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 | from collections import deque
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15 |
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16 | #---------------------------------------------------------------------------------------
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17 |
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18 | class SmoothedValue(object):
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19 | """A smoothed value."""
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20 | def __init__(self):
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21 | """Construct the value."""
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22 | self._deque = deque()
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23 | self._sum = 0
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24 |
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25 | def add(self, length, value):
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26 | """Add the given value and smooth with the given length."""
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27 | dequeLength = len(self._deque)
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28 | while dequeLength>=length:
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29 | self._sum -= self._deque.popleft()
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30 | dequeLength -= 1
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31 |
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32 | self._sum += value
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33 | self._deque.append(value)
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34 |
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35 | def get(self):
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36 | """Get the average."""
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37 | return self._sum / len(self._deque)
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38 |
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39 | #---------------------------------------------------------------------------------------
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40 |
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41 | class Aircraft(object):
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42 | """Base class for aircraft."""
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43 | @staticmethod
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44 | def create(flight):
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45 | """Create an aircraft instance for the type in the given flight."""
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46 | return _classes[flight.aircraftType](flight)
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47 |
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48 | def __init__(self, flight):
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49 | """Construct the aircraft for the given type."""
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50 | self._flight = flight
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51 | self._aircraftState = None
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52 |
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53 | self._maxVS = -10000.0
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54 | self._minVS = 10000.0
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55 |
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56 | self._v1r2LineIndex = None
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57 | self._vrefLineIndex = None
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58 |
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59 | self.humanWeight = 82.0
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60 |
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61 | self._checkers = []
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62 |
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63 | config = flight.config
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64 | # Loggers
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65 |
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66 | self._checkers.append(checks.StageChecker())
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67 | self._checkers.append(checks.TakeOffLogger())
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68 |
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69 | self._checkers.append(checks.AltimeterLogger())
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70 |
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71 | self._checkers.append(checks.NAV1Logger())
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72 | self._checkers.append(checks.NAV2Logger())
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73 | self._checkers.append(checks.SquawkLogger())
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74 |
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75 | self._appendLightsLoggers()
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76 |
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77 | self._checkers.append(checks.FlapsLogger())
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78 |
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79 | self._checkers.append(checks.GearsLogger())
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80 | self._checkers.append(checks.CruiseSpeedLogger())
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81 | self._checkers.append(checks.SpoilerLogger())
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82 |
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83 | if config.isMessageTypeFS(const.MESSAGETYPE_VISIBILITY):
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84 | self._checkers.append(checks.VisibilityChecker())
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85 |
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86 | # FIXME: we should have a central data model object, and not collect
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87 | # the data from the GUI. However, some pieces of data (e.g. V-speeds,
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88 | # etc. that is entered into the GUI) *should* be a part of the GUI and
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89 | # queried from it, so the model should have a reference to the GUI as
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90 | # well and access such data via the GUI!
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91 | if config.onlineACARS and flight.loggedIn and not flight.entranceExam:
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92 | self._checkers.append(checks.ACARSSender(flight._gui))
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93 |
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94 | # Fault checkers
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95 |
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96 | self._appendLightsCheckers()
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97 |
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98 | self._checkers.append(checks.BankChecker())
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99 |
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100 | self._checkers.append(checks.FlapsRetractChecker())
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101 | self._checkers.append(checks.FlapsSpeedLimitChecker())
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102 |
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103 | self._checkers.append(checks.GearsDownChecker())
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104 | self._checkers.append(checks.GearSpeedLimitChecker())
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105 |
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106 | self._checkers.append(checks.GLoadChecker())
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107 |
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108 | self._checkers.append(checks.MLWChecker())
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109 | self._checkers.append(checks.MTOWChecker())
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110 | self._checkers.append(checks.MZFWChecker())
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111 | self._checkers.append(checks.PayloadChecker())
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112 |
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113 | self._checkers.append(checks.SpeedChecker())
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114 | self._checkers.append(checks.VSChecker())
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115 |
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116 | timeout = 5.0 + config.realIASSmoothingLength - 1
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117 | self._checkers.append(checks.OverspeedChecker(timeout = timeout))
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118 |
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119 | self._checkers.append(checks.StallChecker())
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120 |
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121 | self._checkers.append(checks.PitotChecker())
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122 |
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123 | self._checkers.append(checks.ReverserChecker())
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124 |
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125 | self._smoothedIAS = SmoothedValue()
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126 | self._smoothedVS = SmoothedValue()
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127 |
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128 | @property
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129 | def type(self):
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130 | """Get the type of the aircraft."""
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131 | return self._flight.aircraftType
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132 |
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133 | @property
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134 | def flight(self):
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135 | """Get the flight the aircraft belongs to."""
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136 | return self._flight
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137 |
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138 | @property
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139 | def logger(self):
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140 | """Get the logger to use for the aircraft."""
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141 | return self._flight.logger
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142 |
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143 | @property
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144 | def state(self):
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145 | """Get the current aircraft state."""
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146 | return self._aircraftState
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147 |
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148 | @property
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149 | def speedInKnots(self):
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150 | """Indicate if the speed is in knots.
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151 |
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152 | This default implementation returns True."""
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153 | return True
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154 |
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155 | def getFlapsSpeedLimit(self, flaps):
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156 | """Get the speed limit for the given flaps setting."""
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157 | return self.flapSpeedLimits[flaps] if flaps in self.flapSpeedLimits \
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158 | else None
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159 |
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160 | def modelChanged(self, timestamp, aircraftName, modelName):
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161 | """Called when the simulator's aircraft changes."""
