[4] | 1 | # Module for the simulator-independent aircraft classes
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| 2 |
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| 3 | #---------------------------------------------------------------------------------------
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| 4 |
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[8] | 5 | import const
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| 6 | import checks
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[134] | 7 | import fs
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[89] | 8 | import util
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[4] | 9 |
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[139] | 10 | import sys
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[8] | 11 | import time
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[139] | 12 | import traceback
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[7] | 13 |
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[197] | 14 | from collections import deque
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| 15 |
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| 16 | #---------------------------------------------------------------------------------------
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| 17 |
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| 18 | class SmoothedValue(object):
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| 19 | """A smoothed value."""
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| 20 | def __init__(self):
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| 21 | """Construct the value."""
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| 22 | self._deque = deque()
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| 23 | self._sum = 0
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| 24 |
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| 25 | def add(self, length, value):
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| 26 | """Add the given value and smooth with the given length."""
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| 27 | dequeLength = len(self._deque)
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| 28 | while dequeLength>=length:
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| 29 | self._sum -= self._deque.popleft()
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| 30 | dequeLength -= 1
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| 31 |
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| 32 | self._sum += value
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| 33 | self._deque.append(value)
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| 34 |
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| 35 | def get(self):
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| 36 | """Get the average."""
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| 37 | return self._sum / len(self._deque)
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| 38 |
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[4] | 39 | #---------------------------------------------------------------------------------------
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| 40 |
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| 41 | class Aircraft(object):
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| 42 | """Base class for aircraft."""
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[8] | 43 | @staticmethod
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| 44 | def create(flight):
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| 45 | """Create an aircraft instance for the type in the given flight."""
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| 46 | return _classes[flight.aircraftType](flight)
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| 47 |
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| 48 | def __init__(self, flight):
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[4] | 49 | """Construct the aircraft for the given type."""
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[8] | 50 | self._flight = flight
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[4] | 51 | self._aircraftState = None
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[9] | 52 |
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| 53 | self._maxVS = -10000.0
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| 54 | self._minVS = 10000.0
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[4] | 55 |
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[101] | 56 | self._v1r2LineIndex = None
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[96] | 57 | self._vrefLineIndex = None
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| 58 |
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[117] | 59 | self.humanWeight = 82.0
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| 60 |
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[8] | 61 | self._checkers = []
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| 62 |
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[197] | 63 | config = flight.config
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[11] | 64 | # Loggers
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| 65 |
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[8] | 66 | self._checkers.append(checks.StageChecker())
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[9] | 67 | self._checkers.append(checks.TakeOffLogger())
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[8] | 68 |
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| 69 | self._checkers.append(checks.AltimeterLogger())
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| 70 |
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| 71 | self._checkers.append(checks.NAV1Logger())
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| 72 | self._checkers.append(checks.NAV2Logger())
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| 73 | self._checkers.append(checks.SquawkLogger())
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| 74 |
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| 75 | self._checkers.append(checks.AnticollisionLightsLogger())
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| 76 | self._checkers.append(checks.LandingLightsLogger())
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| 77 | self._checkers.append(checks.StrobeLightsLogger())
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| 78 | self._checkers.append(checks.NavLightsLogger())
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| 79 |
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| 80 | self._checkers.append(checks.FlapsLogger())
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| 81 |
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| 82 | self._checkers.append(checks.GearsLogger())
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[9] | 83 | self._checkers.append(checks.CruiseSpeedLogger())
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[10] | 84 | self._checkers.append(checks.SpoilerLogger())
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[9] | 85 |
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[197] | 86 | if config.isMessageTypeFS(const.MESSAGETYPE_VISIBILITY):
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[134] | 87 | self._checkers.append(checks.VisibilityChecker())
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| 88 |
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[139] | 89 | # FIXME: we should have a central data model object, and not collect
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| 90 | # the data from the GUI. However, some pieces of data (e.g. V-speeds,
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| 91 | # etc. that is entered into the GUI) *should* be a part of the GUI and
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| 92 | # queried from it, so the model should have a reference to the GUI as
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| 93 | # well and access such data via the GUI!
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[197] | 94 | if config.onlineACARS and not flight.entranceExam:
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[139] | 95 | self._checkers.append(checks.ACARSSender(flight._gui))
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| 96 |
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[11] | 97 | # Fault checkers
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| 98 |
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| 99 | self._checkers.append(checks.AntiCollisionLightsChecker())
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| 100 | self._checkers.append(checks.LandingLightsChecker())
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| 101 | self._checkers.append(checks.NavLightsChecker())
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| 102 | self._checkers.append(checks.StrobeLightsChecker())
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| 103 |
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| 104 | self._checkers.append(checks.BankChecker())
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| 105 |
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| 106 | self._checkers.append(checks.FlapsRetractChecker())
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| 107 | self._checkers.append(checks.FlapsSpeedLimitChecker())
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| 108 |
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| 109 | self._checkers.append(checks.GearsDownChecker())
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| 110 | self._checkers.append(checks.GearSpeedLimitChecker())
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| 111 |
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| 112 | self._checkers.append(checks.GLoadChecker())
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| 113 |
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| 114 | self._checkers.append(checks.MLWChecker())
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| 115 | self._checkers.append(checks.MTOWChecker())
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| 116 | self._checkers.append(checks.MZFWChecker())
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| 117 | self._checkers.append(checks.PayloadChecker())
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| 118 |
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| 119 | self._checkers.append(checks.SpeedChecker())
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| 120 | self._checkers.append(checks.VSChecker())
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[197] | 121 |
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| 122 | timeout = 5.0 + config.realIASSmoothingLength - 1
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| 123 | self._checkers.append(checks.OverspeedChecker(timeout = timeout))
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| 124 |
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[11] | 125 | self._checkers.append(checks.StallChecker())
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| 126 |
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| 127 | self._checkers.append(checks.PitotChecker())
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| 128 |
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| 129 | self._checkers.append(checks.ReverserChecker())
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| 130 |
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[197] | 131 | self._smoothedIAS = SmoothedValue()
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| 132 | self._smoothedVS = SmoothedValue()
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| 133 |
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[4] | 134 | @property
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| 135 | def type(self):
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| 136 | """Get the type of the aircraft."""
