[4] | 1 | # Module for the simulator-independent aircraft classes
|
---|
| 2 |
|
---|
| 3 | #---------------------------------------------------------------------------------------
|
---|
| 4 |
|
---|
[8] | 5 | import const
|
---|
| 6 | import checks
|
---|
[134] | 7 | import fs
|
---|
[89] | 8 | import util
|
---|
[4] | 9 |
|
---|
[139] | 10 | import sys
|
---|
[8] | 11 | import time
|
---|
[139] | 12 | import traceback
|
---|
[7] | 13 |
|
---|
[197] | 14 | from collections import deque
|
---|
| 15 |
|
---|
| 16 | #---------------------------------------------------------------------------------------
|
---|
| 17 |
|
---|
| 18 | class SmoothedValue(object):
|
---|
| 19 | """A smoothed value."""
|
---|
| 20 | def __init__(self):
|
---|
| 21 | """Construct the value."""
|
---|
| 22 | self._deque = deque()
|
---|
| 23 | self._sum = 0
|
---|
| 24 |
|
---|
| 25 | def add(self, length, value):
|
---|
| 26 | """Add the given value and smooth with the given length."""
|
---|
| 27 | dequeLength = len(self._deque)
|
---|
| 28 | while dequeLength>=length:
|
---|
| 29 | self._sum -= self._deque.popleft()
|
---|
| 30 | dequeLength -= 1
|
---|
| 31 |
|
---|
| 32 | self._sum += value
|
---|
| 33 | self._deque.append(value)
|
---|
| 34 |
|
---|
| 35 | def get(self):
|
---|
| 36 | """Get the average."""
|
---|
| 37 | return self._sum / len(self._deque)
|
---|
| 38 |
|
---|
[4] | 39 | #---------------------------------------------------------------------------------------
|
---|
| 40 |
|
---|
| 41 | class Aircraft(object):
|
---|
| 42 | """Base class for aircraft."""
|
---|
[8] | 43 | @staticmethod
|
---|
| 44 | def create(flight):
|
---|
| 45 | """Create an aircraft instance for the type in the given flight."""
|
---|
| 46 | return _classes[flight.aircraftType](flight)
|
---|
| 47 |
|
---|
| 48 | def __init__(self, flight):
|
---|
[4] | 49 | """Construct the aircraft for the given type."""
|
---|
[8] | 50 | self._flight = flight
|
---|
[4] | 51 | self._aircraftState = None
|
---|
[9] | 52 |
|
---|
| 53 | self._maxVS = -10000.0
|
---|
| 54 | self._minVS = 10000.0
|
---|
[4] | 55 |
|
---|
[101] | 56 | self._v1r2LineIndex = None
|
---|
[96] | 57 | self._vrefLineIndex = None
|
---|
| 58 |
|
---|
[117] | 59 | self.humanWeight = 82.0
|
---|
| 60 |
|
---|
[8] | 61 | self._checkers = []
|
---|
| 62 |
|
---|
[197] | 63 | config = flight.config
|
---|
[11] | 64 | # Loggers
|
---|
| 65 |
|
---|
[8] | 66 | self._checkers.append(checks.StageChecker())
|
---|
[9] | 67 | self._checkers.append(checks.TakeOffLogger())
|
---|
[8] | 68 |
|
---|
| 69 | self._checkers.append(checks.AltimeterLogger())
|
---|
| 70 |
|
---|
| 71 | self._checkers.append(checks.NAV1Logger())
|
---|
| 72 | self._checkers.append(checks.NAV2Logger())
|
---|
| 73 | self._checkers.append(checks.SquawkLogger())
|
---|
| 74 |
|
---|
[211] | 75 | self._appendLightsLoggers()
|
---|
[8] | 76 |
|
---|
| 77 | self._checkers.append(checks.FlapsLogger())
|
---|
| 78 |
|
---|
| 79 | self._checkers.append(checks.GearsLogger())
|
---|
[9] | 80 | self._checkers.append(checks.CruiseSpeedLogger())
|
---|
[10] | 81 | self._checkers.append(checks.SpoilerLogger())
|
---|
[9] | 82 |
|
---|
[197] | 83 | if config.isMessageTypeFS(const.MESSAGETYPE_VISIBILITY):
|
---|
[134] | 84 | self._checkers.append(checks.VisibilityChecker())
|
---|
| 85 |
|
---|
[139] | 86 | # FIXME: we should have a central data model object, and not collect
|
---|
| 87 | # the data from the GUI. However, some pieces of data (e.g. V-speeds,
|
---|
| 88 | # etc. that is entered into the GUI) *should* be a part of the GUI and
|
---|
| 89 | # queried from it, so the model should have a reference to the GUI as
|
---|
| 90 | # well and access such data via the GUI!
|
---|
[215] | 91 | if config.onlineACARS and flight.loggedIn and not flight.entranceExam:
|
---|
[139] | 92 | self._checkers.append(checks.ACARSSender(flight._gui))
|
---|
| 93 |
|
---|
[11] | 94 | # Fault checkers
|
---|
[211] | 95 |
|
---|
| 96 | self._appendLightsCheckers()
|
---|
[11] | 97 |
|
---|
| 98 | self._checkers.append(checks.BankChecker())
|
---|
| 99 |
|
---|
| 100 | self._checkers.append(checks.FlapsRetractChecker())
|
---|
| 101 | self._checkers.append(checks.FlapsSpeedLimitChecker())
|
---|
| 102 |
|
---|
| 103 | self._checkers.append(checks.GearsDownChecker())
|
---|
| 104 | self._checkers.append(checks.GearSpeedLimitChecker())
|
---|
| 105 |
|
---|
| 106 | self._checkers.append(checks.GLoadChecker())
|
---|
| 107 |
|
---|
| 108 | self._checkers.append(checks.MLWChecker())
|
---|
| 109 | self._checkers.append(checks.MTOWChecker())
|
---|
| 110 | self._checkers.append(checks.MZFWChecker())
|
---|
| 111 | self._checkers.append(checks.PayloadChecker())
|
---|
| 112 |
|
---|
| 113 | self._checkers.append(checks.SpeedChecker())
|
---|
| 114 | self._checkers.append(checks.VSChecker())
|
---|
[197] | 115 |
|
---|
| 116 | timeout = 5.0 + config.realIASSmoothingLength - 1
|
---|
| 117 | self._checkers.append(checks.OverspeedChecker(timeout = timeout))
|
---|
| 118 |
|
---|
[11] | 119 | self._checkers.append(checks.StallChecker())
|
---|
| 120 |
|
---|
| 121 | self._checkers.append(checks.PitotChecker())
|
---|
| 122 |
|
---|
| 123 | self._checkers.append(checks.ReverserChecker())
|
---|
| 124 |
|
---|
[197] | 125 | self._smoothedIAS = SmoothedValue()
|
---|
| 126 | self._smoothedVS = SmoothedValue()
|
---|
| 127 |
|
---|
[4] | 128 | @property
|
---|
| 129 | def type(self):
|
---|
| 130 | """Get the type of the aircraft."""
