Auto-generated configs and docs
This commit is contained in:
GitHub gen-configs Action
parent
c63fb29aaf
commit
4f6f985d4f
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@ -58,7 +58,6 @@ entry = injectorLagMs, "fuel: injector lag", float, "%.3f"
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entry = iatCorrection, "fuel: IAT correction", float, "%.3f"
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entry = cltCorrection, "fuel: CLT correction", float, "%.3f"
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entry = baroCorrection, "fuel: Barometric pressure correction", float, "%.3f"
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entry = currentEnginePhase, "Engine Phase", int, "%d"
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entry = wallFuelAmount, "fuel: wall amount", float, "%.3f"
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entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f"
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entry = revolutionCounterSinceStart, "revolutionCounterSinceStart", int, "%d"
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@ -404,7 +403,7 @@ entry = mapVvt_MAP_AT_SPECIAL_POINT, "mapVvt_MAP_AT_SPECIAL_POINT", float, "%.3
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entry = mapVvt_MAP_AT_DIFF, "mapVvt_MAP_AT_DIFF", float, "%.3f"
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entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d"
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entry = mapVvt_map_peak, "mapVvt_map_peak", int, "%d"
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entry = currentEngineDecodedPhase, "Engine Phase2", int, "%d"
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entry = currentEngineDecodedPhase, "Engine Phase", int, "%d"
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entry = totalRevolutionCounter, "Crank revolution counter", int, "%d"
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entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f"
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entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f"
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@ -66,7 +66,6 @@ injectorLagMsGauge = injectorLagMs,"fuel: injector lag", "ms", 0.0,0.0, 0.0,0.0,
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iatCorrectionGauge = iatCorrection,"fuel: IAT correction", "%", 0.0,0.0, 0.0,0.0, 0.0,0.0, 0,0
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cltCorrectionGauge = cltCorrection,"fuel: CLT correction", "%", 0.0,0.0, 0.0,0.0, 0.0,0.0, 0,0
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baroCorrectionGauge = baroCorrection,"fuel: Barometric pressure correction", "%", 0.0,0.0, 0.0,0.0, 0.0,0.0, 0,0
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currentEnginePhaseGauge = currentEnginePhase,"Engine Phase", "deg", 0.0,0.0, 0.0,0.0, 0.0,0.0, 0,0
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wallFuelAmountGauge = wallFuelAmount,"fuel: wall amount", "mg", 0.0,0.0, 0.0,0.0, 0.0,0.0, 0,0
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wallFuelCorrectionGauge = wallFuelCorrection,"fuel: wall correction", "mg", 0.0,0.0, 0.0,0.0, 0.0,0.0, 0,0
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revolutionCounterSinceStartGauge = revolutionCounterSinceStart,"revolutionCounterSinceStart", "", 0.0,0.0, 0.0,0.0, 0.0,0.0, 0,0
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@ -85,6 +84,7 @@ totalFuelConsumptionGauge = totalFuelConsumption,"fuel: Total consumed", "grams"
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fuelFlowRateGauge = fuelFlowRate,"fuel: Flow rate", "gram/s", 0.0,0.0, 0.0,0.0, 0.0,0.0, 0,0
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veTableYAxisGauge = veTableYAxis,"veTableYAxis", "%", 0.0,0.0, 0.0,0.0, 0.0,0.0, 0,0
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afrTableYAxisGauge = afrTableYAxis,"afrTableYAxis", "%", 0.0,0.0, 0.0,0.0, 0.0,0.0, 0,0
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alignmentFill_at_106Gauge = alignmentFill_at_106,"need 4 byte alignment", "units", -20.0,100.0, -20.0,100.0, -20.0,100.0, 0,0
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knockLevelGauge = knockLevel,"knock: current level", "Volts", 0.0,0.0, 0.0,0.0, 0.0,0.0, 0,0
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secondsGauge = seconds,"Uptime", "sec", 0.0,0.0, 0.0,0.0, 0.0,0.0, 0,0
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engineModeGauge = engineMode,"Engine Mode", "em", 0.0,0.0, 0.0,0.0, 0.0,0.0, 0,0
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@ -66,25 +66,24 @@ injectorLagMs = scalar, U16, 62, "ms", 0.0033333333333333335, 0
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iatCorrection = scalar, U16, 64, "%", 0.01, 0
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cltCorrection = scalar, U16, 66, "%", 0.01, 0
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baroCorrection = scalar, U16, 68, "%", 0.01, 0
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currentEnginePhase = scalar, U16, 70, "deg", 1, 0
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wallFuelAmount = scalar, U16, 72, "mg", 0.01, 0
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wallFuelCorrection = scalar, S16, 74, "mg", 0.01, 0
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revolutionCounterSinceStart = scalar, U16, 76, "", 1, 0
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deltaTps = scalar, S16, 78, "ratio", 0.01, 0
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canReadCounter = scalar, U16, 80, "", 1, 0
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tpsAccelFuel = scalar, S16, 82, "ms", 0.0033333333333333335, 0
