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acft.py@ 917:803dc6bacfa5

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Last change on this file since 917:803dc6bacfa5 was 917:803dc6bacfa5, checked in by István Váradi <ivaradi@…>, 5 years ago
Merged 0.39
File size: 50.0 KB

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[298]	1
	2	import const
[619]	3	import gates
[298]	4	import checks
	5	import fs
[384]	6	from i18n import xstr
[298]	7	import util
	8
	9	import sys
	10	import time
	11	import traceback
	12
	13	from collections import deque
	14
	15	#---------------------------------------------------------------------------------------
	16
[297]	17	## @package mlx.acft
	18	#
	19	# The simulator-independent aircraft classes.
	20	#
	21	# This module contains the aircraft classes that contain some general data
	22	# about each aircraft type in the MAVA Fleet. The base class, \ref Aircraft
	23	# also implements some parts of the logging and traces some data. The classes
	24	# are also responsible for creating the \ref mlx.checks "checkers". Most of
	25	# them are created by the \ref Aircraft class' constructor, but there can be
	26	# type-specific differences. For example the lights are different for different
	27	# types, so there is a \ref Aircraft._appendLightsLoggers "function" which can
	28	# be reimplemented in child classes, if needed. This class maintains also the
	29	# \ref SmoothedValue "smoothed values" of the IAS and the VS and set these
	30	# values in the \ref mlx.fs.AircraftState "aircraft state" when it is received
	31	# from the simulator.
[4]	32
	33	#---------------------------------------------------------------------------------------
	34
[512]	35	# Derate type: no derate possible
	36	DERATE_NONE = 0
	37
	38	# Derate type: Boeing, i.e. a percentage value.
	39	# For logging, the percentage value is expected as a string (i.e. whatever the
	40	# pilot enters into the text field).
	41	DERATE_BOEING = 1
	42
	43	# Derate type: EPR, i.e. an EPR value.
	44	# For logging, the EPR value is expected as a string (i.e. whatever the pilot
	45	# enters into the text field).
	46	DERATE_EPR = 2
	47
	48	# Derate type: Tupolev, i.e. nominal or takeoff
	49	# For logging, one of the DERATE_TUPOLEV_xxx values are expected.
	50	DERATE_TUPOLEV = 3
	51
	52	# Tupolev derate value: nominal
	53	DERATE_TUPOLEV_NOMINAL = 1
	54
	55	# Tupolev derate value: takeoff
	56	DERATE_TUPOLEV_TAKEOFF = 2
	57
	58	# Derate type: BAe-146, i.e. enabled or not
	59	# For logging, a boolean is expected.
	60	DERATE_B462 = 4
	61
	62	#---------------------------------------------------------------------------------------
	63
[197]	64	class SmoothedValue(object):
	65	"""A smoothed value."""
	66	def __init__(self):
	67	"""Construct the value."""
	68	self._deque = deque()
	69	self._sum = 0
	70
	71	def add(self, length, value):
	72	"""Add the given value and smooth with the given length."""
	73	dequeLength = len(self._deque)
	74	while dequeLength>=length:
	75	self._sum -= self._deque.popleft()
	76	dequeLength -= 1
	77
	78	self._sum += value
	79	self._deque.append(value)
	80
	81	def get(self):
	82	"""Get the average."""
	83	return self._sum / len(self._deque)
[331]	84
[4]	85	#---------------------------------------------------------------------------------------
	86
[709]	87	class SimBriefData(object):
	88	"""Data to be used when creating SimBrief briefings."""
	89	def __init__(self, climbProfiles, cruiseProfiles, descentProfiles):
	90	"""Construct the SimBrief data with the given profiles."""
	91	self.climbProfiles = climbProfiles
	92	self.cruiseProfiles = cruiseProfiles
	93	self.descentProfiles = descentProfiles
	94
	95	#---------------------------------------------------------------------------------------
	96
[4]	97	class Aircraft(object):
	98	"""Base class for aircraft."""
[898]	99	dowCockpit = 2
	100	dowCabin = 3
	101
[8]	102	@staticmethod
[798]	103	def create(flight, bookedFlight):
[8]	104	"""Create an aircraft instance for the type in the given flight."""
[798]	105	acft = _classes[flight.aircraftType](flight)
	106	acft.setBookedFlight(bookedFlight)
	107	return acft
[8]	108
[592]	109	def __init__(self, flight, minLandingFuel = None,
	110	recommendedLandingFuel = None):
[4]	111	"""Construct the aircraft for the given type."""
[8]	112	self._flight = flight
[591]	113	self._minLandingFuel = minLandingFuel
[592]	114	self._recommendedLandingFuel = recommendedLandingFuel
[369]	115
	116	self._name = None
	117	self._modelName = None
	118
[4]	119	self._aircraftState = None
[331]	120
[9]	121	self._maxVS = -10000.0
	122	self._minVS = 10000.0
[4]	123
[101]	124	self._v1r2LineIndex = None
[384]	125	self._derateLineID = None
[391]	126	self._takeoffAntiIceLineID = None
[96]	127	self._vrefLineIndex = None
[391]	128	self._landingAntiIceLineID = None
[96]	129
[899]	130	self.cockpitCrewWeight = 85.0
	131	self.cabinCrewWeight = 75.0
	132	self.humanWeight = 84.0
[117]	133
[598]	134	self.initialClimbSpeedAltitude = 1500
	135	self.reverseMinSpeed = 50
[360]	136
[644]	137	self.hasStrobeLight = True
	138
[611]	139	self.maxTakeOffPitch = 15.0
	140	self.maxTouchDownPitch = 15.0
[624]	141	self.brakeCoolTime = 10.0
[611]	142
[709]	143	self.simBriefData = None
	144
[8]	145	self._checkers = []
	146
[197]	147	config = flight.config
[11]	148	# Loggers
	149
[8]	150	self._checkers.append(checks.StageChecker())
[9]	151	self._checkers.append(checks.TakeOffLogger())
[8]	152
	153	self._checkers.append(checks.AltimeterLogger())
[321]	154
[366]	155	self._ilsLogger = checks.ILSLogger()
	156	self._checkers.append(self._ilsLogger)
[321]	157	self._nav1Logger = checks.NAV1Logger()
	158	self._checkers.append(self._nav1Logger)
	159	self._nav2Logger = checks.NAV2Logger()
	160	self._checkers.append(self._nav2Logger)
	161
	162	self._adf1Logger = checks.ADF1Logger()
	163	self._checkers.append(self._adf1Logger)
	164	self._adf2Logger = checks.ADF2Logger()
	165	self._checkers.append(self._adf2Logger)
[331]	166
[8]	167	self._checkers.append(checks.SquawkLogger())
	168
[211]	169	self._appendLightsLoggers()
[8]	170
	171	self._checkers.append(checks.FlapsLogger())
	172
	173	self._checkers.append(checks.GearsLogger())
[601]	174	self._checkers.append(checks.InitialClimbSpeedLogger())
[9]	175	self._checkers.append(checks.CruiseSpeedLogger())
[10]	176	self._checkers.append(checks.SpoilerLogger())
[338]	177	self._checkers.append(checks.APLogger())
[9]	178
[197]	179	if config.isMessageTypeFS(const.MESSAGETYPE_VISIBILITY):
[134]	180	self._checkers.append(checks.VisibilityChecker())
	181
[139]	182	# FIXME: we should have a central data model object, and not collect
	183	# the data from the GUI. However, some pieces of data (e.g. V-speeds,
	184	# etc. that is entered into the GUI) should be a part of the GUI and
	185	# queried from it, so the model should have a reference to the GUI as
	186	# well and access such data via the GUI!
