1 |
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2 | import const
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3 | import checks
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4 | import fs
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5 | import util
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6 |
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7 | import sys
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8 | import time
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9 | import traceback
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10 |
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11 | from collections import deque
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12 |
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13 | #---------------------------------------------------------------------------------------
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14 |
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15 | ## @package mlx.acft
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16 | #
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17 | # The simulator-independent aircraft classes.
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18 | #
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19 | # This module contains the aircraft classes that contain some general data
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20 | # about each aircraft type in the MAVA Fleet. The base class, \ref Aircraft
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21 | # also implements some parts of the logging and traces some data. The classes
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22 | # are also responsible for creating the \ref mlx.checks "checkers". Most of
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23 | # them are created by the \ref Aircraft class' constructor, but there can be
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24 | # type-specific differences. For example the lights are different for different
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25 | # types, so there is a \ref Aircraft._appendLightsLoggers "function" which can
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26 | # be reimplemented in child classes, if needed. This class maintains also the
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27 | # \ref SmoothedValue "smoothed values" of the IAS and the VS and set these
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28 | # values in the \ref mlx.fs.AircraftState "aircraft state" when it is received
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29 | # from the simulator.
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30 |
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31 | #---------------------------------------------------------------------------------------
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32 |
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33 | class SmoothedValue(object):
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34 | """A smoothed value."""
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35 | def __init__(self):
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36 | """Construct the value."""
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37 | self._deque = deque()
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38 | self._sum = 0
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39 |
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40 | def add(self, length, value):
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41 | """Add the given value and smooth with the given length."""
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42 | dequeLength = len(self._deque)
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43 | while dequeLength>=length:
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44 | self._sum -= self._deque.popleft()
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45 | dequeLength -= 1
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46 |
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47 | self._sum += value
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48 | self._deque.append(value)
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49 |
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50 | def get(self):
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51 | """Get the average."""
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52 | return self._sum / len(self._deque)
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53 |
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54 | #---------------------------------------------------------------------------------------
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55 |
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56 | class Aircraft(object):
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57 | """Base class for aircraft."""
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58 | @staticmethod
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59 | def create(flight):
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60 | """Create an aircraft instance for the type in the given flight."""
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61 | return _classes[flight.aircraftType](flight)
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62 |
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63 | def __init__(self, flight):
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64 | """Construct the aircraft for the given type."""
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65 | self._flight = flight
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66 | self._aircraftState = None
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67 |
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68 | self._maxVS = -10000.0
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69 | self._minVS = 10000.0
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70 |
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71 | self._v1r2LineIndex = None
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72 | self._vrefLineIndex = None
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73 |
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74 | self.humanWeight = 82.0
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75 |
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76 | self._checkers = []
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77 |
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78 | config = flight.config
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79 | # Loggers
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80 |
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81 | self._checkers.append(checks.StageChecker())
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82 | self._checkers.append(checks.TakeOffLogger())
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83 |
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84 | self._checkers.append(checks.AltimeterLogger())
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85 |
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86 | self._checkers.append(checks.NAV1Logger())
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87 | self._checkers.append(checks.NAV2Logger())
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88 | self._checkers.append(checks.SquawkLogger())
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89 |
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90 | self._appendLightsLoggers()
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91 |
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92 | self._checkers.append(checks.FlapsLogger())
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93 |
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94 | self._checkers.append(checks.GearsLogger())
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95 | self._checkers.append(checks.CruiseSpeedLogger())
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96 | self._checkers.append(checks.SpoilerLogger())
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97 |
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98 | if config.isMessageTypeFS(const.MESSAGETYPE_VISIBILITY):
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99 | self._checkers.append(checks.VisibilityChecker())
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100 |
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101 | # FIXME: we should have a central data model object, and not collect
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102 | # the data from the GUI. However, some pieces of data (e.g. V-speeds,
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103 | # etc. that is entered into the GUI) *should* be a part of the GUI and
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104 | # queried from it, so the model should have a reference to the GUI as
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105 | # well and access such data via the GUI!
