source: src/mlx/acft.py@ 135:940d8d54f6d6

Last change on this file since 135:940d8d54f6d6 was 134:9ce031d5d4a9, checked in by István Váradi <ivaradi@…>, 13 years ago

Most of the remaining messages are implemented
File size: 28.3 KB
Line 
1# Module for the simulator-independent aircraft classes
2
3#---------------------------------------------------------------------------------------
4
5import const
6import checks
7import fs
8import util
9
10import time
11
12#---------------------------------------------------------------------------------------
13
14class Aircraft(object):
15 """Base class for aircraft."""
16 @staticmethod
17 def create(flight):
18 """Create an aircraft instance for the type in the given flight."""
19 return _classes[flight.aircraftType](flight)
20
21 def __init__(self, flight):
22 """Construct the aircraft for the given type."""
23 self._flight = flight
24 self._aircraftState = None
25
26 self._maxVS = -10000.0
27 self._minVS = 10000.0
28
29 self._v1r2LineIndex = None
30 self._vrefLineIndex = None
31
32 self.humanWeight = 82.0
33
34 self._checkers = []
35
36 # Loggers
37
38 self._checkers.append(checks.StageChecker())
39 self._checkers.append(checks.TakeOffLogger())
40
41 self._checkers.append(checks.AltimeterLogger())
42
43 self._checkers.append(checks.NAV1Logger())
44 self._checkers.append(checks.NAV2Logger())
45 self._checkers.append(checks.SquawkLogger())
46
47 self._checkers.append(checks.AnticollisionLightsLogger())
48 self._checkers.append(checks.LandingLightsLogger())
49 self._checkers.append(checks.StrobeLightsLogger())
50 self._checkers.append(checks.NavLightsLogger())
51
52 self._checkers.append(checks.FlapsLogger())
53
54 self._checkers.append(checks.GearsLogger())
55 self._checkers.append(checks.CruiseSpeedLogger())
56 self._checkers.append(checks.SpoilerLogger())
57
58 if flight.config.isMessageTypeFS(const.MESSAGETYPE_VISIBILITY):
59 self._checkers.append(checks.VisibilityChecker())
60
61 # Fault checkers
62
63 self._checkers.append(checks.AntiCollisionLightsChecker())
64 self._checkers.append(checks.LandingLightsChecker())
65 self._checkers.append(checks.NavLightsChecker())
66 self._checkers.append(checks.StrobeLightsChecker())
67
68 self._checkers.append(checks.BankChecker())
69
70 self._checkers.append(checks.FlapsRetractChecker())
71 self._checkers.append(checks.FlapsSpeedLimitChecker())
72
73 self._checkers.append(checks.GearsDownChecker())
74 self._checkers.append(checks.GearSpeedLimitChecker())
75
76 self._checkers.append(checks.GLoadChecker())
77
78 self._checkers.append(checks.MLWChecker())
79 self._checkers.append(checks.MTOWChecker())
80 self._checkers.append(checks.MZFWChecker())
81 self._checkers.append(checks.PayloadChecker())
82
83 self._checkers.append(checks.SpeedChecker())
84 self._checkers.append(checks.VSChecker())
85 self._checkers.append(checks.OverspeedChecker())
86 self._checkers.append(checks.StallChecker())
87
88 self._checkers.append(checks.PitotChecker())
89
90 self._checkers.append(checks.ReverserChecker())
91
92 @property
93 def type(self):
94 """Get the type of the aircraft."""
95 return self._flight.aircraftType
96
97 @property
98 def flight(self):
99 """Get the flight the aircraft belongs to."""
100 return self._flight
101
102 @property
103 def logger(self):
104 """Get the logger to use for the aircraft."""
105 return self._flight.logger
106
107 def getFlapsSpeedLimit(self, flaps):
108 """Get the speed limit for the given flaps setting."""
109 return self.flapSpeedLimits[flaps] if flaps in self.flapSpeedLimits \
110 else None
111
112 def modelChanged(self, timestamp, aircraftName, modelName):
113 """Called when the simulator's aircraft changes."""
