1 |
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2 | import const
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3 | import gates
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4 | import checks
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5 | import fs
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6 | from i18n import xstr
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7 | import util
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8 |
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9 | import sys
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10 | import time
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11 | import traceback
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12 |
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13 | from collections import deque
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14 |
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15 | #---------------------------------------------------------------------------------------
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16 |
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17 | ## @package mlx.acft
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18 | #
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19 | # The simulator-independent aircraft classes.
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20 | #
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21 | # This module contains the aircraft classes that contain some general data
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22 | # about each aircraft type in the MAVA Fleet. The base class, \ref Aircraft
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23 | # also implements some parts of the logging and traces some data. The classes
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24 | # are also responsible for creating the \ref mlx.checks "checkers". Most of
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25 | # them are created by the \ref Aircraft class' constructor, but there can be
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26 | # type-specific differences. For example the lights are different for different
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27 | # types, so there is a \ref Aircraft._appendLightsLoggers "function" which can
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28 | # be reimplemented in child classes, if needed. This class maintains also the
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29 | # \ref SmoothedValue "smoothed values" of the IAS and the VS and set these
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30 | # values in the \ref mlx.fs.AircraftState "aircraft state" when it is received
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31 | # from the simulator.
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32 |
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33 | #---------------------------------------------------------------------------------------
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34 |
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35 | # Derate type: no derate possible
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36 | DERATE_NONE = 0
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37 |
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38 | # Derate type: Boeing, i.e. a percentage value.
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39 | # For logging, the percentage value is expected as a string (i.e. whatever the
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40 | # pilot enters into the text field).
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41 | DERATE_BOEING = 1
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42 |
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43 | # Derate type: EPR, i.e. an EPR value.
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44 | # For logging, the EPR value is expected as a string (i.e. whatever the pilot
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45 | # enters into the text field).
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46 | DERATE_EPR = 2
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47 |
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48 | # Derate type: Tupolev, i.e. nominal or takeoff
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49 | # For logging, one of the DERATE_TUPOLEV_xxx values are expected.
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50 | DERATE_TUPOLEV = 3
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51 |
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52 | # Tupolev derate value: nominal
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53 | DERATE_TUPOLEV_NOMINAL = 1
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54 |
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55 | # Tupolev derate value: takeoff
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56 | DERATE_TUPOLEV_TAKEOFF = 2
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57 |
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58 | # Derate type: BAe-146, i.e. enabled or not
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59 | # For logging, a boolean is expected.
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60 | DERATE_B462 = 4
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61 |
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62 | #---------------------------------------------------------------------------------------
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63 |
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64 | class SmoothedValue(object):
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65 | """A smoothed value."""
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66 | def __init__(self):
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67 | """Construct the value."""
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68 | self._deque = deque()
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69 | self._sum = 0
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70 |
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71 | def add(self, length, value):
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72 | """Add the given value and smooth with the given length."""
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73 | dequeLength = len(self._deque)
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74 | while dequeLength>=length:
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75 | self._sum -= self._deque.popleft()
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76 | dequeLength -= 1
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77 |
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78 | self._sum += value
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79 | self._deque.append(value)
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80 |
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81 | def get(self):
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82 | """Get the average."""
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83 | return self._sum / len(self._deque)
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84 |
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85 | #---------------------------------------------------------------------------------------
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86 |
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87 | class Aircraft(object):
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88 | """Base class for aircraft."""
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89 | @staticmethod
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90 | def create(flight):
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91 | """Create an aircraft instance for the type in the given flight."""
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92 | return _classes[flight.aircraftType](flight)
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93 |
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94 | def __init__(self, flight, minLandingFuel = None,
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95 | recommendedLandingFuel = None):
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96 | """Construct the aircraft for the given type."""
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97 | self._flight = flight
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98 | self._minLandingFuel = minLandingFuel
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99 | self._recommendedLandingFuel = recommendedLandingFuel
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100 |
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101 | self._name = None
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102 | self._modelName = None
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103 |
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104 | self._aircraftState = None
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105 |
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106 | self._maxVS = -10000.0
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107 | self._minVS = 10000.0
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108 |
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109 | self._v1r2LineIndex = None
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110 | self._derateLineID = None
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111 | self._takeoffAntiIceLineID = None
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112 | self._vrefLineIndex = None
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113 | self._landingAntiIceLineID = None
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114 |
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115 | self.humanWeight = 82.0
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116 |
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117 | self.initialClimbSpeedAltitude = 1500
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118 | self.reverseMinSpeed = 50
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119 |
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120 | self.maxTakeOffPitch = 15.0
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121 | self.maxTouchDownPitch = 15.0
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122 | self.brakeCoolTime = 10.0
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123 |
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124 | self._checkers = []
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125 |
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126 | config = flight.config
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127 | # Loggers
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128 |
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129 | self._checkers.append(checks.StageChecker())
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130 | self._checkers.append(checks.TakeOffLogger())
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131 |
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132 | self._checkers.append(checks.AltimeterLogger())
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133 |
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134 | self._ilsLogger = checks.ILSLogger()
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135 | self._checkers.append(self._ilsLogger)
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136 | self._nav1Logger = checks.NAV1Logger()
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137 | self._checkers.append(self._nav1Logger)
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138 | self._nav2Logger = checks.NAV2Logger()
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139 | self._checkers.append(self._nav2Logger)
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140 |
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141 | self._adf1Logger = checks.ADF1Logger()
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142 | self._checkers.append(self._adf1Logger)
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143 | self._adf2Logger = checks.ADF2Logger()
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144 | self._checkers.append(self._adf2Logger)
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145 |
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146 | self._checkers.append(checks.SquawkLogger())
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147 |
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148 | self._appendLightsLoggers()
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149 |
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150 | self._checkers.append(checks.FlapsLogger())
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151 |
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152 | self._checkers.append(checks.GearsLogger())
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153 | self._checkers.append(checks.InitialClimbSpeedLogger())
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154 | self._checkers.append(checks.CruiseSpeedLogger())
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155 | self._checkers.append(checks.SpoilerLogger())
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156 | self._checkers.append(checks.APLogger())
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157 |
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158 | if config.isMessageTypeFS(const.MESSAGETYPE_VISIBILITY):
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159 | self._checkers.append(checks.VisibilityChecker())
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160 |
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161 | # FIXME: we should have a central data model object, and not collect
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162 | # the data from the GUI. However, some pieces of data (e.g. V-speeds,
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163 | # etc. that is entered into the GUI) *should* be a part of the GUI and
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164 | # queried from it, so the model should have a reference to the GUI as
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165 | # well and access such data via the GUI!