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106 | if config.onlineACARS and flight.loggedIn and not flight.entranceExam:
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107 | self._checkers.append(checks.ACARSSender(flight._gui))
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108 |
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109 | # Fault checkers
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110 |
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111 | self._appendLightsCheckers()
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112 |
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113 | self._checkers.append(checks.BankChecker())
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114 |
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115 | self._checkers.append(checks.FlapsRetractChecker())
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116 | self._checkers.append(checks.FlapsSpeedLimitChecker())
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117 |
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118 | self._checkers.append(checks.GearsDownChecker())
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119 | self._checkers.append(checks.GearSpeedLimitChecker())
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120 |
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121 | self._checkers.append(checks.GLoadChecker())
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122 |
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123 | self._checkers.append(checks.MLWChecker())
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124 | self._checkers.append(checks.MTOWChecker())
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125 | self._checkers.append(checks.MZFWChecker())
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126 | self._checkers.append(checks.PayloadChecker())
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127 |
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128 | self._checkers.append(checks.SpeedChecker())
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129 | self._checkers.append(checks.VSChecker())
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130 |
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131 | timeout = 5.0 + config.realIASSmoothingLength - 1
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132 | self._checkers.append(checks.OverspeedChecker(timeout = timeout))
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133 |
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134 | self._checkers.append(checks.StallChecker())
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135 |
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136 | self._checkers.append(checks.PitotChecker())
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137 |
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138 | self._checkers.append(checks.ReverserChecker())
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139 |
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140 | if flight.aircraftType is not None and config.enableApproachCallouts:
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141 | approachCallouts = flight.config.getApproachCallouts(flight.aircraftType)
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142 | if approachCallouts:
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143 | self._checkers.append(checks.ApproachCalloutsPlayer(approachCallouts))
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144 |
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145 | self._smoothedIAS = SmoothedValue()
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146 | self._smoothedVS = SmoothedValue()
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147 |
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148 | @property
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149 | def type(self):
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150 | """Get the type of the aircraft."""
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151 | return self._flight.aircraftType
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152 |
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153 | @property
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154 | def flight(self):
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155 | """Get the flight the aircraft belongs to."""
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156 | return self._flight
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157 |
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158 | @property
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159 | def logger(self):
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160 | """Get the logger to use for the aircraft."""
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161 | return self._flight.logger
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162 |
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163 | @property
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164 | def state(self):
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165 | """Get the current aircraft state."""
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166 | return self._aircraftState
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167 |
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168 | @property
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169 | def speedInKnots(self):
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170 | """Indicate if the speed is in knots.
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171 |
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172 | This default implementation returns True."""
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173 | return True
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174 |
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175 | @property
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176 | def timestamp(self):
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177 | """Get the timestamp of the current state."""
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178 | return None if self._aircraftState is None \
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179 | else self._aircraftState.timestamp
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180 |
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181 | def getFlapsSpeedLimit(self, flaps):
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182 | """Get the speed limit for the given flaps setting."""
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183 | return self.flapSpeedLimits[flaps] if flaps in self.flapSpeedLimits \
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184 | else None
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185 |
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186 | def modelChanged(self, timestamp, aircraftName, modelName):
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187 | """Called when the simulator's aircraft changes."""
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188 | self._flight.logger.message(timestamp,
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189 | "Aircraft: name='%s', model='%s'" % \
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190 | (aircraftName, modelName))
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191 |
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192 | def handleState(self, aircraftState):
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193 | """Called when the state of the aircraft changes.
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194 |
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195 | This is the function that the simulator calls directly with the new
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196 | state."""
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197 | try:
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198 | config = self._flight.config
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199 |
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200 | self._smoothedIAS.add(config.realIASSmoothingLength, aircraftState.ias)
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201 | aircraftState.smoothedIAS = self._smoothedIAS.get()
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202 |
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203 | self._smoothedVS.add(config.realVSSmoothingLength, aircraftState.vs)
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204 | aircraftState.smoothedVS = self._smoothedVS.get()
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205 |
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206 | for checker in self._checkers:
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207 | try:
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208 | checker.check(self._flight, self, self._flight.logger,
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209 | self._aircraftState, aircraftState)
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210 | except:
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211 | print >> sys.stderr, "Checker", checker, "failed"
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212 | traceback.print_exc()
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213 |
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214 | self._flight.handleState(self._aircraftState, aircraftState)
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215 |
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216 | self._maxVS = max(self._maxVS, aircraftState.vs)
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217 | self._minVS = min(self._minVS, aircraftState.vs)
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218 | except:
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219 | print >> sys.stderr, "Failed to handle the state"
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220 | traceback.print_exc()
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221 | finally:
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222 | self._aircraftState = aircraftState
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223 |
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224 | def setStage(self, aircraftState, newStage):
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225 | """Set the given stage as the new one and do whatever should be
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226 | done."""
