformanceData.ias(currentPosition[0], trackmiles - flownDistance))
- if newIAS < currentIAS:
- currentPosition[1] = min(weather.calculateGS(currentPosition[0], newIAS, currentHeading), currentPosition[1])
- currentIAS = newIAS
- flightTimeSeconds += 10
- if flownDistance <= self.Report.distanceToIAF:
- flightTimeUntilIafSeconds += 10
- if flownDistance >= trackmiles:
- break
- # check if we follow a new waypoint pair
- if 0 >= distanceToWaypoint:
- lastWaypointIndex = nextWaypointIndex
- nextWaypointIndex += 1
- # check if a skip from base to final turn waypoints is needed
- if -1 != turnIndices[0] and nextWaypointIndex > turnIndices[0] and nextWaypointIndex < turnIndices[1]:
- nextWaypointIndex = turnIndices[1]
- # update the statistics
- if nextWaypointIndex < len(star.Route):
- distanceToWaypoint = star.Route[lastWaypointIndex].haversine(star.Route[nextWaypointIndex]) * 0.539957
- currentHeading = star.Route[lastWaypointIndex].bearing(star.Route[nextWaypointIndex])
- currentPosition[1] = min(weather.calculateGS(currentPosition[0], currentIAS, currentHeading), currentPosition[1])
- return timedelta(seconds = flightTimeSeconds), timedelta(seconds = flightTimeUntilIafSeconds), trackmiles
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