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ignitionAdvance = scalar, S16, 84, "deg", 0.02, 0
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sparkDwellValue = scalar, U16, 86, "ms", 0.0033333333333333335, 0
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coilDutyCycle = scalar, U16, 88, "%", 0.01, 0
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idleAirValvePosition = scalar, U16, 90, "%", 0.01, 0
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etbTarget = scalar, S16, 92, "%", 0.01, 0
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etb1DutyCycle = scalar, S16, 94, "%", 0.01, 0
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etb1Error = scalar, S16, 96, "%", 0.01, 0
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fuelTankLevel = scalar, S16, 98, "%", 0.01, 0
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totalFuelConsumption = scalar, U16, 100, "grams", 1, 0
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fuelFlowRate = scalar, U16, 102, "gram/s", 0.005, 0
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veTableYAxis = scalar, U16, 104, "%", 0.01, 0
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afrTableYAxis = scalar, U16, 106, "%", 0.01, 0
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wallFuelAmount = scalar, U16, 70, "mg", 0.01, 0
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wallFuelCorrection = scalar, S16, 72, "mg", 0.01, 0
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revolutionCounterSinceStart = scalar, U16, 74, "", 1, 0
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deltaTps = scalar, S16, 76, "ratio", 0.01, 0
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canReadCounter = scalar, U16, 78, "", 1, 0
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tpsAccelFuel = scalar, S16, 80, "ms", 0.0033333333333333335, 0
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ignitionAdvance = scalar, S16, 82, "deg", 0.02, 0
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sparkDwellValue = scalar, U16, 84, "ms", 0.0033333333333333335, 0
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coilDutyCycle = scalar, U16, 86, "%", 0.01, 0
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idleAirValvePosition = scalar, U16, 88, "%", 0.01, 0
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etbTarget = scalar, S16, 90, "%", 0.01, 0
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etb1DutyCycle = scalar, S16, 92, "%", 0.01, 0
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etb1Error = scalar, S16, 94, "%", 0.01, 0
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fuelTankLevel = scalar, S16, 96, "%", 0.01, 0
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totalFuelConsumption = scalar, U16, 98, "grams", 1, 0
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fuelFlowRate = scalar, U16, 100, "gram/s", 0.005, 0
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veTableYAxis = scalar, U16, 102, "%", 0.01, 0
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afrTableYAxis = scalar, U16, 104, "%", 0.01, 0
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knockLevel = scalar, F32, 108, "Volts", 1, 0
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seconds = scalar, U32, 112, "sec", 1, 0
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engineMode = scalar, U32, 116, "em", 1, 0
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@ -34,25 +34,25 @@ injectorLagMs("fuel: injector lag", SensorCategory.SENSOR_INPUTS, FieldType.INT1
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iatCorrection("fuel: IAT correction", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 64, 0.01, 0.0, 0.0, "%"),
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cltCorrection("fuel: CLT correction", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 66, 0.01, 0.0, 0.0, "%"),
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baroCorrection("fuel: Barometric pressure correction", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 68, 0.01, 0.0, 0.0, "%"),
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currentEnginePhase("Engine Phase", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 70, 1.0, 0.0, 0.0, "deg"),
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wallFuelAmount("fuel: wall amount", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 72, 0.01, 0.0, 0.0, "mg"),
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wallFuelCorrection("fuel: wall correction", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 74, 0.01, 0.0, 0.0, "mg"),
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revolutionCounterSinceStart("revolutionCounterSinceStart", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 76, 1.0, 0.0, 0.0, ""),
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deltaTps("fuel: TPS change", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 78, 0.01, 0.0, 0.0, "ratio"),
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canReadCounter("canReadCounter", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 80, 1.0, 0.0, 0.0, ""),
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tpsAccelFuel("fuel: TPS acceleration extra fuel ms", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 82, 0.0033333333333333335, 0.0, 0.0, "ms"),
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ignitionAdvance("timing", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 84, 0.02, 0.0, 0.0, "deg"),
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sparkDwellValue("dwell: coil charge time", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 86, 0.0033333333333333335, 0.0, 0.0, "ms"),
