[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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[4] | 7 |
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[8] | 8 | import time
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[7] | 9 |
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[4] | 10 | #---------------------------------------------------------------------------------------
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| 11 |
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| 12 | class Aircraft(object):
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| 13 | """Base class for aircraft."""
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[8] | 14 | @staticmethod
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| 15 | def create(flight):
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| 16 | """Create an aircraft instance for the type in the given flight."""
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| 17 | return _classes[flight.aircraftType](flight)
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| 18 |
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| 19 | def __init__(self, flight):
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[4] | 20 | """Construct the aircraft for the given type."""
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[8] | 21 | self._flight = flight
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[4] | 22 | self._aircraftState = None
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[9] | 23 |
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| 24 | self._maxVS = -10000.0
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| 25 | self._minVS = 10000.0
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[4] | 26 |
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[8] | 27 | self._checkers = []
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| 28 |
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| 29 | self._checkers.append(checks.StageChecker())
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[9] | 30 | self._checkers.append(checks.TakeOffLogger())
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[8] | 31 |
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| 32 | self._checkers.append(checks.AltimeterLogger())
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| 33 |
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| 34 | self._checkers.append(checks.NAV1Logger())
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| 35 | self._checkers.append(checks.NAV2Logger())
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| 36 | self._checkers.append(checks.SquawkLogger())
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| 37 |
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| 38 | self._checkers.append(checks.AnticollisionLightsLogger())
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| 39 | self._checkers.append(checks.LandingLightsLogger())
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| 40 | self._checkers.append(checks.StrobeLightsLogger())
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| 41 | self._checkers.append(checks.NavLightsLogger())
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| 42 |
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| 43 | self._checkers.append(checks.FlapsLogger())
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| 44 |
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| 45 | self._checkers.append(checks.GearsLogger())
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[9] | 46 | self._checkers.append(checks.CruiseSpeedLogger())
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[10] | 47 | self._checkers.append(checks.SpoilerLogger())
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[9] | 48 |
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[4] | 49 | @property
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| 50 | def type(self):
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| 51 | """Get the type of the aircraft."""
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[8] | 52 | return self._flight.aircraftType
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| 53 |
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| 54 | @property
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| 55 | def flight(self):
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| 56 | """Get the flight the aircraft belongs to."""
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| 57 | return self._flight
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[4] | 58 |
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[8] | 59 | @property
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| 60 | def logger(self):
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| 61 | """Get the logger to use for the aircraft."""
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| 62 | return self._flight.logger
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| 63 |
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| 64 | def modelChanged(self, timestamp, aircraftName, modelName):
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[4] | 65 | """Called when the simulator's aircraft changes."""
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[8] | 66 | self._flight.logger.message(timestamp,
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| 67 | "Aircraft: name='%s', model='%s'" % \
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| 68 | (aircraftName, modelName))
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[4] | 69 |
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| 70 | def handleState(self, aircraftState):
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| 71 | """Called when the state of the aircraft changes."""
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[8] | 72 | for checker in self._checkers:
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| 73 | checker.check(self._flight, self, self._flight.logger,
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| 74 | self._aircraftState, aircraftState)
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[7] | 75 |
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[9] | 76 | self._maxVS = max(self._maxVS, aircraftState.vs)
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| 77 | self._minVS = min(self._minVS, aircraftState.vs)
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| 78 |
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[4] | 79 | self._aircraftState = aircraftState
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[8] | 80 |
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| 81 | def setStage(self, aircraftState, newStage):
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| 82 | """Set the given stage as the new one and do whatever should be
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| 83 | done."""