114 self._flight.logger.message(timestamp,
115 "Aircraft: name='%s', model='%s'" % \
116 (aircraftName, modelName))
117
118 def handleState(self, aircraftState):
119 """Called when the state of the aircraft changes."""
120 for checker in self._checkers:
121 checker.check(self._flight, self, self._flight.logger,
122 self._aircraftState, aircraftState)
123
124 self._flight.handleState(self._aircraftState, aircraftState)
125
126 self._maxVS = max(self._maxVS, aircraftState.vs)
127 self._minVS = min(self._minVS, aircraftState.vs)
128
129 self._aircraftState = aircraftState
130
131 def setStage(self, aircraftState, newStage):
132 """Set the given stage as the new one and do whatever should be
133 done."""
134 if self._flight.setStage(aircraftState.timestamp, newStage):
135 if newStage==const.STAGE_PUSHANDTAXI:
136 self.logger.message(aircraftState.timestamp, "Block time start")
137 self.logFuel(aircraftState)
138 self.logger.message(aircraftState.timestamp,
139 "Zero-fuel weight: %.0f kg" % (aircraftState.zfw))
140 flight = self._flight
141 if flight.v1 is None or flight.vr is None or flight.v2 is None:
142 fs.sendMessage(const.MESSAGETYPE_HELP,
143 "Don't forget to set the takeoff V-speeds!",
144 5)
145 elif newStage==const.STAGE_TAKEOFF:
146 self.logger.message(aircraftState.timestamp, "Flight time start")
147 self.logger.message(aircraftState.timestamp,
148 "Takeoff weight: %.0f kg, MTOW: %.0f kg" % \
149 (aircraftState.grossWeight, self.mtow))
150 self.logger.message(aircraftState.timestamp,
151 "Wind %03.0f degrees at %.0f knots" % \
152 (aircraftState.windDirection,
153 aircraftState.windSpeed))
154 self._logV1R2()
155 elif newStage==const.STAGE_TAXIAFTERLAND:
156 bookedFlight = self._flight.bookedFlight
157 if bookedFlight.arrivalICAO=="LHBP" and \
158 self._flight.config.isMessageTypeFS(const.MESSAGETYPE_GATE_SYSTEM):
159 self._flight.getFleet(callback = self._fleetRetrieved,
160 force = True)
161 self.logger.message(aircraftState.timestamp, "Flight time end")
162 self.logFuel(aircraftState)
163 self.logger.message(aircraftState.timestamp,
164 "Landing weight: %.0f kg, MLW: %.0f" % \
165 (aircraftState.grossWeight, self.mlw))
166 self.logger.message(aircraftState.timestamp,
167 "Vertical speed range: %.0f..%.0f feet/min" % \
168 (self._minVS, self._maxVS))
169 elif newStage==const.STAGE_PARKING:
170 self.logger.message(aircraftState.timestamp, "Block time end")
171 elif newStage==const.STAGE_END:
172 flightLength = self._flight.flightTimeEnd - self._flight.flightTimeStart
173 self.logger.message(aircraftState.timestamp,
174 "Flight time: " +
175 util.getTimeIntervalString(flightLength))
176 self.logger.message(aircraftState.timestamp,
177 "Flown distance: %.2f NM" % \
178 (self._flight.flownDistance,))
179 blockLength = self._flight.blockTimeEnd - self._flight.blockTimeStart
180 self.logger.message(aircraftState.timestamp,
181 "Block time: " +
182 util.getTimeIntervalString(blockLength))
183 bookedFlight = self._flight.bookedFlight
184 # FIXME: translate the ICAO into an airport name
185 fs.sendMessage(const.MESSAGETYPE_ENVIRONMENT,
186 "Flight plan closed. Welcome to %s" % \
187 (bookedFlight.arrivalICAO,),
188 5)
189
190 def prepareFlare(self):
191 """Called when it is detected that we will soon flare.
192
193 On the first call, it should start monitoring some parameters more
194 closely to determine flare time."""
