def __init__(self, parent):
FlightPlanBaseSimpleDlg.__init__(self, parent)
self.setObjectName("DmeToleranceDlg")
self.surfaceType = SurfaceTypes.DmeTolerance
self.dmeTolerance = Distance.NaN()
self.slantTolerance = Distance.NaN()
self.pilotDistance = Distance.NaN()
self.groundDistance = Distance.NaN()
self.initParametersPan()
self.setWindowTitle("DME Tolerance and Slant Range")
self.method_29()
self.method_28()
self.resize(550, 550)
QgisHelper.matchingDialogSize(self, 550, 600)
self.vorDmeFeatureArray = []
self.currentLayer = define._canvas.currentLayer()
self.resultLayerList = []
# self.rwyFeatureArray = []
# self.thrPoint3d = None
# self.thrEndPoint3d = None
self.initBasedOnCmb()
def smethod_0(iwin32Window_0):
num = 0
str0 = ""
navigationalAidList = NavigationalAidList()
NavigationalAidList.NavigationalAidList()
navigationalAidList.append(OmnidirectionalNavigationalAid("DME N", AngleGradientSlope(1), Distance(3000), Distance(300), True))
navigationalAidList.append(OmnidirectionalNavigationalAid("VOR", AngleGradientSlope(1), Distance(3000), Distance(600), True))
navigationalAidList.append(OmnidirectionalNavigationalAid("Directional Finder (DF)", AngleGradientSlope(1), Distance(3000), Distance(500), True))
navigationalAidList.append(OmnidirectionalNavigationalAid("Markers", AngleGradientSlope(20), Distance(200), Distance(50), True))
navigationalAidList.append(OmnidirectionalNavigationalAid("NDB", AngleGradientSlope(5), Distance(1000), Distance(200), True))
navigationalAidList.append(OmnidirectionalNavigationalAid("GBAS ground reference receiver", AngleGradientSlope(3), Distance(3000), Distance(400), True))
navigationalAidList.append(OmnidirectionalNavigationalAid("GBAS VDB station", AngleGradientSlope(0.9), Distance(3000), Distance(300), True))
navigationalAidList.append(OmnidirectionalNavigationalAid("SBAS ground monitoring station", AngleGradientSlope(3), Distance(3000), Distance(400), True))
navigationalAidList.append(OmnidirectionalNavigationalAid("VHF (Communication Tx)", AngleGradientSlope(1), Distance(2000), Distance(300), True))
navigationalAidList.append(OmnidirectionalNavigationalAid("VHF (Communication Rx)", AngleGradientSlope(1), Distance(2000), Distance(300), True))
navigationalAidList.append(OmnidirectionalNavigationalAid("PSR", AngleGradientSlope(0.25), Distance(15000), Distance(500), True))
navigationalAidList.append(OmnidirectionalNavigationalAid("SSR", AngleGradientSlope(0.25), Distance(15000), Distance(500), True))
navigationalAidList.append(DirectionalNavigationalAid("ILS LOC (single freq.)", Distance.NaN(), Distance(500), Altitude(70), Distance(6000), Distance(500), Altitude(10), Distance(2300), AngleGradientSlope(30), True))
navigationalAidList.append(DirectionalNavigationalAid("ILS LOC (dual freq.)", Distance.NaN(), Distance(500), Altitude(70), Distance(6000), Distance(500), Altitude(20), Distance(1500), AngleGradientSlope(20), True))
navigationalAidList.append(DirectionalNavigationalAid("ILS GP M-Type (dual freq.)", Distance(800), Distance(50), Altitude(70), Distance(6000), Distance(250), Altitude(5), Distance(325), AngleGradientSlope(10), True))
navigationalAidList.append(DirectionalNavigationalAid("MLS AZ", Distance.NaN(), Distance(20), Altitude(70), Distance(6000), Distance(600), Altitude(20), Distance(1500), AngleGradientSlope(40), True))
navigationalAidList.append(DirectionalNavigationalAid("MLS EL", Distance(300), Distance(20), Altitude(70), Distance(6000), Distance(200), Altitude(20), Distance(1500), AngleGradientSlope(40), True))
navigationalAidList.append(DirectionalNavigationalAid("DME (directional antennas)", Distance.NaN(), Distance(20), Altitude(70), Distance(6000), Distance(600), Altitude(20), Distance(1500), AngleGradientSlope(40), True))
try:
if (QFile.exists(NavigationalAidList.fileName)):
xmlFile = XmlFile(NavigationalAidList.fileName, "NavigationalAids", False)
xmlNodeLists = xmlFile.elementsByTagName("NavigationalAid")
if (xmlNodeLists != None):