|
---|
[8] | 131 | return self._flight.aircraftType
|
---|
| 132 |
|
---|
| 133 | @property
|
---|
| 134 | def flight(self):
|
---|
| 135 | """Get the flight the aircraft belongs to."""
|
---|
| 136 | return self._flight
|
---|
[4] | 137 |
|
---|
[8] | 138 | @property
|
---|
| 139 | def logger(self):
|
---|
| 140 | """Get the logger to use for the aircraft."""
|
---|
| 141 | return self._flight.logger
|
---|
| 142 |
|
---|
[139] | 143 | @property
|
---|
| 144 | def state(self):
|
---|
| 145 | """Get the current aircraft state."""
|
---|
| 146 | return self._aircraftState
|
---|
| 147 |
|
---|
[11] | 148 | def getFlapsSpeedLimit(self, flaps):
|
---|
| 149 | """Get the speed limit for the given flaps setting."""
|
---|
| 150 | return self.flapSpeedLimits[flaps] if flaps in self.flapSpeedLimits \
|
---|
| 151 | else None
|
---|
| 152 |
|
---|
[8] | 153 | def modelChanged(self, timestamp, aircraftName, modelName):
|
---|
[4] | 154 | """Called when the simulator's aircraft changes."""
|
---|
[8] | 155 | self._flight.logger.message(timestamp,
|
---|
| 156 | "Aircraft: name='%s', model='%s'" % \
|
---|
| 157 | (aircraftName, modelName))
|
---|
[4] | 158 |
|
---|
| 159 | def handleState(self, aircraftState):
|
---|
[197] | 160 | """Called when the state of the aircraft changes.
|
---|
| 161 |
|
---|
| 162 | This is the function that the simulator calls directly with the new
|
---|
| 163 | state."""
|
---|
| 164 | config = self._flight.config
|
---|
| 165 |
|
---|
| 166 | self._smoothedIAS.add(config.realIASSmoothingLength, aircraftState.ias)
|
---|
| 167 | aircraftState.smoothedIAS = self._smoothedIAS.get()
|
---|
| 168 |
|
---|
| 169 | self._smoothedVS.add(config.realVSSmoothingLength, aircraftState.vs)
|
---|
| 170 | aircraftState.smoothedVS = self._smoothedVS.get()
|
---|
| 171 |
|
---|
[8] | 172 | for checker in self._checkers:
|
---|
[139] | 173 | try:
|
---|
| 174 | checker.check(self._flight, self, self._flight.logger,
|
---|
| 175 | self._aircraftState, aircraftState)
|
---|
| 176 | except:
|
---|
| 177 | print >> sys.stderr, "Checker", checker, "failed"
|
---|
| 178 | traceback.print_exc()
|
---|
[7] | 179 |
|
---|
[89] | 180 | self._flight.handleState(self._aircraftState, aircraftState)
|
---|
| 181 |
|
---|
[9] | 182 | self._maxVS = max(self._maxVS, aircraftState.vs)
|
---|
| 183 | self._minVS = min(self._minVS, aircraftState.vs)
|
---|
| 184 |
|
---|
[4] | 185 | self._aircraftState = aircraftState
|
---|
[8] | 186 |
|
---|
| 187 | def setStage(self, aircraftState, newStage):
|
---|
| 188 | """Set the given stage as the new one and do whatever should be
|
---|
| 189 | done."""
|
---|
[9] | 190 | if self._flight.setStage(aircraftState.timestamp, newStage):
|
---|
| 191 | if newStage==const.STAGE_PUSHANDTAXI:
|
---|
| 192 | self.logger.message(aircraftState.timestamp, "Block time start")
|
---|
| 193 | self.logFuel(aircraftState)
|
---|
| 194 | self.logger.message(aircraftState.timestamp,
|
---|
| 195 | "Zero-fuel weight: %.0f kg" % (aircraftState.zfw))
|
---|
[134] | 196 | flight = self._flight
|
---|
| 197 | if flight.v1 is None or flight.vr is None or flight.v2 is None:
|
---|
| 198 | fs.sendMessage(const.MESSAGETYPE_HELP,
|
---|
| 199 | "Don't forget to set the takeoff V-speeds!",
|
---|
| 200 | 5)
|
---|
[9] | 201 | elif newStage==const.STAGE_TAKEOFF:
|
---|
| 202 | self.logger.message(aircraftState.timestamp, "Flight time start")
|
---|
| 203 | self.logger.message(aircraftState.timestamp,
|
---|
| 204 | "Takeoff weight: %.0f kg, MTOW: %.0f kg" % \
|
---|
| 205 | (aircraftState.grossWeight, self.mtow))
|
---|
| 206 | self.logger.message(aircraftState.timestamp,
|
---|
| 207 | "Wind %03.0f degrees at %.0f knots" % \
|
---|
| 208 | (aircraftState.windDirection,
|
---|
| 209 | aircraftState.windSpeed))
|
---|
[101] | 210 | self._logV1R2()
|
---|
[9] | 211 | elif newStage==const.STAGE_TAXIAFTERLAND:
|
---|
[184] | 212 | flight = self._flight
|
---|
| 213 | bookedFlight = flight.bookedFlight
|
---|
| 214 | config = flight.config
|
---|
[136] | 215 | if config.onlineGateSystem and \
|
---|
[215] | 216 | flight.loggedIn and \
|
---|
[184] | 217 | not flight.entranceExam and \
|
---|
[136] | 218 | bookedFlight.arrivalICAO=="LHBP" and \
|
---|
| 219 | config.isMessageTypeFS(const.MESSAGETYPE_GATE_SYSTEM):
|
---|
[134] | 220 | self._flight.getFleet(callback = self._fleetRetrieved,
|
---|
| 221 | force = True)
|
---|
[9] | 222 | self.logger.message(aircraftState.timestamp, "Flight time end")
|
---|
| 223 | self.logFuel(aircraftState)
|
---|
| 224 | self.logger.message(aircraftState.timestamp,
|
---|
| 225 | "Landing weight: %.0f kg, MLW: %.0f" % \
|
---|
| 226 | (aircraftState.grossWeight, self.mlw))
|
---|
| 227 | self.logger.message(aircraftState.timestamp,
|
---|
| 228 | "Vertical speed range: %.0f..%.0f feet/min" % \
|
---|
[12] | 229 | (self._minVS, self._maxVS))
|
---|
[9] | 230 | elif newStage==const.STAGE_PARKING:
|
---|
| 231 | self.logger.message(aircraftState.timestamp, "Block time end")
|
---|
[89] | 232 | elif newStage==const.STAGE_END:
|
---|
| 233 | flightLength = self._flight.flightTimeEnd - self._flight.flightTimeStart
|
---|
| 234 | self.logger.message(aircraftState.timestamp,
|
---|
| 235 | "Flight time: " +
|
---|
| 236 | util.getTimeIntervalString(flightLength))
|
---|
| 237 | self.logger.message(aircraftState.timestamp,
|
---|
| 238 | "Flown distance: %.2f NM" % \
|
---|
| 239 | (self._flight.flownDistance,))
|
---|
| 240 | blockLength = self._flight.blockTimeEnd - self._flight.blockTimeStart
|
---|
| 241 | self.logger.message(aircraftState.timestamp,
|
---|
| 242 | "Block time: " +
|
---|
| 243 | util.getTimeIntervalString(blockLength))
|
---|
[8] | 244 |
|
---|
[9] | 245 | def prepareFlare(self):
|
---|
| 246 | """Called when it is detected that we will soon flare.