195 self.flight.simulator.startFlare()
196
197 def flareStarted(self, windSpeed, windDirection, visibility,
198 flareStart, flareStartFS):
199 """Called when the flare has started."""
200 self.logger.message(self._aircraftState.timestamp, "The flare has begun")
201 self.logger.message(self._aircraftState.timestamp,
202 "Wind %03.0f degrees at %.0f knots" % \
203 (windDirection, windSpeed))
204 self.logger.message(self._aircraftState.timestamp,
205 "Visibility: %.0f metres" % (visibility,))
206 self.logger.message(self._aircraftState.timestamp,
207 "Altimeter setting: %.0f hPa" % \
208 (self._aircraftState.altimeter,))
209 self._logVRef()
210 self.flight.flareStarted(flareStart, flareStartFS)
211 fs.sendMessage(const.MESSAGETYPE_INFORMATION, "Flare-time", 3)
212
213 def flareFinished(self, flareEnd, flareEndFS, tdRate, tdRateCalculatedByFS,
214 ias, pitch, bank, heading):
215 """Called when the flare has finished."""
216 (flareTimeFromFS, flareTime) = self.flight.flareFinished(flareEnd,
217 flareEndFS)
218 self.logger.message(self._aircraftState.timestamp,
219 "Flare time: %.1f s (from %s)" % \
220 (flareTime,
221 "the simulator" if flareTimeFromFS else "real time",))
222 self.logger.message(self._aircraftState.timestamp,
223 "Touchdown rate: %.0f feet/min" % (tdRate,))
224 self.logger.message(self._aircraftState.timestamp,
225 "Touchdown rate was calculated by the %s" % \
226 ("simulator" if tdRateCalculatedByFS else "logger",))
227 self.logger.message(self._aircraftState.timestamp,
228 "Touchdown speed: %.0f knots" % (ias,))
229 self.logger.message(self._aircraftState.timestamp,
230 "Touchdown pitch: %.1f degrees" % (pitch,))
231 self.logger.message(self._aircraftState.timestamp,
232 "Touchdown bank: %.1f degrees" % (bank,))
233 self.logger.message(self._aircraftState.timestamp,
234 "Touchdown heading: %03.0f degrees" % (heading,))
235
236 def cancelFlare(self):
237 """Cancel flare, if it has started."""
238 self.flight.simulator.cancelFlare()
239
240 def checkFlightEnd(self, aircraftState):
241 """Check if the end of the flight has arrived.
242
243 This default implementation checks the N1 values, but for
244 piston-powered aircraft you need to check the RPMs."""
245 for n1 in aircraftState.n1:
246 if n1>=0.5: return False
247 return True
248
249 def updateV1R2(self):
250 """Update the V1, Vr and V2 values from the flight, if the these values
251 have already been logged."""
252 if self._v1r2LineIndex is not None:
253 self._logV1R2()
254
255 def _logV1R2(self):
256 """Log the V1, Vr and V2 value either newly, or by updating the
257 corresponding line."""
258 message = "Speeds calculated by the pilot: V1: %s, VR: %s, V2: %s" % \
259 ("-" if self._flight.v1 is None
260 else str(self._flight.v1),
261 "-" if self._flight.vr is None
262 else str(self._flight.vr),
263 "-" if self._flight.v2 is None
264 else str(self._flight.v2))
265
266 if self._v1r2LineIndex is None:
267 self._v1r2LineIndex = \
268 self.logger.message(self._aircraftState.timestamp, message)
269 else:
270 self.logger.updateLine(self._v1r2LineIndex, message)
271
272 def updateVRef(self):
273 """Update the Vref value from the flight, if the Vref value has already
274 been logged."""
275 if self._vrefLineIndex is not None:
276 self._logVRef()
277
278 def _logVRef(self):
279 """Log the Vref value either newly, or by updating the corresponding
280 line."""