count = xmlNodeLists.count()
for i in range(count):
xmlElement = xmlNodeLists.item(i)
# foreach (XmlElement xmlElement in xmlNodeLists)
result1, num = xmlFile.method_7(xmlElement, "Type")
result2, str0 = xmlFile.method_7(xmlElement, "Name")
if (not result1 or not result2):
continue
for case in switch(num):
if case(NavigationalAidType.Omnidirectional):
navigationalAidList.Add(OmnidirectionalNavigationalAid(None, xmlFile, xmlElement, str0))
continue
elif case(NavigationalAidType.Directional):
navigationalAidList.Add(DirectionalNavigationalAid(None, xmlFile, xmlElement, str0))
continue
elif case(NavigationalAidType.LineOfSight):
navigationalAidList.Add(LineOfSight(None, xmlFile, xmlElement, str0))
continue
else:
continue
except:
# Exception exception = exception1
QMessageBox.warning(iwin32Window_0, "Error", Messages.ERR_FAILED_TO_LOAD_NAVAID_DATA_FILE)
# ErrorMessageBox.smethod_0(iwin32Window_0, string.Format(Messages.ERR_FAILED_TO_LOAD_NAVAID_DATA_FILE, exception.Message))
navigationalAidList.method_1()
return navigationalAidList
def smethod_4(rnavCommonWaypoint_0, aircraftSpeedCategory_0):
if (aircraftSpeedCategory_0 == AircraftSpeedCategory.Custom):
raise UserWarning, Messages.CUSTOM_AC_CATEGORY_NOT_SUPPORTED
if rnavCommonWaypoint_0 == RnavCommonWaypoint.MAHWP:
return Distance(1, DistanceUnits.NM)
elif rnavCommonWaypoint_0 == RnavCommonWaypoint.MAWP:
return Distance.NaN()
elif rnavCommonWaypoint_0 == RnavCommonWaypoint.FAWP:
if (aircraftSpeedCategory_0 == AircraftSpeedCategory.H):
return Distance(1, DistanceUnits.NM)
return Distance(3, DistanceUnits.NM)
elif rnavCommonWaypoint_0 == RnavCommonWaypoint.IWP:
return Distance(2, DistanceUnits.NM)
else:
return Distance(1, DistanceUnits.NM)
def smethod_6(rnavCommonWaypoint_0, aircraftSpeedCategory_0):
if (aircraftSpeedCategory_0 == AircraftSpeedCategory.Custom):
raise Messages.CUSTOM_AC_CATEGORY_NOT_SUPPORTED
if rnavCommonWaypoint_0 == RnavCommonWaypoint.MAHWP:
return Distance(10, DistanceUnits.NM)
elif rnavCommonWaypoint_0 == RnavCommonWaypoint.MAWP:
return Distance.NaN()
elif rnavCommonWaypoint_0 == RnavCommonWaypoint.FAWP:
if (aircraftSpeedCategory_0 == AircraftSpeedCategory.H):
return Distance(2, DistanceUnits.NM)
return Distance(5, DistanceUnits.NM)
elif rnavCommonWaypoint_0 == RnavCommonWaypoint.IWP:
if (aircraftSpeedCategory_0 == AircraftSpeedCategory.H):
return Distance(3, DistanceUnits.NM)
return Distance(5, DistanceUnits.NM)
else:
if (aircraftSpeedCategory_0 != AircraftSpeedCategory.H):
pass
else:
return Distance(3, DistanceUnits.NM)
if (aircraftSpeedCategory_0 != AircraftSpeedCategory.A):
if (aircraftSpeedCategory_0 != AircraftSpeedCategory.B):
return Distance(6, DistanceUnits.NM)
return Distance(5, DistanceUnits.NM)
def method_29(self):
speed = None
speed1 = None
num = None
num1 = None
# Validator validator = new Validator(ValidationFlags.None);
flag = True
flag1 = True
# self.errorProvider.method_1();
# if (!self.cmbType.method_1(validator))
# {
# flag = false;
# }
# if (!self.pnlAltitude.method_1(validator))
# {
# flag = false;
# }
# if (!self.pnlISA.method_2(validator))
# {
# flag = false;
# }
# validator.Flags = ValidationFlags.Positive;
# if (!self.pnlIAS.method_1(validator))
# {
# flag = false;
# }
# validator.Flags = ValidationFlags.AllowEmpty | ValidationFlags.NonNegative;
# if (!self.pnlWind.method_1(validator))
# {
# flag1 = false;
# }
# if (!self.pnlTime.method_1(validator))
# {
# flag1 = false;
# }
if (flag1):
if self.parametersPanel.pnlWind.Value == None:
flag1 = False
else:
try:
time = float(self.parametersPanel.txtTime.text())
flag1 = True
except:
flag1 = False
# flag1 = False if(self.pnlWind.Value.IsNaN) else not double.IsNaN(self.pnlTime.Value));
# }
# self.panelEx.SuspendLayout();
# self.gbResults.SuspendLayout();
# try:
tAS = Captions.TAS
eST = Captions.EST
pILOTREACTION = Captions.PILOT_REACTION
str0 = Captions.c
str1 = ""
self.est = Distance.NaN()
self.rea = Distance.NaN()
self.c = Distance.NaN()