[215]	187	if config.onlineACARS and flight.loggedIn and not flight.entranceExam:
[139]	188	self._checkers.append(checks.ACARSSender(flight._gui))
	189
[11]	190	# Fault checkers
[211]	191
	192	self._appendLightsCheckers()
[11]	193
[335]	194	self._checkers.append(checks.TransponderChecker())
	195
[11]	196	self._checkers.append(checks.BankChecker())
	197
	198	self._checkers.append(checks.FlapsRetractChecker())
	199	self._checkers.append(checks.FlapsSpeedLimitChecker())
	200
	201	self._checkers.append(checks.GearsDownChecker())
	202	self._checkers.append(checks.GearSpeedLimitChecker())
	203
	204	self._checkers.append(checks.GLoadChecker())
	205
	206	self._checkers.append(checks.MLWChecker())
	207	self._checkers.append(checks.MTOWChecker())
	208	self._checkers.append(checks.MZFWChecker())
	209	self._checkers.append(checks.PayloadChecker())
	210
[539]	211	self._checkers.append(checks.SpeedChecker())
[11]	212	self._checkers.append(checks.VSChecker())
[197]	213
[447]	214	timeout = 30.0 + config.realIASSmoothingLength - 1
[622]	215	self._checkers.append(checks.OverspeedChecker(faultTimeout = timeout))
[331]	216
[11]	217	self._checkers.append(checks.StallChecker())
	218
	219	self._checkers.append(checks.PitotChecker())
[331]	220
[598]	221	self._checkers.append(checks.ReverserLogger())
[11]	222	self._checkers.append(checks.ReverserChecker())
	223
[273]	224	if flight.aircraftType is not None and config.enableApproachCallouts:
	225	approachCallouts = flight.config.getApproachCallouts(flight.aircraftType)
	226	if approachCallouts:
	227	self._checkers.append(checks.ApproachCalloutsPlayer(approachCallouts))
	228
[197]	229	self._smoothedIAS = SmoothedValue()
	230	self._smoothedVS = SmoothedValue()
	231
[4]	232	@property
	233	def type(self):
	234	"""Get the type of the aircraft."""
[8]	235	return self._flight.aircraftType
	236
	237	@property
	238	def flight(self):
	239	"""Get the flight the aircraft belongs to."""
	240	return self._flight
[4]	241
[8]	242	@property
[592]	243	def minLandingFuel(self):
	244	"""Get the minimum acceptable amount of the landing fuel."""
	245	return self._minLandingFuel
	246
	247	@property
	248	def recommendedLandingFuel(self):
	249	"""Get the recommended amount of the landing fuel."""
	250	return self._recommendedLandingFuel
	251
	252	@property
[8]	253	def logger(self):
	254	"""Get the logger to use for the aircraft."""
	255	return self._flight.logger
	256
[139]	257	@property
	258	def state(self):
	259	"""Get the current aircraft state."""
	260	return self._aircraftState
[241]	261
	262	@property
	263	def speedInKnots(self):
	264	"""Indicate if the speed is in knots.
	265
	266	This default implementation returns True."""
	267	return True
[304]	268
	269	@property
[635]	270	def aglInFeet(self):
	271	"""Indicate if AGL altitudes are to be logged in feet.
	272
	273	This default implementation returns True."""
	274	return True
	275
	276	@property
[304]	277	def timestamp(self):
	278	"""Get the timestamp of the current state."""
	279	return None if self._aircraftState is None \
	280	else self._aircraftState.timestamp
[331]	281
[384]	282	@property
[512]	283	def derateType(self):
	284	"""Get the derate type for this aircraft.
	285
	286	This default implementation returns DERATE_NONE."""
	287	return DERATE_NONE
[384]	288
[798]	289	def setBookedFlight(self, bookedFlight):
	290	"""Update the aircraft based on the booked flight data (e.g. tail number).
	291
	292	This default implementation does nothing."""
	293
[512]	294	def getDerateLine(self, value):
	295	"""Get the log line for the given derate value.
	296
	297	It uses the the derate type and produces the standard message for
	298	each. This children need not override it, although they can."""
	299	dt = self.derateType
[384]	300
[512]	301	if dt==DERATE_BOEING:
	302	return "Derate calculated by the pilot: %s %%" % \
	303	("-" if value is None else value,)
	304	elif dt==DERATE_EPR:
	305	return "EPR calculated by the pilot: %s" % \
	306	("-" if value is None else value,)
	307	elif dt==DERATE_TUPOLEV:
	308	return "Thrust setting calculated by the pilot: %s" % \
	309	("-" if value is None else
	310	"nominal" if value==DERATE_TUPOLEV_NOMINAL else "takeoff",)
	311	elif dt==DERATE_B462:
	312	return "Derate setting: %s" % \
	313	("-" if value is None else "enabled" if value else "disabled",)
	314	elif dt!=DERATE_NONE:
	315	print "mlx.acft.getDerateLine: invalid derate type: " + dt
[384]	316
	317	return None
	318
[11]	319	def getFlapsSpeedLimit(self, flaps):
	320	"""Get the speed limit for the given flaps setting."""
	321	return self.flapSpeedLimits[flaps] if flaps in self.flapSpeedLimits \
	322	else None
	323
[8]	324	def modelChanged(self, timestamp, aircraftName, modelName):
[4]	325	"""Called when the simulator's aircraft changes."""
[369]	326	self._name = aircraftName
	327	self._modelName = modelName
	328	if self._flight.stage is not None:
	329	self._logNameAndModel(timestamp)
[4]	330
	331	def handleState(self, aircraftState):
[197]	332	"""Called when the state of the aircraft changes.
	333
	334	This is the function that the simulator calls directly with the new
	335	state."""
[274]	336	try:
	337	config = self._flight.config
[197]	338
[274]	339	self._smoothedIAS.add(config.realIASSmoothingLength, aircraftState.ias)
	340	aircraftState.smoothedIAS = self._smoothedIAS.get()
	341
	342	self._smoothedVS.add(config.realVSSmoothingLength, aircraftState.vs)
	343	aircraftState.smoothedVS = self._smoothedVS.get()
[197]	344
[274]	345	for checker in self._checkers:
	346	try:
	347	checker.check(self._flight, self, self._flight.logger,
	348	self._aircraftState, aircraftState)
	349	except:
	350	print >> sys.stderr, "Checker", checker, "failed"
	351	traceback.print_exc()
[7]	352
[274]	353	self._flight.handleState(self._aircraftState, aircraftState)
[89]	354
[274]	355	self._maxVS = max(self._maxVS, aircraftState.vs)
	356	self._minVS = min(self._minVS, aircraftState.vs)
	357	except:
	358	print >> sys.stderr, "Failed to handle the state"
	359	traceback.print_exc()
	360	finally:
	361	self._aircraftState = aircraftState
[331]	362
[8]	363	def setStage(self, aircraftState, newStage):
	364	"""Set the given stage as the new one and do whatever should be
	365	done."""