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166 | if config.onlineACARS and flight.loggedIn and not flight.entranceExam:
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167 | self._checkers.append(checks.ACARSSender(flight._gui))
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168 |
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169 | # Fault checkers
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170 |
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171 | self._appendLightsCheckers()
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172 |
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173 | self._checkers.append(checks.TransponderChecker())
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174 |
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175 | self._checkers.append(checks.BankChecker())
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176 |
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177 | self._checkers.append(checks.FlapsRetractChecker())
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178 | self._checkers.append(checks.FlapsSpeedLimitChecker())
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179 |
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180 | self._checkers.append(checks.GearsDownChecker())
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181 | self._checkers.append(checks.GearSpeedLimitChecker())
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182 |
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183 | self._checkers.append(checks.GLoadChecker())
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184 |
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185 | self._checkers.append(checks.MLWChecker())
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186 | self._checkers.append(checks.MTOWChecker())
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187 | self._checkers.append(checks.MZFWChecker())
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188 | self._checkers.append(checks.PayloadChecker())
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189 |
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190 | self._checkers.append(checks.SpeedChecker())
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191 | self._checkers.append(checks.VSChecker())
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192 |
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193 | timeout = 30.0 + config.realIASSmoothingLength - 1
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194 | self._checkers.append(checks.OverspeedChecker(faultTimeout = timeout))
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195 |
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196 | self._checkers.append(checks.StallChecker())
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197 |
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198 | self._checkers.append(checks.PitotChecker())
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199 |
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200 | self._checkers.append(checks.ReverserLogger())
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201 | self._checkers.append(checks.ReverserChecker())
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202 |
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203 | if flight.aircraftType is not None and config.enableApproachCallouts:
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204 | approachCallouts = flight.config.getApproachCallouts(flight.aircraftType)
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205 | if approachCallouts:
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206 | self._checkers.append(checks.ApproachCalloutsPlayer(approachCallouts))
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207 |
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208 | self._smoothedIAS = SmoothedValue()
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209 | self._smoothedVS = SmoothedValue()
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210 |
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211 | @property
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212 | def type(self):
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213 | """Get the type of the aircraft."""
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214 | return self._flight.aircraftType
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215 |
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216 | @property
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217 | def flight(self):
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218 | """Get the flight the aircraft belongs to."""
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219 | return self._flight
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220 |
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221 | @property
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222 | def minLandingFuel(self):
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223 | """Get the minimum acceptable amount of the landing fuel."""
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224 | return self._minLandingFuel
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225 |
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226 | @property
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227 | def recommendedLandingFuel(self):
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228 | """Get the recommended amount of the landing fuel."""
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229 | return self._recommendedLandingFuel
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230 |
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231 | @property
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232 | def logger(self):
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233 | """Get the logger to use for the aircraft."""
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234 | return self._flight.logger
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235 |
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236 | @property
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237 | def state(self):
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238 | """Get the current aircraft state."""
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239 | return self._aircraftState
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240 |
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241 | @property
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242 | def speedInKnots(self):
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243 | """Indicate if the speed is in knots.
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244 |
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245 | This default implementation returns True."""
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246 | return True
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247 |
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248 | @property
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249 | def timestamp(self):
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250 | """Get the timestamp of the current state."""
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251 | return None if self._aircraftState is None \
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252 | else self._aircraftState.timestamp
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253 |
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254 | @property
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255 | def derateType(self):
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256 | """Get the derate type for this aircraft.
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257 |
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258 | This default implementation returns DERATE_NONE."""
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259 | return DERATE_NONE
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260 |
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261 | def getDerateLine(self, value):
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262 | """Get the log line for the given derate value.
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263 |
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264 | It uses the the derate type and produces the standard message for
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265 | each. This children need not override it, although they can."""
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266 | dt = self.derateType
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267 |
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268 | if dt==DERATE_BOEING:
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269 | return "Derate calculated by the pilot: %s %%" % \
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270 | ("-" if value is None else value,)
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271 | elif dt==DERATE_EPR:
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272 | return "EPR calculated by the pilot: %s" % \
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273 | ("-" if value is None else value,)
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274 | elif dt==DERATE_TUPOLEV:
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275 | return "Thrust setting calculated by the pilot: %s" % \
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276 | ("-" if value is None else
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277 | "nominal" if value==DERATE_TUPOLEV_NOMINAL else "takeoff",)
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278 | elif dt==DERATE_B462:
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279 | return "Derate setting: %s" % \
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280 | ("-" if value is None else "enabled" if value else "disabled",)
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281 | elif dt!=DERATE_NONE:
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282 | print "mlx.acft.getDerateLine: invalid derate type: " + dt
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283 |
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284 | return None
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285 |
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286 | def getFlapsSpeedLimit(self, flaps):
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287 | """Get the speed limit for the given flaps setting."""
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288 | return self.flapSpeedLimits[flaps] if flaps in self.flapSpeedLimits \
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289 | else None
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290 |
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291 | def modelChanged(self, timestamp, aircraftName, modelName):
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292 | """Called when the simulator's aircraft changes."""
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293 | self._name = aircraftName
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294 | self._modelName = modelName
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295 | if self._flight.stage is not None:
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296 | self._logNameAndModel(timestamp)
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297 |
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298 | def handleState(self, aircraftState):
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299 | """Called when the state of the aircraft changes.
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300 |
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301 | This is the function that the simulator calls directly with the new
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302 | state."""
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303 | try:
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304 | config = self._flight.config
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305 |
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306 | self._smoothedIAS.add(config.realIASSmoothingLength, aircraftState.ias)
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307 | aircraftState.smoothedIAS = self._smoothedIAS.get()
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308 |
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309 | self._smoothedVS.add(config.realVSSmoothingLength, aircraftState.vs)
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310 | aircraftState.smoothedVS = self._smoothedVS.get()
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311 |
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312 | for checker in self._checkers:
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313 | try:
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314 | checker.check(self._flight, self, self._flight.logger,
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315 | self._aircraftState, aircraftState)
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316 | except:
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317 | print >> sys.stderr, "Checker", checker, "failed"
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318 | traceback.print_exc()
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319 |
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320 | self._flight.handleState(self._aircraftState, aircraftState)
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321 |
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322 | self._maxVS = max(self._maxVS, aircraftState.vs)
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323 | self._minVS = min(self._minVS, aircraftState.vs)
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324 | except:
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325 | print >> sys.stderr, "Failed to handle the state"
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326 | traceback.print_exc()
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327 | finally:
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328 | self._aircraftState = aircraftState
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329 |
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330 | def setStage(self, aircraftState, newStage):
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331 | """Set the given stage as the new one and do whatever should be
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332 | done."""