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[8] | 137 | return self._flight.aircraftType
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| 138 |
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| 139 | @property
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| 140 | def flight(self):
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| 141 | """Get the flight the aircraft belongs to."""
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| 142 | return self._flight
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[4] | 143 |
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[8] | 144 | @property
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| 145 | def logger(self):
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| 146 | """Get the logger to use for the aircraft."""
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| 147 | return self._flight.logger
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| 148 |
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[139] | 149 | @property
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| 150 | def state(self):
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| 151 | """Get the current aircraft state."""
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| 152 | return self._aircraftState
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| 153 |
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[11] | 154 | def getFlapsSpeedLimit(self, flaps):
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| 155 | """Get the speed limit for the given flaps setting."""
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| 156 | return self.flapSpeedLimits[flaps] if flaps in self.flapSpeedLimits \
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| 157 | else None
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| 158 |
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[8] | 159 | def modelChanged(self, timestamp, aircraftName, modelName):
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[4] | 160 | """Called when the simulator's aircraft changes."""
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[8] | 161 | self._flight.logger.message(timestamp,
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| 162 | "Aircraft: name='%s', model='%s'" % \
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| 163 | (aircraftName, modelName))
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[4] | 164 |
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| 165 | def handleState(self, aircraftState):
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[197] | 166 | """Called when the state of the aircraft changes.
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| 167 |
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| 168 | This is the function that the simulator calls directly with the new
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| 169 | state."""
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| 170 | config = self._flight.config
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| 171 |
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| 172 | self._smoothedIAS.add(config.realIASSmoothingLength, aircraftState.ias)
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| 173 | aircraftState.smoothedIAS = self._smoothedIAS.get()
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| 174 |
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| 175 | self._smoothedVS.add(config.realVSSmoothingLength, aircraftState.vs)
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| 176 | aircraftState.smoothedVS = self._smoothedVS.get()
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| 177 |
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[8] | 178 | for checker in self._checkers:
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[139] | 179 | try:
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| 180 | checker.check(self._flight, self, self._flight.logger,
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| 181 | self._aircraftState, aircraftState)
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| 182 | except:
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| 183 | print >> sys.stderr, "Checker", checker, "failed"
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| 184 | traceback.print_exc()
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[7] | 185 |
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[89] | 186 | self._flight.handleState(self._aircraftState, aircraftState)
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| 187 |
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[9] | 188 | self._maxVS = max(self._maxVS, aircraftState.vs)
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| 189 | self._minVS = min(self._minVS, aircraftState.vs)
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| 190 |
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[4] | 191 | self._aircraftState = aircraftState
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[8] | 192 |
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| 193 | def setStage(self, aircraftState, newStage):
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| 194 | """Set the given stage as the new one and do whatever should be
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| 195 | done."""
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[9] | 196 | if self._flight.setStage(aircraftState.timestamp, newStage):
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| 197 | if newStage==const.STAGE_PUSHANDTAXI:
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| 198 | self.logger.message(aircraftState.timestamp, "Block time start")
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| 199 | self.logFuel(aircraftState)
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| 200 | self.logger.message(aircraftState.timestamp,
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| 201 | "Zero-fuel weight: %.0f kg" % (aircraftState.zfw))
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[134] | 202 | flight = self._flight
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| 203 | if flight.v1 is None or flight.vr is None or flight.v2 is None:
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| 204 | fs.sendMessage(const.MESSAGETYPE_HELP,
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| 205 | "Don't forget to set the takeoff V-speeds!",
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| 206 | 5)
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[9] | 207 | elif newStage==const.STAGE_TAKEOFF:
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| 208 | self.logger.message(aircraftState.timestamp, "Flight time start")
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| 209 | self.logger.message(aircraftState.timestamp,
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| 210 | "Takeoff weight: %.0f kg, MTOW: %.0f kg" % \
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| 211 | (aircraftState.grossWeight, self.mtow))
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| 212 | self.logger.message(aircraftState.timestamp,
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| 213 | "Wind %03.0f degrees at %.0f knots" % \
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| 214 | (aircraftState.windDirection,
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| 215 | aircraftState.windSpeed))
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[101] | 216 | self._logV1R2()
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[9] | 217 | elif newStage==const.STAGE_TAXIAFTERLAND:
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[184] | 218 | flight = self._flight
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| 219 | bookedFlight = flight.bookedFlight
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| 220 | config = flight.config
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[136] | 221 | if config.onlineGateSystem and \
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[184] | 222 | not flight.entranceExam and \
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[136] | 223 | bookedFlight.arrivalICAO=="LHBP" and \
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| 224 | config.isMessageTypeFS(const.MESSAGETYPE_GATE_SYSTEM):
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[134] | 225 | self._flight.getFleet(callback = self._fleetRetrieved,
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| 226 | force = True)
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[9] | 227 | self.logger.message(aircraftState.timestamp, "Flight time end")
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| 228 | self.logFuel(aircraftState)
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| 229 | self.logger.message(aircraftState.timestamp,
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| 230 | "Landing weight: %.0f kg, MLW: %.0f" % \
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| 231 | (aircraftState.grossWeight, self.mlw))
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| 232 | self.logger.message(aircraftState.timestamp,
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| 233 | "Vertical speed range: %.0f..%.0f feet/min" % \
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[12] | 234 | (self._minVS, self._maxVS))
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[9] | 235 | elif newStage==const.STAGE_PARKING:
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| 236 | self.logger.message(aircraftState.timestamp, "Block time end")
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[89] | 237 | elif newStage==const.STAGE_END:
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| 238 | flightLength = self._flight.flightTimeEnd - self._flight.flightTimeStart
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| 239 | self.logger.message(aircraftState.timestamp,
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| 240 | "Flight time: " +
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| 241 | util.getTimeIntervalString(flightLength))
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| 242 | self.logger.message(aircraftState.timestamp,
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| 243 | "Flown distance: %.2f NM" % \
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| 244 | (self._flight.flownDistance,))
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| 245 | blockLength = self._flight.blockTimeEnd - self._flight.blockTimeStart
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| 246 | self.logger.message(aircraftState.timestamp,
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| 247 | "Block time: " +
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| 248 | util.getTimeIntervalString(blockLength))
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[8] | 249 |
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[9] | 250 | def prepareFlare(self):
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| 251 | """Called when it is detected that we will soon flare.