[369]	366	if newStage==const.STAGE_BOARDING:
	367	self._logNameAndModel(aircraftState.timestamp)
	368
[624]	369	oldStage = self._flight.stage
	370
[9]	371	if self._flight.setStage(aircraftState.timestamp, newStage):
	372	if newStage==const.STAGE_PUSHANDTAXI:
	373	self.logger.message(aircraftState.timestamp, "Block time start")
[274]	374	self._flight.logFuel(aircraftState)
[331]	375	self.logger.message(aircraftState.timestamp,
[313]	376	"ZFW: %.2f kg" % (aircraftState.zfw))
[134]	377	flight = self._flight
	378	if flight.v1 is None or flight.vr is None or flight.v2 is None:
	379	fs.sendMessage(const.MESSAGETYPE_HELP,
	380	"Don't forget to set the takeoff V-speeds!",
	381	5)
[9]	382	elif newStage==const.STAGE_TAKEOFF:
[624]	383	if oldStage == const.STAGE_RTO and self._flight.hasRTO:
	384	rtoState = self._flight.rtoState
	385	if (aircraftState.timestamp - rtoState.timestamp) < \
	386	(self.brakeCoolTime * 60.0):
	387	self.logger.fault("brakeCoolTime",
	388	aircraftState.timestamp,
	389	"Did not cool the brakes for at least %.f minutes after the RTO" % (self.brakeCoolTime,),
	390	15.0)
[241]	391	self.logger.message(aircraftState.timestamp,
	392	"Flight time start")
[331]	393	self.logger.message(aircraftState.timestamp,
[9]	394	"Takeoff weight: %.0f kg, MTOW: %.0f kg" % \
	395	(aircraftState.grossWeight, self.mtow))
[409]	396	self._logQNH(aircraftState)
[9]	397	self.logger.message(aircraftState.timestamp,
[333]	398	"Wind %03.0f/%.0f" % \
[331]	399	(aircraftState.windDirection,
[9]	400	aircraftState.windSpeed))
[321]	401	self._logRadios(aircraftState)
[345]	402	self._logV1R2(aircraftState)
[384]	403	self._logDerate(aircraftState)
[391]	404	self._logTakeoffAntiIce(aircraftState)
[321]	405	elif newStage==const.STAGE_DESCENT or newStage==const.STAGE_LANDING:
	406	self._logRadios(aircraftState)
[409]	407	if newStage==const.STAGE_LANDING:
	408	self._logQNH(aircraftState)
[634]	409	elif newStage==const.STAGE_GOAROUND:
	410	from logger import Logger
	411	self._flight.handleFault("goaround",
	412	aircraftState.timestamp,
	413	"Go-around detected, please, explain!",
	414	Logger.NO_SCORE)
[9]	415	elif newStage==const.STAGE_TAXIAFTERLAND:
[184]	416	flight = self._flight
	417	bookedFlight = flight.bookedFlight
	418	config = flight.config
[136]	419	if config.onlineGateSystem and \
[215]	420	flight.loggedIn and \
[184]	421	not flight.entranceExam and \
[136]	422	bookedFlight.arrivalICAO=="LHBP" and \
	423	config.isMessageTypeFS(const.MESSAGETYPE_GATE_SYSTEM):
[134]	424	self._flight.getFleet(callback = self._fleetRetrieved,
	425	force = True)
[9]	426	self.logger.message(aircraftState.timestamp, "Flight time end")
[274]	427	self._flight.logFuel(aircraftState)
[591]	428	if self._minLandingFuel is not None and \
	429	aircraftState.totalFuel<self._minLandingFuel:
[597]	430	self._flight.handleFault(self.__class__,
	431	aircraftState.timestamp,
	432	"The amount of the landing fuel is less than the minimum for this type: %ukgs (possible NO GO!)" %
	433	(self._minLandingFuel,), 0)
[9]	434	self.logger.message(aircraftState.timestamp,
	435	"Landing weight: %.0f kg, MLW: %.0f" % \
	436	(aircraftState.grossWeight, self.mlw))
	437	self.logger.message(aircraftState.timestamp,
	438	"Vertical speed range: %.0f..%.0f feet/min" % \
[12]	439	(self._minVS, self._maxVS))
[359]	440	# elif newStage==const.STAGE_PARKING:
	441	# self.logger.message(aircraftState.timestamp, "Block time end")
[89]	442	elif newStage==const.STAGE_END:
	443	flightLength = self._flight.flightTimeEnd - self._flight.flightTimeStart
[359]	444	self.logger.message(aircraftState.timestamp, "Block time end")
[89]	445	self.logger.message(aircraftState.timestamp,
	446	"Flight time: " +
	447	util.getTimeIntervalString(flightLength))
	448	self.logger.message(aircraftState.timestamp,
	449	"Flown distance: %.2f NM" % \
[331]	450	(self._flight.flownDistance,))
[89]	451	blockLength = self._flight.blockTimeEnd - self._flight.blockTimeStart
	452	self.logger.message(aircraftState.timestamp,
	453	"Block time: " +
	454	util.getTimeIntervalString(blockLength))
[8]	455
[9]	456	def prepareFlare(self):
	457	"""Called when it is detected that we will soon flare.
[8]	458
	459	On the first call, it should start monitoring some parameters more
	460	closely to determine flare time."""
[9]	461	self.flight.simulator.startFlare()
	462
[331]	463	def flareStarted(self, windSpeed, windDirection, visibility,
[9]	464	flareStart, flareStartFS):
	465	"""Called when the flare has started."""
	466	self.logger.message(self._aircraftState.timestamp, "The flare has begun")
	467	self.logger.message(self._aircraftState.timestamp,
[333]	468	"Wind %03.0f/%.0f" % \
[9]	469	(windDirection, windSpeed))
	470	self.logger.message(self._aircraftState.timestamp,
	471	"Visibility: %.0f metres" % (visibility,))
[409]	472	self._logQNH(self._aircraftState)
[101]	473	self._logVRef()
[391]	474	self._logLandingAntiIce(self._aircraftState)
[9]	475	self.flight.flareStarted(flareStart, flareStartFS)
[134]	476	fs.sendMessage(const.MESSAGETYPE_INFORMATION, "Flare-time", 3)
[331]	477
[9]	478	def flareFinished(self, flareEnd, flareEndFS, tdRate, tdRateCalculatedByFS,
	479	ias, pitch, bank, heading):
	480	"""Called when the flare has finished."""