|
---|
[8] | 247 |
|
---|
| 248 | On the first call, it should start monitoring some parameters more
|
---|
| 249 | closely to determine flare time."""
|
---|
[9] | 250 | self.flight.simulator.startFlare()
|
---|
| 251 |
|
---|
| 252 | def flareStarted(self, windSpeed, windDirection, visibility,
|
---|
| 253 | flareStart, flareStartFS):
|
---|
| 254 | """Called when the flare has started."""
|
---|
| 255 | self.logger.message(self._aircraftState.timestamp, "The flare has begun")
|
---|
| 256 | self.logger.message(self._aircraftState.timestamp,
|
---|
| 257 | "Wind %03.0f degrees at %.0f knots" % \
|
---|
| 258 | (windDirection, windSpeed))
|
---|
| 259 | self.logger.message(self._aircraftState.timestamp,
|
---|
| 260 | "Visibility: %.0f metres" % (visibility,))
|
---|
| 261 | self.logger.message(self._aircraftState.timestamp,
|
---|
| 262 | "Altimeter setting: %.0f hPa" % \
|
---|
| 263 | (self._aircraftState.altimeter,))
|
---|
[101] | 264 | self._logVRef()
|
---|
[9] | 265 | self.flight.flareStarted(flareStart, flareStartFS)
|
---|
[134] | 266 | fs.sendMessage(const.MESSAGETYPE_INFORMATION, "Flare-time", 3)
|
---|
[9] | 267 |
|
---|
| 268 | def flareFinished(self, flareEnd, flareEndFS, tdRate, tdRateCalculatedByFS,
|
---|
| 269 | ias, pitch, bank, heading):
|
---|
| 270 | """Called when the flare has finished."""
|
---|
| 271 | (flareTimeFromFS, flareTime) = self.flight.flareFinished(flareEnd,
|
---|
[170] | 272 | flareEndFS,
|
---|
| 273 | tdRate)
|
---|
[9] | 274 | self.logger.message(self._aircraftState.timestamp,
|
---|
[153] | 275 | "Flaretime: %.3f (from %s)" % \
|
---|
[9] | 276 | (flareTime,
|
---|
| 277 | "the simulator" if flareTimeFromFS else "real time",))
|
---|
| 278 | self.logger.message(self._aircraftState.timestamp,
|
---|
| 279 | "Touchdown rate: %.0f feet/min" % (tdRate,))
|
---|
| 280 | self.logger.message(self._aircraftState.timestamp,
|
---|
| 281 | "Touchdown rate was calculated by the %s" % \
|
---|
| 282 | ("simulator" if tdRateCalculatedByFS else "logger",))
|
---|
| 283 | self.logger.message(self._aircraftState.timestamp,
|
---|
| 284 | "Touchdown speed: %.0f knots" % (ias,))
|
---|
| 285 | self.logger.message(self._aircraftState.timestamp,
|
---|
| 286 | "Touchdown pitch: %.1f degrees" % (pitch,))
|
---|
| 287 | self.logger.message(self._aircraftState.timestamp,
|
---|
| 288 | "Touchdown bank: %.1f degrees" % (bank,))
|
---|
| 289 | self.logger.message(self._aircraftState.timestamp,
|
---|
| 290 | "Touchdown heading: %03.0f degrees" % (heading,))
|
---|
[8] | 291 |
|
---|
| 292 | def cancelFlare(self):
|
---|
| 293 | """Cancel flare, if it has started."""
|
---|
[9] | 294 | self.flight.simulator.cancelFlare()
|
---|
[8] | 295 |
|
---|
| 296 | def checkFlightEnd(self, aircraftState):
|
---|
| 297 | """Check if the end of the flight has arrived.
|
---|
| 298 |
|
---|
| 299 | This default implementation checks the N1 values, but for
|
---|
| 300 | piston-powered aircraft you need to check the RPMs."""
|
---|
| 301 | for n1 in aircraftState.n1:
|
---|
| 302 | if n1>=0.5: return False
|
---|
| 303 | return True
|
---|
| 304 |
|
---|
[101] | 305 | def updateV1R2(self):
|
---|
| 306 | """Update the V1, Vr and V2 values from the flight, if the these values
|
---|
| 307 | have already been logged."""
|
---|
| 308 | if self._v1r2LineIndex is not None:
|
---|
| 309 | self._logV1R2()
|
---|
| 310 |
|
---|
[211] | 311 | def _appendLightsLoggers(self):
|
---|
| 312 | """Append the loggers needed for the lights.
|
---|
| 313 |
|
---|
| 314 | This default implementation adds the loggers for the anti-collision
|
---|
| 315 | lights, the landing lights, the strobe lights and the NAV lights."""
|
---|
| 316 | self._checkers.append(checks.AnticollisionLightsLogger())
|
---|
| 317 | self._checkers.append(checks.LandingLightsLogger())
|
---|
| 318 | self._checkers.append(checks.StrobeLightsLogger())
|
---|
| 319 | self._checkers.append(checks.NavLightsLogger())
|
---|
| 320 |
|
---|
| 321 | def _appendLightsCheckers(self):
|
---|
| 322 | """Append the checkers needed for the lights.
|
---|
| 323 |
|
---|
| 324 | This default implementation adds the checkers for the anti-collision
|
---|
| 325 | lights, the landing lights, the strobe lights and the NAV lights."""
|
---|
| 326 | self._checkers.append(checks.AntiCollisionLightsChecker())
|
---|
| 327 | self._checkers.append(checks.LandingLightsChecker())
|
---|
| 328 | self._checkers.append(checks.NavLightsChecker())
|
---|
| 329 | self._checkers.append(checks.StrobeLightsChecker())
|
---|
| 330 |
|
---|
[101] | 331 | def _logV1R2(self):
|
---|
| 332 | """Log the V1, Vr and V2 value either newly, or by updating the
|
---|
| 333 | corresponding line."""