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333 | if newStage==const.STAGE_BOARDING:
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334 | self._logNameAndModel(aircraftState.timestamp)
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335 |
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336 | oldStage = self._flight.stage
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337 |
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338 | if self._flight.setStage(aircraftState.timestamp, newStage):
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339 | if newStage==const.STAGE_PUSHANDTAXI:
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340 | self.logger.message(aircraftState.timestamp, "Block time start")
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341 | self._flight.logFuel(aircraftState)
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342 | self.logger.message(aircraftState.timestamp,
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343 | "ZFW: %.2f kg" % (aircraftState.zfw))
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344 | flight = self._flight
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345 | if flight.v1 is None or flight.vr is None or flight.v2 is None:
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346 | fs.sendMessage(const.MESSAGETYPE_HELP,
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347 | "Don't forget to set the takeoff V-speeds!",
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348 | 5)
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349 | elif newStage==const.STAGE_TAKEOFF:
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350 | if oldStage == const.STAGE_RTO and self._flight.hasRTO:
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351 | rtoState = self._flight.rtoState
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352 | if (aircraftState.timestamp - rtoState.timestamp) < \
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353 | (self.brakeCoolTime * 60.0):
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354 | self.logger.fault("brakeCoolTime",
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355 | aircraftState.timestamp,
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356 | "Did not cool the brakes for at least %.f minutes after the RTO" % (self.brakeCoolTime,),
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357 | 15.0)
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358 | self.logger.message(aircraftState.timestamp,
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359 | "Flight time start")
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360 | self.logger.message(aircraftState.timestamp,
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361 | "Takeoff weight: %.0f kg, MTOW: %.0f kg" % \
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362 | (aircraftState.grossWeight, self.mtow))
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363 | self._logQNH(aircraftState)
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364 | self.logger.message(aircraftState.timestamp,
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365 | "Wind %03.0f/%.0f" % \
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366 | (aircraftState.windDirection,
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367 | aircraftState.windSpeed))
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368 | self._logRadios(aircraftState)
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369 | self._logV1R2(aircraftState)
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370 | self._logDerate(aircraftState)
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371 | self._logTakeoffAntiIce(aircraftState)
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372 | elif newStage==const.STAGE_DESCENT or newStage==const.STAGE_LANDING:
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373 | self._logRadios(aircraftState)
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374 | if newStage==const.STAGE_LANDING:
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375 | self._logQNH(aircraftState)
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376 | elif newStage==const.STAGE_TAXIAFTERLAND:
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377 | flight = self._flight
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378 | bookedFlight = flight.bookedFlight
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379 | config = flight.config
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380 | if config.onlineGateSystem and \
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381 | flight.loggedIn and \
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382 | not flight.entranceExam and \
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383 | bookedFlight.arrivalICAO=="LHBP" and \
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384 | config.isMessageTypeFS(const.MESSAGETYPE_GATE_SYSTEM):
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385 | self._flight.getFleet(callback = self._fleetRetrieved,
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386 | force = True)
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387 | self.logger.message(aircraftState.timestamp, "Flight time end")
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388 | self._flight.logFuel(aircraftState)
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389 | if self._minLandingFuel is not None and \
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390 | aircraftState.totalFuel<self._minLandingFuel:
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391 | self._flight.handleFault(self.__class__,
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392 | aircraftState.timestamp,
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393 | "The amount of the landing fuel is less than the minimum for this type: %ukgs (possible NO GO!)" %
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394 | (self._minLandingFuel,), 0)
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395 | self.logger.message(aircraftState.timestamp,
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396 | "Landing weight: %.0f kg, MLW: %.0f" % \
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397 | (aircraftState.grossWeight, self.mlw))
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398 | self.logger.message(aircraftState.timestamp,
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399 | "Vertical speed range: %.0f..%.0f feet/min" % \
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400 | (self._minVS, self._maxVS))
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401 | # elif newStage==const.STAGE_PARKING:
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402 | # self.logger.message(aircraftState.timestamp, "Block time end")
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403 | elif newStage==const.STAGE_END:
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404 | flightLength = self._flight.flightTimeEnd - self._flight.flightTimeStart
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405 | self.logger.message(aircraftState.timestamp, "Block time end")
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406 | self.logger.message(aircraftState.timestamp,
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407 | "Flight time: " +
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408 | util.getTimeIntervalString(flightLength))
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409 | self.logger.message(aircraftState.timestamp,
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410 | "Flown distance: %.2f NM" % \
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411 | (self._flight.flownDistance,))
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412 | blockLength = self._flight.blockTimeEnd - self._flight.blockTimeStart
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413 | self.logger.message(aircraftState.timestamp,
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414 | "Block time: " +
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415 | util.getTimeIntervalString(blockLength))
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416 |
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417 | def prepareFlare(self):
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418 | """Called when it is detected that we will soon flare.
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419 |
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420 | On the first call, it should start monitoring some parameters more
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421 | closely to determine flare time."""
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422 | self.flight.simulator.startFlare()
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423 |
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424 | def flareStarted(self, windSpeed, windDirection, visibility,
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425 | flareStart, flareStartFS):
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426 | """Called when the flare has started."""
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427 | self.logger.message(self._aircraftState.timestamp, "The flare has begun")
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428 | self.logger.message(self._aircraftState.timestamp,
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429 | "Wind %03.0f/%.0f" % \
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430 | (windDirection, windSpeed))
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431 | self.logger.message(self._aircraftState.timestamp,
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432 | "Visibility: %.0f metres" % (visibility,))
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433 | self._logQNH(self._aircraftState)
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434 | self._logVRef()
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435 | self._logLandingAntiIce(self._aircraftState)
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436 | self.flight.flareStarted(flareStart, flareStartFS)
|
---|
437 | fs.sendMessage(const.MESSAGETYPE_INFORMATION, "Flare-time", 3)
|
---|
438 |
|
---|
439 | def flareFinished(self, flareEnd, flareEndFS, tdRate, tdRateCalculatedByFS,
|
---|
440 | ias, pitch, bank, heading):
|
---|
441 | """Called when the flare has finished."""
|
---|
442 | (flareTimeFromFS, flareTime) = self.flight.flareFinished(flareEnd,
|
---|
443 | flareEndFS,
|
---|
444 | tdRate)
|
---|
445 | self.logger.message(self._aircraftState.timestamp,
|
---|
446 | "Flaretime: %.3f (from %s)" % \
|
---|
447 | (flareTime,
|
---|
448 | "the simulator" if flareTimeFromFS else "real time",))
|
---|
449 | self.logger.message(self._aircraftState.timestamp,
|
---|
450 | "Touchdown rate: %.0f feet/min" % (tdRate,))
|
---|
451 | self.logger.message(self._aircraftState.timestamp,
|
---|
452 | "Touchdown rate was calculated by the %s" % \
|
---|
453 | ("simulator" if tdRateCalculatedByFS else "logger",))
|
---|
454 | flight = self._flight
|
---|
455 | self.logger.message(self._aircraftState.timestamp,
|
---|
456 | "Touchdown speed: %.0f %s" % \
|
---|
457 | (flight.speedFromKnots(ias),
|
---|
458 | flight.getEnglishSpeedUnit()))
|
---|
459 | self.logger.message(self._aircraftState.timestamp,
|
---|
460 | "Touchdown pitch: %.1f degrees" % (pitch,))
|
---|
461 | self.logger.message(self._aircraftState.timestamp,
|
---|
462 | "Touchdown bank: %.1f degrees" % (bank,))
|
---|
463 | self.logger.message(self._aircraftState.timestamp,
|
---|
464 | "Touchdown heading: %03.0f degrees" % (heading,))
|
---|
465 | self.logger.message(self._aircraftState.timestamp,
|
---|
466 | "CG: %.1f%%" % \
|
---|
467 | (self._aircraftState.cog*100.0,))
|
---|
468 |
|
---|
469 | if abs(pitch)>self.maxTouchDownPitch:
|
---|
470 | self._flight.handleNoGo("TDPitch", self._aircraftState.timestamp,
|
---|
471 | "Touchdown pitch higher than aircraft maximum (%.2f)" % \
|
---|
472 | (self.maxTouchDownPitch,),
|
---|
473 | "TD TAILSTRIKE NO GO")
|
---|
474 |
|
---|
475 | def cancelFlare(self):
|
---|
476 | """Cancel flare, if it has started."""
|
---|
477 | self.flight.simulator.cancelFlare()
|
---|
478 |
|
---|
479 | def checkFlightEnd(self, aircraftState):
|
---|
480 | """Check if the end of the flight has arrived.