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162 | self._flight.logger.message(timestamp,
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163 | "Aircraft: name='%s', model='%s'" % \
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164 | (aircraftName, modelName))
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165 |
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166 | def handleState(self, aircraftState):
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167 | """Called when the state of the aircraft changes.
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168 |
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169 | This is the function that the simulator calls directly with the new
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170 | state."""
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171 | config = self._flight.config
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172 |
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173 | self._smoothedIAS.add(config.realIASSmoothingLength, aircraftState.ias)
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174 | aircraftState.smoothedIAS = self._smoothedIAS.get()
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175 |
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176 | self._smoothedVS.add(config.realVSSmoothingLength, aircraftState.vs)
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177 | aircraftState.smoothedVS = self._smoothedVS.get()
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178 |
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179 | for checker in self._checkers:
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180 | try:
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181 | checker.check(self._flight, self, self._flight.logger,
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182 | self._aircraftState, aircraftState)
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183 | except:
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184 | print >> sys.stderr, "Checker", checker, "failed"
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185 | traceback.print_exc()
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186 |
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187 | self._flight.handleState(self._aircraftState, aircraftState)
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188 |
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189 | self._maxVS = max(self._maxVS, aircraftState.vs)
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190 | self._minVS = min(self._minVS, aircraftState.vs)
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191 |
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192 | self._aircraftState = aircraftState
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193 |
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194 | def setStage(self, aircraftState, newStage):
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195 | """Set the given stage as the new one and do whatever should be
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196 | done."""
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197 | if self._flight.setStage(aircraftState.timestamp, newStage):
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198 | if newStage==const.STAGE_PUSHANDTAXI:
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199 | self.logger.message(aircraftState.timestamp, "Block time start")
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200 | self.logFuel(aircraftState)
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201 | self.logger.message(aircraftState.timestamp,
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202 | "Zero-fuel weight: %.0f kg" % (aircraftState.zfw))
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203 | flight = self._flight
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204 | if flight.v1 is None or flight.vr is None or flight.v2 is None:
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205 | fs.sendMessage(const.MESSAGETYPE_HELP,
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206 | "Don't forget to set the takeoff V-speeds!",
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207 | 5)
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208 | elif newStage==const.STAGE_TAKEOFF:
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209 | self.logger.message(aircraftState.timestamp,
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210 | "Flight time start")
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211 | self.logger.message(aircraftState.timestamp,
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212 | "Takeoff weight: %.0f kg, MTOW: %.0f kg" % \
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213 | (aircraftState.grossWeight, self.mtow))
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214 | self.logger.message(aircraftState.timestamp,
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215 | "Wind %03.0f degrees at %.0f knots" % \
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216 | (aircraftState.windDirection,
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217 | aircraftState.windSpeed))
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218 | self._logV1R2()
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219 | elif newStage==const.STAGE_TAXIAFTERLAND:
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220 | flight = self._flight
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221 | bookedFlight = flight.bookedFlight
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222 | config = flight.config
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223 | if config.onlineGateSystem and \
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224 | flight.loggedIn and \
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225 | not flight.entranceExam and \
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226 | bookedFlight.arrivalICAO=="LHBP" and \
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227 | config.isMessageTypeFS(const.MESSAGETYPE_GATE_SYSTEM):
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228 | self._flight.getFleet(callback = self._fleetRetrieved,
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229 | force = True)
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230 | self.logger.message(aircraftState.timestamp, "Flight time end")
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231 | self.logFuel(aircraftState)
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232 | self.logger.message(aircraftState.timestamp,
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233 | "Landing weight: %.0f kg, MLW: %.0f" % \
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234 | (aircraftState.grossWeight, self.mlw))
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235 | self.logger.message(aircraftState.timestamp,
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236 | "Vertical speed range: %.0f..%.0f feet/min" % \
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237 | (self._minVS, self._maxVS))
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238 | elif newStage==const.STAGE_PARKING:
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239 | self.logger.message(aircraftState.timestamp, "Block time end")
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240 | elif newStage==const.STAGE_END:
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241 | flightLength = self._flight.flightTimeEnd - self._flight.flightTimeStart
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242 | self.logger.message(aircraftState.timestamp,
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243 | "Flight time: " +
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244 | util.getTimeIntervalString(flightLength))
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245 | self.logger.message(aircraftState.timestamp,
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246 | "Flown distance: %.2f NM" % \
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247 | (self._flight.flownDistance,))
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248 | blockLength = self._flight.blockTimeEnd - self._flight.blockTimeStart
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249 | self.logger.message(aircraftState.timestamp,
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250 | "Block time: " +
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251 | util.getTimeIntervalString(blockLength))
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252 |
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253 | def prepareFlare(self):
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254 | """Called when it is detected that we will soon flare.
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255 |
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256 | On the first call, it should start monitoring some parameters more
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257 | closely to determine flare time."""
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258 | self.flight.simulator.startFlare()
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259 |
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260 | def flareStarted(self, windSpeed, windDirection, visibility,
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261 | flareStart, flareStartFS):
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262 | """Called when the flare has started."""
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263 | self.logger.message(self._aircraftState.timestamp, "The flare has begun")
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264 | self.logger.message(self._aircraftState.timestamp,
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265 | "Wind %03.0f degrees at %.0f knots" % \
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266 | (windDirection, windSpeed))
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267 | self.logger.message(self._aircraftState.timestamp,
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268 | "Visibility: %.0f metres" % (visibility,))
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269 | self.logger.message(self._aircraftState.timestamp,
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270 | "Altimeter setting: %.0f hPa" % \
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271 | (self._aircraftState.altimeter,))
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272 | self._logVRef()
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273 | self.flight.flareStarted(flareStart, flareStartFS)
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274 | fs.sendMessage(const.MESSAGETYPE_INFORMATION, "Flare-time", 3)
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275 |
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276 | def flareFinished(self, flareEnd, flareEndFS, tdRate, tdRateCalculatedByFS,
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277 | ias, pitch, bank, heading):
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278 | """Called when the flare has finished."""