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coilDutyCycle("dwell: coil duty cycle", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 88, 0.01, 0.0, 0.0, "%"),
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idleAirValvePosition("Idle Air Valve", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 90, 0.01, 0.0, 0.0, "%"),
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etbTarget("ETB Target", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 92, 0.01, 0.0, 0.0, "%"),
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etb1DutyCycle("ETB Duty", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 94, 0.01, 0.0, 0.0, "%"),
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etb1Error("ETB Error", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 96, 0.01, 0.0, 0.0, "%"),
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fuelTankLevel("Fuel level", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 98, 0.01, 0.0, 0.0, "%"),
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totalFuelConsumption("fuel: Total consumed", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 100, 1.0, 0.0, 0.0, "grams"),
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fuelFlowRate("fuel: Flow rate", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 102, 0.005, 0.0, 0.0, "gram/s"),
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veTableYAxis("veTableYAxis", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 104, 0.01, 0.0, 0.0, "%"),
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afrTableYAxis("afrTableYAxis", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 106, 0.01, 0.0, 0.0, "%"),
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wallFuelAmount("fuel: wall amount", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 70, 0.01, 0.0, 0.0, "mg"),
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wallFuelCorrection("fuel: wall correction", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 72, 0.01, 0.0, 0.0, "mg"),
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revolutionCounterSinceStart("revolutionCounterSinceStart", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 74, 1.0, 0.0, 0.0, ""),
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deltaTps("fuel: TPS change", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 76, 0.01, 0.0, 0.0, "ratio"),
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canReadCounter("canReadCounter", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 78, 1.0, 0.0, 0.0, ""),
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tpsAccelFuel("fuel: TPS acceleration extra fuel ms", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 80, 0.0033333333333333335, 0.0, 0.0, "ms"),
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ignitionAdvance("timing", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 82, 0.02, 0.0, 0.0, "deg"),
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sparkDwellValue("dwell: coil charge time", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 84, 0.0033333333333333335, 0.0, 0.0, "ms"),
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coilDutyCycle("dwell: coil duty cycle", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 86, 0.01, 0.0, 0.0, "%"),
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idleAirValvePosition("Idle Air Valve", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 88, 0.01, 0.0, 0.0, "%"),
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etbTarget("ETB Target", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 90, 0.01, 0.0, 0.0, "%"),
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etb1DutyCycle("ETB Duty", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 92, 0.01, 0.0, 0.0, "%"),
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etb1Error("ETB Error", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 94, 0.01, 0.0, 0.0, "%"),
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fuelTankLevel("Fuel level", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 96, 0.01, 0.0, 0.0, "%"),
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totalFuelConsumption("fuel: Total consumed", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 98, 1.0, 0.0, 0.0, "grams"),
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fuelFlowRate("fuel: Flow rate", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 100, 0.005, 0.0, 0.0, "gram/s"),
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veTableYAxis("veTableYAxis", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 102, 0.01, 0.0, 0.0, "%"),
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afrTableYAxis("afrTableYAxis", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 104, 0.01, 0.0, 0.0, "%"),
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alignmentFill_at_106("need 4 byte alignment", SensorCategory.SENSOR_INPUTS, FieldType.INT8, 106, 1.0, -20.0, 100.0, "units"),
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knockLevel("knock: current level", SensorCategory.SENSOR_INPUTS, FieldType.INT, 108, 1.0, 0.0, 0.0, "Volts"),
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seconds("Uptime", SensorCategory.SENSOR_INPUTS, FieldType.INT, 112, 1.0, 0.0, 0.0, "sec"),
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engineMode("Engine Mode", SensorCategory.SENSOR_INPUTS, FieldType.INT, 116, 1.0, 0.0, 0.0, "em"),
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@ -453,7 +453,7 @@ mapVvt_MAP_AT_SPECIAL_POINT("mapVvt_MAP_AT_SPECIAL_POINT", SensorCategory.SENSOR
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mapVvt_MAP_AT_DIFF("mapVvt_MAP_AT_DIFF", SensorCategory.SENSOR_INPUTS, FieldType.INT, 1100, 1.0, -10000.0, 10000.0, ""),