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227 | if self._flight.setStage(aircraftState.timestamp, newStage):
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228 | if newStage==const.STAGE_PUSHANDTAXI:
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229 | self.logger.message(aircraftState.timestamp, "Block time start")
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230 | self._flight.logFuel(aircraftState)
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231 | self.logger.message(aircraftState.timestamp,
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232 | "Zero-fuel weight: %.0f kg" % (aircraftState.zfw))
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233 | flight = self._flight
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234 | if flight.v1 is None or flight.vr is None or flight.v2 is None:
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235 | fs.sendMessage(const.MESSAGETYPE_HELP,
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236 | "Don't forget to set the takeoff V-speeds!",
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237 | 5)
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238 | elif newStage==const.STAGE_TAKEOFF:
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239 | self.logger.message(aircraftState.timestamp,
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240 | "Flight time start")
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241 | self.logger.message(aircraftState.timestamp,
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242 | "Takeoff weight: %.0f kg, MTOW: %.0f kg" % \
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243 | (aircraftState.grossWeight, self.mtow))
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244 | self.logger.message(aircraftState.timestamp,
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245 | "Wind %03.0f degrees at %.0f knots" % \
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246 | (aircraftState.windDirection,
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247 | aircraftState.windSpeed))
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248 | self._logV1R2()
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249 | elif newStage==const.STAGE_TAXIAFTERLAND:
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250 | flight = self._flight
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251 | bookedFlight = flight.bookedFlight
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252 | config = flight.config
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253 | if config.onlineGateSystem and \
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254 | flight.loggedIn and \
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255 | not flight.entranceExam and \
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256 | bookedFlight.arrivalICAO=="LHBP" and \
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257 | config.isMessageTypeFS(const.MESSAGETYPE_GATE_SYSTEM):
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258 | self._flight.getFleet(callback = self._fleetRetrieved,
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259 | force = True)
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260 | self.logger.message(aircraftState.timestamp, "Flight time end")
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261 | self._flight.logFuel(aircraftState)
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262 | self.logger.message(aircraftState.timestamp,
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263 | "Landing weight: %.0f kg, MLW: %.0f" % \
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264 | (aircraftState.grossWeight, self.mlw))
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265 | self.logger.message(aircraftState.timestamp,
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266 | "Vertical speed range: %.0f..%.0f feet/min" % \
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267 | (self._minVS, self._maxVS))
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268 | elif newStage==const.STAGE_PARKING:
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269 | self.logger.message(aircraftState.timestamp, "Block time end")
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270 | elif newStage==const.STAGE_END:
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271 | flightLength = self._flight.flightTimeEnd - self._flight.flightTimeStart
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272 | self.logger.message(aircraftState.timestamp,
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273 | "Flight time: " +
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274 | util.getTimeIntervalString(flightLength))
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275 | self.logger.message(aircraftState.timestamp,
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276 | "Flown distance: %.2f NM" % \
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277 | (self._flight.flownDistance,))
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278 | blockLength = self._flight.blockTimeEnd - self._flight.blockTimeStart
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279 | self.logger.message(aircraftState.timestamp,
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280 | "Block time: " +
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281 | util.getTimeIntervalString(blockLength))
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282 |
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283 | def prepareFlare(self):
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284 | """Called when it is detected that we will soon flare.
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285 |
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286 | On the first call, it should start monitoring some parameters more
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287 | closely to determine flare time."""
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288 | self.flight.simulator.startFlare()
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289 |
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290 | def flareStarted(self, windSpeed, windDirection, visibility,
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291 | flareStart, flareStartFS):
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292 | """Called when the flare has started."""
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293 | self.logger.message(self._aircraftState.timestamp, "The flare has begun")
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294 | self.logger.message(self._aircraftState.timestamp,
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295 | "Wind %03.0f degrees at %.0f knots" % \
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296 | (windDirection, windSpeed))
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297 | self.logger.message(self._aircraftState.timestamp,
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298 | "Visibility: %.0f metres" % (visibility,))
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299 | self.logger.message(self._aircraftState.timestamp,
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300 | "Altimeter setting: %.0f hPa" % \
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301 | (self._aircraftState.altimeter,))
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302 | self._logVRef()
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303 | self.flight.flareStarted(flareStart, flareStartFS)
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304 | fs.sendMessage(const.MESSAGETYPE_INFORMATION, "Flare-time", 3)
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305 |
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306 | def flareFinished(self, flareEnd, flareEndFS, tdRate, tdRateCalculatedByFS,
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307 | ias, pitch, bank, heading):
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308 | """Called when the flare has finished."""
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309 | (flareTimeFromFS, flareTime) = self.flight.flareFinished(flareEnd,
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310 | flareEndFS,
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311 | tdRate)
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312 | self.logger.message(self._aircraftState.timestamp,
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313 | "Flaretime: %.3f (from %s)" % \
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314 | (flareTime,
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315 | "the simulator" if flareTimeFromFS else "real time",))
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316 | self.logger.message(self._aircraftState.timestamp,
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317 | "Touchdown rate: %.0f feet/min" % (tdRate,))
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318 | self.logger.message(self._aircraftState.timestamp,
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319 | "Touchdown rate was calculated by the %s" % \
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320 | ("simulator" if tdRateCalculatedByFS else "logger",))
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321 | flight = self._flight
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322 | self.logger.message(self._aircraftState.timestamp,
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323 | "Touchdown speed: %.0f %s" % \
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324 | (flight.speedFromKnots(ias),
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325 | flight.getEnglishSpeedUnit()))
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326 | self.logger.message(self._aircraftState.timestamp,
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327 | "Touchdown pitch: %.1f degrees" % (pitch,))
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328 | self.logger.message(self._aircraftState.timestamp,
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329 | "Touchdown bank: %.1f degrees" % (bank,))
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330 | self.logger.message(self._aircraftState.timestamp,
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331 | "Touchdown heading: %03.0f degrees" % (heading,))
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332 | self.logger.message(self._aircraftState.timestamp,
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333 | "Centre of gravity: %.1f%%" % \
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334 | (self._aircraftState.cog*100.0,))
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335 |
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336 | def cancelFlare(self):
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337 | """Cancel flare, if it has started."""
