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@ -493,7 +493,8 @@ page = 1
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pageButtons = "&EGO"
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pageButtons = "&EGO"
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gauge1 = tachometer
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gauge1 = tachometer
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gauge2 = AFRactual
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gauge2 = afr1Gauge
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gauge3 = mapGaugeValue
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[VeAnalyze]
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[VeAnalyze]
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@ -531,7 +532,7 @@ fileVersion = { 20150211 }
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tpsADC = scalar, U16, 32, "ADC", 1, 0.0;
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tpsADC = scalar, U16, 32, "ADC", 1, 0.0;
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alignmet = scalar, U16, 34, "al", 1, 0.0;
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alignmet = scalar, U16, 34, "al", 1, 0.0;
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atmPres = scalar, F32, 36, "pres", 1, 0.0;
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atmPres = scalar, F32, 36, "pres", 1, 0.0;
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MAP = scalar, F32, 40, "MAP", 1, 0.0;
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MAPValue = scalar, F32, 40, "MAP", 1, 0.0;
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; total fuel squirt duration (in MS) per engine cycle according to current CLT
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; total fuel squirt duration (in MS) per engine cycle according to current CLT
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crankingFuel = scalar, F32, 44, "ms", 1, 0.0;
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crankingFuel = scalar, F32, 44, "ms", 1, 0.0;
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baseFuel = scalar, F32, 48, "ms", 1, 0
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baseFuel = scalar, F32, 48, "ms", 1, 0
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@ -614,7 +615,7 @@ fileVersion = { 20150211 }
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yAxis = -30, 1300, 10
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yAxis = -30, 1300, 10
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xBins = mafDecodingBins, MAF
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xBins = mafDecodingBins, MAF
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yBins = mafDecoding
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yBins = mafDecoding
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gauge = mafGauge
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gauge = mafGaugeVolts
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curve = iatFuelCorrCurve, "Intake air temp fuel correction"
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curve = iatFuelCorrCurve, "Intake air temp fuel correction"
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columnLabel = "Coolant", "Correction"
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columnLabel = "Coolant", "Correction"
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@ -670,7 +671,7 @@ fileVersion = { 20150211 }
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table = veTableTbl, veTableMap, "VE Table", 1
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table = veTableTbl, veTableMap, "VE Table", 1
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; constant, variable
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; constant, variable
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xBins = veRpmBins, rpm
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xBins = veRpmBins, rpm
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yBins = veLoadBins, MAP
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yBins = veLoadBins, MAPValue
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zBins = veTable
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zBins = veTable
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; gridHeight = 2.0
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; gridHeight = 2.0
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gridOrient = 250, 0, 340 ; Space 123 rotation of grid in degrees.
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gridOrient = 250, 0, 340 ; Space 123 rotation of grid in degrees.
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@ -697,7 +698,7 @@ fileVersion = { 20150211 }
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table = afrTableTbl, afrTableMap, "Target AFR Table", 1
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table = afrTableTbl, afrTableMap, "Target AFR Table", 1
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; constant, variable
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; constant, variable
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xBins = afrRpmBins, rpm
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xBins = afrRpmBins, rpm
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yBins = afrLoadBins, MAP
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yBins = afrLoadBins, MAPValue
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zBins = afrTable
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zBins = afrTable
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; gridHeight = 2.0
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; gridHeight = 2.0
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gridOrient = 250, 0, 340 ; Space 123 rotation of grid in degrees.
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gridOrient = 250, 0, 340 ; Space 123 rotation of grid in degrees.
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@ -710,27 +711,27 @@ fileVersion = { 20150211 }
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#if CELSIUS
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#if CELSIUS
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CLTGauge = coolant, "Coolant Temp", "°C", -40, 140, -15, 1, 95, 110, 1, 1
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CLTGauge = coolant, "Coolant Temp", "°C", -40, 140, -15, 1, 95, 110, 1, 1
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#else
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#else
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CLTGauge = coolant, "Coolant Temp", "°F", -40, 285, 5, 35, 205, 230, 1, 1
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CLTGauge = coolant, "Coolant Temp", "°F", -40, 285, 5, 35, 205, 230, 1, 1
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#endif
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#endif
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#if CELSIUS
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#if CELSIUS
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IATGauge = intake, "Intake Air Temp", "°C", -40, 140, -15, 1, 95, 110, 1, 1
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IATGauge = intake, "Intake Air Temp", "°C", -40, 140, -15, 1, 95, 110, 1, 1