|
---|
| 334 | message = "Speeds calculated by the pilot: V1: %s, VR: %s, V2: %s" % \
|
---|
| 335 | ("-" if self._flight.v1 is None
|
---|
| 336 | else str(self._flight.v1),
|
---|
| 337 | "-" if self._flight.vr is None
|
---|
| 338 | else str(self._flight.vr),
|
---|
| 339 | "-" if self._flight.v2 is None
|
---|
| 340 | else str(self._flight.v2))
|
---|
| 341 |
|
---|
| 342 | if self._v1r2LineIndex is None:
|
---|
| 343 | self._v1r2LineIndex = \
|
---|
| 344 | self.logger.message(self._aircraftState.timestamp, message)
|
---|
| 345 | else:
|
---|
| 346 | self.logger.updateLine(self._v1r2LineIndex, message)
|
---|
| 347 |
|
---|
[96] | 348 | def updateVRef(self):
|
---|
| 349 | """Update the Vref value from the flight, if the Vref value has already
|
---|
| 350 | been logged."""
|
---|
| 351 | if self._vrefLineIndex is not None:
|
---|
| 352 | self._logVRef()
|
---|
| 353 |
|
---|
| 354 | def _logVRef(self):
|
---|
| 355 | """Log the Vref value either newly, or by updating the corresponding
|
---|
| 356 | line."""
|
---|
| 357 | message = "VRef speed calculated by the pilot: %s" % \
|
---|
| 358 | ("-" if self._flight.vref is None else str(self._flight.vref))
|
---|
| 359 | if self._vrefLineIndex is None:
|
---|
| 360 | self._vrefLineIndex = \
|
---|
| 361 | self.logger.message(self._aircraftState.timestamp, message)
|
---|
| 362 | else:
|
---|
| 363 | self.logger.updateLine(self._vrefLineIndex, message)
|
---|
| 364 |
|
---|
[134] | 365 | def _fleetRetrieved(self, fleet):
|
---|
| 366 | """Callback for the fleet retrieval result."""
|
---|
| 367 | if fleet is not None:
|
---|
| 368 | gateList = ""
|
---|
| 369 | occupiedGateNumbers = fleet.getOccupiedGateNumbers()
|
---|
| 370 | for gateNumber in const.lhbpGateNumbers:
|
---|
| 371 | if gateNumber not in occupiedGateNumbers:
|
---|
| 372 | if gateList: gateList += ", "
|
---|
| 373 | gateList += gateNumber
|
---|
| 374 | fs.sendMessage(const.MESSAGETYPE_GATE_SYSTEM,
|
---|
| 375 | "Free gates: " + gateList, 20)
|
---|
| 376 |
|
---|
| 377 |
|
---|
[4] | 378 | #---------------------------------------------------------------------------------------
|
---|
[7] | 379 |
|
---|
| 380 | class Boeing737(Aircraft):
|
---|
| 381 | """Base class for the various aircraft in the Boeing 737 family.
|
---|
| 382 |
|
---|
| 383 | The aircraft type-specific values in the aircraft state have the following
|
---|
| 384 | structure:
|
---|
[140] | 385 | - fuel: left, centre, right
|
---|
[7] | 386 | - n1: left, right
|
---|
| 387 | - reverser: left, right"""
|
---|
[140] | 388 | fuelTanks = [const.FUELTANK_LEFT, const.FUELTANK_CENTRE, const.FUELTANK_RIGHT]
|
---|
| 389 |
|
---|
[9] | 390 | def __init__(self, flight):
|
---|
| 391 | super(Boeing737, self).__init__(flight)
|
---|
[95] | 392 | self._checkers.append(checks.ThrustChecker())
|
---|
| 393 |
|
---|
[9] | 394 | self.gearSpeedLimit = 270
|
---|
| 395 | self.flapSpeedLimits = { 1 : 260,
|
---|
| 396 | 2 : 260,
|
---|
| 397 | 5 : 250,
|
---|
| 398 | 10 : 210,
|
---|
| 399 | 15 : 200,
|
---|
| 400 | 25 : 190,
|
---|
| 401 | 30 : 175,
|
---|
| 402 | 40 : 162 }
|
---|
[7] | 403 |
|
---|
[9] | 404 | def logFuel(self, aircraftState):
|
---|
| 405 | """Log the amount of fuel"""
|
---|
| 406 | self.logger.message(aircraftState.timestamp,
|
---|
| 407 | "Fuel: left=%.0f kg - centre=%.0f kg - right=%.0f kg" % \
|
---|
[150] | 408 | (aircraftState.fuel[0], aircraftState.fuel[1],
|
---|
[9] | 409 | aircraftState.fuel[2]))
|
---|
| 410 | self.logger.message(aircraftState.timestamp,
|
---|
| 411 | "Total fuel: %.0f kg" % (sum(aircraftState.fuel),))
|
---|
| 412 |
|
---|
[7] | 413 | #---------------------------------------------------------------------------------------
|
---|
| 414 |
|
---|
| 415 | class B736(Boeing737):
|
---|
| 416 | """Boeing 737-600 aircraft."""
|
---|
[8] | 417 | def __init__(self, flight):
|
---|
| 418 | super(B736, self).__init__(flight)
|
---|
[9] | 419 | self.dow = 38307
|
---|
| 420 | self.mtow = 58328
|
---|
| 421 | self.mlw = 54657
|
---|
| 422 | self.mzfw = 51482
|
---|
[7] | 423 |
|
---|
| 424 | #---------------------------------------------------------------------------------------
|
---|
| 425 |
|
---|
| 426 | class B737(Boeing737):
|
---|
| 427 | """Boeing 737-700 aircraft."""
|
---|
[8] | 428 | def __init__(self, flight):
|
---|
| 429 | super(B737, self).__init__(flight)
|
---|
[9] | 430 | self.dow = 39250
|
---|
| 431 | self.mtow = 61410
|
---|
| 432 | self.mlw = 58059
|
---|
| 433 | self.mzfw = 54657
|
---|
[7] | 434 |
|
---|
| 435 | #---------------------------------------------------------------------------------------
|
---|
| 436 |
|
---|
| 437 | class B738(Boeing737):
|
---|
| 438 | """Boeing 737-800 aircraft."""
|
---|
[8] | 439 | def __init__(self, flight):
|
---|
| 440 | super(B738, self).__init__(flight)
|
---|
[9] | 441 | self.dow = 42690
|
---|
| 442 | self.mtow = 71709
|
---|
| 443 | self.mlw = 65317
|
---|
| 444 | self.mzfw = 61688
|
---|
| 445 |
|
---|
| 446 | #---------------------------------------------------------------------------------------
|
---|
| 447 |
|
---|
| 448 | class B738Charter(B738):
|
---|
| 449 | """Boeing 737-800 aircraft used for charters."""