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338 | self.flight.simulator.cancelFlare()
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339 |
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340 | def checkFlightEnd(self, aircraftState):
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341 | """Check if the end of the flight has arrived.
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342 |
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343 | This default implementation checks the N1 values, but for
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344 | piston-powered aircraft you need to check the RPMs."""
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345 | for n1 in aircraftState.n1:
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346 | if n1>=0.5: return False
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347 | return True
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348 |
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349 | def updateV1R2(self):
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350 | """Update the V1, Vr and V2 values from the flight, if the these values
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351 | have already been logged."""
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352 | if self._v1r2LineIndex is not None:
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353 | self._logV1R2()
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354 |
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355 | def _appendLightsLoggers(self):
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356 | """Append the loggers needed for the lights.
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357 |
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358 | This default implementation adds the loggers for the anti-collision
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359 | lights, the landing lights, the strobe lights and the NAV lights."""
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360 | self._checkers.append(checks.AnticollisionLightsLogger())
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361 | self._checkers.append(checks.LandingLightsLogger())
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362 | self._checkers.append(checks.StrobeLightsLogger())
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363 | self._checkers.append(checks.NavLightsLogger())
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364 |
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365 | def _appendLightsCheckers(self):
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366 | """Append the checkers needed for the lights.
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367 |
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368 | This default implementation adds the checkers for the anti-collision
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369 | lights, the landing lights, the strobe lights and the NAV lights."""
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370 | self._checkers.append(checks.AntiCollisionLightsChecker())
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371 | self._checkers.append(checks.LandingLightsChecker())
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372 | self._checkers.append(checks.NavLightsChecker())
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373 | self._checkers.append(checks.StrobeLightsChecker())
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374 |
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375 | def _speedToLog(self, speed):
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376 | """Convert the given speed (being either None or expressed in the
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377 | flight's speed unit into a string."""
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378 | if speed is None:
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379 | return "-"
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380 | else:
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381 | return str(speed) + " " + self._flight.getEnglishSpeedUnit()
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382 |
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383 | def _logV1R2(self):
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384 | """Log the V1, Vr and V2 value either newly, or by updating the
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385 | corresponding line."""
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386 | message = "Speeds calculated by the pilot: V1: %s, VR: %s, V2: %s" % \
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387 | (self._speedToLog(self._flight.v1),
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388 | self._speedToLog(self._flight.vr),
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389 | self._speedToLog(self._flight.v2))
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390 |
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391 | if self._v1r2LineIndex is None:
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392 | self._v1r2LineIndex = \
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393 | self.logger.message(self._aircraftState.timestamp, message)
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394 | else:
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395 | self.logger.updateLine(self._v1r2LineIndex, message)
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396 |
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397 | def updateVRef(self):
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398 | """Update the Vref value from the flight, if the Vref value has already
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399 | been logged."""
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400 | if self._vrefLineIndex is not None:
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401 | self._logVRef()
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402 |
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403 | def _logVRef(self):
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404 | """Log the Vref value either newly, or by updating the corresponding
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405 | line."""
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406 | message = "VRef speed calculated by the pilot: %s" % \
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407 | (self._speedToLog(self._flight.vref),)
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408 | if self._vrefLineIndex is None:
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409 | self._vrefLineIndex = \
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410 | self.logger.message(self._aircraftState.timestamp, message)
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411 | else:
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412 | self.logger.updateLine(self._vrefLineIndex, message)
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413 |
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414 | def _fleetRetrieved(self, fleet):
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415 | """Callback for the fleet retrieval result."""
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416 | if fleet is not None:
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417 | gateList = ""
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418 | occupiedGateNumbers = fleet.getOccupiedGateNumbers()
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419 | for gateNumber in const.lhbpGateNumbers:
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420 | if gateNumber not in occupiedGateNumbers:
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421 | if gateList: gateList += ", "
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422 | gateList += gateNumber
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423 | fs.sendMessage(const.MESSAGETYPE_GATE_SYSTEM,
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424 | "Free gates: " + gateList, 20)
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425 |
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426 |
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427 | #---------------------------------------------------------------------------------------
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428 |
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429 | class Boeing737(Aircraft):
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430 | """Base class for the various aircraft in the Boeing 737 family.