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mapVvt_MAP_AT_CYCLE_COUNT("mapVvt_MAP_AT_CYCLE_COUNT", SensorCategory.SENSOR_INPUTS, FieldType.INT8, 1104, 1.0, -10000.0, 10000.0, ""),
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mapVvt_map_peak("mapVvt_map_peak", SensorCategory.SENSOR_INPUTS, FieldType.INT8, 1105, 1.0, -10000.0, 10000.0, ""),
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currentEngineDecodedPhase("Engine Phase2", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 1106, 1.0, 0.0, 0.0, "deg"),
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currentEngineDecodedPhase("Engine Phase", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 1106, 1.0, 0.0, 0.0, "deg"),
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totalRevolutionCounter("Crank revolution counter", SensorCategory.SENSOR_INPUTS, FieldType.INT, 1108, 1.0, -1.0, -1.0, ""),
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vvtSyncGapRatio("vvtSyncGapRatio", SensorCategory.SENSOR_INPUTS, FieldType.INT, 1112, 1.0, -10000.0, 10000.0, ""),
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vvtCurrentPosition("vvtCurrentPosition", SensorCategory.SENSOR_INPUTS, FieldType.INT, 1116, 1.0, -10000.0, 10000.0, ""),
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@ -1,4 +1,4 @@
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// this section was generated automatically by rusEFI tool ConfigDefinition.jar based on (unknown script) console/binary/output_channels.txt Sat Aug 27 18:43:19 UTC 2022
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// this section was generated automatically by rusEFI tool ConfigDefinition.jar based on (unknown script) console/binary/output_channels.txt Thu Sep 01 04:17:54 UTC 2022
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// by class com.rusefi.output.CHeaderConsumer
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// begin
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#pragma once
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@ -342,114 +342,114 @@ struct output_channels_s {
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* offset 68
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*/
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scaled_channel<uint16_t, 100, 1> baroCorrection = (uint16_t)0;
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/**
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* Engine Phase
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deg
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* offset 70
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*/
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scaled_channel<uint16_t, 1, 1> unusedCurrentEnginePhase = (uint16_t)0;
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/**
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* @@GAUGE_NAME_FUEL_WALL_AMOUNT@@
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mg
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* offset 72
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* offset 70
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*/
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scaled_channel<uint16_t, 100, 1> wallFuelAmount = (uint16_t)0;
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/**
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* @@GAUGE_NAME_FUEL_WALL_CORRECTION@@
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mg
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* offset 74
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* offset 72
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*/
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scaled_channel<int16_t, 100, 1> wallFuelCorrection = (int16_t)0;
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/**
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* offset 76
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* offset 74
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*/
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uint16_t revolutionCounterSinceStart = (uint16_t)0;
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/**
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* @@GAUGE_NAME_FUEL_TPS_ROC@@
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ratio
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* offset 78
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* offset 76
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*/
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scaled_channel<int16_t, 100, 1> deltaTps = (int16_t)0;
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/**
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* offset 80
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* offset 78
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*/
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uint16_t canReadCounter = (uint16_t)0;
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/**
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* @@GAUGE_NAME_FUEL_TPS_EXTRA@@
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ms
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* offset 82
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* offset 80
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*/
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scaled_channel<int16_t, 300, 1> tpsAccelFuel = (int16_t)0;
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/**
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* @@GAUGE_NAME_TIMING_ADVANCE@@
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deg
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* offset 84