281 message = "VRef speed calculated by the pilot: %s" % \
282 ("-" if self._flight.vref is None else str(self._flight.vref))
283 if self._vrefLineIndex is None:
284 self._vrefLineIndex = \
285 self.logger.message(self._aircraftState.timestamp, message)
286 else:
287 self.logger.updateLine(self._vrefLineIndex, message)
288
289 def _fleetRetrieved(self, fleet):
290 """Callback for the fleet retrieval result."""
291 if fleet is not None:
292 gateList = ""
293 occupiedGateNumbers = fleet.getOccupiedGateNumbers()
294 for gateNumber in const.lhbpGateNumbers:
295 if gateNumber not in occupiedGateNumbers:
296 if gateList: gateList += ", "
297 gateList += gateNumber
298 fs.sendMessage(const.MESSAGETYPE_GATE_SYSTEM,
299 "Free gates: " + gateList, 20)
300
301
302#---------------------------------------------------------------------------------------
303
304class Boeing737(Aircraft):
305 """Base class for the various aircraft in the Boeing 737 family.
306
307 The aircraft type-specific values in the aircraft state have the following
308 structure:
309 - fuel: centre, left, right
310 - n1: left, right
311 - reverser: left, right"""
312 def __init__(self, flight):
313 super(Boeing737, self).__init__(flight)
314 self._checkers.append(checks.ThrustChecker())
315
316 self.gearSpeedLimit = 270
317 self.flapSpeedLimits = { 1 : 260,
318 2 : 260,
319 5 : 250,
320 10 : 210,
321 15 : 200,
322 25 : 190,
323 30 : 175,
324 40 : 162 }
325
326 def logFuel(self, aircraftState):
327 """Log the amount of fuel"""
328 self.logger.message(aircraftState.timestamp,
329 "Fuel: left=%.0f kg - centre=%.0f kg - right=%.0f kg" % \
330 (aircraftState.fuel[1], aircraftState.fuel[0],
331 aircraftState.fuel[2]))
332 self.logger.message(aircraftState.timestamp,
333 "Total fuel: %.0f kg" % (sum(aircraftState.fuel),))
334
335#---------------------------------------------------------------------------------------
336
337class B736(Boeing737):
338 """Boeing 737-600 aircraft."""
339 def __init__(self, flight):
340 super(B736, self).__init__(flight)
341 self.dow = 38307
342 self.mtow = 58328
343 self.mlw = 54657
344 self.mzfw = 51482
345
346#---------------------------------------------------------------------------------------
347
348class B737(Boeing737):
349 """Boeing 737-700 aircraft."""
350 def __init__(self, flight):
351 super(B737, self).__init__(flight)
352 self.dow = 39250
353 self.mtow = 61410
354 self.mlw = 58059
355 self.mzfw = 54657
356
357#---------------------------------------------------------------------------------------
358
359class B738(Boeing737):
360 """Boeing 737-800 aircraft."""
361 def __init__(self, flight):
362 super(B738, self).__init__(flight)
363 self.dow = 42690
364 self.mtow = 71709
365 self.mlw = 65317
366 self.mzfw = 61688
367
368#---------------------------------------------------------------------------------------
369
370class B738Charter(B738):
371 """Boeing 737-800 aircraft used for charters."""
372 def __init__(self, flight):
373 super(B738Charter, self).__init__(flight)
374 self.mtow = 77791
375
376#---------------------------------------------------------------------------------------
377
378class B733(Boeing737):
379 """Boeing 737-300 aircraft."""
380 def __init__(self, flight):
381 super(B733, self).__init__(flight)
382 self.dow = 32700
383 self.mtow = 62820
384 self.mlw = 51700
385 self.mzfw = 48410
386
387#---------------------------------------------------------------------------------------
388
389class B734(Boeing737):
390 """Boeing 737-400 aircraft."""
391 def __init__(self, flight):
392 super(B734, self).__init__(flight)
393 self.dow = 33200
394 self.mtow = 68050
395 self.mlw = 56200
396 self.mzfw = 53100
397
398#---------------------------------------------------------------------------------------
399
400class B735(Boeing737):
401 """Boeing 737-500 aircraft."""