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431 |
|
---|
432 | The aircraft type-specific values in the aircraft state have the following
|
---|
433 | structure:
|
---|
434 | - fuel: left, centre, right
|
---|
435 | - n1: left, right
|
---|
436 | - reverser: left, right"""
|
---|
437 | def __init__(self, flight):
|
---|
438 | super(Boeing737, self).__init__(flight)
|
---|
439 | self._checkers.append(checks.ThrustChecker())
|
---|
440 |
|
---|
441 | self.gearSpeedLimit = 270
|
---|
442 | self.flapSpeedLimits = { 1 : 260,
|
---|
443 | 2 : 260,
|
---|
444 | 5 : 250,
|
---|
445 | 10 : 210,
|
---|
446 | 15 : 200,
|
---|
447 | 25 : 190,
|
---|
448 | 30 : 175,
|
---|
449 | 40 : 162 }
|
---|
450 |
|
---|
451 | #---------------------------------------------------------------------------------------
|
---|
452 |
|
---|
453 | class B736(Boeing737):
|
---|
454 | """Boeing 737-600 aircraft."""
|
---|
455 | def __init__(self, flight):
|
---|
456 | super(B736, self).__init__(flight)
|
---|
457 | self.dow = 38307
|
---|
458 | self.mtow = 58328
|
---|
459 | self.mlw = 54657
|
---|
460 | self.mzfw = 51482
|
---|
461 |
|
---|
462 | #---------------------------------------------------------------------------------------
|
---|
463 |
|
---|
464 | class B737(Boeing737):
|
---|
465 | """Boeing 737-700 aircraft."""
|
---|
466 | def __init__(self, flight):
|
---|
467 | super(B737, self).__init__(flight)
|
---|
468 | self.dow = 39250
|
---|
469 | self.mtow = 61410
|
---|
470 | self.mlw = 58059
|
---|
471 | self.mzfw = 54657
|
---|
472 |
|
---|
473 | #---------------------------------------------------------------------------------------
|
---|
474 |
|
---|
475 | class B738(Boeing737):
|
---|
476 | """Boeing 737-800 aircraft."""
|
---|
477 | def __init__(self, flight):
|
---|
478 | super(B738, self).__init__(flight)
|
---|
479 | self.dow = 42690
|
---|
480 | self.mtow = 71709
|
---|
481 | self.mlw = 65317
|
---|
482 | self.mzfw = 61688
|
---|
483 |
|
---|
484 | #---------------------------------------------------------------------------------------
|
---|
485 |
|
---|
486 | class B738Charter(B738):
|
---|
487 | """Boeing 737-800 aircraft used for charters."""
|
---|
488 | def __init__(self, flight):
|
---|
489 | super(B738Charter, self).__init__(flight)
|
---|
490 | self.mtow = 77791
|
---|
491 |
|
---|
492 | #---------------------------------------------------------------------------------------
|
---|
493 |
|
---|
494 | class B733(Boeing737):
|
---|
495 | """Boeing 737-300 aircraft."""
|
---|
496 | def __init__(self, flight):
|
---|
497 | super(B733, self).__init__(flight)
|
---|
498 | self.dow = 32700
|
---|
499 | self.mtow = 62820
|
---|
500 | self.mlw = 51700
|
---|
501 | self.mzfw = 48410
|
---|
502 |
|
---|
503 | #---------------------------------------------------------------------------------------
|
---|
504 |
|
---|
505 | class B734(Boeing737):
|
---|
506 | """Boeing 737-400 aircraft."""
|
---|
507 | def __init__(self, flight):
|
---|
508 | super(B734, self).__init__(flight)
|
---|
509 | self.dow = 33200
|
---|
510 | self.mtow = 68050
|
---|
511 | self.mlw = 56200
|
---|
512 | self.mzfw = 53100
|
---|
513 |
|
---|
514 | #---------------------------------------------------------------------------------------
|
---|
515 |
|
---|
516 | class B735(Boeing737):
|
---|
517 | """Boeing 737-500 aircraft."""
|
---|
518 | def __init__(self, flight):
|
---|
519 | super(B735, self).__init__(flight)
|
---|
520 | self.dow = 31300
|
---|
521 | self.mtow = 60550
|
---|
522 | self.mlw = 50000
|
---|
523 | self.mzfw = 46700
|
---|
524 |
|
---|
525 | #---------------------------------------------------------------------------------------
|
---|
526 |
|
---|
527 | class DH8D(Aircraft):
|
---|
528 | """Bombardier Dash-8 Q400 aircraft.
|
---|
529 |
|
---|
530 | The aircraft type-specific values in the aircraft state have the following
|
---|
531 | structure:
|
---|
532 | - fuel: left, right
|
---|
533 | - n1: left, right
|
---|
534 | - reverser: left, right."""