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[9] | 84 | if self._flight.setStage(aircraftState.timestamp, newStage):
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| 85 | if newStage==const.STAGE_PUSHANDTAXI:
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| 86 | self.logger.message(aircraftState.timestamp, "Block time start")
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| 87 | self.logFuel(aircraftState)
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| 88 | self.logger.message(aircraftState.timestamp,
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| 89 | "Zero-fuel weight: %.0f kg" % (aircraftState.zfw))
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| 90 | elif newStage==const.STAGE_TAKEOFF:
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| 91 | self.logger.message(aircraftState.timestamp, "Flight time start")
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| 92 | self.logger.message(aircraftState.timestamp,
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| 93 | "Takeoff weight: %.0f kg, MTOW: %.0f kg" % \
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| 94 | (aircraftState.grossWeight, self.mtow))
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| 95 | self.logger.message(aircraftState.timestamp,
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| 96 | "Wind %03.0f degrees at %.0f knots" % \
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| 97 | (aircraftState.windDirection,
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| 98 | aircraftState.windSpeed))
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| 99 | elif newStage==const.STAGE_TAXIAFTERLAND:
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| 100 | self.logger.message(aircraftState.timestamp, "Flight time end")
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| 101 | self.logFuel(aircraftState)
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| 102 | self.logger.message(aircraftState.timestamp,
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| 103 | "Landing weight: %.0f kg, MLW: %.0f" % \
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| 104 | (aircraftState.grossWeight, self.mlw))
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| 105 | self.logger.message(aircraftState.timestamp,
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| 106 | "Vertical speed range: %.0f..%.0f feet/min" % \
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| 107 | (self._maxVS, self._minVS))
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| 108 | elif newStage==const.STAGE_PARKING:
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| 109 | self.logger.message(aircraftState.timestamp, "Block time end")
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[8] | 110 |
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[9] | 111 | def prepareFlare(self):
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| 112 | """Called when it is detected that we will soon flare.
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[8] | 113 |
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| 114 | On the first call, it should start monitoring some parameters more
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| 115 | closely to determine flare time."""
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[9] | 116 | self.flight.simulator.startFlare()
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| 117 |
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| 118 | def flareStarted(self, windSpeed, windDirection, visibility,
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| 119 | flareStart, flareStartFS):
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| 120 | """Called when the flare has started."""
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| 121 | self.logger.message(self._aircraftState.timestamp, "The flare has begun")
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| 122 | self.logger.message(self._aircraftState.timestamp,
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| 123 | "Wind %03.0f degrees at %.0f knots" % \
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| 124 | (windDirection, windSpeed))
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| 125 | self.logger.message(self._aircraftState.timestamp,
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| 126 | "Visibility: %.0f metres" % (visibility,))
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| 127 | self.logger.message(self._aircraftState.timestamp,
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| 128 | "Altimeter setting: %.0f hPa" % \
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| 129 | (self._aircraftState.altimeter,))
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| 130 | self.flight.flareStarted(flareStart, flareStartFS)
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| 131 |
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| 132 | def flareFinished(self, flareEnd, flareEndFS, tdRate, tdRateCalculatedByFS,
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| 133 | ias, pitch, bank, heading):
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| 134 | """Called when the flare has finished."""
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| 135 | (flareTimeFromFS, flareTime) = self.flight.flareFinished(flareEnd,
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| 136 | flareEndFS)
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| 137 | self.logger.message(self._aircraftState.timestamp,
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| 138 | "Flare time: %.1f s (from %s)" % \
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| 139 | (flareTime,
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| 140 | "the simulator" if flareTimeFromFS else "real time",))
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| 141 | self.logger.message(self._aircraftState.timestamp,
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| 142 | "Touchdown rate: %.0f feet/min" % (tdRate,))
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| 143 | self.logger.message(self._aircraftState.timestamp,
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| 144 | "Touchdown rate was calculated by the %s" % \
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| 145 | ("simulator" if tdRateCalculatedByFS else "logger",))
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| 146 | self.logger.message(self._aircraftState.timestamp,
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| 147 | "Touchdown speed: %.0f knots" % (ias,))
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| 148 | self.logger.message(self._aircraftState.timestamp,
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| 149 | "Touchdown pitch: %.1f degrees" % (pitch,))
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| 150 | self.logger.message(self._aircraftState.timestamp,
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| 151 | "Touchdown bank: %.1f degrees" % (bank,))
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| 152 | self.logger.message(self._aircraftState.timestamp,
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| 153 | "Touchdown heading: %03.0f degrees" % (heading,))
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[8] | 154 |
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| 155 | def cancelFlare(self):
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| 156 | """Cancel flare, if it has started."""
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[9] | 157 | self.flight.simulator.cancelFlare()
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[8] | 158 |
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| 159 | def checkFlightEnd(self, aircraftState):
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| 160 | """Check if the end of the flight has arrived.
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| 161 |
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| 162 | This default implementation checks the N1 values, but for
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| 163 | piston-powered aircraft you need to check the RPMs."""