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[8] | 252 |
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| 253 | On the first call, it should start monitoring some parameters more
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| 254 | closely to determine flare time."""
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[9] | 255 | self.flight.simulator.startFlare()
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| 256 |
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| 257 | def flareStarted(self, windSpeed, windDirection, visibility,
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| 258 | flareStart, flareStartFS):
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| 259 | """Called when the flare has started."""
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| 260 | self.logger.message(self._aircraftState.timestamp, "The flare has begun")
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| 261 | self.logger.message(self._aircraftState.timestamp,
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| 262 | "Wind %03.0f degrees at %.0f knots" % \
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| 263 | (windDirection, windSpeed))
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| 264 | self.logger.message(self._aircraftState.timestamp,
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| 265 | "Visibility: %.0f metres" % (visibility,))
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| 266 | self.logger.message(self._aircraftState.timestamp,
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| 267 | "Altimeter setting: %.0f hPa" % \
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| 268 | (self._aircraftState.altimeter,))
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[101] | 269 | self._logVRef()
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[9] | 270 | self.flight.flareStarted(flareStart, flareStartFS)
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[134] | 271 | fs.sendMessage(const.MESSAGETYPE_INFORMATION, "Flare-time", 3)
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[9] | 272 |
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| 273 | def flareFinished(self, flareEnd, flareEndFS, tdRate, tdRateCalculatedByFS,
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| 274 | ias, pitch, bank, heading):
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| 275 | """Called when the flare has finished."""
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| 276 | (flareTimeFromFS, flareTime) = self.flight.flareFinished(flareEnd,
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[170] | 277 | flareEndFS,
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| 278 | tdRate)
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[9] | 279 | self.logger.message(self._aircraftState.timestamp,
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[153] | 280 | "Flaretime: %.3f (from %s)" % \
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[9] | 281 | (flareTime,
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| 282 | "the simulator" if flareTimeFromFS else "real time",))
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| 283 | self.logger.message(self._aircraftState.timestamp,
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| 284 | "Touchdown rate: %.0f feet/min" % (tdRate,))
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| 285 | self.logger.message(self._aircraftState.timestamp,
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| 286 | "Touchdown rate was calculated by the %s" % \
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| 287 | ("simulator" if tdRateCalculatedByFS else "logger",))
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| 288 | self.logger.message(self._aircraftState.timestamp,
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| 289 | "Touchdown speed: %.0f knots" % (ias,))
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| 290 | self.logger.message(self._aircraftState.timestamp,
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| 291 | "Touchdown pitch: %.1f degrees" % (pitch,))
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| 292 | self.logger.message(self._aircraftState.timestamp,
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| 293 | "Touchdown bank: %.1f degrees" % (bank,))
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| 294 | self.logger.message(self._aircraftState.timestamp,
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| 295 | "Touchdown heading: %03.0f degrees" % (heading,))
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[8] | 296 |
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| 297 | def cancelFlare(self):
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| 298 | """Cancel flare, if it has started."""
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[9] | 299 | self.flight.simulator.cancelFlare()
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[8] | 300 |
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| 301 | def checkFlightEnd(self, aircraftState):
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| 302 | """Check if the end of the flight has arrived.
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| 303 |
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| 304 | This default implementation checks the N1 values, but for
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| 305 | piston-powered aircraft you need to check the RPMs."""
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| 306 | for n1 in aircraftState.n1:
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| 307 | if n1>=0.5: return False
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| 308 | return True
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| 309 |
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[101] | 310 | def updateV1R2(self):
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| 311 | """Update the V1, Vr and V2 values from the flight, if the these values
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| 312 | have already been logged."""
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| 313 | if self._v1r2LineIndex is not None:
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| 314 | self._logV1R2()
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| 315 |
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| 316 | def _logV1R2(self):
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| 317 | """Log the V1, Vr and V2 value either newly, or by updating the
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| 318 | corresponding line."""
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| 319 | message = "Speeds calculated by the pilot: V1: %s, VR: %s, V2: %s" % \
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| 320 | ("-" if self._flight.v1 is None
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| 321 | else str(self._flight.v1),
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| 322 | "-" if self._flight.vr is None
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| 323 | else str(self._flight.vr),
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| 324 | "-" if self._flight.v2 is None
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| 325 | else str(self._flight.v2))
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| 326 |
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| 327 | if self._v1r2LineIndex is None:
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| 328 | self._v1r2LineIndex = \
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| 329 | self.logger.message(self._aircraftState.timestamp, message)
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| 330 | else:
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| 331 | self.logger.updateLine(self._v1r2LineIndex, message)
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| 332 |
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[96] | 333 | def updateVRef(self):
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| 334 | """Update the Vref value from the flight, if the Vref value has already
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| 335 | been logged."""
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| 336 | if self._vrefLineIndex is not None:
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| 337 | self._logVRef()
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| 338 |
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| 339 | def _logVRef(self):
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| 340 | """Log the Vref value either newly, or by updating the corresponding
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| 341 | line."""
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| 342 | message = "VRef speed calculated by the pilot: %s" % \
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| 343 | ("-" if self._flight.vref is None else str(self._flight.vref))
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| 344 | if self._vrefLineIndex is None:
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| 345 | self._vrefLineIndex = \
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| 346 | self.logger.message(self._aircraftState.timestamp, message)
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| 347 | else:
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| 348 | self.logger.updateLine(self._vrefLineIndex, message)
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| 349 |
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[134] | 350 | def _fleetRetrieved(self, fleet):
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| 351 | """Callback for the fleet retrieval result."""