|
---|
535 |
|
---|
536 | def __init__(self, flight):
|
---|
537 | super(DH8D, self).__init__(flight)
|
---|
538 | self.dow = 17185
|
---|
539 | self.mtow = 29257
|
---|
540 | self.mlw = 28009
|
---|
541 | self.mzfw = 25855
|
---|
542 | self.gearSpeedLimit = 215
|
---|
543 | self.flapSpeedLimits = { 5 : 200,
|
---|
544 | 10 : 181,
|
---|
545 | 15 : 172,
|
---|
546 | 35 : 158 }
|
---|
547 |
|
---|
548 | #---------------------------------------------------------------------------------------
|
---|
549 |
|
---|
550 | class Boeing767(Aircraft):
|
---|
551 | """Base class for the various aircraft in the Boeing 767 family.
|
---|
552 |
|
---|
553 | The aircraft type-specific values in the aircraft state have the following
|
---|
554 | structure:
|
---|
555 | - fuel: left, centre, right
|
---|
556 | - n1: left, right
|
---|
557 | - reverser: left, right"""
|
---|
558 |
|
---|
559 | def __init__(self, flight):
|
---|
560 | super(Boeing767, self).__init__(flight)
|
---|
561 | self._checkers.append(checks.ThrustChecker())
|
---|
562 | self.gearSpeedLimit = 270
|
---|
563 | self.flapSpeedLimits = { 1 : 255,
|
---|
564 | 5 : 235,
|
---|
565 | 10 : 215,
|
---|
566 | 20 : 215,
|
---|
567 | 25 : 185,
|
---|
568 | 30 : 175 }
|
---|
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 | def __init__(self, flight):
|
---|
603 | super(CRJ2, self).__init__(flight)
|
---|
604 | self._checkers.append(checks.ThrustChecker())
|
---|
605 | self.dow = 14549
|
---|
606 | self.mtow = 22995
|
---|
607 | self.mlw = 21319
|
---|
608 | self.mzfw = 19958
|
---|
609 | self.gearSpeedLimit = 240
|
---|
610 | self.flapSpeedLimits = { 8 : 260,
|
---|
611 | 20 : 220,
|
---|
612 | 30 : 190,
|
---|
613 | 45 : 175 }
|
---|
614 |
|
---|
615 | #---------------------------------------------------------------------------------------
|
---|
616 |
|
---|
617 | class F70(Aircraft):
|
---|
618 | """Fokker 70 aircraft.
|
---|
619 |
|
---|
620 | The aircraft type-specific values in the aircraft state have the following
|
---|
621 | structure:
|
---|
622 | - fuel: left, centre, right
|
---|
623 | - n1: left, right
|
---|
624 | - reverser: left, right."""
|
---|
625 | def __init__(self, flight):
|
---|
626 | super(F70, self).__init__(flight)
|
---|
627 | self._checkers.append(checks.ThrustChecker())
|
---|
628 | self.dow = 24283
|
---|
629 | self.mtow = 38100 # FIXME: differentiate by registration number,
|
---|
630 | # MTOW of HA-LMF: 41955
|
---|
631 | self.mlw = 36740
|
---|
632 | self.mzfw = 32655
|
---|
633 | self.gearSpeedLimit = 200
|
---|
634 | self.flapSpeedLimits = { 8 : 250,
|
---|
635 | 15 : 220,
|
---|
636 | 25 : 220,
|
---|
637 | 42 : 180 }
|
---|
638 |
|
---|
639 | #---------------------------------------------------------------------------------------
|
---|
640 |
|
---|
641 | class DC3(Aircraft):
|
---|
642 | """Lisunov Li-2 (DC-3) aircraft.
|
---|
643 |
|
---|
644 | The aircraft type-specific values in the aircraft state have the following
|
---|
645 | structure:
|
---|
646 | - fuel: left aux, left, right, right aux
|
---|
647 | - rpm: left, right
|
---|
648 | - reverser: left, right."""
|
---|
649 | def __init__(self, flight):
|
---|
650 | super(DC3, self).__init__(flight)
|
---|
651 | self.dow = 8627
|
---|
652 | self.mtow = 11884
|
---|
653 | self.mlw = 11793
|
---|
654 | self.mzfw = 11780
|
---|
655 | self.gearSpeedLimit = 148
|
---|
656 | self.flapSpeedLimits = { 15 : 135,
|
---|
657 | 30 : 99,
|
---|
658 | 45 : 97 }
|
---|
659 |
|
---|
660 | def _checkFlightEnd(self, aircraftState):
|
---|
661 | """Check if the end of the flight has arrived.
|
---|
662 |
|
---|
663 | This implementation checks the RPM values to be 0."""
|
---|
664 | for rpm in aircraftState.rpm:
|
---|
665 | if rpm>0: return False
|
---|
666 | return True
|
---|
667 |
|
---|
668 | #---------------------------------------------------------------------------------------
|
---|
669 |
|
---|
670 | class T134(Aircraft):
|
---|
671 | """Tupolev Tu-134 aircraft.