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#else
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#else
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IATGauge = intake, "Intake Air Temp", "°F", -40, 285, 5, 35, 205, 230, 1, 1
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IATGauge = intake, "Intake Air Temp", "°F", -40, 285, 5, 35, 205, 230, 1, 1
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#endif
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#endif
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throttleGauge = TPS, "Throttle Position", "%", 0, 100, 0, 0, 100, 100, 0, 0
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throttleGauge = TPS, "Throttle Position", "%", 0, 100, 0, 0, 100, 100, 0, 0
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afr1Gauge = AFRactual, "Air:Fuel Ratio 1", "", 10, 19.4, 12, 13, 15, 16, 2, 2
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afr1Gauge = AFRactual, "Air:Fuel Ratio 1", "", 10, 19.4, 12, 13, 15, 16, 2, 2
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mafGauge = MAF, "Mass Air Flow", "v", 0, 5, 0, 1, 3, 4, 1, 1
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mafGaugeVolts = MAF, "Mass Air Flow", "v", 0, 5, 0, 1, 3, 4, 1, 1
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VBattGauge = VBatt, "Battery Voltage", "V", 8, 21, 9, 10, 17, 19, 1, 1
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VBattGauge = VBatt, "Battery Voltage", "V", 8, 21, 9, 10, 17, 19, 1, 1
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tpsADCGauge = tpsADC, "tps ADC", "ADC", 0, 1024, 0, 0, 0, 0, 0, 0
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tpsADCGauge = tpsADC, "tps ADC", "ADC", 0, 1024, 0, 0, 0, 0, 0, 0
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atmPresCGauge = atmPres, "atmo pressu", "kPa", 0, 1024, 0, 0, 0, 0, 0, 0
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atmPresCGauge = atmPres, "atmo pressu", "kPa", 0, 1024, 0, 0, 0, 0, 0, 0
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mapCGauge = MAP, "MAP", "kPa", 0, 1024, 0, 0, 0, 0, 0, 0
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mapGaugeValue = MAPValue, "MAP", "kPa", 0, 300, 0, 300, 300, 0, 0, 0
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pulseWidthGauge = pulseWidth, "Pulse Width", "mSec", 0, 25.5, 1.0, 1.2, 20, 25, 3, 1
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pulseWidthGauge = pulseWidth, "Pulse Width", "mSec", 0, 25.5, 1.0, 1.2, 20, 25, 3, 1
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baseFuelGauge = baseFuel, "Base Width", "mSec", 0, 25.5, 1.0, 1.2, 20, 25, 3, 1
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baseFuelGauge = baseFuel, "Base Width", "mSec", 0, 25.5, 1.0, 1.2, 20, 25, 3, 1
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crankingFuelGauge = crankingFuel, "crank Width", "mSec", 0, 25.5, 1.0, 1.2, 20, 25, 3, 1
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crankingFuelGauge = crankingFuel, "crank Width", "mSec", 0, 25.5, 1.0, 1.2, 20, 25, 3, 1
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ignadvGauge = ign_adv, "Ignition Advance 1", "degrees", -100, 100, -999, -999, 999, 999, 1, 1
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ignadvGauge = ign_adv, "Ignition Advance 1", "degrees", -100, 100, -999, -999, 999, 999, 1, 1
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; warmupEnrichGauge = warmupEnrich, "Warmup Enrichment", "%", 100, 150, -1, -1, 101, 105, 0, 0
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; warmupEnrichGauge = warmupEnrich, "Warmup Enrichment", "%", 100, 150, -1, -1, 101, 105, 0, 0
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; accelEnrichGauge = accDecEnrich, "Accel Enrich", "%", 50, 150, -1, -1, 999, 999, 0, 0
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; accelEnrichGauge = accDecEnrich, "Accel Enrich", "%", 50, 150, -1, -1, 999, 999, 0, 0
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dwellGauge = sparkDwell, "Dwell", "mSec", 0, 10, 0.5, 1.0, 6.0, 8.0, 1, 1
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dwellGauge = sparkDwell, "Dwell", "mSec", 0, 10, 0.5, 1.0, 6.0, 8.0, 1, 1
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egt1Gauge = egt1, "EGT#1", "C", 0, 2000
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egt1Gauge = egt1, "EGT#1", "C", 0, 2000
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egt2Gauge = egt2, "EGT#2", "C", 0, 2000
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egt2Gauge = egt2, "EGT#2", "C", 0, 2000
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egt3Gauge = egt3, "EGT#3", "C", 0, 2000
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egt3Gauge = egt3, "EGT#3", "C", 0, 2000
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@ -752,7 +753,7 @@ fileVersion = { 20150211 }
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gauge1 = tachometer
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gauge1 = tachometer
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gauge2 = CLTGauge
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gauge2 = CLTGauge
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gauge3 = throttleGauge
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gauge3 = throttleGauge
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gauge4 = mafGauge
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gauge4 = mafGaugeVolts
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gauge5 = afr1Gauge
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gauge5 = afr1Gauge
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gauge6 = tpsADCGauge
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gauge6 = tpsADCGauge
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gauge7 = dwellGauge
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gauge7 = dwellGauge
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@ -792,7 +793,7 @@ fileVersion = { 20150211 }
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entry = intake, "IAT", float, "%.1f"
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entry = intake, "IAT", float, "%.1f"
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entry = TPS, "TPS", float, "%d"
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entry = TPS, "TPS", float, "%d"
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entry = MAF, "MAF", float, "%.2f"
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entry = MAF, "MAF", float, "%.2f"
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entry = MAP, "MAP", float, "%d"
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entry = MAPValue, "MAP", float, "%d"
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entry = AFRactual, "AFR", float, "%.2f"
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entry = AFRactual, "AFR", float, "%.2f"
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entry = VBatt, "vBatt", float, "%.2f"
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entry = VBatt, "vBatt", float, "%.2f"
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entry = engineLoad, "Load", float, "%d"
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entry = engineLoad, "Load", float, "%d"
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