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| 352 | if fleet is not None:
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| 353 | gateList = ""
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| 354 | occupiedGateNumbers = fleet.getOccupiedGateNumbers()
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| 355 | for gateNumber in const.lhbpGateNumbers:
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| 356 | if gateNumber not in occupiedGateNumbers:
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| 357 | if gateList: gateList += ", "
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| 358 | gateList += gateNumber
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| 359 | fs.sendMessage(const.MESSAGETYPE_GATE_SYSTEM,
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| 360 | "Free gates: " + gateList, 20)
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| 361 |
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| 362 |
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[4] | 363 | #---------------------------------------------------------------------------------------
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[7] | 364 |
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| 365 | class Boeing737(Aircraft):
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| 366 | """Base class for the various aircraft in the Boeing 737 family.
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| 367 |
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| 368 | The aircraft type-specific values in the aircraft state have the following
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| 369 | structure:
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[140] | 370 | - fuel: left, centre, right
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[7] | 371 | - n1: left, right
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| 372 | - reverser: left, right"""
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[140] | 373 | fuelTanks = [const.FUELTANK_LEFT, const.FUELTANK_CENTRE, const.FUELTANK_RIGHT]
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| 374 |
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[9] | 375 | def __init__(self, flight):
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| 376 | super(Boeing737, self).__init__(flight)
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[95] | 377 | self._checkers.append(checks.ThrustChecker())
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| 378 |
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[9] | 379 | self.gearSpeedLimit = 270
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| 380 | self.flapSpeedLimits = { 1 : 260,
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| 381 | 2 : 260,
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| 382 | 5 : 250,
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| 383 | 10 : 210,
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| 384 | 15 : 200,
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| 385 | 25 : 190,
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| 386 | 30 : 175,
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| 387 | 40 : 162 }
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[7] | 388 |
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[9] | 389 | def logFuel(self, aircraftState):
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| 390 | """Log the amount of fuel"""
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| 391 | self.logger.message(aircraftState.timestamp,
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| 392 | "Fuel: left=%.0f kg - centre=%.0f kg - right=%.0f kg" % \
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[150] | 393 | (aircraftState.fuel[0], aircraftState.fuel[1],
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[9] | 394 | aircraftState.fuel[2]))
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| 395 | self.logger.message(aircraftState.timestamp,
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| 396 | "Total fuel: %.0f kg" % (sum(aircraftState.fuel),))
|
---|
| 397 |
|
---|
[7] | 398 | #---------------------------------------------------------------------------------------
|
---|
| 399 |
|
---|
| 400 | class B736(Boeing737):
|
---|
| 401 | """Boeing 737-600 aircraft."""
|
---|
[8] | 402 | def __init__(self, flight):
|
---|
| 403 | super(B736, self).__init__(flight)
|
---|
[9] | 404 | self.dow = 38307
|
---|
| 405 | self.mtow = 58328
|
---|
| 406 | self.mlw = 54657
|
---|
| 407 | self.mzfw = 51482
|
---|
[7] | 408 |
|
---|
| 409 | #---------------------------------------------------------------------------------------
|
---|
| 410 |
|
---|
| 411 | class B737(Boeing737):
|
---|
| 412 | """Boeing 737-700 aircraft."""
|
---|
[8] | 413 | def __init__(self, flight):
|
---|
| 414 | super(B737, self).__init__(flight)
|
---|
[9] | 415 | self.dow = 39250
|
---|
| 416 | self.mtow = 61410
|
---|
| 417 | self.mlw = 58059
|
---|
| 418 | self.mzfw = 54657
|
---|
[7] | 419 |
|
---|
| 420 | #---------------------------------------------------------------------------------------
|
---|
| 421 |
|
---|
| 422 | class B738(Boeing737):
|
---|
| 423 | """Boeing 737-800 aircraft."""
|
---|
[8] | 424 | def __init__(self, flight):
|
---|
| 425 | super(B738, self).__init__(flight)
|
---|
[9] | 426 | self.dow = 42690
|
---|
| 427 | self.mtow = 71709
|
---|
| 428 | self.mlw = 65317
|
---|
| 429 | self.mzfw = 61688
|
---|
| 430 |
|
---|
| 431 | #---------------------------------------------------------------------------------------
|
---|
| 432 |
|
---|
| 433 | class B738Charter(B738):
|
---|
| 434 | """Boeing 737-800 aircraft used for charters."""
|
---|
| 435 | def __init__(self, flight):
|
---|
| 436 | super(B738Charter, self).__init__(flight)
|
---|
| 437 | self.mtow = 77791
|
---|
[7] | 438 |
|
---|
| 439 | #---------------------------------------------------------------------------------------
|
---|
| 440 |
|
---|
| 441 | class B733(Boeing737):
|
---|
| 442 | """Boeing 737-300 aircraft."""
|
---|
[8] | 443 | def __init__(self, flight):
|
---|
| 444 | super(B733, self).__init__(flight)
|
---|
[9] | 445 | self.dow = 32700
|
---|
| 446 | self.mtow = 62820
|
---|
| 447 | self.mlw = 51700
|
---|
| 448 | self.mzfw = 48410
|
---|
[7] | 449 |
|
---|
| 450 | #---------------------------------------------------------------------------------------
|
---|
| 451 |
|
---|
| 452 | class B734(Boeing737):
|
---|
| 453 | """Boeing 737-400 aircraft."""
|
---|
[8] | 454 | def __init__(self, flight):
|
---|
| 455 | super(B734, self).__init__(flight)
|
---|
[9] | 456 | self.dow = 33200
|
---|
| 457 | self.mtow = 68050
|
---|
| 458 | self.mlw = 56200
|
---|
| 459 | self.mzfw = 53100
|
---|
[7] | 460 |
|
---|
| 461 | #---------------------------------------------------------------------------------------
|
---|
| 462 |
|
---|
| 463 | class B735(Boeing737):
|
---|
| 464 | """Boeing 737-500 aircraft."""