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279 | (flareTimeFromFS, flareTime) = self.flight.flareFinished(flareEnd,
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280 | flareEndFS,
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281 | tdRate)
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282 | self.logger.message(self._aircraftState.timestamp,
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283 | "Flaretime: %.3f (from %s)" % \
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284 | (flareTime,
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285 | "the simulator" if flareTimeFromFS else "real time",))
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286 | self.logger.message(self._aircraftState.timestamp,
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287 | "Touchdown rate: %.0f feet/min" % (tdRate,))
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288 | self.logger.message(self._aircraftState.timestamp,
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289 | "Touchdown rate was calculated by the %s" % \
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290 | ("simulator" if tdRateCalculatedByFS else "logger",))
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291 | flight = self._flight
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292 | self.logger.message(self._aircraftState.timestamp,
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293 | "Touchdown speed: %.0f %s" % \
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294 | (flight.speedFromKnots(ias),
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295 | flight.getEnglishSpeedUnit()))
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296 | self.logger.message(self._aircraftState.timestamp,
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297 | "Touchdown pitch: %.1f degrees" % (pitch,))
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298 | self.logger.message(self._aircraftState.timestamp,
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299 | "Touchdown bank: %.1f degrees" % (bank,))
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300 | self.logger.message(self._aircraftState.timestamp,
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301 | "Touchdown heading: %03.0f degrees" % (heading,))
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302 | self.logger.message(self._aircraftState.timestamp,
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303 | "Centre of gravity: %.03f" % \
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304 | (self._aircraftState.cog,))
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305 |
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306 | def cancelFlare(self):
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307 | """Cancel flare, if it has started."""
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308 | self.flight.simulator.cancelFlare()
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309 |
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310 | def checkFlightEnd(self, aircraftState):
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311 | """Check if the end of the flight has arrived.
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312 |
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313 | This default implementation checks the N1 values, but for
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314 | piston-powered aircraft you need to check the RPMs."""
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315 | for n1 in aircraftState.n1:
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316 | if n1>=0.5: return False
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317 | return True
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318 |
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319 | def updateV1R2(self):
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320 | """Update the V1, Vr and V2 values from the flight, if the these values
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321 | have already been logged."""
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322 | if self._v1r2LineIndex is not None:
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323 | self._logV1R2()
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324 |
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325 | def _appendLightsLoggers(self):
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326 | """Append the loggers needed for the lights.
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327 |
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328 | This default implementation adds the loggers for the anti-collision
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329 | lights, the landing lights, the strobe lights and the NAV lights."""
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330 | self._checkers.append(checks.AnticollisionLightsLogger())
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331 | self._checkers.append(checks.LandingLightsLogger())
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332 | self._checkers.append(checks.StrobeLightsLogger())
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333 | self._checkers.append(checks.NavLightsLogger())
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334 |
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335 | def _appendLightsCheckers(self):
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336 | """Append the checkers needed for the lights.
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337 |
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338 | This default implementation adds the checkers for the anti-collision
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339 | lights, the landing lights, the strobe lights and the NAV lights."""
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340 | self._checkers.append(checks.AntiCollisionLightsChecker())
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341 | self._checkers.append(checks.LandingLightsChecker())
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342 | self._checkers.append(checks.NavLightsChecker())
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343 | self._checkers.append(checks.StrobeLightsChecker())
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344 |
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345 | def _speedToLog(self, speed):
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346 | """Convert the given speed (being either None or expressed in the
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347 | flight's speed unit into a string."""
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348 | if speed is None:
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349 | return "-"
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350 | else:
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351 | return str(speed) + " " + self._flight.getEnglishSpeedUnit()
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352 |
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353 | def _logV1R2(self):
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354 | """Log the V1, Vr and V2 value either newly, or by updating the
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355 | corresponding line."""
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356 | message = "Speeds calculated by the pilot: V1: %s, VR: %s, V2: %s" % \
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357 | (self._speedToLog(self._flight.v1),
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358 | self._speedToLog(self._flight.vr),
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359 | self._speedToLog(self._flight.v2))
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360 |
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361 | if self._v1r2LineIndex is None:
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362 | self._v1r2LineIndex = \
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363 | self.logger.message(self._aircraftState.timestamp, message)
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364 | else:
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365 | self.logger.updateLine(self._v1r2LineIndex, message)
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366 |
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367 | def updateVRef(self):
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368 | """Update the Vref value from the flight, if the Vref value has already
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369 | been logged."""
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370 | if self._vrefLineIndex is not None:
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371 | self._logVRef()
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372 |
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373 | def _logVRef(self):
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374 | """Log the Vref value either newly, or by updating the corresponding
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375 | line."""
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376 | message = "VRef speed calculated by the pilot: %s" % \
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377 | (self._speedToLog(self._flight.vref),)
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378 | if self._vrefLineIndex is None:
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379 | self._vrefLineIndex = \
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380 | self.logger.message(self._aircraftState.timestamp, message)
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381 | else:
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382 | self.logger.updateLine(self._vrefLineIndex, message)
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383 |
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384 | def _fleetRetrieved(self, fleet):
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385 | """Callback for the fleet retrieval result."""