	481	(flareTimeFromFS, flareTime) = self.flight.flareFinished(flareEnd,
[170]	482	flareEndFS,
	483	tdRate)
[9]	484	self.logger.message(self._aircraftState.timestamp,
[153]	485	"Flaretime: %.3f (from %s)" % \
[331]	486	(flareTime,
[9]	487	"the simulator" if flareTimeFromFS else "real time",))
	488	self.logger.message(self._aircraftState.timestamp,
	489	"Touchdown rate: %.0f feet/min" % (tdRate,))
	490	self.logger.message(self._aircraftState.timestamp,
	491	"Touchdown rate was calculated by the %s" % \
	492	("simulator" if tdRateCalculatedByFS else "logger",))
[241]	493	flight = self._flight
[9]	494	self.logger.message(self._aircraftState.timestamp,
[241]	495	"Touchdown speed: %.0f %s" % \
	496	(flight.speedFromKnots(ias),
	497	flight.getEnglishSpeedUnit()))
[9]	498	self.logger.message(self._aircraftState.timestamp,
	499	"Touchdown pitch: %.1f degrees" % (pitch,))
	500	self.logger.message(self._aircraftState.timestamp,
	501	"Touchdown bank: %.1f degrees" % (bank,))
	502	self.logger.message(self._aircraftState.timestamp,
	503	"Touchdown heading: %03.0f degrees" % (heading,))
[331]	504	self.logger.message(self._aircraftState.timestamp,
[340]	505	"CG: %.1f%%" % \
[271]	506	(self._aircraftState.cog*100.0,))
[8]	507
[611]	508	if abs(pitch)>self.maxTouchDownPitch:
	509	self._flight.handleNoGo("TDPitch", self._aircraftState.timestamp,
	510	"Touchdown pitch higher than aircraft maximum (%.2f)" % \
	511	(self.maxTouchDownPitch,),
	512	"TD TAILSTRIKE NO GO")
	513
[8]	514	def cancelFlare(self):
	515	"""Cancel flare, if it has started."""
[9]	516	self.flight.simulator.cancelFlare()
[8]	517
	518	def checkFlightEnd(self, aircraftState):
	519	"""Check if the end of the flight has arrived.
	520
	521	This default implementation checks the N1 values, but for
	522	piston-powered aircraft you need to check the RPMs."""
	523	for n1 in aircraftState.n1:
	524	if n1>=0.5: return False
	525	return True
	526
[101]	527	def updateV1R2(self):
	528	"""Update the V1, Vr and V2 values from the flight, if the these values
	529	have already been logged."""
	530	if self._v1r2LineIndex is not None:
	531	self._logV1R2()
	532
[384]	533	def updateDerate(self):
	534	"""Update the derate value from the flight, if the these values
	535	have already been logged."""
	536	if self._derateLineID is not None:
	537	self._logDerate()
	538
[391]	539	def updateTakeoffAntiIce(self):
	540	"""Update the take-off anti-ice setting."""
	541	if self._takeoffAntiIceLineID is not None:
	542	self._logTakeoffAntiIce()
	543
[211]	544	def _appendLightsLoggers(self):
	545	"""Append the loggers needed for the lights.
	546
	547	This default implementation adds the loggers for the anti-collision
	548	lights, the landing lights, the strobe lights and the NAV lights."""
	549	self._checkers.append(checks.AnticollisionLightsLogger())
	550	self._checkers.append(checks.LandingLightsLogger())
	551	self._checkers.append(checks.StrobeLightsLogger())
	552	self._checkers.append(checks.NavLightsLogger())
	553
	554	def _appendLightsCheckers(self):
	555	"""Append the checkers needed for the lights.
	556
	557	This default implementation adds the checkers for the anti-collision
	558	lights, the landing lights, the strobe lights and the NAV lights."""
	559	self._checkers.append(checks.AntiCollisionLightsChecker())
	560	self._checkers.append(checks.LandingLightsChecker())
	561	self._checkers.append(checks.NavLightsChecker())
	562	self._checkers.append(checks.StrobeLightsChecker())
	563
[241]	564	def _speedToLog(self, speed):
	565	"""Convert the given speed (being either None or expressed in the
	566	flight's speed unit into a string."""
	567	if speed is None:
	568	return "-"
	569	else:
	570	return str(speed) + " " + self._flight.getEnglishSpeedUnit()
	571
[345]	572	def _logV1R2(self, state = None):
[101]	573	"""Log the V1, Vr and V2 value either newly, or by updating the
	574	corresponding line."""
[526]	575	message = "Calc. TO speeds: V1: %s, VR: %s, V2: %s" % \
[241]	576	(self._speedToLog(self._flight.v1),
	577	self._speedToLog(self._flight.vr),
	578	self._speedToLog(self._flight.v2))
[101]	579
	580	if self._v1r2LineIndex is None:
[345]	581	if state is None:
	582	state = self._aircraftState
[101]	583	self._v1r2LineIndex = \
[345]	584	self.logger.message(state.timestamp, message)
[101]	585	else:
	586	self.logger.updateLine(self._v1r2LineIndex, message)
	587
[384]	588	def _logDerate(self, state = None):
	589	"""Log the derate values either newly or by updating the corresponding
	590	line."""
[512]	591	dt = self.derateType
	592	if dt==DERATE_NONE:
[384]	593	return
	594
[512]	595	message = self.getDerateLine(self._flight.derate)
	596	if message is not None:
	597	if self._derateLineID is None:
	598	if state is None:
	599	state = self._aircraftState
	600	self._derateLineID = \
	601	self.logger.message(state.timestamp, message)
	602	else:
	603	self.logger.updateLine(self._derateLineID, message)
[384]	604
[391]	605	def _logTakeoffAntiIce(self, state = None):
	606	"""Log the take-off anti-ice setting either newly or by updating the
	607	corresponding line."""
	608	antiIceOn = self._flight.takeoffAntiIceOn
	609	if state is not None:
	610	antiIceOn = antiIceOn or state.antiIceOn is True
	611	self._flight.takeoffAntiIceOn = antiIceOn
	612
	613	message = "Anti-ice was turned %s" % \
	614	("ON" if antiIceOn else "OFF")
	615
	616	if self._takeoffAntiIceLineID is None:
	617	if state is None:
	618	state = self._aircraftState
	619	self._takeoffAntiIceLineID = \
	620	self.logger.message(state.timestamp, message)
	621	else:
	622	self.logger.updateLine(self._takeoffAntiIceLineID, message)
	623
[96]	624	def updateVRef(self):
	625	"""Update the Vref value from the flight, if the Vref value has already
	626	been logged."""
	627	if self._vrefLineIndex is not None:
	628	self._logVRef()
	629
	630	def _logVRef(self):
	631	"""Log the Vref value either newly, or by updating the corresponding
	632	line."""
	633	message = "VRef speed calculated by the pilot: %s" % \
[241]	634	(self._speedToLog(self._flight.vref),)
[96]	635	if self._vrefLineIndex is None:
	636	self._vrefLineIndex = \
	637	self.logger.message(self._aircraftState.timestamp, message)
	638	else:
	639	self.logger.updateLine(self._vrefLineIndex, message)
	640
[391]	641	def updateLandingAntiIce(self):
	642	"""Update the landing anti-ice setting."""
	643	if self._landingAntiIceLineID is not None:
	644	self._logLandingAntiIce()
	645
	646	def _logLandingAntiIce(self, state = None):
	647	"""Log the landing anti-ice setting either newly or by updating the
	648	corresponding line."""
	649	antiIceOn = self._flight.landingAntiIceOn
	650	if state is not None:
	651	antiIceOn = antiIceOn or state.antiIceOn is True
	652	self._flight.landingAntiIceOn = antiIceOn
	653
	654	message = "Anti-ice was turned %s" % \
	655	("ON" if antiIceOn else "OFF")
	656
	657	if self._landingAntiIceLineID is None:
	658	if state is None:
	659	state = self._aircraftState
	660	self._landingAntiIceLineID = \
	661	self.logger.message(state.timestamp, message)
	662	else:
	663	self.logger.updateLine(self._landingAntiIceLineID, message)
	664
[134]	665	def _fleetRetrieved(self, fleet):
	666	"""Callback for the fleet retrieval result."""