|
---|
481 |
|
---|
482 | This default implementation checks the N1 values, but for
|
---|
483 | piston-powered aircraft you need to check the RPMs."""
|
---|
484 | for n1 in aircraftState.n1:
|
---|
485 | if n1>=0.5: return False
|
---|
486 | return True
|
---|
487 |
|
---|
488 | def updateV1R2(self):
|
---|
489 | """Update the V1, Vr and V2 values from the flight, if the these values
|
---|
490 | have already been logged."""
|
---|
491 | if self._v1r2LineIndex is not None:
|
---|
492 | self._logV1R2()
|
---|
493 |
|
---|
494 | def updateDerate(self):
|
---|
495 | """Update the derate value from the flight, if the these values
|
---|
496 | have already been logged."""
|
---|
497 | if self._derateLineID is not None:
|
---|
498 | self._logDerate()
|
---|
499 |
|
---|
500 | def updateTakeoffAntiIce(self):
|
---|
501 | """Update the take-off anti-ice setting."""
|
---|
502 | if self._takeoffAntiIceLineID is not None:
|
---|
503 | self._logTakeoffAntiIce()
|
---|
504 |
|
---|
505 | def _appendLightsLoggers(self):
|
---|
506 | """Append the loggers needed for the lights.
|
---|
507 |
|
---|
508 | This default implementation adds the loggers for the anti-collision
|
---|
509 | lights, the landing lights, the strobe lights and the NAV lights."""
|
---|
510 | self._checkers.append(checks.AnticollisionLightsLogger())
|
---|
511 | self._checkers.append(checks.LandingLightsLogger())
|
---|
512 | self._checkers.append(checks.StrobeLightsLogger())
|
---|
513 | self._checkers.append(checks.NavLightsLogger())
|
---|
514 |
|
---|
515 | def _appendLightsCheckers(self):
|
---|
516 | """Append the checkers needed for the lights.
|
---|
517 |
|
---|
518 | This default implementation adds the checkers for the anti-collision
|
---|
519 | lights, the landing lights, the strobe lights and the NAV lights."""
|
---|
520 | self._checkers.append(checks.AntiCollisionLightsChecker())
|
---|
521 | self._checkers.append(checks.LandingLightsChecker())
|
---|
522 | self._checkers.append(checks.NavLightsChecker())
|
---|
523 | self._checkers.append(checks.StrobeLightsChecker())
|
---|
524 |
|
---|
525 | def _speedToLog(self, speed):
|
---|
526 | """Convert the given speed (being either None or expressed in the
|
---|
527 | flight's speed unit into a string."""
|
---|
528 | if speed is None:
|
---|
529 | return "-"
|
---|
530 | else:
|
---|
531 | return str(speed) + " " + self._flight.getEnglishSpeedUnit()
|
---|
532 |
|
---|
533 | def _logV1R2(self, state = None):
|
---|
534 | """Log the V1, Vr and V2 value either newly, or by updating the
|
---|
535 | corresponding line."""
|
---|
536 | message = "Calc. TO speeds: V1: %s, VR: %s, V2: %s" % \
|
---|
537 | (self._speedToLog(self._flight.v1),
|
---|
538 | self._speedToLog(self._flight.vr),
|
---|
539 | self._speedToLog(self._flight.v2))
|
---|
540 |
|
---|
541 | if self._v1r2LineIndex is None:
|
---|
542 | if state is None:
|
---|
543 | state = self._aircraftState
|
---|
544 | self._v1r2LineIndex = \
|
---|
545 | self.logger.message(state.timestamp, message)
|
---|
546 | else:
|
---|
547 | self.logger.updateLine(self._v1r2LineIndex, message)
|
---|
548 |
|
---|
549 | def _logDerate(self, state = None):
|
---|
550 | """Log the derate values either newly or by updating the corresponding
|
---|
551 | line."""
|
---|
552 | dt = self.derateType
|
---|
553 | if dt==DERATE_NONE:
|
---|
554 | return
|
---|
555 |
|
---|
556 | message = self.getDerateLine(self._flight.derate)
|
---|
557 | if message is not None:
|
---|
558 | if self._derateLineID is None:
|
---|
559 | if state is None:
|
---|
560 | state = self._aircraftState
|
---|
561 | self._derateLineID = \
|
---|
562 | self.logger.message(state.timestamp, message)
|
---|
563 | else:
|
---|
564 | self.logger.updateLine(self._derateLineID, message)
|
---|
565 |
|
---|
566 | def _logTakeoffAntiIce(self, state = None):
|
---|
567 | """Log the take-off anti-ice setting either newly or by updating the
|
---|
568 | corresponding line."""
|
---|
569 | antiIceOn = self._flight.takeoffAntiIceOn
|
---|
570 | if state is not None:
|
---|
571 | antiIceOn = antiIceOn or state.antiIceOn is True
|
---|
572 | self._flight.takeoffAntiIceOn = antiIceOn
|
---|
573 |
|
---|
574 | message = "Anti-ice was turned %s" % \
|
---|
575 | ("ON" if antiIceOn else "OFF")
|
---|
576 |
|
---|
577 | if self._takeoffAntiIceLineID is None:
|
---|
578 | if state is None:
|
---|
579 | state = self._aircraftState
|
---|
580 | self._takeoffAntiIceLineID = \
|
---|
581 | self.logger.message(state.timestamp, message)
|
---|
582 | else:
|
---|
583 | self.logger.updateLine(self._takeoffAntiIceLineID, message)
|
---|
584 |
|
---|
585 | def updateVRef(self):
|
---|
586 | """Update the Vref value from the flight, if the Vref value has already
|
---|
587 | been logged."""
|
---|
588 | if self._vrefLineIndex is not None:
|
---|
589 | self._logVRef()
|
---|
590 |
|
---|
591 | def _logVRef(self):
|
---|
592 | """Log the Vref value either newly, or by updating the corresponding
|
---|
593 | line."""
|
---|
594 | message = "VRef speed calculated by the pilot: %s" % \
|
---|
595 | (self._speedToLog(self._flight.vref),)
|
---|
596 | if self._vrefLineIndex is None:
|
---|
597 | self._vrefLineIndex = \
|
---|
598 | self.logger.message(self._aircraftState.timestamp, message)
|
---|
599 | else:
|
---|
600 | self.logger.updateLine(self._vrefLineIndex, message)
|
---|
601 |
|
---|
602 | def updateLandingAntiIce(self):
|
---|
603 | """Update the landing anti-ice setting."""
|
---|
604 | if self._landingAntiIceLineID is not None:
|
---|
605 | self._logLandingAntiIce()
|
---|
606 |
|
---|
607 | def _logLandingAntiIce(self, state = None):
|
---|
608 | """Log the landing anti-ice setting either newly or by updating the
|
---|
609 | corresponding line."""
|
---|
610 | antiIceOn = self._flight.landingAntiIceOn
|
---|
611 | if state is not None:
|
---|
612 | antiIceOn = antiIceOn or state.antiIceOn is True
|
---|
613 | self._flight.landingAntiIceOn = antiIceOn
|
---|
614 |
|
---|
615 | message = "Anti-ice was turned %s" % \
|
---|
616 | ("ON" if antiIceOn else "OFF")
|
---|
617 |
|
---|
618 | if self._landingAntiIceLineID is None:
|
---|
619 | if state is None:
|
---|
620 | state = self._aircraftState
|
---|
621 | self._landingAntiIceLineID = \
|
---|
622 | self.logger.message(state.timestamp, message)
|
---|
623 | else:
|
---|
624 | self.logger.updateLine(self._landingAntiIceLineID, message)
|
---|
625 |
|
---|
626 | def _fleetRetrieved(self, fleet):
|
---|
627 | """Callback for the fleet retrieval result."""