|
---|
| 450 | def __init__(self, flight):
|
---|
| 451 | super(B738Charter, self).__init__(flight)
|
---|
| 452 | self.mtow = 77791
|
---|
[7] | 453 |
|
---|
| 454 | #---------------------------------------------------------------------------------------
|
---|
| 455 |
|
---|
| 456 | class B733(Boeing737):
|
---|
| 457 | """Boeing 737-300 aircraft."""
|
---|
[8] | 458 | def __init__(self, flight):
|
---|
| 459 | super(B733, self).__init__(flight)
|
---|
[9] | 460 | self.dow = 32700
|
---|
| 461 | self.mtow = 62820
|
---|
| 462 | self.mlw = 51700
|
---|
| 463 | self.mzfw = 48410
|
---|
[7] | 464 |
|
---|
| 465 | #---------------------------------------------------------------------------------------
|
---|
| 466 |
|
---|
| 467 | class B734(Boeing737):
|
---|
| 468 | """Boeing 737-400 aircraft."""
|
---|
[8] | 469 | def __init__(self, flight):
|
---|
| 470 | super(B734, self).__init__(flight)
|
---|
[9] | 471 | self.dow = 33200
|
---|
| 472 | self.mtow = 68050
|
---|
| 473 | self.mlw = 56200
|
---|
| 474 | self.mzfw = 53100
|
---|
[7] | 475 |
|
---|
| 476 | #---------------------------------------------------------------------------------------
|
---|
| 477 |
|
---|
| 478 | class B735(Boeing737):
|
---|
| 479 | """Boeing 737-500 aircraft."""
|
---|
[8] | 480 | def __init__(self, flight):
|
---|
| 481 | super(B735, self).__init__(flight)
|
---|
[9] | 482 | self.dow = 31300
|
---|
| 483 | self.mtow = 60550
|
---|
| 484 | self.mlw = 50000
|
---|
| 485 | self.mzfw = 46700
|
---|
[7] | 486 |
|
---|
| 487 | #---------------------------------------------------------------------------------------
|
---|
| 488 |
|
---|
| 489 | class DH8D(Aircraft):
|
---|
| 490 | """Bombardier Dash-8 Q400 aircraft.
|
---|
| 491 |
|
---|
| 492 | The aircraft type-specific values in the aircraft state have the following
|
---|
| 493 | structure:
|
---|
[140] | 494 | - fuel: left, right
|
---|
[7] | 495 | - n1: left, right
|
---|
| 496 | - reverser: left, right."""
|
---|
[140] | 497 | fuelTanks = [const.FUELTANK_LEFT, const.FUELTANK_RIGHT]
|
---|
| 498 |
|
---|
[8] | 499 | def __init__(self, flight):
|
---|
| 500 | super(DH8D, self).__init__(flight)
|
---|
[9] | 501 | self.dow = 17185
|
---|
| 502 | self.mtow = 29257
|
---|
| 503 | self.mlw = 28009
|
---|
| 504 | self.mzfw = 25855
|
---|
| 505 | self.gearSpeedLimit = 215
|
---|
| 506 | self.flapSpeedLimits = { 5 : 200,
|
---|
| 507 | 10 : 181,
|
---|
| 508 | 15 : 172,
|
---|
| 509 | 35 : 158 }
|
---|
| 510 |
|
---|
| 511 | def logFuel(self, aircraftState):
|
---|
| 512 | """Log the amount of fuel"""
|
---|
| 513 | self.logger.message(aircraftState.timestamp,
|
---|
[150] | 514 | "Fuel: left=%.0f kg - right=%.0f kg" % \
|
---|
| 515 | (aircraftState.fuel[0], aircraftState.fuel[1]))
|
---|
[9] | 516 | self.logger.message(aircraftState.timestamp,
|
---|
| 517 | "Total fuel: %.0f kg" % (sum(aircraftState.fuel),))
|
---|
[7] | 518 |
|
---|
| 519 | #---------------------------------------------------------------------------------------
|
---|
| 520 |
|
---|
| 521 | class Boeing767(Aircraft):
|
---|
| 522 | """Base class for the various aircraft in the Boeing 767 family.
|
---|
| 523 |
|
---|
| 524 | The aircraft type-specific values in the aircraft state have the following
|
---|
| 525 | structure:
|
---|
[140] | 526 | - fuel: left, centre, right
|
---|
[7] | 527 | - n1: left, right
|
---|
| 528 | - reverser: left, right"""
|
---|
[140] | 529 | fuelTanks = [const.FUELTANK_LEFT, const.FUELTANK_CENTRE, const.FUELTANK_RIGHT]
|
---|
| 530 |
|
---|
[9] | 531 | def __init__(self, flight):
|
---|
| 532 | super(Boeing767, self).__init__(flight)
|
---|
[95] | 533 | self._checkers.append(checks.ThrustChecker())
|
---|
[9] | 534 | self.gearSpeedLimit = 270
|
---|
| 535 | self.flapSpeedLimits = { 1 : 255,
|
---|
| 536 | 5 : 235,
|
---|
| 537 | 10 : 215,
|
---|
| 538 | 20 : 215,
|
---|
| 539 | 25 : 185,
|
---|
| 540 | 30 : 175 }
|
---|
[7] | 541 |
|
---|
[9] | 542 | def logFuel(self, aircraftState):
|
---|
| 543 | """Log the amount of fuel"""
|
---|
| 544 | self.logger.message(aircraftState.timestamp,
|
---|
| 545 | "Fuel: left=%.0f kg - centre=%.0f kg - right=%.0f kg" % \
|
---|
[150] | 546 | (aircraftState.fuel[0], aircraftState.fuel[1],
|
---|
[9] | 547 | aircraftState.fuel[2]))
|
---|
| 548 | self.logger.message(aircraftState.timestamp,
|
---|
| 549 | "Total fuel: %.0f kg" % (sum(aircraftState.fuel),))
|
---|
| 550 |
|
---|
[7] | 551 | #---------------------------------------------------------------------------------------
|
---|
| 552 |
|
---|
| 553 | class B762(Boeing767):
|
---|
| 554 | """Boeing 767-200 aircraft."""
|
---|
[8] | 555 | def __init__(self, flight):
|
---|
| 556 | super(B762, self).__init__(flight)
|
---|
[9] | 557 | self.dow = 84507
|
---|
| 558 | self.mtow = 175540
|
---|
| 559 | self.mlw = 126098
|
---|
| 560 | self.mzfw = 114758
|
---|
[7] | 561 |
|
---|
| 562 | #---------------------------------------------------------------------------------------
|
---|
| 563 |
|
---|
| 564 | class B763(Boeing767):
|
---|
| 565 | """Boeing 767-300 aircraft."""
|
---|
[8] | 566 | def __init__(self, flight):
|
---|
| 567 | super(B763, self).__init__(cflight)
|
---|
[9] | 568 | self.dow = 91311
|
---|
| 569 | self.mtow = 181436
|
---|
| 570 | self.mlw = 137892
|
---|
| 571 | self.mzfw = 130635
|
---|
[7] | 572 |
|
---|
| 573 | #---------------------------------------------------------------------------------------
|
---|
| 574 |
|
---|
| 575 | class CRJ2(Aircraft):
|
---|
| 576 | """Bombardier CRJ-200 aircraft.