	667	if fleet is not None:
	668	gateList = ""
	669	occupiedGateNumbers = fleet.getOccupiedGateNumbers()
[619]	670	for gate in gates.lhbpGates.gates:
	671	if gate.isAvailable(gates.lhbpGates, occupiedGateNumbers):
[134]	672	if gateList: gateList += ", "
[619]	673	gateList += gate.number
[134]	674	fs.sendMessage(const.MESSAGETYPE_GATE_SYSTEM,
	675	"Free gates: " + gateList, 20)
[331]	676
[134]	677
[321]	678	def _logRadios(self, aircraftState):
	679	"""Log the radios from the given aircraft state."""
	680	flight = self._flight
	681	logger = flight.logger
	682
[366]	683	self._ilsLogger.forceLog(flight, logger, aircraftState)
[321]	684	self._nav1Logger.forceLog(flight, logger, aircraftState)
	685	self._nav2Logger.forceLog(flight, logger, aircraftState)
[329]	686	self._adf1Logger.forceLog(flight, logger, aircraftState)
	687	self._adf2Logger.forceLog(flight, logger, aircraftState)
[321]	688
[409]	689	def _logQNH(self, aircraftState):
	690	"""Log the current QNH along with the altimeter setting."""
	691	self.logger.message(aircraftState.timestamp,
	692	"QNH: %.2f hPa, altimeter: %.2f hPa" % \
	693	(aircraftState.qnh, aircraftState.altimeter))
	694
[369]	695	def _logNameAndModel(self, timestamp):
	696	"""Log the aircraft's name and model with taking the timestamp from the
	697	given state."""
	698	self._flight.logger.message(timestamp,
	699	"Aircraft: name='%s', model='%s'" % \
	700	(self._name, self._modelName))
	701
[4]	702	#---------------------------------------------------------------------------------------
[7]	703
	704	class Boeing737(Aircraft):
	705	"""Base class for the various aircraft in the Boeing 737 family.
	706
	707	The aircraft type-specific values in the aircraft state have the following
	708	structure:
[140]	709	- fuel: left, centre, right
[7]	710	- n1: left, right
[331]	711	- reverser: left, right"""
[592]	712	def __init__(self, flight, minLandingFuel = 2500,
	713	recommendedLandingFuel = 3500):
	714	super(Boeing737, self).__init__(flight,
	715	minLandingFuel = minLandingFuel,
	716	recommendedLandingFuel =
	717	recommendedLandingFuel)
[95]	718
[9]	719	self.gearSpeedLimit = 270
	720	self.flapSpeedLimits = { 1 : 260,
	721	2 : 260,
	722	5 : 250,
	723	10 : 210,
	724	15 : 200,
	725	25 : 190,
	726	30 : 175,
	727	40 : 162 }
[7]	728
[384]	729	@property
[512]	730	def derateType(self):
	731	"""Get the derate type for this type."""
	732	return DERATE_BOEING
[384]	733
[7]	734	#---------------------------------------------------------------------------------------
	735
	736	class B736(Boeing737):
	737	"""Boeing 737-600 aircraft."""
[861]	738	dow = 38307
	739
[8]	740	def __init__(self, flight):
	741	super(B736, self).__init__(flight)
[9]	742	self.mtow = 58328
	743	self.mlw = 54657
	744	self.mzfw = 51482
[611]	745	self.maxTakeOffPitch = 16.2
	746	self.maxTouchDownPitch = 14.7
[709]	747	self.simBriefData = SimBriefData(["250/280/78"],
	748	["CI", "M75", "M78", "M79", "M80", "LRC"],
	749	["78/280/250"])
[7]	750
	751	#---------------------------------------------------------------------------------------
	752
	753	class B737(Boeing737):
	754	"""Boeing 737-700 aircraft."""
[861]	755	dow = 39250
	756
[8]	757	def __init__(self, flight):
	758	super(B737, self).__init__(flight)
[9]	759	self.mtow = 61410
	760	self.mlw = 58059
	761	self.mzfw = 54657
[611]	762	self.maxTakeOffPitch = 14.7
	763	self.maxTouchDownPitch = 13.2
[709]	764	self.simBriefData = SimBriefData(["250/280/78"],
	765	["CI", "M75", "M78", "M79", "M80", "LRC"],
	766	["78/280/250", "78/250/250"])
[7]	767
	768	#---------------------------------------------------------------------------------------
	769
	770	class B738(Boeing737):
	771	"""Boeing 737-800 aircraft."""
[861]	772	dow = 42690
	773
[8]	774	def __init__(self, flight):
	775	super(B738, self).__init__(flight)
[797]	776	self.mtow = 71791
[9]	777	self.mlw = 65317
	778	self.mzfw = 61688
[611]	779	self.maxTakeOffPitch = 11
	780	self.maxTouchDownPitch = 9.5
[709]	781	self.simBriefData = SimBriefData(["250/280/78"],
	782	["CI", "M76", "M78", "M79", "M80", "LRC"],
	783	["78/280/250", "78/250/250"])
[9]	784
	785	#---------------------------------------------------------------------------------------
	786
	787	class B738Charter(B738):
	788	"""Boeing 737-800 aircraft used for charters."""
	789	def __init__(self, flight):
	790	super(B738Charter, self).__init__(flight)
	791	self.mtow = 77791
[709]	792	self.simBriefData = SimBriefData(["AUTO"],
	793	["280/M74"],
	794	["AUTO"])
[7]	795
	796	#---------------------------------------------------------------------------------------
	797
[591]	798	class Boeing737CL(Boeing737):
	799	"""Base class for the various aircraft in the Boeing 737 Classic family."""
	800	def __init__(self, flight):
[592]	801	super(Boeing737CL, self).__init__(flight, minLandingFuel = 3500,
	802	recommendedLandingFuel = None)
[591]	803
	804	#---------------------------------------------------------------------------------------
	805
[790]	806	class B732(Boeing737CL):
	807	"""Boeing 737-200 aircraft."""
[861]	808	dow = 27646
	809
[790]	810	def __init__(self, flight):
	811	super(B732, self).__init__(flight)
[796]	812	self.mtow = 52390
	813	self.mlw = 46720
	814	self.mzfw = 43091
	815	self.maxTakeOffPitch = 15.5
	816	self.maxTouchDownPitch = 15.5
[790]	817
	818	#---------------------------------------------------------------------------------------
	819
[591]	820	class B733(Boeing737CL):
[7]	821	"""Boeing 737-300 aircraft."""
[861]	822	dow = 32900
	823
[8]	824	def __init__(self, flight):
	825	super(B733, self).__init__(flight)
[797]	826	self.mtow = 56472
	827	self.mlw = 51710
	828	self.mzfw = 47625
[611]	829	self.maxTakeOffPitch = 13.4
	830	self.maxTouchDownPitch = 12.0
[7]	831
	832	#---------------------------------------------------------------------------------------
	833
[591]	834	class B734(Boeing737CL):
[7]	835	"""Boeing 737-400 aircraft."""