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| 164 | for n1 in aircraftState.n1:
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| 165 | if n1>=0.5: return False
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| 166 | return True
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| 167 |
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[4] | 168 | #---------------------------------------------------------------------------------------
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[7] | 169 |
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| 170 | class Boeing737(Aircraft):
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| 171 | """Base class for the various aircraft in the Boeing 737 family.
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| 172 |
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| 173 | The aircraft type-specific values in the aircraft state have the following
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| 174 | structure:
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| 175 | - fuel: centre, left, right
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| 176 | - n1: left, right
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| 177 | - reverser: left, right"""
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[9] | 178 | def __init__(self, flight):
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| 179 | super(Boeing737, self).__init__(flight)
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| 180 | self.gearSpeedLimit = 270
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| 181 | self.flapSpeedLimits = { 1 : 260,
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| 182 | 2 : 260,
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| 183 | 5 : 250,
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| 184 | 10 : 210,
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| 185 | 15 : 200,
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| 186 | 25 : 190,
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| 187 | 30 : 175,
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| 188 | 40 : 162 }
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[7] | 189 |
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[9] | 190 | def logFuel(self, aircraftState):
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| 191 | """Log the amount of fuel"""
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| 192 | self.logger.message(aircraftState.timestamp,
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| 193 | "Fuel: left=%.0f kg - centre=%.0f kg - right=%.0f kg" % \
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| 194 | (aircraftState.fuel[1], aircraftState.fuel[0],
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| 195 | aircraftState.fuel[2]))
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| 196 | self.logger.message(aircraftState.timestamp,
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| 197 | "Total fuel: %.0f kg" % (sum(aircraftState.fuel),))
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| 198 |
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[7] | 199 | #---------------------------------------------------------------------------------------
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| 200 |
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| 201 | class B736(Boeing737):
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| 202 | """Boeing 737-600 aircraft."""
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[8] | 203 | def __init__(self, flight):
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| 204 | super(B736, self).__init__(flight)
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[9] | 205 | self.dow = 38307
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| 206 | self.mtow = 58328
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| 207 | self.mlw = 54657
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| 208 | self.mzfw = 51482
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[7] | 209 |
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| 210 | #---------------------------------------------------------------------------------------
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| 211 |
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| 212 | class B737(Boeing737):
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| 213 | """Boeing 737-700 aircraft."""
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[8] | 214 | def __init__(self, flight):
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| 215 | super(B737, self).__init__(flight)
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[9] | 216 | self.dow = 39250
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| 217 | self.mtow = 61410
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| 218 | self.mlw = 58059
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| 219 | self.mzfw = 54657
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[7] | 220 |
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| 221 | #---------------------------------------------------------------------------------------
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| 222 |
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| 223 | class B738(Boeing737):
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| 224 | """Boeing 737-800 aircraft."""
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[8] | 225 | def __init__(self, flight):
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| 226 | super(B738, self).__init__(flight)
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[9] | 227 | self.dow = 42690
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| 228 | self.mtow = 71709
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| 229 | self.mlw = 65317
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| 230 | self.mzfw = 61688
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| 231 |
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| 232 | #---------------------------------------------------------------------------------------
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| 233 |
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| 234 | class B738Charter(B738):
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| 235 | """Boeing 737-800 aircraft used for charters."""
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| 236 | def __init__(self, flight):
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| 237 | super(B738Charter, self).__init__(flight)
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| 238 | self.mtow = 77791
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[7] | 239 |
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| 240 | #---------------------------------------------------------------------------------------
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| 241 |
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| 242 | class B733(Boeing737):
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| 243 | """Boeing 737-300 aircraft."""
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[8] | 244 | def __init__(self, flight):
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| 245 | super(B733, self).__init__(flight)
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[9] | 246 | self.dow = 32700
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| 247 | self.mtow = 62820
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| 248 | self.mlw = 51700
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| 249 | self.mzfw = 48410
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[7] | 250 |
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| 251 | #---------------------------------------------------------------------------------------
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| 252 |
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| 253 | class B734(Boeing737):
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| 254 | """Boeing 737-400 aircraft."""