|
---|
| 577 |
|
---|
| 578 | The aircraft type-specific values in the aircraft state have the following
|
---|
| 579 | structure:
|
---|
[140] | 580 | - fuel: left, centre, right
|
---|
[7] | 581 | - n1: left, right
|
---|
| 582 | - reverser: left, right."""
|
---|
[140] | 583 | fuelTanks = [const.FUELTANK_LEFT, const.FUELTANK_CENTRE, const.FUELTANK_RIGHT]
|
---|
| 584 |
|
---|
[8] | 585 | def __init__(self, flight):
|
---|
| 586 | super(CRJ2, self).__init__(flight)
|
---|
[95] | 587 | self._checkers.append(checks.ThrustChecker())
|
---|
[9] | 588 | self.dow = 14549
|
---|
| 589 | self.mtow = 22995
|
---|
| 590 | self.mlw = 21319
|
---|
| 591 | self.mzfw = 19958
|
---|
| 592 | self.gearSpeedLimit = 240
|
---|
| 593 | self.flapSpeedLimits = { 8 : 260,
|
---|
| 594 | 20 : 220,
|
---|
| 595 | 30 : 190,
|
---|
| 596 | 45 : 175 }
|
---|
[7] | 597 |
|
---|
[9] | 598 | def logFuel(self, aircraftState):
|
---|
| 599 | """Log the amount of fuel"""
|
---|
| 600 | self.logger.message(aircraftState.timestamp,
|
---|
| 601 | "Fuel: left=%.0f kg - centre=%.0f kg - right=%.0f kg" % \
|
---|
[150] | 602 | (aircraftState.fuel[0], aircraftState.fuel[1],
|
---|
[9] | 603 | aircraftState.fuel[2]))
|
---|
| 604 | self.logger.message(aircraftState.timestamp,
|
---|
| 605 | "Total fuel: %.0f kg" % (sum(aircraftState.fuel),))
|
---|
| 606 |
|
---|
[7] | 607 | #---------------------------------------------------------------------------------------
|
---|
| 608 |
|
---|
| 609 | class F70(Aircraft):
|
---|
| 610 | """Fokker 70 aircraft.
|
---|
| 611 |
|
---|
| 612 | The aircraft type-specific values in the aircraft state have the following
|
---|
| 613 | structure:
|
---|
[140] | 614 | - fuel: left, centre, right
|
---|
[7] | 615 | - n1: left, right
|
---|
| 616 | - reverser: left, right."""
|
---|
[140] | 617 | fuelTanks = [const.FUELTANK_LEFT, const.FUELTANK_CENTRE, const.FUELTANK_RIGHT]
|
---|
| 618 |
|
---|
[8] | 619 | def __init__(self, flight):
|
---|
| 620 | super(F70, self).__init__(flight)
|
---|
[95] | 621 | self._checkers.append(checks.ThrustChecker())
|
---|
[9] | 622 | self.dow = 24283
|
---|
| 623 | self.mtow = 38100 # FIXME: differentiate by registration number,
|
---|
| 624 | # MTOW of HA-LMF: 41955
|
---|
| 625 | self.mlw = 36740
|
---|
| 626 | self.mzfw = 32655
|
---|
| 627 | self.gearSpeedLimit = 200
|
---|
| 628 | self.flapSpeedLimits = { 8 : 250,
|
---|
| 629 | 15 : 220,
|
---|
| 630 | 25 : 220,
|
---|
| 631 | 42 : 180 }
|
---|
[7] | 632 |
|
---|
[9] | 633 | def logFuel(self, aircraftState):
|
---|
| 634 | """Log the amount of fuel"""
|
---|
| 635 | self.logger.message(aircraftState.timestamp,
|
---|
| 636 | "Fuel: left=%.0f kg - centre=%.0f kg - right=%.0f kg" % \
|
---|
[150] | 637 | (aircraftState.fuel[0], aircraftState.fuel[1],
|
---|
[9] | 638 | aircraftState.fuel[2]))
|
---|
| 639 | self.logger.message(aircraftState.timestamp,
|
---|
| 640 | "Total fuel: %.0f kg" % (sum(aircraftState.fuel),))
|
---|
| 641 |
|
---|
[7] | 642 | #---------------------------------------------------------------------------------------
|
---|
| 643 |
|
---|
| 644 | class DC3(Aircraft):
|
---|
| 645 | """Lisunov Li-2 (DC-3) aircraft.
|
---|
| 646 |
|
---|
| 647 | The aircraft type-specific values in the aircraft state have the following
|
---|
| 648 | structure:
|
---|
[140] | 649 | - fuel: left aux, left, right, right aux
|
---|
[7] | 650 | - rpm: left, right
|
---|
| 651 | - reverser: left, right."""
|
---|
[140] | 652 | fuelTanks = [const.FUELTANK_LEFT_AUX, const.FUELTANK_LEFT,
|
---|
| 653 | const.FUELTANK_RIGHT, const.FUELTANK_RIGHT_AUX]
|
---|
| 654 |
|
---|
[8] | 655 | def __init__(self, flight):
|
---|
| 656 | super(DC3, self).__init__(flight)
|
---|
[9] | 657 | self.dow = 8627
|
---|
| 658 | self.mtow = 11884
|
---|
| 659 | self.mlw = 11793
|
---|
| 660 | self.mzfw = 11780
|
---|
| 661 | self.gearSpeedLimit = 148
|
---|
| 662 | self.flapSpeedLimits = { 15 : 135,
|
---|
| 663 | 30 : 99,
|
---|
| 664 | 45 : 97 }
|
---|
[8] | 665 |
|
---|
| 666 | def _checkFlightEnd(self, aircraftState):
|
---|
| 667 | """Check if the end of the flight has arrived.
|
---|
| 668 |
|
---|
| 669 | This implementation checks the RPM values to be 0."""
|
---|
| 670 | for rpm in aircraftState.rpm:
|
---|
[29] | 671 | if rpm>0: return False
|
---|
| 672 | return True
|
---|
[7] | 673 |
|
---|
[9] | 674 | def logFuel(self, aircraftState):
|
---|
| 675 | """Log the amount of fuel"""
|
---|
| 676 | self.logger.message(aircraftState.timestamp,
|
---|
| 677 | "Fuel: left aux=%.0f kg - left=%.0f kg - right=%.0f kg - right aux=%.0f kg" % \
|
---|
[150] | 678 | (aircraftState.fuel[0], aircraftState.fuel[1],
|
---|
| 679 | aircraftState.fuel[2], aircraftState.fuel[3]))
|
---|
[9] | 680 | self.logger.message(aircraftState.timestamp,
|
---|
| 681 | "Total fuel: %.0f kg" % (sum(aircraftState.fuel),))
|
---|
| 682 |
|
---|
[7] | 683 | #---------------------------------------------------------------------------------------
|
---|
| 684 |
|
---|
| 685 | class T134(Aircraft):
|
---|
| 686 | """Tupolev Tu-134 aircraft.