[898]	836	dow = 35100
	837
[8]	838	def __init__(self, flight):
	839	super(B734, self).__init__(flight)
[797]	840	self.mtow = 62822
	841	self.mlw = 54885
	842	self.mzfw = 51256
[611]	843	self.maxTakeOffPitch = 11.4
	844	self.maxTouchDownPitch = 10
[7]	845
	846	#---------------------------------------------------------------------------------------
	847
[591]	848	class B735(Boeing737CL):
[7]	849	"""Boeing 737-500 aircraft."""
[861]	850	dow = 31900
	851
[8]	852	def __init__(self, flight):
	853	super(B735, self).__init__(flight)
[797]	854	self.mtow = 62823
	855	self.mlw = 49895
	856	self.mzfw = 46720
[611]	857	self.maxTakeOffPitch = 14.7
	858	self.maxTouchDownPitch = 13.2
[7]	859
	860	#---------------------------------------------------------------------------------------
	861
	862	class DH8D(Aircraft):
	863	"""Bombardier Dash-8 Q400 aircraft.
	864
	865	The aircraft type-specific values in the aircraft state have the following
	866	structure:
[140]	867	- fuel: left, right
[7]	868	- n1: left, right
	869	- reverser: left, right."""
[861]	870	dow = 18508
[140]	871
[8]	872	def __init__(self, flight):
[591]	873	super(DH8D, self).__init__(flight, minLandingFuel = 2000)
[797]	874	self.mtow = 29574
	875	self.mlw = 28123
	876	self.mzfw = 26308
[9]	877	self.gearSpeedLimit = 215
	878	self.flapSpeedLimits = { 5 : 200,
	879	10 : 181,
	880	15 : 172,
	881	35 : 158 }
[611]	882	self.maxTakeOffPitch = 8.0
	883	self.maxTouchDownPitch = 7.0
[709]	884	self.simBriefData = SimBriefData(["I-900", "II-900", "III-900",
	885	"I-850", "II-850", "III-850"],
	886	["MCR", "ISC", "LRC", "HSC"],
	887	["I-850", "II-850", "III-850"])
[9]	888
[7]	889	#---------------------------------------------------------------------------------------
	890
	891	class Boeing767(Aircraft):
	892	"""Base class for the various aircraft in the Boeing 767 family.
	893
	894	The aircraft type-specific values in the aircraft state have the following
	895	structure:
[140]	896	- fuel: left, centre, right
[7]	897	- n1: left, right
	898	- reverser: left, right"""
[140]	899
[612]	900	def __init__(self, flight, minLandingFuel = 7000):
[591]	901	super(Boeing767, self).__init__(flight, minLandingFuel = minLandingFuel)
[9]	902	self.gearSpeedLimit = 270
	903	self.flapSpeedLimits = { 1 : 255,
	904	5 : 235,
	905	10 : 215,
	906	20 : 215,
	907	25 : 185,
	908	30 : 175 }
[7]	909
[384]	910	@property
[512]	911	def derateType(self):
	912	"""Get the derate type for this type."""
	913	return DERATE_BOEING
[384]	914
[7]	915	#---------------------------------------------------------------------------------------
	916
	917	class B762(Boeing767):
	918	"""Boeing 767-200 aircraft."""
[861]	919	dow = 84507
	920
[8]	921	def __init__(self, flight):
	922	super(B762, self).__init__(flight)
[797]	923	self.mtow = 159210
[9]	924	self.mlw = 126098
	925	self.mzfw = 114758
[611]	926	self.maxTakeOffPitch = 13.1
	927	self.maxTouchDownPitch = 11.6
[7]	928
	929	#---------------------------------------------------------------------------------------
	930
	931	class B763(Boeing767):
	932	"""Boeing 767-300 aircraft."""
[861]	933	dow = 91311
	934
[8]	935	def __init__(self, flight):
[331]	936	super(B763, self).__init__(flight)
[9]	937	self.mtow = 181436
	938	self.mlw = 137892
[797]	939	self.mzfw = 114758
[611]	940	self.maxTakeOffPitch = 9.6
	941	self.maxTouchDownPitch = 8.1
[709]	942	self.simBriefData = SimBriefData(["250/290/78"],
	943	["CI", "M76", "M78", "M80", "M82", "M84", "LRC"],
	944	["78/290/250"])
[7]	945
[799]	946	def setBookedFlight(self, bookedFlight):
	947	"""Update the aircraft based on the booked flight data (e.g. tail number)."""
	948	if bookedFlight.tailNumber=="HA-LHD":
	949	self.mtow = 159210
	950	self.mlw = 126098
	951
[7]	952	#---------------------------------------------------------------------------------------
	953
	954	class CRJ2(Aircraft):
	955	"""Bombardier CRJ-200 aircraft.
	956
	957	The aircraft type-specific values in the aircraft state have the following
	958	structure:
[140]	959	- fuel: left, centre, right
[7]	960	- n1: left, right
	961	- reverser: left, right."""
[861]	962	dow = 14549
	963
[8]	964	def __init__(self, flight):
[591]	965	super(CRJ2, self).__init__(flight, minLandingFuel = 1000)
[9]	966	self.mtow = 22995
	967	self.mlw = 21319
	968	self.mzfw = 19958
	969	self.gearSpeedLimit = 240
	970	self.flapSpeedLimits = { 8 : 260,
	971	20 : 220,
	972	30 : 190,
	973	45 : 175 }
[611]	974	self.maxTakeOffPitch = 18.0
	975	self.maxTouchDownPitch = 18.0
[709]	976	self.simBriefData = SimBriefData(["250/70", "290/74"],
	977	["CI", "LRC", "M70", "M72", "M74", "M77", "M80"],
	978	["74/290/250", "77/320/250"])
[7]	979
	980	#---------------------------------------------------------------------------------------
	981
	982	class F70(Aircraft):
	983	"""Fokker 70 aircraft.
	984
	985	The aircraft type-specific values in the aircraft state have the following
	986	structure:
[140]	987	- fuel: left, centre, right
[7]	988	- n1: left, right
	989	- reverser: left, right."""
[861]	990	dow = 24283
	991
[8]	992	def __init__(self, flight):
[591]	993	super(F70, self).__init__(flight, minLandingFuel = 1900)
[9]	994	self.mtow = 38100 # FIXME: differentiate by registration number,
	995	# MTOW of HA-LMF: 41955
	996	self.mlw = 36740
	997	self.mzfw = 32655
	998	self.gearSpeedLimit = 200
	999	self.flapSpeedLimits = { 8 : 250,
	1000	15 : 220,
	1001	25 : 220,
	1002	42 : 180 }
[360]	1003	self.reverseMinSpeed = 50
[611]	1004	self.maxTakeOffPitch = 16.0
	1005	self.maxTouchDownPitch = 16.0
[7]	1006
[384]	1007	@property
[512]	1008	def derateType(self):
	1009	"""Get the derate type for this type."""
	1010	return DERATE_EPR
[384]	1011
[7]	1012	#---------------------------------------------------------------------------------------
	1013
	1014	class DC3(Aircraft):
	1015	"""Lisunov Li-2 (DC-3) aircraft.
	1016
	1017	The aircraft type-specific values in the aircraft state have the following
	1018	structure:
[140]	1019	- fuel: left aux, left, right, right aux
[7]	1020	- rpm: left, right
	1021	- reverser: left, right."""
