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