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386 | if fleet is not None:
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387 | gateList = ""
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388 | occupiedGateNumbers = fleet.getOccupiedGateNumbers()
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389 | for gateNumber in const.lhbpGateNumbers:
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390 | if gateNumber not in occupiedGateNumbers:
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391 | if gateList: gateList += ", "
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392 | gateList += gateNumber
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393 | fs.sendMessage(const.MESSAGETYPE_GATE_SYSTEM,
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394 | "Free gates: " + gateList, 20)
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395 |
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396 |
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397 | #---------------------------------------------------------------------------------------
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398 |
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399 | class Boeing737(Aircraft):
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400 | """Base class for the various aircraft in the Boeing 737 family.
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401 |
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402 | The aircraft type-specific values in the aircraft state have the following
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403 | structure:
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404 | - fuel: left, centre, right
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405 | - n1: left, right
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406 | - reverser: left, right"""
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407 | fuelTanks = [const.FUELTANK_LEFT, const.FUELTANK_CENTRE, const.FUELTANK_RIGHT]
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408 |
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409 | def __init__(self, flight):
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410 | super(Boeing737, self).__init__(flight)
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411 | self._checkers.append(checks.ThrustChecker())
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412 |
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413 | self.gearSpeedLimit = 270
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414 | self.flapSpeedLimits = { 1 : 260,
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415 | 2 : 260,
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416 | 5 : 250,
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417 | 10 : 210,
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418 | 15 : 200,
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419 | 25 : 190,
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420 | 30 : 175,
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421 | 40 : 162 }
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422 |
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423 | def logFuel(self, aircraftState):
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424 | """Log the amount of fuel"""
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425 | self.logger.message(aircraftState.timestamp,
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426 | "Fuel: left=%.0f kg - centre=%.0f kg - right=%.0f kg" % \
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427 | (aircraftState.fuel[0], aircraftState.fuel[1],
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428 | aircraftState.fuel[2]))
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429 | self.logger.message(aircraftState.timestamp,
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430 | "Total fuel: %.0f kg" % (sum(aircraftState.fuel),))
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431 |
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432 | #---------------------------------------------------------------------------------------
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433 |
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434 | class B736(Boeing737):
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435 | """Boeing 737-600 aircraft."""
|
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436 | def __init__(self, flight):
|
---|
437 | super(B736, self).__init__(flight)
|
---|
438 | self.dow = 38307
|
---|
439 | self.mtow = 58328
|
---|
440 | self.mlw = 54657
|
---|
441 | self.mzfw = 51482
|
---|
442 |
|
---|
443 | #---------------------------------------------------------------------------------------
|
---|
444 |
|
---|
445 | class B737(Boeing737):
|
---|
446 | """Boeing 737-700 aircraft."""
|
---|
447 | def __init__(self, flight):
|
---|
448 | super(B737, self).__init__(flight)
|
---|
449 | self.dow = 39250
|
---|
450 | self.mtow = 61410
|
---|
451 | self.mlw = 58059
|
---|
452 | self.mzfw = 54657
|
---|
453 |
|
---|
454 | #---------------------------------------------------------------------------------------
|
---|
455 |
|
---|
456 | class B738(Boeing737):
|
---|
457 | """Boeing 737-800 aircraft."""
|
---|
458 | def __init__(self, flight):
|
---|
459 | super(B738, self).__init__(flight)
|
---|
460 | self.dow = 42690
|
---|
461 | self.mtow = 71709
|
---|
462 | self.mlw = 65317
|
---|
463 | self.mzfw = 61688
|
---|
464 |
|
---|
465 | #---------------------------------------------------------------------------------------
|
---|
466 |
|
---|
467 | class B738Charter(B738):
|
---|
468 | """Boeing 737-800 aircraft used for charters."""
|
---|
469 | def __init__(self, flight):
|
---|
470 | super(B738Charter, self).__init__(flight)
|
---|
471 | self.mtow = 77791
|
---|
472 |
|
---|
473 | #---------------------------------------------------------------------------------------
|
---|
474 |
|
---|
475 | class B733(Boeing737):
|
---|
476 | """Boeing 737-300 aircraft."""
|
---|
477 | def __init__(self, flight):
|
---|
478 | super(B733, self).__init__(flight)
|
---|
479 | self.dow = 32700
|
---|
480 | self.mtow = 62820
|
---|
481 | self.mlw = 51700
|
---|
482 | self.mzfw = 48410
|
---|
483 |
|
---|
484 | #---------------------------------------------------------------------------------------
|
---|
485 |
|
---|
486 | class B734(Boeing737):
|
---|
487 | """Boeing 737-400 aircraft."""
|
---|
488 | def __init__(self, flight):
|
---|
489 | super(B734, self).__init__(flight)
|
---|
490 | self.dow = 33200
|
---|
491 | self.mtow = 68050
|
---|
492 | self.mlw = 56200
|
---|
493 | self.mzfw = 53100
|
---|
494 |
|
---|
495 | #---------------------------------------------------------------------------------------
|
---|
496 |
|
---|
497 | class B735(Boeing737):
|
---|
498 | """Boeing 737-500 aircraft."""
|
---|
499 | def __init__(self, flight):
|
---|
500 | super(B735, self).__init__(flight)
|
---|
501 | self.dow = 31300
|
---|
502 | self.mtow = 60550
|
---|
503 | self.mlw = 50000
|
---|
504 | self.mzfw = 46700
|
---|
505 |
|
---|
506 | #---------------------------------------------------------------------------------------
|
---|
507 |
|
---|
508 | class DH8D(Aircraft):
|
---|
509 | """Bombardier Dash-8 Q400 aircraft.
|
---|
510 |
|
---|
511 | The aircraft type-specific values in the aircraft state have the following
|
---|
512 | structure:
|
---|
513 | - fuel: left, right
|
---|
514 | - n1: left, right
|
---|
515 | - reverser: left, right."""