402 def __init__(self, flight):
403 super(B735, self).__init__(flight)
404 self.dow = 31300
405 self.mtow = 60550
406 self.mlw = 50000
407 self.mzfw = 46700
408
409#---------------------------------------------------------------------------------------
410
411class DH8D(Aircraft):
412 """Bombardier Dash-8 Q400 aircraft.
413
414 The aircraft type-specific values in the aircraft state have the following
415 structure:
416 - fuel: centre, left, right
417 - n1: left, right
418 - reverser: left, right."""
419 def __init__(self, flight):
420 super(DH8D, self).__init__(flight)
421 self.dow = 17185
422 self.mtow = 29257
423 self.mlw = 28009
424 self.mzfw = 25855
425 self.gearSpeedLimit = 215
426 self.flapSpeedLimits = { 5 : 200,
427 10 : 181,
428 15 : 172,
429 35 : 158 }
430
431 def logFuel(self, aircraftState):
432 """Log the amount of fuel"""
433 self.logger.message(aircraftState.timestamp,
434 "Fuel: left=%.0f kg - centre=%.0f kg - right=%.0f kg" % \
435 (aircraftState.fuel[1], aircraftState.fuel[0],
436 aircraftState.fuel[2]))
437 self.logger.message(aircraftState.timestamp,
438 "Total fuel: %.0f kg" % (sum(aircraftState.fuel),))
439
440#---------------------------------------------------------------------------------------
441
442class Boeing767(Aircraft):
443 """Base class for the various aircraft in the Boeing 767 family.
444
445 The aircraft type-specific values in the aircraft state have the following
446 structure:
447 - fuel: centre, left, right
448 - n1: left, right
449 - reverser: left, right"""
450 def __init__(self, flight):
451 super(Boeing767, self).__init__(flight)
452 self._checkers.append(checks.ThrustChecker())
453 self.gearSpeedLimit = 270
454 self.flapSpeedLimits = { 1 : 255,
455 5 : 235,
456 10 : 215,
457 20 : 215,
458 25 : 185,
459 30 : 175 }
460
461 def logFuel(self, aircraftState):
462 """Log the amount of fuel"""
463 self.logger.message(aircraftState.timestamp,
464 "Fuel: left=%.0f kg - centre=%.0f kg - right=%.0f kg" % \
465 (aircraftState.fuel[1], aircraftState.fuel[0],
466 aircraftState.fuel[2]))
467 self.logger.message(aircraftState.timestamp,
468 "Total fuel: %.0f kg" % (sum(aircraftState.fuel),))
469
470#---------------------------------------------------------------------------------------
471
472class B762(Boeing767):
473 """Boeing 767-200 aircraft."""
474 def __init__(self, flight):
475 super(B762, self).__init__(flight)
476 self.dow = 84507
477 self.mtow = 175540
478 self.mlw = 126098
479 self.mzfw = 114758
480
481#---------------------------------------------------------------------------------------
482
483class B763(Boeing767):
484 """Boeing 767-300 aircraft."""
485 def __init__(self, flight):
486 super(B763, self).__init__(cflight)
487 self.dow = 91311
488 self.mtow = 181436
489 self.mlw = 137892
490 self.mzfw = 130635
491
492#---------------------------------------------------------------------------------------
493
494class CRJ2(Aircraft):
495 """Bombardier CRJ-200 aircraft.
496
497 The aircraft type-specific values in the aircraft state have the following
498 structure:
499 - fuel: centre, left, right
500 - n1: left, right
501 - reverser: left, right."""