|
---|
628 | if fleet is not None:
|
---|
629 | gateList = ""
|
---|
630 | occupiedGateNumbers = fleet.getOccupiedGateNumbers()
|
---|
631 | for gate in gates.lhbpGates.gates:
|
---|
632 | if gate.isAvailable(gates.lhbpGates, occupiedGateNumbers):
|
---|
633 | if gateList: gateList += ", "
|
---|
634 | gateList += gate.number
|
---|
635 | fs.sendMessage(const.MESSAGETYPE_GATE_SYSTEM,
|
---|
636 | "Free gates: " + gateList, 20)
|
---|
637 |
|
---|
638 |
|
---|
639 | def _logRadios(self, aircraftState):
|
---|
640 | """Log the radios from the given aircraft state."""
|
---|
641 | flight = self._flight
|
---|
642 | logger = flight.logger
|
---|
643 |
|
---|
644 | self._ilsLogger.forceLog(flight, logger, aircraftState)
|
---|
645 | self._nav1Logger.forceLog(flight, logger, aircraftState)
|
---|
646 | self._nav2Logger.forceLog(flight, logger, aircraftState)
|
---|
647 | self._adf1Logger.forceLog(flight, logger, aircraftState)
|
---|
648 | self._adf2Logger.forceLog(flight, logger, aircraftState)
|
---|
649 |
|
---|
650 | def _logQNH(self, aircraftState):
|
---|
651 | """Log the current QNH along with the altimeter setting."""
|
---|
652 | self.logger.message(aircraftState.timestamp,
|
---|
653 | "QNH: %.2f hPa, altimeter: %.2f hPa" % \
|
---|
654 | (aircraftState.qnh, aircraftState.altimeter))
|
---|
655 |
|
---|
656 | def _logNameAndModel(self, timestamp):
|
---|
657 | """Log the aircraft's name and model with taking the timestamp from the
|
---|
658 | given state."""
|
---|
659 | self._flight.logger.message(timestamp,
|
---|
660 | "Aircraft: name='%s', model='%s'" % \
|
---|
661 | (self._name, self._modelName))
|
---|
662 |
|
---|
663 | #---------------------------------------------------------------------------------------
|
---|
664 |
|
---|
665 | class Boeing737(Aircraft):
|
---|
666 | """Base class for the various aircraft in the Boeing 737 family.
|
---|
667 |
|
---|
668 | The aircraft type-specific values in the aircraft state have the following
|
---|
669 | structure:
|
---|
670 | - fuel: left, centre, right
|
---|
671 | - n1: left, right
|
---|
672 | - reverser: left, right"""
|
---|
673 | def __init__(self, flight, minLandingFuel = 2500,
|
---|
674 | recommendedLandingFuel = 3500):
|
---|
675 | super(Boeing737, self).__init__(flight,
|
---|
676 | minLandingFuel = minLandingFuel,
|
---|
677 | recommendedLandingFuel =
|
---|
678 | recommendedLandingFuel)
|
---|
679 |
|
---|
680 | self.gearSpeedLimit = 270
|
---|
681 | self.flapSpeedLimits = { 1 : 260,
|
---|
682 | 2 : 260,
|
---|
683 | 5 : 250,
|
---|
684 | 10 : 210,
|
---|
685 | 15 : 200,
|
---|
686 | 25 : 190,
|
---|
687 | 30 : 175,
|
---|
688 | 40 : 162 }
|
---|
689 |
|
---|
690 | @property
|
---|
691 | def derateType(self):
|
---|
692 | """Get the derate type for this type."""
|
---|
693 | return DERATE_BOEING
|
---|
694 |
|
---|
695 | #---------------------------------------------------------------------------------------
|
---|
696 |
|
---|
697 | class B736(Boeing737):
|
---|
698 | """Boeing 737-600 aircraft."""
|
---|
699 | def __init__(self, flight):
|
---|
700 | super(B736, self).__init__(flight)
|
---|
701 | self.dow = 38307
|
---|
702 | self.mtow = 58328
|
---|
703 | self.mlw = 54657
|
---|
704 | self.mzfw = 51482
|
---|
705 | self.maxTakeOffPitch = 16.2
|
---|
706 | self.maxTouchDownPitch = 14.7
|
---|
707 |
|
---|
708 | #---------------------------------------------------------------------------------------
|
---|
709 |
|
---|
710 | class B737(Boeing737):
|
---|
711 | """Boeing 737-700 aircraft."""
|
---|
712 | def __init__(self, flight):
|
---|
713 | super(B737, self).__init__(flight)
|
---|
714 | self.dow = 39250
|
---|
715 | self.mtow = 61410
|
---|
716 | self.mlw = 58059
|
---|
717 | self.mzfw = 54657
|
---|
718 | self.maxTakeOffPitch = 14.7
|
---|
719 | self.maxTouchDownPitch = 13.2
|
---|
720 |
|
---|
721 | #---------------------------------------------------------------------------------------
|
---|
722 |
|
---|
723 | class B738(Boeing737):
|
---|
724 | """Boeing 737-800 aircraft."""
|
---|
725 | def __init__(self, flight):
|
---|
726 | super(B738, self).__init__(flight)
|
---|
727 | self.dow = 42690
|
---|
728 | self.mtow = 71709
|
---|
729 | self.mlw = 65317
|
---|
730 | self.mzfw = 61688
|
---|
731 | self.maxTakeOffPitch = 11
|
---|
732 | self.maxTouchDownPitch = 9.5
|
---|
733 |
|
---|
734 | #---------------------------------------------------------------------------------------
|
---|
735 |
|
---|
736 | class B738Charter(B738):
|
---|
737 | """Boeing 737-800 aircraft used for charters."""
|
---|
738 | def __init__(self, flight):
|
---|
739 | super(B738Charter, self).__init__(flight)
|
---|
740 | self.mtow = 77791
|
---|
741 |
|
---|
742 | #---------------------------------------------------------------------------------------
|
---|
743 |
|
---|
744 | class Boeing737CL(Boeing737):
|
---|
745 | """Base class for the various aircraft in the Boeing 737 Classic family."""
|
---|
746 | def __init__(self, flight):
|
---|
747 | super(Boeing737CL, self).__init__(flight, minLandingFuel = 3500,
|
---|
748 | recommendedLandingFuel = None)
|
---|
749 |
|
---|
750 | #---------------------------------------------------------------------------------------
|
---|
751 |
|
---|
752 | class B733(Boeing737CL):
|
---|
753 | """Boeing 737-300 aircraft."""