|
---|
[8] | 465 | def __init__(self, flight):
|
---|
| 466 | super(B735, self).__init__(flight)
|
---|
[9] | 467 | self.dow = 31300
|
---|
| 468 | self.mtow = 60550
|
---|
| 469 | self.mlw = 50000
|
---|
| 470 | self.mzfw = 46700
|
---|
[7] | 471 |
|
---|
| 472 | #---------------------------------------------------------------------------------------
|
---|
| 473 |
|
---|
| 474 | class DH8D(Aircraft):
|
---|
| 475 | """Bombardier Dash-8 Q400 aircraft.
|
---|
| 476 |
|
---|
| 477 | The aircraft type-specific values in the aircraft state have the following
|
---|
| 478 | structure:
|
---|
[140] | 479 | - fuel: left, right
|
---|
[7] | 480 | - n1: left, right
|
---|
| 481 | - reverser: left, right."""
|
---|
[140] | 482 | fuelTanks = [const.FUELTANK_LEFT, const.FUELTANK_RIGHT]
|
---|
| 483 |
|
---|
[8] | 484 | def __init__(self, flight):
|
---|
| 485 | super(DH8D, self).__init__(flight)
|
---|
[9] | 486 | self.dow = 17185
|
---|
| 487 | self.mtow = 29257
|
---|
| 488 | self.mlw = 28009
|
---|
| 489 | self.mzfw = 25855
|
---|
| 490 | self.gearSpeedLimit = 215
|
---|
| 491 | self.flapSpeedLimits = { 5 : 200,
|
---|
| 492 | 10 : 181,
|
---|
| 493 | 15 : 172,
|
---|
| 494 | 35 : 158 }
|
---|
| 495 |
|
---|
| 496 | def logFuel(self, aircraftState):
|
---|
| 497 | """Log the amount of fuel"""
|
---|
| 498 | self.logger.message(aircraftState.timestamp,
|
---|
[150] | 499 | "Fuel: left=%.0f kg - right=%.0f kg" % \
|
---|
| 500 | (aircraftState.fuel[0], aircraftState.fuel[1]))
|
---|
[9] | 501 | self.logger.message(aircraftState.timestamp,
|
---|
| 502 | "Total fuel: %.0f kg" % (sum(aircraftState.fuel),))
|
---|
[7] | 503 |
|
---|
| 504 | #---------------------------------------------------------------------------------------
|
---|
| 505 |
|
---|
| 506 | class Boeing767(Aircraft):
|
---|
| 507 | """Base class for the various aircraft in the Boeing 767 family.
|
---|
| 508 |
|
---|
| 509 | The aircraft type-specific values in the aircraft state have the following
|
---|
| 510 | structure:
|
---|
[140] | 511 | - fuel: left, centre, right
|
---|
[7] | 512 | - n1: left, right
|
---|
| 513 | - reverser: left, right"""
|
---|
[140] | 514 | fuelTanks = [const.FUELTANK_LEFT, const.FUELTANK_CENTRE, const.FUELTANK_RIGHT]
|
---|
| 515 |
|
---|
[9] | 516 | def __init__(self, flight):
|
---|
| 517 | super(Boeing767, self).__init__(flight)
|
---|
[95] | 518 | self._checkers.append(checks.ThrustChecker())
|
---|
[9] | 519 | self.gearSpeedLimit = 270
|
---|
| 520 | self.flapSpeedLimits = { 1 : 255,
|
---|
| 521 | 5 : 235,
|
---|
| 522 | 10 : 215,
|
---|
| 523 | 20 : 215,
|
---|
| 524 | 25 : 185,
|
---|
| 525 | 30 : 175 }
|
---|
[7] | 526 |
|
---|
[9] | 527 | def logFuel(self, aircraftState):
|
---|
| 528 | """Log the amount of fuel"""
|
---|
| 529 | self.logger.message(aircraftState.timestamp,
|
---|
| 530 | "Fuel: left=%.0f kg - centre=%.0f kg - right=%.0f kg" % \
|
---|
[150] | 531 | (aircraftState.fuel[0], aircraftState.fuel[1],
|
---|
[9] | 532 | aircraftState.fuel[2]))
|
---|
| 533 | self.logger.message(aircraftState.timestamp,
|
---|
| 534 | "Total fuel: %.0f kg" % (sum(aircraftState.fuel),))
|
---|
| 535 |
|
---|
[7] | 536 | #---------------------------------------------------------------------------------------
|
---|
| 537 |
|
---|
| 538 | class B762(Boeing767):
|
---|
| 539 | """Boeing 767-200 aircraft."""
|
---|
[8] | 540 | def __init__(self, flight):
|
---|
| 541 | super(B762, self).__init__(flight)
|
---|
[9] | 542 | self.dow = 84507
|
---|
| 543 | self.mtow = 175540
|
---|
| 544 | self.mlw = 126098
|
---|
| 545 | self.mzfw = 114758
|
---|
[7] | 546 |
|
---|
| 547 | #---------------------------------------------------------------------------------------
|
---|
| 548 |
|
---|
| 549 | class B763(Boeing767):
|
---|
| 550 | """Boeing 767-300 aircraft."""
|
---|
[8] | 551 | def __init__(self, flight):
|
---|
| 552 | super(B763, self).__init__(cflight)
|
---|
[9] | 553 | self.dow = 91311
|
---|
| 554 | self.mtow = 181436
|
---|
| 555 | self.mlw = 137892
|
---|
| 556 | self.mzfw = 130635
|
---|
[7] | 557 |
|
---|
| 558 | #---------------------------------------------------------------------------------------
|
---|
| 559 |
|
---|
| 560 | class CRJ2(Aircraft):
|
---|
| 561 | """Bombardier CRJ-200 aircraft.