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[8] | 255 | def __init__(self, flight):
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| 256 | super(B734, self).__init__(flight)
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[9] | 257 | self.dow = 33200
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| 258 | self.mtow = 68050
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| 259 | self.mlw = 56200
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| 260 | self.mzfw = 53100
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[7] | 261 |
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| 262 | #---------------------------------------------------------------------------------------
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| 263 |
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| 264 | class B735(Boeing737):
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| 265 | """Boeing 737-500 aircraft."""
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[8] | 266 | def __init__(self, flight):
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| 267 | super(B735, self).__init__(flight)
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[9] | 268 | self.dow = 31300
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| 269 | self.mtow = 60550
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| 270 | self.mlw = 50000
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| 271 | self.mzfw = 46700
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[7] | 272 |
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| 273 | #---------------------------------------------------------------------------------------
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| 274 |
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| 275 | class DH8D(Aircraft):
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| 276 | """Bombardier Dash-8 Q400 aircraft.
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| 277 |
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| 278 | The aircraft type-specific values in the aircraft state have the following
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| 279 | structure:
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| 280 | - fuel: centre, left, right
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| 281 | - n1: left, right
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| 282 | - reverser: left, right."""
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[8] | 283 | def __init__(self, flight):
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| 284 | super(DH8D, self).__init__(flight)
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[9] | 285 | self.dow = 17185
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| 286 | self.mtow = 29257
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| 287 | self.mlw = 28009
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| 288 | self.mzfw = 25855
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| 289 | self.gearSpeedLimit = 215
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| 290 | self.flapSpeedLimits = { 5 : 200,
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| 291 | 10 : 181,
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| 292 | 15 : 172,
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| 293 | 35 : 158 }
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| 294 |
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| 295 | def logFuel(self, aircraftState):
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| 296 | """Log the amount of fuel"""
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| 297 | self.logger.message(aircraftState.timestamp,
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| 298 | "Fuel: left=%.0f kg - centre=%.0f kg - right=%.0f kg" % \
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| 299 | (aircraftState.fuel[1], aircraftState.fuel[0],
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| 300 | aircraftState.fuel[2]))
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| 301 | self.logger.message(aircraftState.timestamp,
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| 302 | "Total fuel: %.0f kg" % (sum(aircraftState.fuel),))
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[7] | 303 |
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| 304 | #---------------------------------------------------------------------------------------
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| 305 |
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| 306 | class Boeing767(Aircraft):
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| 307 | """Base class for the various aircraft in the Boeing 767 family.
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| 308 |
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| 309 | The aircraft type-specific values in the aircraft state have the following
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| 310 | structure:
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| 311 | - fuel: centre, left, right
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| 312 | - n1: left, right
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| 313 | - reverser: left, right"""
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[9] | 314 | def __init__(self, flight):
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| 315 | super(Boeing767, self).__init__(flight)
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| 316 | self.gearSpeedLimit = 270
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| 317 | self.flapSpeedLimits = { 1 : 255,
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| 318 | 5 : 235,
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| 319 | 10 : 215,
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| 320 | 20 : 215,
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| 321 | 25 : 185,
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| 322 | 30 : 175 }
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[7] | 323 |
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[9] | 324 | def logFuel(self, aircraftState):
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| 325 | """Log the amount of fuel"""
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| 326 | self.logger.message(aircraftState.timestamp,
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| 327 | "Fuel: left=%.0f kg - centre=%.0f kg - right=%.0f kg" % \
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| 328 | (aircraftState.fuel[1], aircraftState.fuel[0],
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| 329 | aircraftState.fuel[2]))
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| 330 | self.logger.message(aircraftState.timestamp,
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| 331 | "Total fuel: %.0f kg" % (sum(aircraftState.fuel),))
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| 332 |
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[7] | 333 | #---------------------------------------------------------------------------------------
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| 334 |
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| 335 | class B762(Boeing767):
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| 336 | """Boeing 767-200 aircraft."""
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[8] | 337 | def __init__(self, flight):
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| 338 | super(B762, self).__init__(flight)
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[9] | 339 | self.dow = 84507
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| 340 | self.mtow = 175540
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| 341 | self.mlw = 126098
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| 342 | self.mzfw = 114758
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[7] | 343 |
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| 344 | #---------------------------------------------------------------------------------------
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| 345 |
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| 346 | class B763(Boeing767):
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| 347 | """Boeing 767-300 aircraft."""