|
---|
754 | def __init__(self, flight):
|
---|
755 | super(B733, self).__init__(flight)
|
---|
756 | self.dow = 32700
|
---|
757 | self.mtow = 62820
|
---|
758 | self.mlw = 51700
|
---|
759 | self.mzfw = 48410
|
---|
760 | self.maxTakeOffPitch = 13.4
|
---|
761 | self.maxTouchDownPitch = 12.0
|
---|
762 |
|
---|
763 | #---------------------------------------------------------------------------------------
|
---|
764 |
|
---|
765 | class B734(Boeing737CL):
|
---|
766 | """Boeing 737-400 aircraft."""
|
---|
767 | def __init__(self, flight):
|
---|
768 | super(B734, self).__init__(flight)
|
---|
769 | self.dow = 33200
|
---|
770 | self.mtow = 68050
|
---|
771 | self.mlw = 56200
|
---|
772 | self.mzfw = 53100
|
---|
773 | self.maxTakeOffPitch = 11.4
|
---|
774 | self.maxTouchDownPitch = 10
|
---|
775 |
|
---|
776 | #---------------------------------------------------------------------------------------
|
---|
777 |
|
---|
778 | class B735(Boeing737CL):
|
---|
779 | """Boeing 737-500 aircraft."""
|
---|
780 | def __init__(self, flight):
|
---|
781 | super(B735, self).__init__(flight)
|
---|
782 | self.dow = 31300
|
---|
783 | self.mtow = 60550
|
---|
784 | self.mlw = 50000
|
---|
785 | self.mzfw = 46700
|
---|
786 | self.maxTakeOffPitch = 14.7
|
---|
787 | self.maxTouchDownPitch = 13.2
|
---|
788 |
|
---|
789 | #---------------------------------------------------------------------------------------
|
---|
790 |
|
---|
791 | class DH8D(Aircraft):
|
---|
792 | """Bombardier Dash-8 Q400 aircraft.
|
---|
793 |
|
---|
794 | The aircraft type-specific values in the aircraft state have the following
|
---|
795 | structure:
|
---|
796 | - fuel: left, right
|
---|
797 | - n1: left, right
|
---|
798 | - reverser: left, right."""
|
---|
799 |
|
---|
800 | def __init__(self, flight):
|
---|
801 | super(DH8D, self).__init__(flight, minLandingFuel = 2000)
|
---|
802 | self.dow = 17185
|
---|
803 | self.mtow = 29257
|
---|
804 | self.mlw = 28009
|
---|
805 | self.mzfw = 25855
|
---|
806 | self.gearSpeedLimit = 215
|
---|
807 | self.flapSpeedLimits = { 5 : 200,
|
---|
808 | 10 : 181,
|
---|
809 | 15 : 172,
|
---|
810 | 35 : 158 }
|
---|
811 | self.maxTakeOffPitch = 8.0
|
---|
812 | self.maxTouchDownPitch = 7.0
|
---|
813 |
|
---|
814 | #---------------------------------------------------------------------------------------
|
---|
815 |
|
---|
816 | class Boeing767(Aircraft):
|
---|
817 | """Base class for the various aircraft in the Boeing 767 family.
|
---|
818 |
|
---|
819 | The aircraft type-specific values in the aircraft state have the following
|
---|
820 | structure:
|
---|
821 | - fuel: left, centre, right
|
---|
822 | - n1: left, right
|
---|
823 | - reverser: left, right"""
|
---|
824 |
|
---|
825 | def __init__(self, flight, minLandingFuel = 7000):
|
---|
826 | super(Boeing767, self).__init__(flight, minLandingFuel = minLandingFuel)
|
---|
827 | self.gearSpeedLimit = 270
|
---|
828 | self.flapSpeedLimits = { 1 : 255,
|
---|
829 | 5 : 235,
|
---|
830 | 10 : 215,
|
---|
831 | 20 : 215,
|
---|
832 | 25 : 185,
|
---|
833 | 30 : 175 }
|
---|
834 |
|
---|
835 | @property
|
---|
836 | def derateType(self):
|
---|
837 | """Get the derate type for this type."""
|
---|
838 | return DERATE_BOEING
|
---|
839 |
|
---|
840 | #---------------------------------------------------------------------------------------
|
---|
841 |
|
---|
842 | class B762(Boeing767):
|
---|
843 | """Boeing 767-200 aircraft."""
|
---|
844 | def __init__(self, flight):
|
---|
845 | super(B762, self).__init__(flight)
|
---|
846 | self.dow = 84507
|
---|
847 | self.mtow = 175540
|
---|
848 | self.mlw = 126098
|
---|
849 | self.mzfw = 114758
|
---|
850 | self.maxTakeOffPitch = 13.1
|
---|
851 | self.maxTouchDownPitch = 11.6
|
---|
852 |
|
---|
853 | #---------------------------------------------------------------------------------------
|
---|
854 |
|
---|
855 | class B763(Boeing767):
|
---|
856 | """Boeing 767-300 aircraft."""
|
---|
857 | def __init__(self, flight):
|
---|
858 | super(B763, self).__init__(flight)
|
---|
859 | self.dow = 91311
|
---|
860 | self.mtow = 181436
|
---|
861 | self.mlw = 137892
|
---|
862 | self.mzfw = 130635
|
---|
863 | self.maxTakeOffPitch = 9.6
|
---|
864 | self.maxTouchDownPitch = 8.1
|
---|
865 |
|
---|
866 | #---------------------------------------------------------------------------------------
|
---|
867 |
|
---|
868 | class CRJ2(Aircraft):
|
---|
869 | """Bombardier CRJ-200 aircraft.
|
---|
870 |
|
---|
871 | The aircraft type-specific values in the aircraft state have the following
|
---|
872 | structure:
|
---|
873 | - fuel: left, centre, right
|
---|
874 | - n1: left, right
|
---|
875 | - reverser: left, right."""
|
---|
876 | def __init__(self, flight):
|
---|
877 | super(CRJ2, self).__init__(flight, minLandingFuel = 1000)
|
---|
878 | self.dow = 14549
|
---|
879 | self.mtow = 22995
|
---|
880 | self.mlw = 21319
|
---|
881 | self.mzfw = 19958
|
---|
882 | self.gearSpeedLimit = 240
|
---|
883 | self.flapSpeedLimits = { 8 : 260,
|
---|
884 | 20 : 220,
|
---|
885 | 30 : 190,
|
---|
886 | 45 : 175 }
|
---|
887 | self.maxTakeOffPitch = 18.0
|
---|
888 | self.maxTouchDownPitch = 18.0
|
---|
889 |
|
---|
890 | #---------------------------------------------------------------------------------------
|
---|
891 |
|
---|
892 | class F70(Aircraft):
|
---|
893 | """Fokker 70 aircraft.
|
---|
894 |
|
---|
895 | The aircraft type-specific values in the aircraft state have the following
|
---|
896 | structure:
|
---|
897 | - fuel: left, centre, right
|
---|
898 | - n1: left, right
|
---|
899 | - reverser: left, right."""
|
---|
900 | def __init__(self, flight):
|
---|
901 | super(F70, self).__init__(flight, minLandingFuel = 1900)
|
---|
902 | self.dow = 24283
|
---|
903 | self.mtow = 38100 # FIXME: differentiate by registration number,
|
---|
904 | # MTOW of HA-LMF: 41955
|
---|
905 | self.mlw = 36740
|
---|
906 | self.mzfw = 32655
|
---|
907 | self.gearSpeedLimit = 200
|
---|
908 | self.flapSpeedLimits = { 8 : 250,
|
---|
909 | 15 : 220,
|
---|
910 | 25 : 220,
|
---|
911 | 42 : 180 }
|
---|
912 | self.reverseMinSpeed = 50
|
---|
913 | self.maxTakeOffPitch = 16.0
|
---|
914 | self.maxTouchDownPitch = 16.0
|
---|
915 |
|
---|
916 | @property
|
---|
917 | def derateType(self):
|
---|
918 | """Get the derate type for this type."""
