aman-sys/aman/types/Inbound.py

#!/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.ArrivalWaypoint import ArrivalWaypoint
from aman.types.PerformanceData import PerformanceData
from aman.types.ArrivalRoute import ArrivalRoute
from aman.types.ArrivalData import ArrivalData
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.PlannedArrivalRoute = None
        self.PlannedTrackmiles = None
        self.ArrivalCandidates = {}
        self.WTC = None
        self.FixedSequence = False

        # 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, arrivalRoute = self.arrivalEstimation(identifier.Runway, star, weatherModel)

                avgSpeed = trackmiles / (float(flightTime.seconds) / 3600.0)
                # the closer we get to the IAF the less time delta can be achieved by short cuts, delay vectors or speeds
                ratio = min(2.0, max(0.0, self.Report.distanceToIAF / (trackmiles - self.Report.distanceToIAF)))
                possibleTimeDelta = (trackmiles / (avgSpeed * 0.9)) * 60
                ttg = timedelta(minutes = (possibleTimeDelta - flightTime.total_seconds() / 60) * ratio)
                ttl = timedelta(minutes = (possibleTimeDelta - flightTime.total_seconds() / 60))
                ita = self.ReportTime + flightTime
                earliest = ita - ttg
                latest = ita + ttl

                self.ArrivalCandidates[identifier.Runway.Name] = ArrivalData(ttg = ttg, star = star, ita = ita, earliest = earliest,
                                                                             entry = flightTimeUntilIaf, touchdown = flightTime,
                                                                             ttl = ttl, latest = latest, route = arrivalRoute, trackmiles = trackmiles)

        # 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
        arrivalRoute = [ ArrivalWaypoint(waypoint = star.Route[0], trackmiles = distanceToWaypoint) ]

        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

                arrivalRoute[-1].FlightTime = timedelta(seconds = flightTimeSeconds)
                arrivalRoute[-1].ETA = self.ReportTime + arrivalRoute[-1].FlightTime
                arrivalRoute[-1].PTA = arrivalRoute[-1].ETA
                arrivalRoute[-1].Altitude = currentPosition[0]
                arrivalRoute[-1].IndicatedAirspeed = currentIAS
                arrivalRoute[-1].GroundSpeed = currentPosition[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])

                    arrivalRoute.append(ArrivalWaypoint(waypoint = star.Route[nextWaypointIndex], trackmiles = arrivalRoute[-1].Trackmiles + distanceToWaypoint))

        return timedelta(seconds = flightTimeSeconds), timedelta(seconds = flightTimeUntilIafSeconds), trackmiles, arrivalRoute