|
---|
| 562 |
|
---|
| 563 | The aircraft type-specific values in the aircraft state have the following
|
---|
| 564 | structure:
|
---|
[140] | 565 | - fuel: left, centre, right
|
---|
[7] | 566 | - n1: left, right
|
---|
| 567 | - reverser: left, right."""
|
---|
[140] | 568 | fuelTanks = [const.FUELTANK_LEFT, const.FUELTANK_CENTRE, const.FUELTANK_RIGHT]
|
---|
| 569 |
|
---|
[8] | 570 | def __init__(self, flight):
|
---|
| 571 | super(CRJ2, self).__init__(flight)
|
---|
[95] | 572 | self._checkers.append(checks.ThrustChecker())
|
---|
[9] | 573 | self.dow = 14549
|
---|
| 574 | self.mtow = 22995
|
---|
| 575 | self.mlw = 21319
|
---|
| 576 | self.mzfw = 19958
|
---|
| 577 | self.gearSpeedLimit = 240
|
---|
| 578 | self.flapSpeedLimits = { 8 : 260,
|
---|
| 579 | 20 : 220,
|
---|
| 580 | 30 : 190,
|
---|
| 581 | 45 : 175 }
|
---|
[7] | 582 |
|
---|
[9] | 583 | def logFuel(self, aircraftState):
|
---|
| 584 | """Log the amount of fuel"""
|
---|
| 585 | self.logger.message(aircraftState.timestamp,
|
---|
| 586 | "Fuel: left=%.0f kg - centre=%.0f kg - right=%.0f kg" % \
|
---|
[150] | 587 | (aircraftState.fuel[0], aircraftState.fuel[1],
|
---|
[9] | 588 | aircraftState.fuel[2]))
|
---|
| 589 | self.logger.message(aircraftState.timestamp,
|
---|
| 590 | "Total fuel: %.0f kg" % (sum(aircraftState.fuel),))
|
---|
| 591 |
|
---|
[7] | 592 | #---------------------------------------------------------------------------------------
|
---|
| 593 |
|
---|
| 594 | class F70(Aircraft):
|
---|
| 595 | """Fokker 70 aircraft.
|
---|
| 596 |
|
---|
| 597 | The aircraft type-specific values in the aircraft state have the following
|
---|
| 598 | structure:
|
---|
[140] | 599 | - fuel: left, centre, right
|
---|
[7] | 600 | - n1: left, right
|
---|
| 601 | - reverser: left, right."""
|
---|
[140] | 602 | fuelTanks = [const.FUELTANK_LEFT, const.FUELTANK_CENTRE, const.FUELTANK_RIGHT]
|
---|
| 603 |
|
---|
[8] | 604 | def __init__(self, flight):
|
---|
| 605 | super(F70, self).__init__(flight)
|
---|
[95] | 606 | self._checkers.append(checks.ThrustChecker())
|
---|
[9] | 607 | self.dow = 24283
|
---|
| 608 | self.mtow = 38100 # FIXME: differentiate by registration number,
|
---|
| 609 | # MTOW of HA-LMF: 41955
|
---|
| 610 | self.mlw = 36740
|
---|
| 611 | self.mzfw = 32655
|
---|
| 612 | self.gearSpeedLimit = 200
|
---|
| 613 | self.flapSpeedLimits = { 8 : 250,
|
---|
| 614 | 15 : 220,
|
---|
| 615 | 25 : 220,
|
---|
| 616 | 42 : 180 }
|
---|
[7] | 617 |
|
---|
[9] | 618 | def logFuel(self, aircraftState):
|
---|
| 619 | """Log the amount of fuel"""
|
---|
| 620 | self.logger.message(aircraftState.timestamp,
|
---|
| 621 | "Fuel: left=%.0f kg - centre=%.0f kg - right=%.0f kg" % \
|
---|
[150] | 622 | (aircraftState.fuel[0], aircraftState.fuel[1],
|
---|
[9] | 623 | aircraftState.fuel[2]))
|
---|
| 624 | self.logger.message(aircraftState.timestamp,
|
---|
| 625 | "Total fuel: %.0f kg" % (sum(aircraftState.fuel),))
|
---|
| 626 |
|
---|
[7] | 627 | #---------------------------------------------------------------------------------------
|
---|
| 628 |
|
---|
| 629 | class DC3(Aircraft):
|
---|
| 630 | """Lisunov Li-2 (DC-3) aircraft.
|
---|
| 631 |
|
---|
| 632 | The aircraft type-specific values in the aircraft state have the following
|
---|
| 633 | structure:
|
---|
[140] | 634 | - fuel: left aux, left, right, right aux
|
---|
[7] | 635 | - rpm: left, right
|
---|
| 636 | - reverser: left, right."""
|
---|
[140] | 637 | fuelTanks = [const.FUELTANK_LEFT_AUX, const.FUELTANK_LEFT,
|
---|
| 638 | const.FUELTANK_RIGHT, const.FUELTANK_RIGHT_AUX]
|
---|
| 639 |
|
---|
[8] | 640 | def __init__(self, flight):
|
---|
| 641 | super(DC3, self).__init__(flight)
|
---|
[9] | 642 | self.dow = 8627
|
---|
| 643 | self.mtow = 11884
|
---|
| 644 | self.mlw = 11793
|
---|
| 645 | self.mzfw = 11780
|
---|
| 646 | self.gearSpeedLimit = 148
|
---|
| 647 | self.flapSpeedLimits = { 15 : 135,
|
---|
| 648 | 30 : 99,
|
---|
| 649 | 45 : 97 }
|
---|
[8] | 650 |
|
---|
| 651 | def _checkFlightEnd(self, aircraftState):
|
---|
| 652 | """Check if the end of the flight has arrived.
|
---|
| 653 |
|
---|
| 654 | This implementation checks the RPM values to be 0."""