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[8] | 348 | def __init__(self, flight):
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| 349 | super(B763, self).__init__(cflight)
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[9] | 350 | self.dow = 91311
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| 351 | self.mtow = 181436
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| 352 | self.mlw = 137892
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| 353 | self.mzfw = 130635
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[7] | 354 |
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| 355 | #---------------------------------------------------------------------------------------
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| 356 |
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| 357 | class CRJ2(Aircraft):
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| 358 | """Bombardier CRJ-200 aircraft.
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| 359 |
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| 360 | The aircraft type-specific values in the aircraft state have the following
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| 361 | structure:
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| 362 | - fuel: centre, left, right
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| 363 | - n1: left, right
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| 364 | - reverser: left, right."""
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[8] | 365 | def __init__(self, flight):
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| 366 | super(CRJ2, self).__init__(flight)
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[9] | 367 | self.dow = 14549
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| 368 | self.mtow = 22995
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| 369 | self.mlw = 21319
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| 370 | self.mzfw = 19958
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| 371 | self.gearSpeedLimit = 240
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| 372 | self.flapSpeedLimits = { 8 : 260,
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| 373 | 20 : 220,
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| 374 | 30 : 190,
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| 375 | 45 : 175 }
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[7] | 376 |
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[9] | 377 | def logFuel(self, aircraftState):
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| 378 | """Log the amount of fuel"""
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| 379 | self.logger.message(aircraftState.timestamp,
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| 380 | "Fuel: left=%.0f kg - centre=%.0f kg - right=%.0f kg" % \
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| 381 | (aircraftState.fuel[1], aircraftState.fuel[0],
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| 382 | aircraftState.fuel[2]))
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| 383 | self.logger.message(aircraftState.timestamp,
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| 384 | "Total fuel: %.0f kg" % (sum(aircraftState.fuel),))
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| 385 |
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[7] | 386 | #---------------------------------------------------------------------------------------
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| 387 |
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| 388 | class F70(Aircraft):
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| 389 | """Fokker 70 aircraft.
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| 390 |
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| 391 | The aircraft type-specific values in the aircraft state have the following
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| 392 | structure:
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| 393 | - fuel: centre, left, right
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| 394 | - n1: left, right
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| 395 | - reverser: left, right."""
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[8] | 396 | def __init__(self, flight):
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| 397 | super(F70, self).__init__(flight)
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[9] | 398 | self.dow = 24283
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| 399 | self.mtow = 38100 # FIXME: differentiate by registration number,
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| 400 | # MTOW of HA-LMF: 41955
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| 401 | self.mlw = 36740
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| 402 | self.mzfw = 32655
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| 403 | self.gearSpeedLimit = 200
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| 404 | self.flapSpeedLimits = { 8 : 250,
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| 405 | 15 : 220,
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| 406 | 25 : 220,
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| 407 | 42 : 180 }
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[7] | 408 |
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[9] | 409 | def logFuel(self, aircraftState):
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| 410 | """Log the amount of fuel"""
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| 411 | self.logger.message(aircraftState.timestamp,
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| 412 | "Fuel: left=%.0f kg - centre=%.0f kg - right=%.0f kg" % \
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| 413 | (aircraftState.fuel[1], aircraftState.fuel[0],
|
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| 414 | aircraftState.fuel[2]))
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| 415 | self.logger.message(aircraftState.timestamp,
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| 416 | "Total fuel: %.0f kg" % (sum(aircraftState.fuel),))
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| 417 |
|
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[7] | 418 | #---------------------------------------------------------------------------------------
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| 419 |
|
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| 420 | class DC3(Aircraft):
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| 421 | """Lisunov Li-2 (DC-3) aircraft.