|
---|
| 687 |
|
---|
| 688 | The aircraft type-specific values in the aircraft state have the following
|
---|
| 689 | structure:
|
---|
[140] | 690 | - fuel: left tip, left aux, centre, right aux, right tip, external 1,
|
---|
[7] | 691 | external 2
|
---|
| 692 | - n1: left, right
|
---|
| 693 | - reverser: left, right."""
|
---|
[206] | 694 | fuelTanks = [const.FUELTANK_LEFT_TIP, const.FUELTANK_EXTERNAL1,
|
---|
| 695 | const.FUELTANK_LEFT_AUX,
|
---|
[140] | 696 | const.FUELTANK_CENTRE,
|
---|
[206] | 697 | const.FUELTANK_RIGHT_AUX,
|
---|
| 698 | const.FUELTANK_EXTERNAL2, const.FUELTANK_RIGHT_TIP]
|
---|
[140] | 699 |
|
---|
[8] | 700 | def __init__(self, flight):
|
---|
| 701 | super(T134, self).__init__(flight)
|
---|
[95] | 702 | self._checkers.append(checks.ThrustChecker())
|
---|
[210] | 703 | self.dow = 29500
|
---|
| 704 | self.mtow = 49000
|
---|
[9] | 705 | self.mlw = 43000
|
---|
| 706 | self.mzfw = 38500
|
---|
| 707 | self.gearSpeedLimit = 216
|
---|
[210] | 708 | self.flapSpeedLimits = { 10 : 450,
|
---|
| 709 | 20 : 400,
|
---|
| 710 | 30 : 300 }
|
---|
[7] | 711 |
|
---|
[9] | 712 | def logFuel(self, aircraftState):
|
---|
| 713 | """Log the amount of fuel"""
|
---|
| 714 | self.logger.message(aircraftState.timestamp,
|
---|
[207] | 715 | "Fuel: left tip=%.0f kg - external 1=%.0f kg - left aux=%.0f kg - centre= %.0f kg - right aux=%.0f kg - external 2=%.0f kg - right tip=%.0f kg" % \
|
---|
| 716 | (aircraftState.fuel[0], aircraftState.fuel[1],
|
---|
[150] | 717 | aircraftState.fuel[2],
|
---|
[207] | 718 | aircraftState.fuel[3], aircraftState.fuel[4],
|
---|
[9] | 719 | aircraftState.fuel[5], aircraftState.fuel[6]))
|
---|
| 720 | self.logger.message(aircraftState.timestamp,
|
---|
| 721 | "Total fuel: %.0f kg" % (sum(aircraftState.fuel),))
|
---|
| 722 |
|
---|
[211] | 723 | def _appendLightsLoggers(self):
|
---|
| 724 | """Append the loggers needed for the lights."""
|
---|
| 725 | self._checkers.append(checks.AnticollisionLightsLogger())
|
---|
| 726 | self._checkers.append(checks.LandingLightsLogger())
|
---|
| 727 | self._checkers.append(checks.NavLightsLogger())
|
---|
| 728 |
|
---|
| 729 | def _appendLightsCheckers(self):
|
---|
| 730 | """Append the checkers needed for the lights."""
|
---|
| 731 | self._checkers.append(checks.TupolevAntiCollisionLightsChecker())
|
---|
| 732 | self._checkers.append(checks.LandingLightsChecker())
|
---|
| 733 | self._checkers.append(checks.NavLightsChecker())
|
---|
| 734 |
|
---|
[7] | 735 | #---------------------------------------------------------------------------------------
|
---|
| 736 |
|
---|
| 737 | class T154(Aircraft):
|
---|
| 738 | """Tupolev Tu-154 aircraft.
|
---|
| 739 |
|
---|
| 740 | The aircraft type-specific values in the aircraft state have the following
|
---|
| 741 | structure:
|
---|
[140] | 742 | - fuel: left aux, left, centre, centre 2, right, right aux
|
---|
[7] | 743 | - n1: left, centre, right
|
---|
| 744 | - reverser: left, right"""
|
---|
[140] | 745 | fuelTanks = [const.FUELTANK_LEFT_AUX, const.FUELTANK_LEFT,
|
---|
| 746 | const.FUELTANK_CENTRE, const.FUELTANK_CENTRE2,
|
---|
| 747 | const.FUELTANK_RIGHT, const.FUELTANK_RIGHT_AUX]
|
---|
[8] | 748 | def __init__(self, flight):
|
---|
| 749 | super(T154, self).__init__(flight)
|
---|
[95] | 750 | self._checkers.append(checks.ThrustChecker())
|
---|
[9] | 751 | self.dow = 53259
|
---|
| 752 | self.mtow = 98000
|
---|
| 753 | self.mlw = 78000
|
---|
| 754 | self.mzfw = 72000
|
---|
| 755 | self.gearSpeedLimit = 216
|
---|
| 756 | self.flapSpeedLimits = { 15 : 227,
|
---|
| 757 | 28 : 194,
|
---|
| 758 | 45 : 162 }
|
---|
| 759 |
|
---|
| 760 | def logFuel(self, aircraftState):
|
---|
| 761 | """Log the amount of fuel"""
|
---|
| 762 | self.logger.message(aircraftState.timestamp,
|
---|
| 763 | "Fuel: left aux=%.0f kg - left=%.0f kg - centre=%.0f kg - centre 2=%.0f kg - right=%.0f kg - right aux=%.0f kg" % \
|
---|
[150] | 764 | (aircraftState.fuel[0], aircraftState.fuel[1],
|
---|
| 765 | aircraftState.fuel[2], aircraftState.fuel[3],
|
---|
| 766 | aircraftState.fuel[4], aircraftState.fuel[5]))
|
---|
[9] | 767 | self.logger.message(aircraftState.timestamp,
|
---|
| 768 | "Total fuel: %.0f kg" % (sum(aircraftState.fuel),))
|
---|
[7] | 769 |
|
---|
[211] | 770 | def _appendLightsLoggers(self):
|
---|
| 771 | """Append the loggers needed for the lights."""
|
---|
| 772 | self._checkers.append(checks.AnticollisionLightsLogger())
|
---|
| 773 | self._checkers.append(checks.LandingLightsLogger())
|
---|
| 774 | self._checkers.append(checks.NavLightsLogger())
|
---|
| 775 |
|
---|
| 776 | def _appendLightsCheckers(self):
|
---|
| 777 | """Append the checkers needed for the lights."""