|
---|
| 655 | for rpm in aircraftState.rpm:
|
---|
[29] | 656 | if rpm>0: return False
|
---|
| 657 | return True
|
---|
[7] | 658 |
|
---|
[9] | 659 | def logFuel(self, aircraftState):
|
---|
| 660 | """Log the amount of fuel"""
|
---|
| 661 | self.logger.message(aircraftState.timestamp,
|
---|
| 662 | "Fuel: left aux=%.0f kg - left=%.0f kg - right=%.0f kg - right aux=%.0f kg" % \
|
---|
[150] | 663 | (aircraftState.fuel[0], aircraftState.fuel[1],
|
---|
| 664 | aircraftState.fuel[2], aircraftState.fuel[3]))
|
---|
[9] | 665 | self.logger.message(aircraftState.timestamp,
|
---|
| 666 | "Total fuel: %.0f kg" % (sum(aircraftState.fuel),))
|
---|
| 667 |
|
---|
[7] | 668 | #---------------------------------------------------------------------------------------
|
---|
| 669 |
|
---|
| 670 | class T134(Aircraft):
|
---|
| 671 | """Tupolev Tu-134 aircraft.
|
---|
| 672 |
|
---|
| 673 | The aircraft type-specific values in the aircraft state have the following
|
---|
| 674 | structure:
|
---|
[140] | 675 | - fuel: left tip, left aux, centre, right aux, right tip, external 1,
|
---|
[7] | 676 | external 2
|
---|
| 677 | - n1: left, right
|
---|
| 678 | - reverser: left, right."""
|
---|
[140] | 679 | fuelTanks = [const.FUELTANK_LEFT_TIP, const.FUELTANK_LEFT_AUX,
|
---|
| 680 | const.FUELTANK_CENTRE,
|
---|
| 681 | const.FUELTANK_RIGHT_AUX, const.FUELTANK_RIGHT_TIP,
|
---|
| 682 | const.FUELTANK_EXTERNAL1, const.FUELTANK_EXTERNAL2]
|
---|
| 683 |
|
---|
[8] | 684 | def __init__(self, flight):
|
---|
| 685 | super(T134, self).__init__(flight)
|
---|
[95] | 686 | self._checkers.append(checks.ThrustChecker())
|
---|
[9] | 687 | self.dow = 29927
|
---|
| 688 | self.mtow = 47600
|
---|
| 689 | self.mlw = 43000
|
---|
| 690 | self.mzfw = 38500
|
---|
| 691 | self.gearSpeedLimit = 216
|
---|
| 692 | self.flapSpeedLimits = { 10 : 240,
|
---|
| 693 | 20 : 216,
|
---|
| 694 | 30 : 161 }
|
---|
[7] | 695 |
|
---|
[9] | 696 | def logFuel(self, aircraftState):
|
---|
| 697 | """Log the amount of fuel"""
|
---|
| 698 | self.logger.message(aircraftState.timestamp,
|
---|
| 699 | "Fuel: left aux=%.0f kg - left tip=%.0f kg - centre= %.0f kg - right tip=%.0f kg - right aux=%.0f kg - external 1=%.0f kg - external 2=%.0f kg" % \
|
---|
[150] | 700 | (aircraftState.fuel[1], aircraftState.fuel[0],
|
---|
| 701 | aircraftState.fuel[2],
|
---|
| 702 | aircraftState.fuel[4], aircraftState.fuel[3],
|
---|
[9] | 703 | aircraftState.fuel[5], aircraftState.fuel[6]))
|
---|
| 704 | self.logger.message(aircraftState.timestamp,
|
---|
| 705 | "Total fuel: %.0f kg" % (sum(aircraftState.fuel),))
|
---|
| 706 |
|
---|
[7] | 707 | #---------------------------------------------------------------------------------------
|
---|
| 708 |
|
---|
| 709 | class T154(Aircraft):
|
---|
| 710 | """Tupolev Tu-154 aircraft.
|
---|
| 711 |
|
---|
| 712 | The aircraft type-specific values in the aircraft state have the following
|
---|
| 713 | structure:
|
---|
[140] | 714 | - fuel: left aux, left, centre, centre 2, right, right aux
|
---|
[7] | 715 | - n1: left, centre, right
|
---|
| 716 | - reverser: left, right"""
|
---|
[140] | 717 | fuelTanks = [const.FUELTANK_LEFT_AUX, const.FUELTANK_LEFT,
|
---|
| 718 | const.FUELTANK_CENTRE, const.FUELTANK_CENTRE2,
|
---|
| 719 | const.FUELTANK_RIGHT, const.FUELTANK_RIGHT_AUX]
|
---|
[8] | 720 | def __init__(self, flight):
|
---|
| 721 | super(T154, self).__init__(flight)
|
---|
[95] | 722 | self._checkers.append(checks.ThrustChecker())
|
---|
[9] | 723 | self.dow = 53259
|
---|
| 724 | self.mtow = 98000
|
---|
| 725 | self.mlw = 78000
|
---|
| 726 | self.mzfw = 72000
|
---|
| 727 | self.gearSpeedLimit = 216
|
---|
| 728 | self.flapSpeedLimits = { 15 : 227,
|
---|
| 729 | 28 : 194,
|
---|
| 730 | 45 : 162 }
|
---|
| 731 |
|
---|
| 732 | def logFuel(self, aircraftState):
|
---|
| 733 | """Log the amount of fuel"""
|
---|
| 734 | self.logger.message(aircraftState.timestamp,
|
---|
| 735 | "Fuel: left aux=%.0f kg - left=%.0f kg - centre=%.0f kg - centre 2=%.0f kg - right=%.0f kg - right aux=%.0f kg" % \
|
---|
[150] | 736 | (aircraftState.fuel[0], aircraftState.fuel[1],
|
---|
| 737 | aircraftState.fuel[2], aircraftState.fuel[3],
|
---|
| 738 | aircraftState.fuel[4], aircraftState.fuel[5]))
|
---|
[9] | 739 | self.logger.message(aircraftState.timestamp,
|
---|
| 740 | "Total fuel: %.0f kg" % (sum(aircraftState.fuel),))
|
---|
[7] | 741 |
|
---|
| 742 | #---------------------------------------------------------------------------------------
|
---|
| 743 |
|
---|
[9] | 744 |
|
---|
[7] | 745 | class YK40(Aircraft):
|
---|
| 746 | """Yakovlev Yak-40 aircraft.