|
---|
672 |
|
---|
673 | The aircraft type-specific values in the aircraft state have the following
|
---|
674 | structure:
|
---|
675 | - fuel: left tip, left aux, centre, right aux, right tip, external 1,
|
---|
676 | external 2
|
---|
677 | - n1: left, right
|
---|
678 | - reverser: left, right."""
|
---|
679 | def __init__(self, flight):
|
---|
680 | super(T134, self).__init__(flight)
|
---|
681 | self._checkers.append(checks.ThrustChecker())
|
---|
682 | self.dow = 29500
|
---|
683 | self.mtow = 49000
|
---|
684 | self.mlw = 43000
|
---|
685 | self.mzfw = 38500
|
---|
686 | self.gearSpeedLimit = 216
|
---|
687 | self.flapSpeedLimits = { 10 : 450,
|
---|
688 | 20 : 400,
|
---|
689 | 30 : 300 }
|
---|
690 |
|
---|
691 | @property
|
---|
692 | def speedInKnots(self):
|
---|
693 | """Indicate if the speed is in knots."""
|
---|
694 | return False
|
---|
695 |
|
---|
696 | def _appendLightsLoggers(self):
|
---|
697 | """Append the loggers needed for the lights."""
|
---|
698 | self._checkers.append(checks.AnticollisionLightsLogger())
|
---|
699 | self._checkers.append(checks.LandingLightsLogger())
|
---|
700 | self._checkers.append(checks.NavLightsLogger())
|
---|
701 |
|
---|
702 | def _appendLightsCheckers(self):
|
---|
703 | """Append the checkers needed for the lights."""
|
---|
704 | self._checkers.append(checks.TupolevAntiCollisionLightsChecker())
|
---|
705 | self._checkers.append(checks.LandingLightsChecker())
|
---|
706 | self._checkers.append(checks.NavLightsChecker())
|
---|
707 |
|
---|
708 | #---------------------------------------------------------------------------------------
|
---|
709 |
|
---|
710 | class T154(Aircraft):
|
---|
711 | """Tupolev Tu-154 aircraft.
|
---|
712 |
|
---|
713 | The aircraft type-specific values in the aircraft state have the following
|
---|
714 | structure:
|
---|
715 | - fuel: left aux, left, centre, centre 2, right, right aux
|
---|
716 | - n1: left, centre, right
|
---|
717 | - reverser: left, right"""
|
---|
718 | def __init__(self, flight):
|
---|
719 | super(T154, self).__init__(flight)
|
---|
720 | self.dow = 53259
|
---|
721 | self.mtow = 98000
|
---|
722 | self.mlw = 78000
|
---|
723 | self.mzfw = 72000
|
---|
724 | self.gearSpeedLimit = 216
|
---|
725 | self.flapSpeedLimits = { 15 : 227,
|
---|
726 | 28 : 194,
|
---|
727 | 45 : 162 }
|
---|
728 |
|
---|
729 | @property
|
---|
730 | def speedInKnots(self):
|
---|
731 | """Indicate if the speed is in knots."""
|
---|
732 | return False
|
---|
733 |
|
---|
734 | def _appendLightsLoggers(self):
|
---|
735 | """Append the loggers needed for the lights."""
|
---|
736 | self._checkers.append(checks.AnticollisionLightsLogger())
|
---|
737 | self._checkers.append(checks.LandingLightsLogger())
|
---|
738 | self._checkers.append(checks.NavLightsLogger())
|
---|
739 |
|
---|
740 | def _appendLightsCheckers(self):
|
---|
741 | """Append the checkers needed for the lights."""
|
---|
742 | self._checkers.append(checks.TupolevAntiCollisionLightsChecker())
|
---|
743 | self._checkers.append(checks.LandingLightsChecker())
|
---|
744 | self._checkers.append(checks.NavLightsChecker())
|
---|
745 |
|
---|
746 | #---------------------------------------------------------------------------------------
|
---|
747 |
|
---|
748 |
|
---|
749 | class YK40(Aircraft):
|
---|
750 | """Yakovlev Yak-40 aircraft.
|
---|
751 |
|
---|
752 | The aircraft type-specific values in the aircraft state have the following
|
---|
753 | structure:
|
---|
754 | - fuel: left, right
|
---|
755 | - n1: left, right
|
---|
756 | - reverser: left, right"""
|
---|
757 | def __init__(self, flight):
|
---|
758 | super(YK40, self).__init__(flight)
|
---|
759 | self._checkers.append(checks.ThrustChecker())
|
---|
760 | self.dow = 9400
|
---|
761 | self.mtow = 17200
|
---|
762 | self.mlw = 16800
|
---|
763 | self.mzfw = 12100
|
---|
764 | self.gearSpeedLimit = 165
|
---|
765 | self.flapSpeedLimits = { 20 : 165,
|
---|
766 | 35 : 135 }
|
---|
767 |
|
---|
768 | @property
|
---|
769 | def speedInKnots(self):
|
---|
770 | """Indicate if the speed is in knots."""