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| 422 |
|
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| 423 | The aircraft type-specific values in the aircraft state have the following
|
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| 424 | structure:
|
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| 425 | - fuel: left, right, left aux, right aix
|
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| 426 | - rpm: left, right
|
---|
| 427 | - reverser: left, right."""
|
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[8] | 428 | def __init__(self, flight):
|
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| 429 | super(DC3, self).__init__(flight)
|
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[9] | 430 | self.dow = 8627
|
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| 431 | self.mtow = 11884
|
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| 432 | self.mlw = 11793
|
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| 433 | self.mzfw = 11780
|
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| 434 | self.gearSpeedLimit = 148
|
---|
| 435 | self.flapSpeedLimits = { 15 : 135,
|
---|
| 436 | 30 : 99,
|
---|
| 437 | 45 : 97 }
|
---|
[8] | 438 |
|
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| 439 | def _checkFlightEnd(self, aircraftState):
|
---|
| 440 | """Check if the end of the flight has arrived.
|
---|
| 441 |
|
---|
| 442 | This implementation checks the RPM values to be 0."""
|
---|
| 443 | for rpm in aircraftState.rpm:
|
---|
| 444 | if rpm>0: return
|
---|
| 445 | self._setStage(aircraftState, const.STAGE_END)
|
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[7] | 446 |
|
---|
[9] | 447 | def logFuel(self, aircraftState):
|
---|
| 448 | """Log the amount of fuel"""
|
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| 449 | self.logger.message(aircraftState.timestamp,
|
---|
| 450 | "Fuel: left aux=%.0f kg - left=%.0f kg - right=%.0f kg - right aux=%.0f kg" % \
|
---|
| 451 | (aircraftState.fuel[2], aircraftState.fuel[0],
|
---|
| 452 | aircraftState.fuel[1], aircraftState.fuel[3]))
|
---|
| 453 | self.logger.message(aircraftState.timestamp,
|
---|
| 454 | "Total fuel: %.0f kg" % (sum(aircraftState.fuel),))
|
---|
| 455 |
|
---|
[7] | 456 | #---------------------------------------------------------------------------------------
|
---|
| 457 |
|
---|
| 458 | class T134(Aircraft):
|
---|
| 459 | """Tupolev Tu-134 aircraft.
|
---|
| 460 |
|
---|
| 461 | The aircraft type-specific values in the aircraft state have the following
|
---|
| 462 | structure:
|
---|
| 463 | - fuel: centre, left tip, left aux, right tip, right aux, external 1,
|
---|
| 464 | external 2
|
---|
| 465 | - n1: left, right
|
---|
| 466 | - reverser: left, right."""
|
---|
[8] | 467 | def __init__(self, flight):
|
---|
| 468 | super(T134, self).__init__(flight)
|
---|
[9] | 469 | self.dow = 29927
|
---|
| 470 | self.mtow = 47600
|
---|
| 471 | self.mlw = 43000
|
---|
| 472 | self.mzfw = 38500
|
---|
| 473 | self.gearSpeedLimit = 216
|
---|
| 474 | self.flapSpeedLimits = { 10 : 240,
|
---|
| 475 | 20 : 216,
|
---|
| 476 | 30 : 161 }
|
---|
[7] | 477 |
|
---|
[9] | 478 | def logFuel(self, aircraftState):
|
---|
| 479 | """Log the amount of fuel"""
|
---|
| 480 | self.logger.message(aircraftState.timestamp,
|
---|
| 481 | "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" % \
|
---|
| 482 | (aircraftState.fuel[2], aircraftState.fuel[1],
|
---|
| 483 | aircraftState.fuel[0],
|
---|
| 484 | aircraftState.fuel[3], aircraftState.fuel[4],
|
---|
| 485 | aircraftState.fuel[5], aircraftState.fuel[6]))
|
---|
| 486 | self.logger.message(aircraftState.timestamp,
|
---|
| 487 | "Total fuel: %.0f kg" % (sum(aircraftState.fuel),))
|
---|
| 488 |
|
---|
[7] | 489 | #---------------------------------------------------------------------------------------
|
---|
| 490 |
|
---|
| 491 | class T154(Aircraft):
|
---|
| 492 | """Tupolev Tu-154 aircraft.