|
---|
516 | fuelTanks = [const.FUELTANK_LEFT, const.FUELTANK_RIGHT]
|
---|
517 |
|
---|
518 | def __init__(self, flight):
|
---|
519 | super(DH8D, self).__init__(flight)
|
---|
520 | self.dow = 17185
|
---|
521 | self.mtow = 29257
|
---|
522 | self.mlw = 28009
|
---|
523 | self.mzfw = 25855
|
---|
524 | self.gearSpeedLimit = 215
|
---|
525 | self.flapSpeedLimits = { 5 : 200,
|
---|
526 | 10 : 181,
|
---|
527 | 15 : 172,
|
---|
528 | 35 : 158 }
|
---|
529 |
|
---|
530 | def logFuel(self, aircraftState):
|
---|
531 | """Log the amount of fuel"""
|
---|
532 | self.logger.message(aircraftState.timestamp,
|
---|
533 | "Fuel: left=%.0f kg - right=%.0f kg" % \
|
---|
534 | (aircraftState.fuel[0], aircraftState.fuel[1]))
|
---|
535 | self.logger.message(aircraftState.timestamp,
|
---|
536 | "Total fuel: %.0f kg" % (sum(aircraftState.fuel),))
|
---|
537 |
|
---|
538 | #---------------------------------------------------------------------------------------
|
---|
539 |
|
---|
540 | class Boeing767(Aircraft):
|
---|
541 | """Base class for the various aircraft in the Boeing 767 family.
|
---|
542 |
|
---|
543 | The aircraft type-specific values in the aircraft state have the following
|
---|
544 | structure:
|
---|
545 | - fuel: left, centre, right
|
---|
546 | - n1: left, right
|
---|
547 | - reverser: left, right"""
|
---|
548 | fuelTanks = [const.FUELTANK_LEFT, const.FUELTANK_CENTRE, const.FUELTANK_RIGHT]
|
---|
549 |
|
---|
550 | def __init__(self, flight):
|
---|
551 | super(Boeing767, self).__init__(flight)
|
---|
552 | self._checkers.append(checks.ThrustChecker())
|
---|
553 | self.gearSpeedLimit = 270
|
---|
554 | self.flapSpeedLimits = { 1 : 255,
|
---|
555 | 5 : 235,
|
---|
556 | 10 : 215,
|
---|
557 | 20 : 215,
|
---|
558 | 25 : 185,
|
---|
559 | 30 : 175 }
|
---|
560 |
|
---|
561 | def logFuel(self, aircraftState):
|
---|
562 | """Log the amount of fuel"""
|
---|
563 | self.logger.message(aircraftState.timestamp,
|
---|
564 | "Fuel: left=%.0f kg - centre=%.0f kg - right=%.0f kg" % \
|
---|
565 | (aircraftState.fuel[0], aircraftState.fuel[1],
|
---|
566 | aircraftState.fuel[2]))
|
---|
567 | self.logger.message(aircraftState.timestamp,
|
---|
568 | "Total fuel: %.0f kg" % (sum(aircraftState.fuel),))
|
---|
569 |
|
---|
570 | #---------------------------------------------------------------------------------------
|
---|
571 |
|
---|
572 | class B762(Boeing767):
|
---|
573 | """Boeing 767-200 aircraft."""
|
---|
574 | def __init__(self, flight):
|
---|
575 | super(B762, self).__init__(flight)
|
---|
576 | self.dow = 84507
|
---|
577 | self.mtow = 175540
|
---|
578 | self.mlw = 126098
|
---|
579 | self.mzfw = 114758
|
---|
580 |
|
---|
581 | #---------------------------------------------------------------------------------------
|
---|
582 |
|
---|
583 | class B763(Boeing767):
|
---|
584 | """Boeing 767-300 aircraft."""
|
---|
585 | def __init__(self, flight):
|
---|
586 | super(B763, self).__init__(cflight)
|
---|
587 | self.dow = 91311
|
---|
588 | self.mtow = 181436
|
---|
589 | self.mlw = 137892
|
---|
590 | self.mzfw = 130635
|
---|
591 |
|
---|
592 | #---------------------------------------------------------------------------------------
|
---|
593 |
|
---|
594 | class CRJ2(Aircraft):
|
---|
595 | """Bombardier CRJ-200 aircraft.
|
---|
596 |
|
---|
597 | The aircraft type-specific values in the aircraft state have the following
|
---|
598 | structure:
|
---|
599 | - fuel: left, centre, right
|
---|
600 | - n1: left, right
|
---|
601 | - reverser: left, right."""
|
---|
602 | fuelTanks = [const.FUELTANK_LEFT, const.FUELTANK_CENTRE, const.FUELTANK_RIGHT]
|
---|
603 |
|
---|
604 | def __init__(self, flight):
|
---|
605 | super(CRJ2, self).__init__(flight)
|
---|
606 | self._checkers.append(checks.ThrustChecker())
|
---|
607 | self.dow = 14549
|
---|
608 | self.mtow = 22995
|
---|
609 | self.mlw = 21319
|
---|
610 | self.mzfw = 19958
|
---|
611 | self.gearSpeedLimit = 240
|
---|
612 | self.flapSpeedLimits = { 8 : 260,
|
---|
613 | 20 : 220,
|
---|
614 | 30 : 190,
|
---|
615 | 45 : 175 }
|
---|
616 |
|
---|
617 | def logFuel(self, aircraftState):
|
---|
618 | """Log the amount of fuel"""
|
---|
619 | self.logger.message(aircraftState.timestamp,
|
---|
620 | "Fuel: left=%.0f kg - centre=%.0f kg - right=%.0f kg" % \
|
---|
621 | (aircraftState.fuel[0], aircraftState.fuel[1],
|
---|
622 | aircraftState.fuel[2]))
|
---|
623 | self.logger.message(aircraftState.timestamp,
|
---|
624 | "Total fuel: %.0f kg" % (sum(aircraftState.fuel),))
|
---|
625 |
|
---|
626 | #---------------------------------------------------------------------------------------
|
---|
627 |
|
---|
628 | class F70(Aircraft):
|
---|
629 | """Fokker 70 aircraft.