502 def __init__(self, flight):
503 super(CRJ2, self).__init__(flight)
504 self._checkers.append(checks.ThrustChecker())
505 self.dow = 14549
506 self.mtow = 22995
507 self.mlw = 21319
508 self.mzfw = 19958
509 self.gearSpeedLimit = 240
510 self.flapSpeedLimits = { 8 : 260,
511 20 : 220,
512 30 : 190,
513 45 : 175 }
514
515 def logFuel(self, aircraftState):
516 """Log the amount of fuel"""
517 self.logger.message(aircraftState.timestamp,
518 "Fuel: left=%.0f kg - centre=%.0f kg - right=%.0f kg" % \
519 (aircraftState.fuel[1], aircraftState.fuel[0],
520 aircraftState.fuel[2]))
521 self.logger.message(aircraftState.timestamp,
522 "Total fuel: %.0f kg" % (sum(aircraftState.fuel),))
523
524#---------------------------------------------------------------------------------------
525
526class F70(Aircraft):
527 """Fokker 70 aircraft.
528
529 The aircraft type-specific values in the aircraft state have the following
530 structure:
531 - fuel: centre, left, right
532 - n1: left, right
533 - reverser: left, right."""
534 def __init__(self, flight):
535 super(F70, self).__init__(flight)
536 self._checkers.append(checks.ThrustChecker())
537 self.dow = 24283
538 self.mtow = 38100 # FIXME: differentiate by registration number,
539 # MTOW of HA-LMF: 41955
540 self.mlw = 36740
541 self.mzfw = 32655
542 self.gearSpeedLimit = 200
543 self.flapSpeedLimits = { 8 : 250,
544 15 : 220,
545 25 : 220,
546 42 : 180 }
547
548 def logFuel(self, aircraftState):
549 """Log the amount of fuel"""
550 self.logger.message(aircraftState.timestamp,
551 "Fuel: left=%.0f kg - centre=%.0f kg - right=%.0f kg" % \
552 (aircraftState.fuel[1], aircraftState.fuel[0],
553 aircraftState.fuel[2]))
554 self.logger.message(aircraftState.timestamp,
555 "Total fuel: %.0f kg" % (sum(aircraftState.fuel),))
556
557#---------------------------------------------------------------------------------------
558
559class DC3(Aircraft):
560 """Lisunov Li-2 (DC-3) aircraft.
561
562 The aircraft type-specific values in the aircraft state have the following
563 structure:
564 - fuel: left, right, left aux, right aux
565 - rpm: left, right
566 - reverser: left, right."""
567 def __init__(self, flight):
568 super(DC3, self).__init__(flight)
569 self.dow = 8627
570 self.mtow = 11884
571 self.mlw = 11793
572 self.mzfw = 11780
573 self.gearSpeedLimit = 148
574 self.flapSpeedLimits = { 15 : 135,
575 30 : 99,
576 45 : 97 }
577
578 def _checkFlightEnd(self, aircraftState):
579 """Check if the end of the flight has arrived.
580
581 This implementation checks the RPM values to be 0."""
582 for rpm in aircraftState.rpm:
583 if rpm>0: return False
584 return True
585
586 def logFuel(self, aircraftState):
587 """Log the amount of fuel"""
588 self.logger.message(aircraftState.timestamp,
589 "Fuel: left aux=%.0f kg - left=%.0f kg - right=%.0f kg - right aux=%.0f kg" % \
590 (aircraftState.fuel[2], aircraftState.fuel[0],
591 aircraftState.fuel[1], aircraftState.fuel[3]))
592 self.logger.message(aircraftState.timestamp,
593 "Total fuel: %.0f kg" % (sum(aircraftState.fuel),))
594
595#---------------------------------------------------------------------------------------
596
597class T134(Aircraft):
598 """Tupolev Tu-134 aircraft.
599
600 The aircraft type-specific values in the aircraft state have the following
601 structure:
602 - fuel: centre, left tip, left aux, right tip, right aux, external 1,
603 external 2
604 - n1: left, right
605 - reverser: left, right."""