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* offset 82
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*/
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scaled_channel<int16_t, 50, 1> ignitionAdvance = (int16_t)0;
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/**
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* @@GAUGE_COIL_DWELL_TIME@@
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ms
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* offset 86
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* offset 84
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*/
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scaled_channel<uint16_t, 300, 1> sparkDwellValue = (uint16_t)0;
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/**
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* @@GAUGE_NAME_DWELL_DUTY@@
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%
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* offset 88
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* offset 86
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*/
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scaled_channel<uint16_t, 100, 1> coilDutyCycle = (uint16_t)0;
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/**
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* @@GAUGE_NAME_IAC@@
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%
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* offset 90
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* offset 88
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*/
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scaled_channel<uint16_t, 100, 1> idleAirValvePosition = (uint16_t)0;
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/**
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* ETB Target
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%
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* offset 92
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* offset 90
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*/
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scaled_channel<int16_t, 100, 1> etbTarget = (int16_t)0;
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/**
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* @@GAUGE_NAME_ETB_DUTY@@
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%
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* offset 94
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* offset 92
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*/
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scaled_channel<int16_t, 100, 1> etb1DutyCycle = (int16_t)0;
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/**
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* ETB Error
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%
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* offset 96
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* offset 94
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*/
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scaled_channel<int16_t, 100, 1> etb1Error = (int16_t)0;
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/**
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* Fuel level
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%
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* offset 98
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* offset 96
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*/
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scaled_channel<int16_t, 100, 1> fuelTankLevel = (int16_t)0;
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/**
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* @@GAUGE_NAME_FUEL_CONSUMPTION@@
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grams
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* offset 100
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* offset 98
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*/
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scaled_channel<uint16_t, 1, 1> totalFuelConsumption = (uint16_t)0;
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/**
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* @@GAUGE_NAME_FUEL_FLOW@@
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gram/s
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* offset 102
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* offset 100
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*/
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scaled_channel<uint16_t, 200, 1> fuelFlowRate = (uint16_t)0;
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/**
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%
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* offset 104
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* offset 102
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*/
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scaled_channel<uint16_t, 100, 1> veTableYAxis = (uint16_t)0;
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/**
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%
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* offset 106
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* offset 104
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*/
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scaled_channel<uint16_t, 100, 1> afrTableYAxis = (uint16_t)0;
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/**
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* need 4 byte alignment
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units
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* offset 106