[861]	1022	dow = 8627
	1023
[8]	1024	def __init__(self, flight):
	1025	super(DC3, self).__init__(flight)
[9]	1026	self.mtow = 11884
	1027	self.mlw = 11793
	1028	self.mzfw = 11780
	1029	self.gearSpeedLimit = 148
	1030	self.flapSpeedLimits = { 15 : 135,
	1031	30 : 99,
	1032	45 : 97 }
[8]	1033
	1034	def _checkFlightEnd(self, aircraftState):
	1035	"""Check if the end of the flight has arrived.
	1036
	1037	This implementation checks the RPM values to be 0."""
	1038	for rpm in aircraftState.rpm:
[29]	1039	if rpm>0: return False
	1040	return True
[7]	1041
	1042	#---------------------------------------------------------------------------------------
	1043
	1044	class T134(Aircraft):
	1045	"""Tupolev Tu-134 aircraft.
	1046
	1047	The aircraft type-specific values in the aircraft state have the following
	1048	structure:
[140]	1049	- fuel: left tip, left aux, centre, right aux, right tip, external 1,
[7]	1050	external 2
	1051	- n1: left, right
	1052	- reverser: left, right."""
[861]	1053	dow = 29500
	1054
[8]	1055	def __init__(self, flight):
[591]	1056	super(T134, self).__init__(flight, minLandingFuel = 3000)
[210]	1057	self.mtow = 49000
[9]	1058	self.mlw = 43000
	1059	self.mzfw = 38500
	1060	self.gearSpeedLimit = 216
[210]	1061	self.flapSpeedLimits = { 10 : 450,
	1062	20 : 400,
	1063	30 : 300 }
[360]	1064	self.reverseMinSpeed = 50
[7]	1065
[644]	1066	self.hasStrobeLight = False
	1067
[611]	1068	self.maxTakeOffPitch = 16.0
	1069	self.maxTouchDownPitch = 16.0
	1070
[241]	1071	@property
[512]	1072	def derateType(self):
	1073	"""Get the derate type for this type."""
	1074	return DERATE_TUPOLEV
[384]	1075
	1076	@property
[241]	1077	def speedInKnots(self):
	1078	"""Indicate if the speed is in knots."""
	1079	return False
[331]	1080
[635]	1081	@property
	1082	def aglInFeet(self):
	1083	"""Indicate if AGL altituedes are in feet."""
	1084	return False
	1085
[211]	1086	def _appendLightsLoggers(self):
	1087	"""Append the loggers needed for the lights."""
	1088	self._checkers.append(checks.AnticollisionLightsLogger())
	1089	self._checkers.append(checks.LandingLightsLogger())
	1090	self._checkers.append(checks.NavLightsLogger())
	1091
	1092	def _appendLightsCheckers(self):
	1093	"""Append the checkers needed for the lights."""
	1094	self._checkers.append(checks.TupolevAntiCollisionLightsChecker())
[631]	1095	self._checkers.append(checks.TupolevLandingLightsChecker())
[211]	1096	self._checkers.append(checks.LandingLightsChecker())
	1097	self._checkers.append(checks.NavLightsChecker())
	1098
[7]	1099	#---------------------------------------------------------------------------------------
	1100
	1101	class T154(Aircraft):
	1102	"""Tupolev Tu-154 aircraft.
	1103
	1104	The aircraft type-specific values in the aircraft state have the following
	1105	structure:
[140]	1106	- fuel: left aux, left, centre, centre 2, right, right aux
[7]	1107	- n1: left, centre, right
	1108	- reverser: left, right"""
[888]	1109	dow = 53259
[861]	1110
[8]	1111	def __init__(self, flight):
[591]	1112	super(T154, self).__init__(flight, minLandingFuel = 5000)
[9]	1113	self.mtow = 98000
	1114	self.mlw = 78000
	1115	self.mzfw = 72000
	1116	self.gearSpeedLimit = 216
	1117	self.flapSpeedLimits = { 15 : 227,
	1118	28 : 194,
	1119	45 : 162 }
[360]	1120	self.reverseMinSpeed = 50
[9]	1121
[644]	1122	self.hasStrobeLight = False
	1123
[611]	1124	self.maxTakeOffPitch = 16.0
	1125	self.maxTouchDownPitch = 16.0
[709]	1126	self.simBriefData = SimBriefData(["AUTO"],
	1127	["300/M80"],
	1128	["AUTO"])
[611]	1129
[241]	1130	@property
	1131	def speedInKnots(self):
	1132	"""Indicate if the speed is in knots."""
	1133	return False
[331]	1134
[384]	1135	@property
[635]	1136	def aglInFeet(self):
	1137	"""Indicate if AGL altituedes are in feet."""
	1138	return False
	1139
	1140	@property
[512]	1141	def derateType(self):
	1142	"""Get the derate type for this type."""
	1143	return DERATE_TUPOLEV
[384]	1144
[799]	1145	def setBookedFlight(self, bookedFlight):
	1146	"""Update the aircraft based on the booked flight data (e.g. tail number)."""
	1147	if bookedFlight.tailNumber in ["HA-LCM", "HA-LCN", "HA-LCO", "HA-LCP",
	1148	"HA-LCR", "HA-LCU", "HA-LCV"]:
	1149	self.mtow = 100000
	1150	self.mlw = 80000
[904]	1151	elif bookedFlight.tailNumber=="HA-LCX":
	1152	self.mtow = 100000
	1153	self.mlw = 80000
	1154	self.mzfw = 74000
	1155
	1156	self.flapSpeedLimits = { 15 : 227,
	1157	28 : 194,
[905]	1158	36 : 178,
[904]	1159	45 : 162 }
[799]	1160
[211]	1161	def _appendLightsLoggers(self):
	1162	"""Append the loggers needed for the lights."""
	1163	self._checkers.append(checks.AnticollisionLightsLogger())
	1164	self._checkers.append(checks.LandingLightsLogger())
	1165	self._checkers.append(checks.NavLightsLogger())
	1166
	1167	def _appendLightsCheckers(self):
	1168	"""Append the checkers needed for the lights."""
	1169	self._checkers.append(checks.AntiCollisionLightsChecker())
[631]	1170	self._checkers.append(checks.TupolevLandingLightsChecker())
[211]	1171	self._checkers.append(checks.LandingLightsChecker())
	1172	self._checkers.append(checks.NavLightsChecker())
	1173
[539]	1174	#---------------------------------------------------------------------------------------
	1175
	1176	class YK40(Aircraft):
	1177	"""Yakovlev Yak-40 aircraft.
	1178
	1179	The aircraft type-specific values in the aircraft state have the following
	1180	structure:
	1181	- fuel: left, right
	1182	- n1: left, right
	1183	- reverser: left, right"""
[861]	1184	dow = 9400
	1185
[539]	1186	def __init__(self, flight):
	1187	super(YK40, self).__init__(flight)
	1188	self.mtow = 17200
	1189	self.mlw = 16800
	1190	self.mzfw = 12100
	1191	self.gearSpeedLimit = 165
	1192	self.flapSpeedLimits = { 20 : 165,
	1193	35 : 135 }
	1194
[644]	1195	self.hasStrobeLight = False
	1196
[539]	1197	@property
	1198	def speedInKnots(self):
	1199	"""Indicate if the speed is in knots."""