|
---|
771 | return False
|
---|
772 |
|
---|
773 | def _appendLightsLoggers(self):
|
---|
774 | """Append the loggers needed for the lights."""
|
---|
775 | self._checkers.append(checks.AnticollisionLightsLogger())
|
---|
776 | self._checkers.append(checks.LandingLightsLogger())
|
---|
777 | self._checkers.append(checks.NavLightsLogger())
|
---|
778 |
|
---|
779 | def _appendLightsCheckers(self):
|
---|
780 | """Append the checkers needed for the lights."""
|
---|
781 | self._checkers.append(checks.AntiCollisionLightsChecker())
|
---|
782 | self._checkers.append(checks.LandingLightsChecker())
|
---|
783 | self._checkers.append(checks.NavLightsChecker())
|
---|
784 |
|
---|
785 | #---------------------------------------------------------------------------------------
|
---|
786 |
|
---|
787 | mostFuelTanks = [const.FUELTANK_LEFT_TIP, const.FUELTANK_EXTERNAL1,
|
---|
788 | const.FUELTANK_LEFT_AUX,
|
---|
789 | const.FUELTANK_CENTRE,
|
---|
790 | const.FUELTANK_RIGHT_AUX,
|
---|
791 | const.FUELTANK_EXTERNAL2, const.FUELTANK_RIGHT_TIP]
|
---|
792 |
|
---|
793 | #---------------------------------------------------------------------------------------
|
---|
794 |
|
---|
795 | _classes = { const.AIRCRAFT_B736 : B736,
|
---|
796 | const.AIRCRAFT_B737 : B737,
|
---|
797 | const.AIRCRAFT_B738 : B738,
|
---|
798 | const.AIRCRAFT_B738C : B738Charter,
|
---|
799 | const.AIRCRAFT_B733 : B733,
|
---|
800 | const.AIRCRAFT_B734 : B734,
|
---|
801 | const.AIRCRAFT_B735 : B735,
|
---|
802 | const.AIRCRAFT_DH8D : DH8D,
|
---|
803 | const.AIRCRAFT_B762 : B762,
|
---|
804 | const.AIRCRAFT_B763 : B763,
|
---|
805 | const.AIRCRAFT_CRJ2 : CRJ2,
|
---|
806 | const.AIRCRAFT_F70 : F70,
|
---|
807 | const.AIRCRAFT_DC3 : DC3,
|
---|
808 | const.AIRCRAFT_T134 : T134,
|
---|
809 | const.AIRCRAFT_T154 : T154,
|
---|
810 | const.AIRCRAFT_YK40 : YK40 }
|
---|
811 |
|
---|
812 | #---------------------------------------------------------------------------------------
|
---|
813 |
|
---|
814 | if __name__ == "__main__":
|
---|
815 | value = SmoothedValue()
|
---|
816 |
|
---|
817 | print "Adding 1, 12.0"
|
---|
818 | value.add(1, 12.0)
|
---|
819 | print value.get()
|
---|
820 |
|
---|
821 | print "Adding 1, 15.0"
|
---|
822 | value.add(1, 15.0)
|
---|
823 | print value.get()
|
---|
824 |
|
---|
825 | print "Adding 2, 18.0"
|
---|
826 | value.add(2, 18.0)
|
---|
827 | print value.get()
|
---|
828 |
|
---|
829 | print "Adding 2, 20.0"
|
---|
830 | value.add(2, 20.0)
|
---|
831 | print value.get()
|
---|
832 |
|
---|
833 | print "Adding 5, 22.0"
|
---|
834 | value.add(5, 22.0)
|
---|
835 | print value.get()
|
---|
836 |
|
---|
837 | print "Adding 5, 25.0"
|
---|
838 | value.add(5, 25.0)
|
---|
839 | print value.get()
|
---|
840 |
|
---|
841 | print "Adding 5, 29.0"
|
---|
842 | value.add(5, 29.0)
|
---|
843 | print value.get()
|
---|
844 |
|
---|
845 | print "Adding 5, 21.0"
|
---|
846 | value.add(5, 21.0)
|
---|
847 | print value.get()
|
---|
848 |
|
---|
849 | print "Adding 5, 26.0"
|
---|
850 | value.add(5, 26.0)
|
---|
851 | print value.get()
|
---|
852 |
|
---|
853 | print "Adding 2, 30.0"
|
---|
854 | value.add(2, 30.0)
|
---|
855 | print value.get()
|
---|
856 |
|
---|
857 | print "Adding 2, 55.0"
|
---|
858 | value.add(2, 55.0)
|
---|
859 | print value.get()
|
---|
860 |
|
---|
861 | #---------------------------------------------------------------------------------------
|
---|