Fix O2 gauge
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07e5a708ba
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26e68bfb72
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@ -574,15 +574,15 @@ help = helpEnrichments, "Enrichments Help"
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tpsADCGauge = tpsADC, "TPS ADC", "", 0, 255, -1, -1, 256, 256, 0, 0
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tpsADCGauge = tpsADC, "TPS ADC", "", 0, 255, -1, -1, 256, 256, 0, 0
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#batVoltGauge = batteryVoltage, "BAT V", "", 0, 255, -1, -1, 256, 256, 0, 0
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#batVoltGauge = batteryVoltage, "BAT V", "", 0, 255, -1, -1, 256, 256, 0, 0
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#if NARROW_BAND_EGO
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;#if NARROW_BAND_EGO
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egoGauge = egoVoltage, "Exhaust Gas Oxygen", "volts", 0, 1.0, 0.2, 0.3, 0.6, 0.8, 2, 2
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; egoGauge = egoVoltage, "Exhaust Gas Oxygen", "volts", 0, 1.0, 0.2, 0.3, 0.6, 0.8, 2, 2
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#else
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;#else
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egoGauge = egoVoltage, "Exhaust Gas Oxygen", "volts", 0.5, 4.5, 0.0, 0.0, 5.0, 5.0, 2, 2
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; egoGauge = egoVoltage, "Exhaust Gas Oxygen", "volts", 0.5, 4.5, 0.0, 0.0, 5.0, 5.0, 2, 2
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#endif
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;#endif
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lambdaGauge = lambda, "Lambda", "", 0.5, 1.5, 0.5, 0.7, 2, 1.1, 2, 2
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;lambdaGauge = lambda, "Lambda", "", 0.5, 1.5, 0.5, 0.7, 2, 1.1, 2, 2
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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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afrGauge = afr, "Air:Fuel Ratio", "", 10, 19.4, 12, 13, 15, 16, 2, 2
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afrGauge = afr, "Air:Fuel Ratio", "", 7, 25, 12, 13, 15, 16, 2, 2
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clockGauge = secl, "Clock", "Seconds", 0, 255, 10, 10, 245, 245, 0, 0
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clockGauge = secl, "Clock", "Seconds", 0, 255, 10, 10, 245, 245, 0, 0
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deadGauge = deadValue, "---", "", 0, 1, -1, -1, 2, 2, 0, 0
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deadGauge = deadValue, "---", "", 0, 1, -1, -1, 2, 2, 0, 0
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dutyCycleGauge = dutyCycle, "Duty Cycle", "%", 0, 100, -1, -1, 85, 90, 1, 1
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dutyCycleGauge = dutyCycle, "Duty Cycle", "%", 0, 100, -1, -1, 85, 90, 1, 1
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@ -767,7 +767,8 @@ help = helpEnrichments, "Enrichments Help"
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#endif
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#endif
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tpsADC = scalar, U08, 7, "ADC", 1.000, 0.000
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tpsADC = scalar, U08, 7, "ADC", 1.000, 0.000
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batteryVoltage = scalar, U08, 8, "V", 0.100, 0.000
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batteryVoltage = scalar, U08, 8, "V", 0.100, 0.000
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egoADC = scalar, U08, 9, "ADC", 1.000, 0.000
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#egoADC = scalar, U08, 9, "ADC", 1.000, 0.000
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afr = scalar, U08, 9, "O2", 0.100, 0.000
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egoCorrection = scalar, U08, 10, "%", 1.000, 0.000
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egoCorrection = scalar, U08, 10, "%", 1.000, 0.000
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airCorrection = scalar, U08, 11, "%", 1.000, 0.000
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airCorrection = scalar, U08, 11, "%", 1.000, 0.000
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warmupEnrich = scalar, U08, 12, "%", 1.000, 0.000
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warmupEnrich = scalar, U08, 12, "%", 1.000, 0.000
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@ -792,13 +793,13 @@ help = helpEnrichments, "Enrichments Help"
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#batteryVoltage = { batADC / 255.0 * 30.0 } ; Current MS power supply voltage.
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#batteryVoltage = { batADC / 255.0 * 30.0 } ; Current MS power supply voltage.
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coolant = { coolantRaw - 40 } ; Coolant sensor temperature in user units.
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coolant = { coolantRaw - 40 } ; Coolant sensor temperature in user units.
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#mat = { tempCvt(table(matADC, "matfactor.inc")-40) } ; Manifold temperature in user units.
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#mat = { tempCvt(table(matADC, "matfactor.inc")-40) } ; Manifold temperature in user units.
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egoVoltage = { egoADC / 255.0 * 5.0 } ; EGO sensor voltage.
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; egoVoltage = { egoADC / 255.0 * 5.0 } ; EGO sensor voltage.
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rpm = { rpm100*100 } ; True RPM.
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rpm = { rpm100*100 } ; True RPM.
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time = { timeNow } ; "timeNow" is a parameterless built-in function.
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time = { timeNow } ; "timeNow" is a parameterless built-in function.
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;loopsPerSecond = { loopsPerSecond10*10 } ; True number of mainloops per second
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;loopsPerSecond = { loopsPerSecond10*10 } ; True number of mainloops per second
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afrtarget = { 0 }
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afrtarget = { 0 }
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#include "lambdaSensors.ini"
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; #include "lambdaSensors.ini"
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#if MPX4250
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#if MPX4250
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barometer = { table(baroADC, "kpafactor4250.inc") }
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barometer = { table(baroADC, "kpafactor4250.inc") }
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@ -865,7 +866,7 @@ help = helpEnrichments, "Enrichments Help"
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entry = rpm100, "RPM100", int, "%d"
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entry = rpm100, "RPM100", int, "%d"
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entry = map, "MAP", int, "%d"
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entry = map, "MAP", int, "%d"
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entry = tpsADC, "TPS", int, "%d"
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entry = tpsADC, "TPS", int, "%d"
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entry = egoVoltage, "O2", float, "%.3f"
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entry = afr, "O2", float, "%.3f"
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entry = mat, "MAT", float, "%.1f"
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entry = mat, "MAT", float, "%.1f"
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entry = coolant, "CLT", float, "%.1f"
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entry = coolant, "CLT", float, "%.1f"
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entry = engine, "Engine", int, "%d"
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entry = engine, "Engine", int, "%d"
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