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*/
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uint8_t alignmentFill_at_106[2];
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/**
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* @@GAUGE_NAME_KNOCK_LEVEL@@
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Volts
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@ -1318,4 +1318,4 @@ struct output_channels_s {
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static_assert(sizeof(output_channels_s) == 756);
|
||||
|
||||
// end
|
||||
// this section was generated automatically by rusEFI tool ConfigDefinition.jar based on (unknown script) console/binary/output_channels.txt Sat Aug 27 18:43:19 UTC 2022
|
||||
// this section was generated automatically by rusEFI tool ConfigDefinition.jar based on (unknown script) console/binary/output_channels.txt Thu Sep 01 04:17:54 UTC 2022
|
||||
|
|
|
|||
|
|
@ -1,4 +1,4 @@
|
|||
// this section was generated automatically by rusEFI tool ConfigDefinition.jar based on (unknown script) controllers/trigger/trigger_central.txt Thu Sep 01 03:55:33 UTC 2022
|
||||
// this section was generated automatically by rusEFI tool ConfigDefinition.jar based on (unknown script) controllers/trigger/trigger_central.txt Thu Sep 01 04:17:54 UTC 2022
|
||||
// by class com.rusefi.output.CHeaderConsumer
|
||||
// begin
|
||||
#pragma once
|
||||
|
|
@ -32,7 +32,7 @@ struct trigger_central_s {
|
|||
*/
|
||||
uint8_t mapVvt_map_peak = (uint8_t)0;
|
||||
/**
|
||||
* Engine Phase2
|
||||
* Engine Phase
|
||||
deg
|
||||
* offset 38
|
||||
*/
|
||||
|
|
@ -41,4 +41,4 @@ struct trigger_central_s {
|
|||
static_assert(sizeof(trigger_central_s) == 40);
|
||||
|
||||
// end
|
||||
// this section was generated automatically by rusEFI tool ConfigDefinition.jar based on (unknown script) controllers/trigger/trigger_central.txt Thu Sep 01 03:55:33 UTC 2022
|
||||
// this section was generated automatically by rusEFI tool ConfigDefinition.jar based on (unknown script) controllers/trigger/trigger_central.txt Thu Sep 01 04:17:54 UTC 2022
|
||||
|
|
|
|||
|
|
@ -86,7 +86,7 @@ enable2ndByteCanID = false
|
|||
; name = scalar, type, offset, units, scale, translate, lo, hi, digits
|
||||
|
||||
; CONFIG_DEFINITION_START
|
||||
; this section was generated automatically by rusEFI tool ConfigDefinition.jar based on gen_config.sh integration/rusefi_config.txt Thu Sep 01 03:56:35 UTC 2022
|
||||
; this section was generated automatically by rusEFI tool ConfigDefinition.jar based on gen_config.sh integration/rusefi_config.txt Thu Sep 01 04:18:47 UTC 2022
|
||||
|
||||
pageSize = 21300
|
||||
page = 1
|
||||
|
|
@ -2192,25 +2192,24 @@ injectorLagMs = scalar, U16, 62, "ms", 0.0033333333333333335, 0
|
|||
iatCorrection = scalar, U16, 64, "%", 0.01, 0
|
||||
cltCorrection = scalar, U16, 66, "%", 0.01, 0
|
||||
baroCorrection = scalar, U16, 68, "%", 0.01, 0
|
||||
currentEnginePhase = scalar, U16, 70, "deg", 1, 0
|
||||
wallFuelAmount = scalar, U16, 72, "mg", 0.01, 0
|
||||
wallFuelCorrection = scalar, S16, 74, "mg", 0.01, 0
|
||||
revolutionCounterSinceStart = scalar, U16, 76, "", 1, 0
|
||||
deltaTps = scalar, S16, 78, "ratio", 0.01, 0
|
||||
canReadCounter = scalar, U16, 80, "", 1, 0
|
||||
tpsAccelFuel = scalar, S16, 82, "ms", 0.0033333333333333335, 0
|
||||
ignitionAdvance = scalar, S16, 84, "deg", 0.02, 0
|
||||
sparkDwellValue = scalar, U16, 86, "ms", 0.0033333333333333335, 0
|
||||
coilDutyCycle = scalar, U16, 88, "%", 0.01, 0
|
||||
idleAirValvePosition = scalar, U16, 90, "%", 0.01, 0
|
||||
etbTarget = scalar, S16, 92, "%", 0.01, 0
|
||||
etb1DutyCycle = scalar, S16, 94, "%", 0.01, 0
|
||||
etb1Error = scalar, S16, 96, "%", 0.01, 0
|
||||
fuelTankLevel = scalar, S16, 98, "%", 0.01, 0
|
||||
totalFuelConsumption = scalar, U16, 100, "grams", 1, 0
|
||||
fuelFlowRate = scalar, U16, 102, "gram/s", 0.005, 0
|
||||
veTableYAxis = scalar, U16, 104, "%", 0.01, 0
|
||||
afrTableYAxis = scalar, U16, 106, "%", 0.01, 0
|
||||
wallFuelAmount = scalar, U16, 70, "mg", 0.01, 0
|
||||
wallFuelCorrection = scalar, S16, 72, "mg", 0.01, 0
|
||||
revolutionCounterSinceStart = scalar, U16, 74, "", 1, 0
|
||||
deltaTps = scalar, S16, 76, "ratio", 0.01, 0
|
||||
canReadCounter = scalar, U16, 78, "", 1, 0
|
||||
tpsAccelFuel = scalar, S16, 80, "ms", 0.0033333333333333335, 0
|
||||
ignitionAdvance = scalar, S16, 82, "deg", 0.02, 0
|
||||
sparkDwellValue = scalar, U16, 84, "ms", 0.0033333333333333335, 0
|
||||
coilDutyCycle = scalar, U16, 86, "%", 0.01, 0
|
||||
idleAirValvePosition = scalar, U16, 88, "%", 0.01, 0
|
||||
etbTarget = scalar, S16, 90, "%", 0.01, 0
|
||||
etb1DutyCycle = scalar, S16, 92, "%", 0.01, 0
|
||||
etb1Error = scalar, S16, 94, "%", 0.01, 0
|
||||
fuelTankLevel = scalar, S16, 96, "%", 0.01, 0
|
||||
totalFuelConsumption = scalar, U16, 98, "grams", 1, 0
|
||||
fuelFlowRate = scalar, U16, 100, "gram/s", 0.005, 0
|
||||
veTableYAxis = scalar, U16, 102, "%", 0.01, 0
|
||||
afrTableYAxis = scalar, U16, 104, "%", 0.01, 0
|
||||
knockLevel = scalar, F32, 108, "Volts", 1, 0
|
||||
seconds = scalar, U32, 112, "sec", 1, 0
|
||||
engineMode = scalar, U32, 116, "em", 1, 0
|
||||
|
|
@ -4501,7 +4500,6 @@ entry = injectorLagMs, "fuel: injector lag", float, "%.3f"
|
|||
entry = iatCorrection, "fuel: IAT correction", float, "%.3f"
|
||||
entry = cltCorrection, "fuel: CLT correction", float, "%.3f"
|
||||
entry = baroCorrection, "fuel: Barometric pressure correction", float, "%.3f"
|
||||
entry = currentEnginePhase, "Engine Phase", int, "%d"
|
||||
entry = wallFuelAmount, "fuel: wall amount", float, "%.3f"
|
||||
entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f"
|
||||
entry = revolutionCounterSinceStart, "revolutionCounterSinceStart", int, "%d"
|
||||
|
|
@ -4847,7 +4845,7 @@ entry = mapVvt_MAP_AT_SPECIAL_POINT, "mapVvt_MAP_AT_SPECIAL_POINT", float, "%.3
|
|||
entry = mapVvt_MAP_AT_DIFF, "mapVvt_MAP_AT_DIFF", float, "%.3f"
|
||||
entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d"
|
||||
entry = mapVvt_map_peak, "mapVvt_map_peak", int, "%d"
|
||||
entry = currentEngineDecodedPhase, "Engine Phase2", int, "%d"
|
||||
entry = currentEngineDecodedPhase, "Engine Phase", int, "%d"
|
||||
entry = totalRevolutionCounter, "Crank revolution counter", int, "%d"
|
||||
entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f"
|
||||
entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f"
|
||||
|
|
|
|||
|
|
@ -86,7 +86,7 @@ enable2ndByteCanID = false
|
|||
; name = scalar, type, offset, units, scale, translate, lo, hi, digits
|
||||
|
||||
; CONFIG_DEFINITION_START
|
||||
; this section was generated automatically by rusEFI tool ConfigDefinition.jar based on gen_config.sh integration/rusefi_config.txt Thu Sep 01 03:56:14 UTC 2022
|
||||
; this section was generated automatically by rusEFI tool ConfigDefinition.jar based on gen_config.sh integration/rusefi_config.txt Thu Sep 01 04:18:29 UTC 2022
|
||||
|
||||
pageSize = 21300
|
||||
page = 1
|
||||
|
|
@ -2192,25 +2192,24 @@ injectorLagMs = scalar, U16, 62, "ms", 0.0033333333333333335, 0
|
|||
iatCorrection = scalar, U16, 64, "%", 0.01, 0
|
||||
cltCorrection = scalar, U16, 66, "%", 0.01, 0
|
||||
baroCorrection = scalar, U16, 68, "%", 0.01, 0
|
||||
currentEnginePhase = scalar, U16, 70, "deg", 1, 0
|
||||
wallFuelAmount = scalar, U16, 72, "mg", 0.01, 0
|
||||
wallFuelCorrection = scalar, S16, 74, "mg", 0.01, 0
|
||||
revolutionCounterSinceStart = scalar, U16, 76, "", 1, 0
|
||||
deltaTps = scalar, S16, 78, "ratio", 0.01, 0
|
||||
canReadCounter = scalar, U16, 80, "", 1, 0
|
||||
tpsAccelFuel = scalar, S16, 82, "ms", 0.0033333333333333335, 0
|
||||
ignitionAdvance = scalar, S16, 84, "deg", 0.02, 0
|
||||
sparkDwellValue = scalar, U16, 86, "ms", 0.0033333333333333335, 0
|
||||
coilDutyCycle = scalar, U16, 88, "%", 0.01, 0
|
||||
idleAirValvePosition = scalar, U16, 90, "%", 0.01, 0
|
||||
etbTarget = scalar, S16, 92, "%", 0.01, 0
|
||||
etb1DutyCycle = scalar, S16, 94, "%", 0.01, 0
|
||||
etb1Error = scalar, S16, 96, "%", 0.01, 0
|
||||
fuelTankLevel = scalar, S16, 98, "%", 0.01, 0
|
||||
totalFuelConsumption = scalar, U16, 100, "grams", 1, 0
|
||||
fuelFlowRate = scalar, U16, 102, "gram/s", 0.005, 0
|
||||
veTableYAxis = scalar, U16, 104, "%", 0.01, 0
|
||||
afrTableYAxis = scalar, U16, 106, "%", 0.01, 0
|
||||
wallFuelAmount = scalar, U16, 70, "mg", 0.01, 0
|
||||
wallFuelCorrection = scalar, S16, 72, "mg", 0.01, 0
|
||||
revolutionCounterSinceStart = scalar, U16, 74, "", 1, 0
|
||||
deltaTps = scalar, S16, 76, "ratio", 0.01, 0
|
||||
canReadCounter = scalar, U16, 78, "", 1, 0
|
||||
tpsAccelFuel = scalar, S16, 80, "ms", 0.0033333333333333335, 0
|
||||
ignitionAdvance = scalar, S16, 82, "deg", 0.02, 0
|
||||
sparkDwellValue = scalar, U16, 84, "ms", 0.0033333333333333335, 0
|
||||
coilDutyCycle = scalar, U16, 86, "%", 0.01, 0
|
||||
idleAirValvePosition = scalar, U16, 88, "%", 0.01, 0
|
||||
etbTarget = scalar, S16, 90, "%", 0.01, 0
|
||||
etb1DutyCycle = scalar, S16, 92, "%", 0.01, 0
|
||||
etb1Error = scalar, S16, 94, "%", 0.01, 0
|
||||
fuelTankLevel = scalar, S16, 96, "%", 0.01, 0
|
||||
totalFuelConsumption = scalar, U16, 98, "grams", 1, 0
|
||||
fuelFlowRate = scalar, U16, 100, "gram/s", 0.005, 0
|
||||
veTableYAxis = scalar, U16, 102, "%", 0.01, 0
|
||||
afrTableYAxis = scalar, U16, 104, "%", 0.01, 0
|
||||
knockLevel = scalar, F32, 108, "Volts", 1, 0
|
||||
seconds = scalar, U32, 112, "sec", 1, 0
|
||||
engineMode = scalar, U32, 116, "em", 1, 0
|
||||
|
|
@ -4501,7 +4500,6 @@ entry = injectorLagMs, "fuel: injector lag", float, "%.3f"
|
|||
entry = iatCorrection, "fuel: IAT correction", float, "%.3f"
|
||||
entry = cltCorrection, "fuel: CLT correction", float, "%.3f"
|
||||
entry = baroCorrection, "fuel: Barometric pressure correction", float, "%.3f"
|
||||
entry = currentEnginePhase, "Engine Phase", int, "%d"
|
||||
entry = wallFuelAmount, "fuel: wall amount", float, "%.3f"
|
||||
entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f"
|
||||
entry = revolutionCounterSinceStart, "revolutionCounterSinceStart", int, "%d"
|
||||
|
|
@ -4847,7 +4845,7 @@ entry = mapVvt_MAP_AT_SPECIAL_POINT, "mapVvt_MAP_AT_SPECIAL_POINT", float, "%.3
|
|||
entry = mapVvt_MAP_AT_DIFF, "mapVvt_MAP_AT_DIFF", float, "%.3f"
|
||||
entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d"
|
||||
entry = mapVvt_map_peak, "mapVvt_map_peak", int, "%d"
|
||||
entry = currentEngineDecodedPhase, "Engine Phase2", int, "%d"
|
||||
entry = currentEngineDecodedPhase, "Engine Phase", int, "%d"
|
||||
entry = totalRevolutionCounter, "Crank revolution counter", int, "%d"
|
||||
entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f"
|
||||
entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f"
|
||||
|
|
|
|||
|
|
@ -86,7 +86,7 @@ enable2ndByteCanID = false
|
|||
; name = scalar, type, offset, units, scale, translate, lo, hi, digits
|
||||
|
||||
; CONFIG_DEFINITION_START
|
||||
; this section was generated automatically by rusEFI tool ConfigDefinition.jar based on gen_config.sh integration/rusefi_config.txt Thu Sep 01 03:55:40 UTC 2022
|
||||
; this section was generated automatically by rusEFI tool ConfigDefinition.jar based on gen_config.sh integration/rusefi_config.txt Thu Sep 01 04:18:00 UTC 2022
|
||||
|
||||
pageSize = 21300
|
||||
page = 1
|
||||
|
|