|
---|
630 |
|
---|
631 | The aircraft type-specific values in the aircraft state have the following
|
---|
632 | structure:
|
---|
633 | - fuel: left, centre, right
|
---|
634 | - n1: left, right
|
---|
635 | - reverser: left, right."""
|
---|
636 | fuelTanks = [const.FUELTANK_LEFT, const.FUELTANK_CENTRE, const.FUELTANK_RIGHT]
|
---|
637 |
|
---|
638 | def __init__(self, flight):
|
---|
639 | super(F70, self).__init__(flight)
|
---|
640 | self._checkers.append(checks.ThrustChecker())
|
---|
641 | self.dow = 24283
|
---|
642 | self.mtow = 38100 # FIXME: differentiate by registration number,
|
---|
643 | # MTOW of HA-LMF: 41955
|
---|
644 | self.mlw = 36740
|
---|
645 | self.mzfw = 32655
|
---|
646 | self.gearSpeedLimit = 200
|
---|
647 | self.flapSpeedLimits = { 8 : 250,
|
---|
648 | 15 : 220,
|
---|
649 | 25 : 220,
|
---|
650 | 42 : 180 }
|
---|
651 |
|
---|
652 | def logFuel(self, aircraftState):
|
---|
653 | """Log the amount of fuel"""
|
---|
654 | self.logger.message(aircraftState.timestamp,
|
---|
655 | "Fuel: left=%.0f kg - centre=%.0f kg - right=%.0f kg" % \
|
---|
656 | (aircraftState.fuel[0], aircraftState.fuel[1],
|
---|
657 | aircraftState.fuel[2]))
|
---|
658 | self.logger.message(aircraftState.timestamp,
|
---|
659 | "Total fuel: %.0f kg" % (sum(aircraftState.fuel),))
|
---|
660 |
|
---|
661 | #---------------------------------------------------------------------------------------
|
---|
662 |
|
---|
663 | class DC3(Aircraft):
|
---|
664 | """Lisunov Li-2 (DC-3) aircraft.
|
---|
665 |
|
---|
666 | The aircraft type-specific values in the aircraft state have the following
|
---|
667 | structure:
|
---|
668 | - fuel: left aux, left, right, right aux
|
---|
669 | - rpm: left, right
|
---|
670 | - reverser: left, right."""
|
---|
671 | fuelTanks = [const.FUELTANK_LEFT_AUX, const.FUELTANK_LEFT,
|
---|
672 | const.FUELTANK_RIGHT, const.FUELTANK_RIGHT_AUX]
|
---|
673 |
|
---|
674 | def __init__(self, flight):
|
---|
675 | super(DC3, self).__init__(flight)
|
---|
676 | self.dow = 8627
|
---|
677 | self.mtow = 11884
|
---|
678 | self.mlw = 11793
|
---|
679 | self.mzfw = 11780
|
---|
680 | self.gearSpeedLimit = 148
|
---|
681 | self.flapSpeedLimits = { 15 : 135,
|
---|
682 | 30 : 99,
|
---|
683 | 45 : 97 }
|
---|
684 |
|
---|
685 | def _checkFlightEnd(self, aircraftState):
|
---|
686 | """Check if the end of the flight has arrived.
|
---|
687 |
|
---|
688 | This implementation checks the RPM values to be 0."""
|
---|
689 | for rpm in aircraftState.rpm:
|
---|
690 | if rpm>0: return False
|
---|
691 | return True
|
---|
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 - right=%.0f kg - right aux=%.0f kg" % \
|
---|
697 | (aircraftState.fuel[0], aircraftState.fuel[1],
|
---|
698 | aircraftState.fuel[2], aircraftState.fuel[3]))
|
---|
699 | self.logger.message(aircraftState.timestamp,
|
---|
700 | "Total fuel: %.0f kg" % (sum(aircraftState.fuel),))
|
---|
701 |
|
---|
702 | #---------------------------------------------------------------------------------------
|
---|
703 |
|
---|
704 | class T134(Aircraft):
|
---|
705 | """Tupolev Tu-134 aircraft.
|
---|
706 |
|
---|
707 | The aircraft type-specific values in the aircraft state have the following
|
---|
708 | structure:
|
---|
709 | - fuel: left tip, left aux, centre, right aux, right tip, external 1,
|
---|
710 | external 2
|
---|
711 | - n1: left, right
|
---|
712 | - reverser: left, right."""
|
---|
713 | fuelTanks = [const.FUELTANK_LEFT_TIP, const.FUELTANK_EXTERNAL1,
|
---|
714 | const.FUELTANK_LEFT_AUX,
|
---|
715 | const.FUELTANK_CENTRE,
|
---|
716 | const.FUELTANK_RIGHT_AUX,
|
---|
717 | const.FUELTANK_EXTERNAL2, const.FUELTANK_RIGHT_TIP]
|
---|
718 |
|
---|
719 | def __init__(self, flight):
|
---|
720 | super(T134, self).__init__(flight)
|
---|
721 | self._checkers.append(checks.ThrustChecker())
|
---|
722 | self.dow = 29500
|
---|
723 | self.mtow = 49000
|
---|
724 | self.mlw = 43000
|
---|
725 | self.mzfw = 38500
|
---|
726 | self.gearSpeedLimit = 216
|
---|
727 | self.flapSpeedLimits = { 10 : 450,
|
---|
728 | 20 : 400,
|
---|
729 | 30 : 300 }
|
---|
730 |
|
---|
731 | @property
|
---|
732 | def speedInKnots(self):
|
---|
733 | """Indicate if the speed is in knots."""