|
---|
| 493 |
|
---|
| 494 | The aircraft type-specific values in the aircraft state have the following
|
---|
| 495 | structure:
|
---|
| 496 | - fuel: centre, left, right, centre 2, left aux, right aux
|
---|
| 497 | - n1: left, centre, right
|
---|
| 498 | - reverser: left, right"""
|
---|
[8] | 499 | def __init__(self, flight):
|
---|
| 500 | super(T154, self).__init__(flight)
|
---|
[9] | 501 | self.dow = 53259
|
---|
| 502 | self.mtow = 98000
|
---|
| 503 | self.mlw = 78000
|
---|
| 504 | self.mzfw = 72000
|
---|
| 505 | self.gearSpeedLimit = 216
|
---|
| 506 | self.flapSpeedLimits = { 15 : 227,
|
---|
| 507 | 28 : 194,
|
---|
| 508 | 45 : 162 }
|
---|
| 509 |
|
---|
| 510 | def logFuel(self, aircraftState):
|
---|
| 511 | """Log the amount of fuel"""
|
---|
| 512 | self.logger.message(aircraftState.timestamp,
|
---|
| 513 | "Fuel: left aux=%.0f kg - left=%.0f kg - centre=%.0f kg - centre 2=%.0f kg - right=%.0f kg - right aux=%.0f kg" % \
|
---|
| 514 | (aircraftState.fuel[4], aircraftState.fuel[1],
|
---|
| 515 | aircraftState.fuel[0], aircraftState.fuel[3],
|
---|
| 516 | aircraftState.fuel[2], aircraftState.fuel[5]))
|
---|
| 517 | self.logger.message(aircraftState.timestamp,
|
---|
| 518 | "Total fuel: %.0f kg" % (sum(aircraftState.fuel),))
|
---|
[7] | 519 |
|
---|
| 520 | #---------------------------------------------------------------------------------------
|
---|
| 521 |
|
---|
[9] | 522 |
|
---|
[7] | 523 | class YK40(Aircraft):
|
---|
| 524 | """Yakovlev Yak-40 aircraft.
|
---|
| 525 |
|
---|
| 526 | The aircraft type-specific values in the aircraft state have the following
|
---|
| 527 | structure:
|
---|
| 528 | - fuel: left, right
|
---|
| 529 | - n1: left, right
|
---|
| 530 | - reverser: left, right"""
|
---|
[8] | 531 | def __init__(self, flight):
|
---|
| 532 | super(YK40, self).__init__(flight)
|
---|
[9] | 533 | self.dow = 9400
|
---|
| 534 | self.mtow = 17200
|
---|
| 535 | self.mlw = 16800
|
---|
| 536 | self.mzfw = 12100
|
---|
| 537 | self.gearSpeedLimit = 165
|
---|
| 538 | self.flapSpeedLimits = { 20 : 165,
|
---|
| 539 | 35 : 135 }
|
---|
| 540 |
|
---|
| 541 | def logFuel(self, aircraftState):
|
---|
| 542 | """Log the amount of fuel"""
|
---|
| 543 | self.logger.message(aircraftState.timestamp,
|
---|
| 544 | "Fuel: left=%.0f kg - right=%.0f kg" % \
|
---|
| 545 | (aircraftState.fuel[0], aircraftState.fuel[1]))
|
---|
| 546 | self.logger.message(aircraftState.timestamp,
|
---|
| 547 | "Total fuel: %.0f kg" % (sum(aircraftState.fuel),))
|
---|
[7] | 548 |
|
---|
| 549 | #---------------------------------------------------------------------------------------
|
---|
| 550 |
|
---|
[8] | 551 | _classes = { const.AIRCRAFT_B736 : B736,
|
---|
| 552 | const.AIRCRAFT_B737 : B737,
|
---|
| 553 | const.AIRCRAFT_B738 : B738,
|
---|
| 554 | const.AIRCRAFT_B733 : B733,
|
---|
| 555 | const.AIRCRAFT_B734 : B734,
|
---|
| 556 | const.AIRCRAFT_B735 : B735,
|
---|
| 557 | const.AIRCRAFT_DH8D : DH8D,
|
---|
| 558 | const.AIRCRAFT_B762 : B762,
|
---|
| 559 | const.AIRCRAFT_B763 : B763,
|
---|
| 560 | const.AIRCRAFT_CRJ2 : CRJ2,
|
---|
| 561 | const.AIRCRAFT_F70 : F70,
|
---|
| 562 | const.AIRCRAFT_DC3 : DC3,
|
---|
| 563 | const.AIRCRAFT_T134 : T134,
|
---|
| 564 | const.AIRCRAFT_T154 : T154,
|
---|
| 565 | const.AIRCRAFT_YK40 : YK40 }
|
---|
| 566 |
|
---|
| 567 | #---------------------------------------------------------------------------------------
|
---|