606 def __init__(self, flight):
607 super(T134, self).__init__(flight)
608 self._checkers.append(checks.ThrustChecker())
609 self.dow = 29927
610 self.mtow = 47600
611 self.mlw = 43000
612 self.mzfw = 38500
613 self.gearSpeedLimit = 216
614 self.flapSpeedLimits = { 10 : 240,
615 20 : 216,
616 30 : 161 }
617
618 def logFuel(self, aircraftState):
619 """Log the amount of fuel"""
620 self.logger.message(aircraftState.timestamp,
621 "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" % \
622 (aircraftState.fuel[2], aircraftState.fuel[1],
623 aircraftState.fuel[0],
624 aircraftState.fuel[3], aircraftState.fuel[4],
625 aircraftState.fuel[5], aircraftState.fuel[6]))
626 self.logger.message(aircraftState.timestamp,
627 "Total fuel: %.0f kg" % (sum(aircraftState.fuel),))
628
629#---------------------------------------------------------------------------------------
630
631class T154(Aircraft):
632 """Tupolev Tu-154 aircraft.
633
634 The aircraft type-specific values in the aircraft state have the following
635 structure:
636 - fuel: centre, left, right, centre 2, left aux, right aux
637 - n1: left, centre, right
638 - reverser: left, right"""
639 def __init__(self, flight):
640 super(T154, self).__init__(flight)
641 self._checkers.append(checks.ThrustChecker())
642 self.dow = 53259
643 self.mtow = 98000
644 self.mlw = 78000
645 self.mzfw = 72000
646 self.gearSpeedLimit = 216
647 self.flapSpeedLimits = { 15 : 227,
648 28 : 194,
649 45 : 162 }
650
651 def logFuel(self, aircraftState):
652 """Log the amount of fuel"""
653 self.logger.message(aircraftState.timestamp,
654 "Fuel: left aux=%.0f kg - left=%.0f kg - centre=%.0f kg - centre 2=%.0f kg - right=%.0f kg - right aux=%.0f kg" % \
655 (aircraftState.fuel[4], aircraftState.fuel[1],
656 aircraftState.fuel[0], aircraftState.fuel[3],
657 aircraftState.fuel[2], aircraftState.fuel[5]))
658 self.logger.message(aircraftState.timestamp,
659 "Total fuel: %.0f kg" % (sum(aircraftState.fuel),))
660
661#---------------------------------------------------------------------------------------
662
663
664class YK40(Aircraft):
665 """Yakovlev Yak-40 aircraft.
666
667 The aircraft type-specific values in the aircraft state have the following
668 structure:
669 - fuel: left, right
670 - n1: left, right
671 - reverser: left, right"""
672 def __init__(self, flight):
673 super(YK40, self).__init__(flight)
674 self._checkers.append(checks.ThrustChecker())
675 self.dow = 9400
676 self.mtow = 17200
677 self.mlw = 16800
678 self.mzfw = 12100
679 self.gearSpeedLimit = 165
680 self.flapSpeedLimits = { 20 : 165,
681 35 : 135 }
682
683 def logFuel(self, aircraftState):
684 """Log the amount of fuel"""
685 self.logger.message(aircraftState.timestamp,
686 "Fuel: left=%.0f kg - right=%.0f kg" % \
687 (aircraftState.fuel[0], aircraftState.fuel[1]))
688 self.logger.message(aircraftState.timestamp,
689 "Total fuel: %.0f kg" % (sum(aircraftState.fuel),))
690
691#---------------------------------------------------------------------------------------
692
693_classes = { const.AIRCRAFT_B736 : B736,
694 const.AIRCRAFT_B737 : B737,
695 const.AIRCRAFT_B738 : B738,
696 const.AIRCRAFT_B733 : B733,
697 const.AIRCRAFT_B734 : B734,
698 const.AIRCRAFT_B735 : B735,
699 const.AIRCRAFT_DH8D : DH8D,
700 const.AIRCRAFT_B762 : B762,
701 const.AIRCRAFT_B763 : B763,
702 const.AIRCRAFT_CRJ2 : CRJ2,
703 const.AIRCRAFT_F70 : F70,
704 const.AIRCRAFT_DC3 : DC3,
705 const.AIRCRAFT_T134 : T134,
706 const.AIRCRAFT_T154 : T154,
707 const.AIRCRAFT_YK40 : YK40 }
708
709#---------------------------------------------------------------------------------------
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