|
---|
734 | return False
|
---|
735 |
|
---|
736 | def logFuel(self, aircraftState):
|
---|
737 | """Log the amount of fuel"""
|
---|
738 | self.logger.message(aircraftState.timestamp,
|
---|
739 | "Fuel: left tip=%.0f kg - external 1=%.0f kg - left aux=%.0f kg - centre= %.0f kg - right aux=%.0f kg - external 2=%.0f kg - right tip=%.0f kg" % \
|
---|
740 | (aircraftState.fuel[0], aircraftState.fuel[1],
|
---|
741 | aircraftState.fuel[2],
|
---|
742 | aircraftState.fuel[3], aircraftState.fuel[4],
|
---|
743 | aircraftState.fuel[5], aircraftState.fuel[6]))
|
---|
744 | self.logger.message(aircraftState.timestamp,
|
---|
745 | "Total fuel: %.0f kg" % (sum(aircraftState.fuel),))
|
---|
746 |
|
---|
747 | def _appendLightsLoggers(self):
|
---|
748 | """Append the loggers needed for the lights."""
|
---|
749 | self._checkers.append(checks.AnticollisionLightsLogger())
|
---|
750 | self._checkers.append(checks.LandingLightsLogger())
|
---|
751 | self._checkers.append(checks.NavLightsLogger())
|
---|
752 |
|
---|
753 | def _appendLightsCheckers(self):
|
---|
754 | """Append the checkers needed for the lights."""
|
---|
755 | self._checkers.append(checks.TupolevAntiCollisionLightsChecker())
|
---|
756 | self._checkers.append(checks.LandingLightsChecker())
|
---|
757 | self._checkers.append(checks.NavLightsChecker())
|
---|
758 |
|
---|
759 | #---------------------------------------------------------------------------------------
|
---|
760 |
|
---|
761 | class T154(Aircraft):
|
---|
762 | """Tupolev Tu-154 aircraft.
|
---|
763 |
|
---|
764 | The aircraft type-specific values in the aircraft state have the following
|
---|
765 | structure:
|
---|
766 | - fuel: left aux, left, centre, centre 2, right, right aux
|
---|
767 | - n1: left, centre, right
|
---|
768 | - reverser: left, right"""
|
---|
769 | fuelTanks = [const.FUELTANK_LEFT_AUX, const.FUELTANK_LEFT,
|
---|
770 | const.FUELTANK_CENTRE, const.FUELTANK_CENTRE2,
|
---|
771 | const.FUELTANK_RIGHT, const.FUELTANK_RIGHT_AUX]
|
---|
772 | def __init__(self, flight):
|
---|
773 | super(T154, self).__init__(flight)
|
---|
774 | self._checkers.append(checks.ThrustChecker())
|
---|
775 | self.dow = 53259
|
---|
776 | self.mtow = 98000
|
---|
777 | self.mlw = 78000
|
---|
778 | self.mzfw = 72000
|
---|
779 | self.gearSpeedLimit = 216
|
---|
780 | self.flapSpeedLimits = { 15 : 227,
|
---|
781 | 28 : 194,
|
---|
782 | 45 : 162 }
|
---|
783 |
|
---|
784 | @property
|
---|
785 | def speedInKnots(self):
|
---|
786 | """Indicate if the speed is in knots."""
|
---|
787 | return False
|
---|
788 |
|
---|
789 | def logFuel(self, aircraftState):
|
---|
790 | """Log the amount of fuel"""
|
---|
791 | self.logger.message(aircraftState.timestamp,
|
---|
792 | "Fuel: left aux=%.0f kg - left=%.0f kg - centre=%.0f kg - centre 2=%.0f kg - right=%.0f kg - right aux=%.0f kg" % \
|
---|
793 | (aircraftState.fuel[0], aircraftState.fuel[1],
|
---|
794 | aircraftState.fuel[2], aircraftState.fuel[3],
|
---|
795 | aircraftState.fuel[4], aircraftState.fuel[5]))
|
---|
796 | self.logger.message(aircraftState.timestamp,
|
---|
797 | "Total fuel: %.0f kg" % (sum(aircraftState.fuel),))
|
---|
798 |
|
---|
799 | def _appendLightsLoggers(self):
|
---|
800 | """Append the loggers needed for the lights."""
|
---|
801 | self._checkers.append(checks.AnticollisionLightsLogger())
|
---|
802 | self._checkers.append(checks.LandingLightsLogger())
|
---|
803 | self._checkers.append(checks.NavLightsLogger())
|
---|
804 |
|
---|
805 | def _appendLightsCheckers(self):
|
---|
806 | """Append the checkers needed for the lights."""
|
---|
807 | self._checkers.append(checks.TupolevAntiCollisionLightsChecker())
|
---|
808 | self._checkers.append(checks.LandingLightsChecker())
|
---|
809 | self._checkers.append(checks.NavLightsChecker())
|
---|
810 |
|
---|
811 | #---------------------------------------------------------------------------------------
|
---|
812 |
|
---|
813 |
|
---|
814 | class YK40(Aircraft):
|
---|
815 | """Yakovlev Yak-40 aircraft.