|
---|
919 | return DERATE_EPR
|
---|
920 |
|
---|
921 | #---------------------------------------------------------------------------------------
|
---|
922 |
|
---|
923 | class DC3(Aircraft):
|
---|
924 | """Lisunov Li-2 (DC-3) aircraft.
|
---|
925 |
|
---|
926 | The aircraft type-specific values in the aircraft state have the following
|
---|
927 | structure:
|
---|
928 | - fuel: left aux, left, right, right aux
|
---|
929 | - rpm: left, right
|
---|
930 | - reverser: left, right."""
|
---|
931 | def __init__(self, flight):
|
---|
932 | super(DC3, self).__init__(flight)
|
---|
933 | self.dow = 8627
|
---|
934 | self.mtow = 11884
|
---|
935 | self.mlw = 11793
|
---|
936 | self.mzfw = 11780
|
---|
937 | self.gearSpeedLimit = 148
|
---|
938 | self.flapSpeedLimits = { 15 : 135,
|
---|
939 | 30 : 99,
|
---|
940 | 45 : 97 }
|
---|
941 |
|
---|
942 | def _checkFlightEnd(self, aircraftState):
|
---|
943 | """Check if the end of the flight has arrived.
|
---|
944 |
|
---|
945 | This implementation checks the RPM values to be 0."""
|
---|
946 | for rpm in aircraftState.rpm:
|
---|
947 | if rpm>0: return False
|
---|
948 | return True
|
---|
949 |
|
---|
950 | #---------------------------------------------------------------------------------------
|
---|
951 |
|
---|
952 | class T134(Aircraft):
|
---|
953 | """Tupolev Tu-134 aircraft.
|
---|
954 |
|
---|
955 | The aircraft type-specific values in the aircraft state have the following
|
---|
956 | structure:
|
---|
957 | - fuel: left tip, left aux, centre, right aux, right tip, external 1,
|
---|
958 | external 2
|
---|
959 | - n1: left, right
|
---|
960 | - reverser: left, right."""
|
---|
961 | def __init__(self, flight):
|
---|
962 | super(T134, self).__init__(flight, minLandingFuel = 3000)
|
---|
963 | self.dow = 29500
|
---|
964 | self.mtow = 49000
|
---|
965 | self.mlw = 43000
|
---|
966 | self.mzfw = 38500
|
---|
967 | self.gearSpeedLimit = 216
|
---|
968 | self.flapSpeedLimits = { 10 : 450,
|
---|
969 | 20 : 400,
|
---|
970 | 30 : 300 }
|
---|
971 | self.reverseMinSpeed = 50
|
---|
972 |
|
---|
973 | self.maxTakeOffPitch = 16.0
|
---|
974 | self.maxTouchDownPitch = 16.0
|
---|
975 |
|
---|
976 | @property
|
---|
977 | def derateType(self):
|
---|
978 | """Get the derate type for this type."""
|
---|
979 | return DERATE_TUPOLEV
|
---|
980 |
|
---|
981 | @property
|
---|
982 | def speedInKnots(self):
|
---|
983 | """Indicate if the speed is in knots."""
|
---|
984 | return False
|
---|
985 |
|
---|
986 | def _appendLightsLoggers(self):
|
---|
987 | """Append the loggers needed for the lights."""
|
---|
988 | self._checkers.append(checks.AnticollisionLightsLogger())
|
---|
989 | self._checkers.append(checks.LandingLightsLogger())
|
---|
990 | self._checkers.append(checks.NavLightsLogger())
|
---|
991 |
|
---|
992 | def _appendLightsCheckers(self):
|
---|
993 | """Append the checkers needed for the lights."""
|
---|
994 | self._checkers.append(checks.TupolevAntiCollisionLightsChecker())
|
---|
995 | self._checkers.append(checks.TupolevLandingLightsChecker())
|
---|
996 | self._checkers.append(checks.LandingLightsChecker())
|
---|
997 | self._checkers.append(checks.NavLightsChecker())
|
---|
998 |
|
---|
999 | #---------------------------------------------------------------------------------------
|
---|
1000 |
|
---|
1001 | class T154(Aircraft):
|
---|
1002 | """Tupolev Tu-154 aircraft.
|
---|
1003 |
|
---|
1004 | The aircraft type-specific values in the aircraft state have the following
|
---|
1005 | structure:
|
---|
1006 | - fuel: left aux, left, centre, centre 2, right, right aux
|
---|
1007 | - n1: left, centre, right
|
---|
1008 | - reverser: left, right"""
|
---|
1009 | def __init__(self, flight):
|
---|
1010 | super(T154, self).__init__(flight, minLandingFuel = 5000)
|
---|
1011 | self.dow = 53259
|
---|
1012 | self.mtow = 98000
|
---|
1013 | self.mlw = 78000
|
---|
1014 | self.mzfw = 72000
|
---|
1015 | self.gearSpeedLimit = 216
|
---|
1016 | self.flapSpeedLimits = { 15 : 227,
|
---|
1017 | 28 : 194,
|
---|
1018 | 45 : 162 }
|
---|
1019 | self.reverseMinSpeed = 50
|
---|
1020 |
|
---|
1021 | self.maxTakeOffPitch = 16.0
|
---|
1022 | self.maxTouchDownPitch = 16.0
|
---|
1023 |
|
---|
1024 | @property
|
---|
1025 | def speedInKnots(self):
|
---|
1026 | """Indicate if the speed is in knots."""
|
---|
1027 | return False
|
---|
1028 |
|
---|
1029 | @property
|
---|
1030 | def derateType(self):
|
---|
1031 | """Get the derate type for this type."""
|
---|
1032 | return DERATE_TUPOLEV
|
---|
1033 |
|
---|
1034 | def _appendLightsLoggers(self):
|
---|
1035 | """Append the loggers needed for the lights."""
|
---|
1036 | self._checkers.append(checks.AnticollisionLightsLogger())
|
---|
1037 | self._checkers.append(checks.LandingLightsLogger())
|
---|
1038 | self._checkers.append(checks.NavLightsLogger())
|
---|
1039 |
|
---|
1040 | def _appendLightsCheckers(self):
|
---|
1041 | """Append the checkers needed for the lights."""
|
---|
1042 | self._checkers.append(checks.AntiCollisionLightsChecker())
|
---|
1043 | self._checkers.append(checks.TupolevLandingLightsChecker())
|
---|
1044 | self._checkers.append(checks.LandingLightsChecker())
|
---|
1045 | self._checkers.append(checks.NavLightsChecker())
|
---|
1046 |
|
---|
1047 | #---------------------------------------------------------------------------------------
|
---|
1048 |
|
---|
1049 | class YK40(Aircraft):
|
---|
1050 | """Yakovlev Yak-40 aircraft.