|
---|
| 778 | self._checkers.append(checks.TupolevAntiCollisionLightsChecker())
|
---|
| 779 | self._checkers.append(checks.LandingLightsChecker())
|
---|
| 780 | self._checkers.append(checks.NavLightsChecker())
|
---|
| 781 |
|
---|
[7] | 782 | #---------------------------------------------------------------------------------------
|
---|
| 783 |
|
---|
[9] | 784 |
|
---|
[7] | 785 | class YK40(Aircraft):
|
---|
| 786 | """Yakovlev Yak-40 aircraft.
|
---|
| 787 |
|
---|
| 788 | The aircraft type-specific values in the aircraft state have the following
|
---|
| 789 | structure:
|
---|
| 790 | - fuel: left, right
|
---|
| 791 | - n1: left, right
|
---|
| 792 | - reverser: left, right"""
|
---|
[140] | 793 | fuelTanks = [const.FUELTANK_LEFT, const.FUELTANK_RIGHT]
|
---|
| 794 |
|
---|
[8] | 795 | def __init__(self, flight):
|
---|
| 796 | super(YK40, self).__init__(flight)
|
---|
[95] | 797 | self._checkers.append(checks.ThrustChecker())
|
---|
[9] | 798 | self.dow = 9400
|
---|
| 799 | self.mtow = 17200
|
---|
| 800 | self.mlw = 16800
|
---|
| 801 | self.mzfw = 12100
|
---|
| 802 | self.gearSpeedLimit = 165
|
---|
| 803 | self.flapSpeedLimits = { 20 : 165,
|
---|
| 804 | 35 : 135 }
|
---|
| 805 |
|
---|
| 806 | def logFuel(self, aircraftState):
|
---|
| 807 | """Log the amount of fuel"""
|
---|
| 808 | self.logger.message(aircraftState.timestamp,
|
---|
| 809 | "Fuel: left=%.0f kg - right=%.0f kg" % \
|
---|
| 810 | (aircraftState.fuel[0], aircraftState.fuel[1]))
|
---|
| 811 | self.logger.message(aircraftState.timestamp,
|
---|
| 812 | "Total fuel: %.0f kg" % (sum(aircraftState.fuel),))
|
---|
[7] | 813 |
|
---|
[211] | 814 | def _appendLightsLoggers(self):
|
---|
| 815 | """Append the loggers needed for the lights."""
|
---|
| 816 | self._checkers.append(checks.AnticollisionLightsLogger())
|
---|
| 817 | self._checkers.append(checks.LandingLightsLogger())
|
---|
| 818 | self._checkers.append(checks.NavLightsLogger())
|
---|
| 819 |
|
---|
| 820 | def _appendLightsCheckers(self):
|
---|
| 821 | """Append the checkers needed for the lights."""
|
---|
| 822 | self._checkers.append(checks.AntiCollisionLightsChecker())
|
---|
| 823 | self._checkers.append(checks.LandingLightsChecker())
|
---|
| 824 | self._checkers.append(checks.NavLightsChecker())
|
---|
| 825 |
|
---|
[7] | 826 | #---------------------------------------------------------------------------------------
|
---|
| 827 |
|
---|
[141] | 828 | MostFuelTankAircraft = T134
|
---|
| 829 |
|
---|
| 830 | #---------------------------------------------------------------------------------------
|
---|
| 831 |
|
---|
[191] | 832 | _classes = { const.AIRCRAFT_B736 : B736,
|
---|
| 833 | const.AIRCRAFT_B737 : B737,
|
---|
| 834 | const.AIRCRAFT_B738 : B738,
|
---|
| 835 | const.AIRCRAFT_B738C : B738Charter,
|
---|
| 836 | const.AIRCRAFT_B733 : B733,
|
---|
| 837 | const.AIRCRAFT_B734 : B734,
|
---|
| 838 | const.AIRCRAFT_B735 : B735,
|
---|
| 839 | const.AIRCRAFT_DH8D : DH8D,
|
---|
| 840 | const.AIRCRAFT_B762 : B762,
|
---|
| 841 | const.AIRCRAFT_B763 : B763,
|
---|
| 842 | const.AIRCRAFT_CRJ2 : CRJ2,
|
---|
| 843 | const.AIRCRAFT_F70 : F70,
|
---|
| 844 | const.AIRCRAFT_DC3 : DC3,
|
---|
| 845 | const.AIRCRAFT_T134 : T134,
|
---|
| 846 | const.AIRCRAFT_T154 : T154,
|
---|
| 847 | const.AIRCRAFT_YK40 : YK40 }
|
---|
[8] | 848 |
|
---|
| 849 | #---------------------------------------------------------------------------------------
|
---|
[197] | 850 |
|
---|
| 851 | if __name__ == "__main__":
|
---|
| 852 | value = SmoothedValue()
|
---|
| 853 |
|
---|
| 854 | print "Adding 1, 12.0"
|
---|
| 855 | value.add(1, 12.0)
|
---|
| 856 | print value.get()
|
---|
| 857 |
|
---|
| 858 | print "Adding 1, 15.0"
|
---|
| 859 | value.add(1, 15.0)
|
---|
| 860 | print value.get()
|
---|
| 861 |
|
---|
| 862 | print "Adding 2, 18.0"
|
---|
| 863 | value.add(2, 18.0)
|
---|
| 864 | print value.get()
|
---|
| 865 |
|
---|
| 866 | print "Adding 2, 20.0"
|
---|
| 867 | value.add(2, 20.0)
|
---|
| 868 | print value.get()
|
---|
| 869 |
|
---|
| 870 | print "Adding 5, 22.0"
|
---|
| 871 | value.add(5, 22.0)
|
---|
| 872 | print value.get()
|
---|
| 873 |
|
---|
| 874 | print "Adding 5, 25.0"
|
---|
| 875 | value.add(5, 25.0)
|
---|
| 876 | print value.get()
|
---|
| 877 |
|
---|
| 878 | print "Adding 5, 29.0"
|
---|
| 879 | value.add(5, 29.0)
|
---|
| 880 | print value.get()
|
---|
| 881 |
|
---|
| 882 | print "Adding 5, 21.0"
|
---|
| 883 | value.add(5, 21.0)
|
---|
| 884 | print value.get()
|
---|
| 885 |
|
---|
| 886 | print "Adding 5, 26.0"
|
---|
| 887 | value.add(5, 26.0)
|
---|
| 888 | print value.get()
|
---|
| 889 |
|
---|
| 890 | print "Adding 2, 30.0"
|
---|
| 891 | value.add(2, 30.0)
|
---|
| 892 | print value.get()
|
---|
| 893 |
|
---|
| 894 | print "Adding 2, 55.0"
|
---|
| 895 | value.add(2, 55.0)
|
---|
| 896 | print value.get()
|
---|
| 897 |
|
---|
| 898 | #---------------------------------------------------------------------------------------
|
---|