|
---|
816 |
|
---|
817 | The aircraft type-specific values in the aircraft state have the following
|
---|
818 | structure:
|
---|
819 | - fuel: left, right
|
---|
820 | - n1: left, right
|
---|
821 | - reverser: left, right"""
|
---|
822 | fuelTanks = [const.FUELTANK_LEFT, const.FUELTANK_RIGHT]
|
---|
823 |
|
---|
824 | def __init__(self, flight):
|
---|
825 | super(YK40, self).__init__(flight)
|
---|
826 | self._checkers.append(checks.ThrustChecker())
|
---|
827 | self.dow = 9400
|
---|
828 | self.mtow = 17200
|
---|
829 | self.mlw = 16800
|
---|
830 | self.mzfw = 12100
|
---|
831 | self.gearSpeedLimit = 165
|
---|
832 | self.flapSpeedLimits = { 20 : 165,
|
---|
833 | 35 : 135 }
|
---|
834 |
|
---|
835 | @property
|
---|
836 | def speedInKnots(self):
|
---|
837 | """Indicate if the speed is in knots."""
|
---|
838 | return False
|
---|
839 |
|
---|
840 | def logFuel(self, aircraftState):
|
---|
841 | """Log the amount of fuel"""
|
---|
842 | self.logger.message(aircraftState.timestamp,
|
---|
843 | "Fuel: left=%.0f kg - right=%.0f kg" % \
|
---|
844 | (aircraftState.fuel[0], aircraftState.fuel[1]))
|
---|
845 | self.logger.message(aircraftState.timestamp,
|
---|
846 | "Total fuel: %.0f kg" % (sum(aircraftState.fuel),))
|
---|
847 |
|
---|
848 | def _appendLightsLoggers(self):
|
---|
849 | """Append the loggers needed for the lights."""
|
---|
850 | self._checkers.append(checks.AnticollisionLightsLogger())
|
---|
851 | self._checkers.append(checks.LandingLightsLogger())
|
---|
852 | self._checkers.append(checks.NavLightsLogger())
|
---|
853 |
|
---|
854 | def _appendLightsCheckers(self):
|
---|
855 | """Append the checkers needed for the lights."""
|
---|
856 | self._checkers.append(checks.AntiCollisionLightsChecker())
|
---|
857 | self._checkers.append(checks.LandingLightsChecker())
|
---|
858 | self._checkers.append(checks.NavLightsChecker())
|
---|
859 |
|
---|
860 | #---------------------------------------------------------------------------------------
|
---|
861 |
|
---|
862 | MostFuelTankAircraft = T134
|
---|
863 |
|
---|
864 | #---------------------------------------------------------------------------------------
|
---|
865 |
|
---|
866 | _classes = { const.AIRCRAFT_B736 : B736,
|
---|
867 | const.AIRCRAFT_B737 : B737,
|
---|
868 | const.AIRCRAFT_B738 : B738,
|
---|
869 | const.AIRCRAFT_B738C : B738Charter,
|
---|
870 | const.AIRCRAFT_B733 : B733,
|
---|
871 | const.AIRCRAFT_B734 : B734,
|
---|
872 | const.AIRCRAFT_B735 : B735,
|
---|
873 | const.AIRCRAFT_DH8D : DH8D,
|
---|
874 | const.AIRCRAFT_B762 : B762,
|
---|
875 | const.AIRCRAFT_B763 : B763,
|
---|
876 | const.AIRCRAFT_CRJ2 : CRJ2,
|
---|
877 | const.AIRCRAFT_F70 : F70,
|
---|
878 | const.AIRCRAFT_DC3 : DC3,
|
---|
879 | const.AIRCRAFT_T134 : T134,
|
---|
880 | const.AIRCRAFT_T154 : T154,
|
---|
881 | const.AIRCRAFT_YK40 : YK40 }
|
---|
882 |
|
---|
883 | #---------------------------------------------------------------------------------------
|
---|
884 |
|
---|
885 | if __name__ == "__main__":
|
---|
886 | value = SmoothedValue()
|
---|
887 |
|
---|
888 | print "Adding 1, 12.0"
|
---|
889 | value.add(1, 12.0)
|
---|
890 | print value.get()
|
---|
891 |
|
---|
892 | print "Adding 1, 15.0"
|
---|
893 | value.add(1, 15.0)
|
---|
894 | print value.get()
|
---|
895 |
|
---|
896 | print "Adding 2, 18.0"
|
---|
897 | value.add(2, 18.0)
|
---|
898 | print value.get()
|
---|
899 |
|
---|
900 | print "Adding 2, 20.0"
|
---|
901 | value.add(2, 20.0)
|
---|
902 | print value.get()
|
---|
903 |
|
---|
904 | print "Adding 5, 22.0"
|
---|
905 | value.add(5, 22.0)
|
---|
906 | print value.get()
|
---|
907 |
|
---|
908 | print "Adding 5, 25.0"
|
---|
909 | value.add(5, 25.0)
|
---|
910 | print value.get()
|
---|
911 |
|
---|
912 | print "Adding 5, 29.0"
|
---|
913 | value.add(5, 29.0)
|
---|
914 | print value.get()
|
---|
915 |
|
---|
916 | print "Adding 5, 21.0"
|
---|
917 | value.add(5, 21.0)
|
---|
918 | print value.get()
|
---|
919 |
|
---|
920 | print "Adding 5, 26.0"
|
---|
921 | value.add(5, 26.0)
|
---|
922 | print value.get()
|
---|
923 |
|
---|
924 | print "Adding 2, 30.0"
|
---|
925 | value.add(2, 30.0)
|
---|
926 | print value.get()
|
---|
927 |
|
---|
928 | print "Adding 2, 55.0"
|
---|
929 | value.add(2, 55.0)
|
---|
930 | print value.get()
|
---|
931 |
|
---|
932 | #---------------------------------------------------------------------------------------
|
---|