|
---|
1051 |
|
---|
1052 | The aircraft type-specific values in the aircraft state have the following
|
---|
1053 | structure:
|
---|
1054 | - fuel: left, right
|
---|
1055 | - n1: left, right
|
---|
1056 | - reverser: left, right"""
|
---|
1057 | def __init__(self, flight):
|
---|
1058 | super(YK40, self).__init__(flight)
|
---|
1059 | self.dow = 9400
|
---|
1060 | self.mtow = 17200
|
---|
1061 | self.mlw = 16800
|
---|
1062 | self.mzfw = 12100
|
---|
1063 | self.gearSpeedLimit = 165
|
---|
1064 | self.flapSpeedLimits = { 20 : 165,
|
---|
1065 | 35 : 135 }
|
---|
1066 |
|
---|
1067 | @property
|
---|
1068 | def speedInKnots(self):
|
---|
1069 | """Indicate if the speed is in knots."""
|
---|
1070 | return False
|
---|
1071 |
|
---|
1072 | @property
|
---|
1073 | def derateType(self):
|
---|
1074 | """Get the derate type for this type."""
|
---|
1075 | return DERATE_TUPOLEV
|
---|
1076 |
|
---|
1077 | def _appendLightsLoggers(self):
|
---|
1078 | """Append the loggers needed for the lights."""
|
---|
1079 | self._checkers.append(checks.AnticollisionLightsLogger())
|
---|
1080 | self._checkers.append(checks.LandingLightsLogger())
|
---|
1081 | self._checkers.append(checks.NavLightsLogger())
|
---|
1082 |
|
---|
1083 | def _appendLightsCheckers(self):
|
---|
1084 | """Append the checkers needed for the lights."""
|
---|
1085 | self._checkers.append(checks.AntiCollisionLightsChecker())
|
---|
1086 | self._checkers.append(checks.LandingLightsChecker())
|
---|
1087 | self._checkers.append(checks.NavLightsChecker())
|
---|
1088 |
|
---|
1089 | #---------------------------------------------------------------------------------------
|
---|
1090 |
|
---|
1091 | class B462(Aircraft):
|
---|
1092 | """British Aerospace BAe-146 aircraft.
|
---|
1093 |
|
---|
1094 | The aircraft type-specific values in the aircraft state have the following
|
---|
1095 | structure:
|
---|
1096 | - fuel: left, centre, right
|
---|
1097 | - n1: left outer, left inner, right inner, right outer
|
---|
1098 | - reverser: empty (the plane has no reversers)"""
|
---|
1099 | def __init__(self, flight):
|
---|
1100 | super(B462, self).__init__(flight)
|
---|
1101 | self.dow = 25706
|
---|
1102 | self.mtow = 43998
|
---|
1103 | self.mlw = 38599
|
---|
1104 | self.mzfw = 33792
|
---|
1105 | self.gearSpeedLimit = 210
|
---|
1106 | self.flapSpeedLimits = { 18 : 217,
|
---|
1107 | 24 : 180,
|
---|
1108 | 30 : 170,
|
---|
1109 | 33 : 150 }
|
---|
1110 |
|
---|
1111 | @property
|
---|
1112 | def derateType(self):
|
---|
1113 | """Get the derate type for this type."""
|
---|
1114 | return DERATE_B462
|
---|
1115 |
|
---|
1116 | #---------------------------------------------------------------------------------------
|
---|
1117 |
|
---|
1118 | mostFuelTanks = [const.FUELTANK_LEFT_TIP, const.FUELTANK_EXTERNAL1,
|
---|
1119 | const.FUELTANK_LEFT_AUX,
|
---|
1120 | const.FUELTANK_CENTRE,
|
---|
1121 | const.FUELTANK_RIGHT_AUX,
|
---|
1122 | const.FUELTANK_EXTERNAL2, const.FUELTANK_RIGHT_TIP]
|
---|
1123 |
|
---|
1124 | #---------------------------------------------------------------------------------------
|
---|
1125 |
|
---|
1126 | _classes = { const.AIRCRAFT_B736 : B736,
|
---|
1127 | const.AIRCRAFT_B737 : B737,
|
---|
1128 | const.AIRCRAFT_B738 : B738,
|
---|
1129 | const.AIRCRAFT_B738C : B738Charter,
|
---|
1130 | const.AIRCRAFT_B733 : B733,
|
---|
1131 | const.AIRCRAFT_B734 : B734,
|
---|
1132 | const.AIRCRAFT_B735 : B735,
|
---|
1133 | const.AIRCRAFT_DH8D : DH8D,
|
---|
1134 | const.AIRCRAFT_B762 : B762,
|
---|
1135 | const.AIRCRAFT_B763 : B763,
|
---|
1136 | const.AIRCRAFT_CRJ2 : CRJ2,
|
---|
1137 | const.AIRCRAFT_F70 : F70,
|
---|
1138 | const.AIRCRAFT_DC3 : DC3,
|
---|
1139 | const.AIRCRAFT_T134 : T134,
|
---|
1140 | const.AIRCRAFT_T154 : T154,
|
---|
1141 | const.AIRCRAFT_YK40 : YK40,
|
---|
1142 | const.AIRCRAFT_B462 : B462 }
|
---|
1143 |
|
---|
1144 | #---------------------------------------------------------------------------------------
|
---|
1145 |
|
---|
1146 | if __name__ == "__main__":
|
---|
1147 | value = SmoothedValue()
|
---|
1148 |
|
---|
1149 | print "Adding 1, 12.0"
|
---|
1150 | value.add(1, 12.0)
|
---|
1151 | print value.get()
|
---|
1152 |
|
---|
1153 | print "Adding 1, 15.0"
|
---|
1154 | value.add(1, 15.0)
|
---|
1155 | print value.get()
|
---|
1156 |
|
---|
1157 | print "Adding 2, 18.0"
|
---|
1158 | value.add(2, 18.0)
|
---|
1159 | print value.get()
|
---|
1160 |
|
---|
1161 | print "Adding 2, 20.0"
|
---|
1162 | value.add(2, 20.0)
|
---|
1163 | print value.get()
|
---|
1164 |
|
---|
1165 | print "Adding 5, 22.0"
|
---|
1166 | value.add(5, 22.0)
|
---|
1167 | print value.get()
|
---|
1168 |
|
---|
1169 | print "Adding 5, 25.0"
|
---|
1170 | value.add(5, 25.0)
|
---|
1171 | print value.get()
|
---|
1172 |
|
---|
1173 | print "Adding 5, 29.0"
|
---|
1174 | value.add(5, 29.0)
|
---|
1175 | print value.get()
|
---|
1176 |
|
---|
1177 | print "Adding 5, 21.0"
|
---|
1178 | value.add(5, 21.0)
|
---|
1179 | print value.get()
|
---|
1180 |
|
---|
1181 | print "Adding 5, 26.0"
|
---|
1182 | value.add(5, 26.0)
|
---|
1183 | print value.get()
|
---|
1184 |
|
---|
1185 | print "Adding 2, 30.0"
|
---|
1186 | value.add(2, 30.0)
|
---|
1187 | print value.get()
|
---|
1188 |
|
---|
1189 | print "Adding 2, 55.0"
|
---|
1190 | value.add(2, 55.0)
|
---|
1191 | print value.get()
|
---|
1192 |
|
---|
1193 | #---------------------------------------------------------------------------------------
|
---|