self.x = Distance.NaN()
self.d = Distance.NaN()
self.custom = Distance.NaN()
if (not flag):
self.parametersPanel.txtTAS.setText(Captions.NOT_APPLICABLE)
self.parametersPanel.txtEST.setText(Captions.NOT_APPLICABLE)
self.parametersPanel.txtREA.setText(Captions.NOT_APPLICABLE)
self.parametersPanel.txtC.setText(Captions.NOT_APPLICABLE)
self.parametersPanel.txtX.setText(Captions.NOT_APPLICABLE)
self.parametersPanel.txtD.setText(Captions.NOT_APPLICABLE)
self.parametersPanel.txtNonStandardResult.setText(
Captions.NOT_APPLICABLE)
else:
value = Speed(float(self.parametersPanel.txtIAS.text()),
SpeedUnits.KTS)
altitude = Altitude(float(self.parametersPanel.txtAltitude.text()),
AltitudeUnits.FT)
value1 = float(self.parametersPanel.txtISA.text())
selectedIndex = self.parametersPanel.cmbType.currentText()
if selectedIndex == IasTasSegmentType.Departure or selectedIndex == IasTasSegmentType.MissedApproach:
speed = Speed(30)
num = 3
speed1 = Speed(30)
num1 = 3
elif selectedIndex == IasTasSegmentType.Enroute:
speed = Speed.smethod_1(altitude)
num = 5
speed1 = Speed.smethod_1(altitude)
num1 = 10
elif selectedIndex == IasTasSegmentType.Holding or selectedIndex == IasTasSegmentType.InitialRR:
speed = Speed.smethod_1(altitude)
num = 5
speed1 = Speed.smethod_1(altitude)
num1 = 6
elif selectedIndex == IasTasSegmentType.InitialDR or selectedIndex == IasTasSegmentType.IafIfFaf:
speed = Speed(30)
num = 5
speed1 = Speed(30)
num1 = 6
else:
pass
# throw new Exception(Messages.ERR_UNSUPPORTED_PROCEDURE_SEGMENT_TYPE);
if (selectedIndex == IasTasSegmentType.Departure):
m = value
n = (value / 10)
value = m + n
tAS = tAS + " (" + Captions.IAS + "+ 10%)"
speed2 = Speed.smethod_0(value, value1, altitude)
self.est = self.method_27(speed2, speed, num)
self.rea = self.method_27(speed2, speed1, num1)
self.c = self.est + self.rea
self.x = self.method_27(speed2, Speed(10), 15)
self.d = self.method_27(speed2, Speed(10), 3)
eST = eST + " (%i kts / %i s)" % (speed.Knots, num)
pILOTREACTION = pILOTREACTION + " (%i kts / %i s)" % (speed1.Knots,
num1)
str0 = str0 + " (%i kts / %i + %i s)" % (speed.Knots, num, num1)
self.parametersPanel.label_10.setText(tAS)
self.parametersPanel.txtTAS.setText(str(speed2.Knots) + "kts")
self.parametersPanel.label_73.setText(eST)
self.parametersPanel.txtEST.setText(str(self.est.Metres) + "m")
self.parametersPanel.label_74.setText(pILOTREACTION)
self.parametersPanel.txtREA.setText(str(self.rea.Metres) + "m")
self.parametersPanel.label_75.setText(str0)
self.parametersPanel.txtC.setText(str(self.c.Metres) + "m")
self.parametersPanel.txtX.setText(str(self.x.Metres) + "m")
self.parametersPanel.txtD.setText(str(self.d.Metres) + "m")
if (not flag1):
self.parametersPanel.txtNonStandardResult.setText(
Captions.NOT_APPLICABLE)
else:
self.custom = self.method_27(
speed2, self.parametersPanel.pnlWind.Value,
float(self.parametersPanel.txtTime.text()))
str2 = str(self.parametersPanel.pnlWind.Value.Knots) + "kts"
value2 = float(self.parametersPanel.txtTime.text())
str1 = "%s / %i s" % (str2, value2)
self.parametersPanel.txtNonStandardResult.setText(
str(self.custom.Metres) + "m")
self.parametersPanel.label_10.setText(tAS)
self.parametersPanel.label_73.setText(eST)
self.parametersPanel.label_74.setText(pILOTREACTION)
self.parametersPanel.label_75.setText(str0)
self.parametersPanel.label_11.setText(str1)
# self.method_28(self.pnlEST);
# self.method_28(self.pnlREA);
# self.method_28(self.pnlC);
# self.method_28(self.pnlX);
# self.method_28(self.pnlD);
# self.method_28(self.pnlNonStandardResult);
self.parametersPanel.frame_X.setVisible(
self.parametersPanel.cmbType.currentIndex() == 6)
self.parametersPanel.frame_D.setVisible(
self.parametersPanel.cmbType.currentIndex() == 6)
self.parametersPanel.gbNonStandardResult.setVisible(
self.parametersPanel.txtNonStandardResult.text() !=
Captions.NOT_APPLICABLE)
def get_Xtt(self):
try:
return Distance(float(self.txtXtt.text()), DistanceUnits.NM)
except:
return Distance.NaN()