|
---|
| 747 |
|
---|
| 748 | The aircraft type-specific values in the aircraft state have the following
|
---|
| 749 | structure:
|
---|
| 750 | - fuel: left, right
|
---|
| 751 | - n1: left, right
|
---|
| 752 | - reverser: left, right"""
|
---|
[140] | 753 | fuelTanks = [const.FUELTANK_LEFT, const.FUELTANK_RIGHT]
|
---|
| 754 |
|
---|
[8] | 755 | def __init__(self, flight):
|
---|
| 756 | super(YK40, self).__init__(flight)
|
---|
[95] | 757 | self._checkers.append(checks.ThrustChecker())
|
---|
[9] | 758 | self.dow = 9400
|
---|
| 759 | self.mtow = 17200
|
---|
| 760 | self.mlw = 16800
|
---|
| 761 | self.mzfw = 12100
|
---|
| 762 | self.gearSpeedLimit = 165
|
---|
| 763 | self.flapSpeedLimits = { 20 : 165,
|
---|
| 764 | 35 : 135 }
|
---|
| 765 |
|
---|
| 766 | def logFuel(self, aircraftState):
|
---|
| 767 | """Log the amount of fuel"""
|
---|
| 768 | self.logger.message(aircraftState.timestamp,
|
---|
| 769 | "Fuel: left=%.0f kg - right=%.0f kg" % \
|
---|
| 770 | (aircraftState.fuel[0], aircraftState.fuel[1]))
|
---|
| 771 | self.logger.message(aircraftState.timestamp,
|
---|
| 772 | "Total fuel: %.0f kg" % (sum(aircraftState.fuel),))
|
---|
[7] | 773 |
|
---|
| 774 | #---------------------------------------------------------------------------------------
|
---|
| 775 |
|
---|
[141] | 776 | MostFuelTankAircraft = T134
|
---|
| 777 |
|
---|
| 778 | #---------------------------------------------------------------------------------------
|
---|
| 779 |
|
---|
[191] | 780 | _classes = { const.AIRCRAFT_B736 : B736,
|
---|
| 781 | const.AIRCRAFT_B737 : B737,
|
---|
| 782 | const.AIRCRAFT_B738 : B738,
|
---|
| 783 | const.AIRCRAFT_B738C : B738Charter,
|
---|
| 784 | const.AIRCRAFT_B733 : B733,
|
---|
| 785 | const.AIRCRAFT_B734 : B734,
|
---|
| 786 | const.AIRCRAFT_B735 : B735,
|
---|
| 787 | const.AIRCRAFT_DH8D : DH8D,
|
---|
| 788 | const.AIRCRAFT_B762 : B762,
|
---|
| 789 | const.AIRCRAFT_B763 : B763,
|
---|
| 790 | const.AIRCRAFT_CRJ2 : CRJ2,
|
---|
| 791 | const.AIRCRAFT_F70 : F70,
|
---|
| 792 | const.AIRCRAFT_DC3 : DC3,
|
---|
| 793 | const.AIRCRAFT_T134 : T134,
|
---|
| 794 | const.AIRCRAFT_T154 : T154,
|
---|
| 795 | const.AIRCRAFT_YK40 : YK40 }
|
---|
[8] | 796 |
|
---|
| 797 | #---------------------------------------------------------------------------------------
|
---|
[197] | 798 |
|
---|
| 799 | if __name__ == "__main__":
|
---|
| 800 | value = SmoothedValue()
|
---|
| 801 |
|
---|
| 802 | print "Adding 1, 12.0"
|
---|
| 803 | value.add(1, 12.0)
|
---|
| 804 | print value.get()
|
---|
| 805 |
|
---|
| 806 | print "Adding 1, 15.0"
|
---|
| 807 | value.add(1, 15.0)
|
---|
| 808 | print value.get()
|
---|
| 809 |
|
---|
| 810 | print "Adding 2, 18.0"
|
---|
| 811 | value.add(2, 18.0)
|
---|
| 812 | print value.get()
|
---|
| 813 |
|
---|
| 814 | print "Adding 2, 20.0"
|
---|
| 815 | value.add(2, 20.0)
|
---|
| 816 | print value.get()
|
---|
| 817 |
|
---|
| 818 | print "Adding 5, 22.0"
|
---|
| 819 | value.add(5, 22.0)
|
---|
| 820 | print value.get()
|
---|
| 821 |
|
---|
| 822 | print "Adding 5, 25.0"
|
---|
| 823 | value.add(5, 25.0)
|
---|
| 824 | print value.get()
|
---|
| 825 |
|
---|
| 826 | print "Adding 5, 29.0"
|
---|
| 827 | value.add(5, 29.0)
|
---|
| 828 | print value.get()
|
---|
| 829 |
|
---|
| 830 | print "Adding 5, 21.0"
|
---|
| 831 | value.add(5, 21.0)
|
---|
| 832 | print value.get()
|
---|
| 833 |
|
---|
| 834 | print "Adding 5, 26.0"
|
---|
| 835 | value.add(5, 26.0)
|
---|
| 836 | print value.get()
|
---|
| 837 |
|
---|
| 838 | print "Adding 2, 30.0"
|
---|
| 839 | value.add(2, 30.0)
|
---|
| 840 | print value.get()
|
---|
| 841 |
|
---|
| 842 | print "Adding 2, 55.0"
|
---|
| 843 | value.add(2, 55.0)
|
---|
| 844 | print value.get()
|
---|
| 845 |
|
---|
| 846 | #---------------------------------------------------------------------------------------
|
---|