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