	1200	return False
	1201
	1202	@property
[635]	1203	def aglInFeet(self):
	1204	"""Indicate if AGL altituedes are in feet."""
	1205	return False
	1206
	1207	@property
[539]	1208	def derateType(self):
	1209	"""Get the derate type for this type."""
	1210	return DERATE_TUPOLEV
	1211
	1212	def _appendLightsLoggers(self):
	1213	"""Append the loggers needed for the lights."""
	1214	self._checkers.append(checks.AnticollisionLightsLogger())
	1215	self._checkers.append(checks.LandingLightsLogger())
	1216	self._checkers.append(checks.NavLightsLogger())
	1217
	1218	def _appendLightsCheckers(self):
	1219	"""Append the checkers needed for the lights."""
	1220	self._checkers.append(checks.AntiCollisionLightsChecker())
	1221	self._checkers.append(checks.LandingLightsChecker())
	1222	self._checkers.append(checks.NavLightsChecker())
[403]	1223
[7]	1224	#---------------------------------------------------------------------------------------
	1225
[443]	1226	class B462(Aircraft):
	1227	"""British Aerospace BAe-146 aircraft.
	1228
	1229	The aircraft type-specific values in the aircraft state have the following
	1230	structure:
	1231	- fuel: left, centre, right
	1232	- n1: left outer, left inner, right inner, right outer
	1233	- reverser: empty (the plane has no reversers)"""
[861]	1234	dow = 25706
	1235
[443]	1236	def __init__(self, flight):
	1237	super(B462, self).__init__(flight)
	1238	self.mtow = 43998
	1239	self.mlw = 38599
	1240	self.mzfw = 33792
	1241	self.gearSpeedLimit = 210
	1242	self.flapSpeedLimits = { 18 : 217,
	1243	24 : 180,
	1244	30 : 170,
	1245	33 : 150 }
	1246
[445]	1247	@property
[512]	1248	def derateType(self):
	1249	"""Get the derate type for this type."""
	1250	return DERATE_B462
[445]	1251
[443]	1252	#---------------------------------------------------------------------------------------
	1253
[895]	1254	class IL62(Aircraft):
	1255	"""Ilyushin IL-62 aircraft.
	1256
	1257	The aircraft type-specific values in the aircraft state have the following
	1258	structure:
	1259	- fuel: left, centre, right
	1260	- n1: left outer, left inner, right inner, right outer
	1261	- reverser: empty (the plane has no reversers)"""
	1262	dow = 69500
	1263
	1264	def __init__(self, flight):
	1265	super(B462, self).__init__(flight)
	1266	self.mtow = 165000
	1267	self.mlw = 165000
	1268	self.mzfw = 165000
	1269	self.gearSpeedLimit = 210
	1270	self.flapSpeedLimits = { 18 : 217,
	1271	24 : 180,
	1272	30 : 170,
	1273	33 : 150 }
	1274
	1275	@property
	1276	def derateType(self):
	1277	"""Get the derate type for this type."""
	1278	return DERATE_NONE
	1279
	1280	#---------------------------------------------------------------------------------------
	1281
[274]	1282	mostFuelTanks = [const.FUELTANK_LEFT_TIP, const.FUELTANK_EXTERNAL1,
	1283	const.FUELTANK_LEFT_AUX,
	1284	const.FUELTANK_CENTRE,
	1285	const.FUELTANK_RIGHT_AUX,
	1286	const.FUELTANK_EXTERNAL2, const.FUELTANK_RIGHT_TIP]
[141]	1287
	1288	#---------------------------------------------------------------------------------------
	1289
[191]	1290	_classes = { const.AIRCRAFT_B736 : B736,
	1291	const.AIRCRAFT_B737 : B737,
	1292	const.AIRCRAFT_B738 : B738,
	1293	const.AIRCRAFT_B738C : B738Charter,
[790]	1294	const.AIRCRAFT_B732 : B732,
[191]	1295	const.AIRCRAFT_B733 : B733,
	1296	const.AIRCRAFT_B734 : B734,
	1297	const.AIRCRAFT_B735 : B735,
	1298	const.AIRCRAFT_DH8D : DH8D,
	1299	const.AIRCRAFT_B762 : B762,
	1300	const.AIRCRAFT_B763 : B763,
	1301	const.AIRCRAFT_CRJ2 : CRJ2,
	1302	const.AIRCRAFT_F70 : F70,
	1303	const.AIRCRAFT_DC3 : DC3,
	1304	const.AIRCRAFT_T134 : T134,
	1305	const.AIRCRAFT_T154 : T154,
[443]	1306	const.AIRCRAFT_YK40 : YK40,
[895]	1307	const.AIRCRAFT_B462 : B462,
	1308	const.AIRCRAFT_IL62 : IL62 }
[8]	1309
	1310	#---------------------------------------------------------------------------------------
[197]	1311
[862]	1312	def getClass(aircraftType):
	1313	"""Get the class representing the given aircraft types"""
	1314	return _classes[aircraftType]
	1315
	1316	#---------------------------------------------------------------------------------------
	1317
[898]	1318	def setupTypes(aircraftTypes):
	1319	"""Setup the values in the given types using the info retrieved
	1320	from the server."""
	1321	for aircraftTypeInfo in aircraftTypes:
	1322	clazz = getClass(aircraftTypeInfo.aircraftType)
	1323
	1324	clazz.dow = aircraftTypeInfo.dow
	1325	clazz.dowCockpit = aircraftTypeInfo.dowCockpit
	1326	clazz.dowCabin = aircraftTypeInfo.dowCabin
	1327
	1328	#---------------------------------------------------------------------------------------
	1329
[197]	1330	if __name__ == "__main__":
	1331	value = SmoothedValue()
	1332
	1333	print "Adding 1, 12.0"
	1334	value.add(1, 12.0)
	1335	print value.get()
	1336
	1337	print "Adding 1, 15.0"
	1338	value.add(1, 15.0)
	1339	print value.get()
	1340
	1341	print "Adding 2, 18.0"
	1342	value.add(2, 18.0)
	1343	print value.get()
	1344
	1345	print "Adding 2, 20.0"
	1346	value.add(2, 20.0)
	1347	print value.get()
	1348
	1349	print "Adding 5, 22.0"
	1350	value.add(5, 22.0)
	1351	print value.get()
	1352
	1353	print "Adding 5, 25.0"
	1354	value.add(5, 25.0)
	1355	print value.get()
	1356
	1357	print "Adding 5, 29.0"
	1358	value.add(5, 29.0)
	1359	print value.get()
	1360
	1361	print "Adding 5, 21.0"
	1362	value.add(5, 21.0)
	1363	print value.get()
	1364
	1365	print "Adding 5, 26.0"
	1366	value.add(5, 26.0)
	1367	print value.get()
	1368
	1369	print "Adding 2, 30.0"
	1370	value.add(2, 30.0)
	1371	print value.get()
	1372
	1373	print "Adding 2, 55.0"
	1374	value.add(2, 55.0)
	1375	print value.get()
	1376
	1377	#---------------------------------------------------------------------------------------

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source: src/mlx/acft.py@ 917:803dc6bacfa5

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