@ -2192,25 +2192,24 @@ injectorLagMs = scalar, U16, 62, "ms", 0.0033333333333333335, 0
|
|||
iatCorrection = scalar, U16, 64, "%", 0.01, 0
|
||||
cltCorrection = scalar, U16, 66, "%", 0.01, 0
|
||||
baroCorrection = scalar, U16, 68, "%", 0.01, 0
|
||||
currentEnginePhase = scalar, U16, 70, "deg", 1, 0
|
||||
wallFuelAmount = scalar, U16, 72, "mg", 0.01, 0
|
||||
wallFuelCorrection = scalar, S16, 74, "mg", 0.01, 0
|
||||
revolutionCounterSinceStart = scalar, U16, 76, "", 1, 0
|
||||
deltaTps = scalar, S16, 78, "ratio", 0.01, 0
|
||||
canReadCounter = scalar, U16, 80, "", 1, 0
|
||||
tpsAccelFuel = scalar, S16, 82, "ms", 0.0033333333333333335, 0
|
||||
ignitionAdvance = scalar, S16, 84, "deg", 0.02, 0
|
||||
sparkDwellValue = scalar, U16, 86, "ms", 0.0033333333333333335, 0
|
||||
coilDutyCycle = scalar, U16, 88, "%", 0.01, 0
|
||||
idleAirValvePosition = scalar, U16, 90, "%", 0.01, 0
|
||||
etbTarget = scalar, S16, 92, "%", 0.01, 0
|
||||
etb1DutyCycle = scalar, S16, 94, "%", 0.01, 0
|
||||
etb1Error = scalar, S16, 96, "%", 0.01, 0
|
||||
fuelTankLevel = scalar, S16, 98, "%", 0.01, 0
|
||||
totalFuelConsumption = scalar, U16, 100, "grams", 1, 0
|
||||
fuelFlowRate = scalar, U16, 102, "gram/s", 0.005, 0
|
||||
veTableYAxis = scalar, U16, 104, "%", 0.01, 0
|
||||
afrTableYAxis = scalar, U16, 106, "%", 0.01, 0
|
||||
wallFuelAmount = scalar, U16, 70, "mg", 0.01, 0
|
||||
wallFuelCorrection = scalar, S16, 72, "mg", 0.01, 0
|
||||
revolutionCounterSinceStart = scalar, U16, 74, "", 1, 0
|
||||
deltaTps = scalar, S16, 76, "ratio", 0.01, 0
|
||||
canReadCounter = scalar, U16, 78, "", 1, 0
|
||||
tpsAccelFuel = scalar, S16, 80, "ms", 0.0033333333333333335, 0
|
||||
ignitionAdvance = scalar, S16, 82, "deg", 0.02, 0
|
||||
sparkDwellValue = scalar, U16, 84, "ms", 0.0033333333333333335, 0
|
||||
coilDutyCycle = scalar, U16, 86, "%", 0.01, 0
|
||||
idleAirValvePosition = scalar, U16, 88, "%", 0.01, 0
|
||||
etbTarget = scalar, S16, 90, "%", 0.01, 0
|
||||
etb1DutyCycle = scalar, S16, 92, "%", 0.01, 0
|
||||
etb1Error = scalar, S16, 94, "%", 0.01, 0
|
||||
fuelTankLevel = scalar, S16, 96, "%", 0.01, 0
|
||||
totalFuelConsumption = scalar, U16, 98, "grams", 1, 0
|
||||
fuelFlowRate = scalar, U16, 100, "gram/s", 0.005, 0
|
||||
veTableYAxis = scalar, U16, 102, "%", 0.01, 0
|
||||
afrTableYAxis = scalar, U16, 104, "%", 0.01, 0
|
||||
knockLevel = scalar, F32, 108, "Volts", 1, 0
|
||||
seconds = scalar, U32, 112, "sec", 1, 0
|
||||
engineMode = scalar, U32, 116, "em", 1, 0
|
||||
|
|
@ -4501,7 +4500,6 @@ entry = injectorLagMs, "fuel: injector lag", float, "%.3f"
|
|||
entry = iatCorrection, "fuel: IAT correction", float, "%.3f"
|
||||
entry = cltCorrection, "fuel: CLT correction", float, "%.3f"
|
||||
entry = baroCorrection, "fuel: Barometric pressure correction", float, "%.3f"
|
||||
entry = currentEnginePhase, "Engine Phase", int, "%d"
|
||||
entry = wallFuelAmount, "fuel: wall amount", float, "%.3f"
|
||||
entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f"
|
||||
entry = revolutionCounterSinceStart, "revolutionCounterSinceStart", int, "%d"
|
||||
|
|
@ -4847,7 +4845,7 @@ entry = mapVvt_MAP_AT_SPECIAL_POINT, "mapVvt_MAP_AT_SPECIAL_POINT", float, "%.3
|
|||
entry = mapVvt_MAP_AT_DIFF, "mapVvt_MAP_AT_DIFF", float, "%.3f"
|
||||
entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d"
|
||||
entry = mapVvt_map_peak, "mapVvt_map_peak", int, "%d"
|
||||
entry = currentEngineDecodedPhase, "Engine Phase2", int, "%d"
|
||||
entry = currentEngineDecodedPhase, "Engine Phase", int, "%d"
|
||||
entry = totalRevolutionCounter, "Crank revolution counter", int, "%d"
|
||||
entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f"
|
||||
entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f"
|
||||
|
|
|
|||
|
|
@ -86,7 +86,7 @@ enable2ndByteCanID = false
|
|||
; name = scalar, type, offset, units, scale, translate, lo, hi, digits
|
||||
|
||||
; CONFIG_DEFINITION_START
|
||||
; this section was generated automatically by rusEFI tool ConfigDefinition.jar based on gen_config.sh integration/rusefi_config.txt Thu Sep 01 03:55:42 UTC 2022
|
||||
; this section was generated automatically by rusEFI tool ConfigDefinition.jar based on gen_config.sh integration/rusefi_config.txt Thu Sep 01 04:18:02 UTC 2022
|
||||
|
||||
pageSize = 21300
|
||||
page = 1
|
||||
|
|
@ -2192,25 +2192,24 @@ injectorLagMs = scalar, U16, 62, "ms", 0.0033333333333333335, 0
|
|||
iatCorrection = scalar, U16, 64, "%", 0.01, 0
|
||||
cltCorrection = scalar, U16, 66, "%", 0.01, 0
|
||||
baroCorrection = scalar, U16, 68, "%", 0.01, 0
|
||||
currentEnginePhase = scalar, U16, 70, "deg", 1, 0
|
||||
wallFuelAmount = scalar, U16, 72, "mg", 0.01, 0
|
||||
wallFuelCorrection = scalar, S16, 74, "mg", 0.01, 0
|
||||
revolutionCounterSinceStart = scalar, U16, 76, "", 1, 0
|
||||
deltaTps = scalar, S16, 78, "ratio", 0.01, 0
|
||||
canReadCounter = scalar, U16, 80, "", 1, 0
|
||||
tpsAccelFuel = scalar, S16, 82, "ms", 0.0033333333333333335, 0
|
||||
ignitionAdvance = scalar, S16, 84, "deg", 0.02, 0
|
||||
sparkDwellValue = scalar, U16, 86, "ms", 0.0033333333333333335, 0
|
||||
coilDutyCycle = scalar, U16, 88, "%", 0.01, 0
|
||||
idleAirValvePosition = scalar, U16, 90, "%", 0.01, 0
|
||||
etbTarget = scalar, S16, 92, "%", 0.01, 0
|
||||
etb1DutyCycle = scalar, S16, 94, "%", 0.01, 0
|
||||
etb1Error = scalar, S16, 96, "%", 0.01, 0
|
||||
fuelTankLevel = scalar, S16, 98, "%", 0.01, 0
|
||||
totalFuelConsumption = scalar, U16, 100, "grams", 1, 0
|
||||
fuelFlowRate = scalar, U16, 102, "gram/s", 0.005, 0
|
||||
veTableYAxis = scalar, U16, 104, "%", 0.01, 0
|
||||
afrTableYAxis = scalar, U16, 106, "%", 0.01, 0
|
||||
wallFuelAmount = scalar, U16, 70, "mg", 0.01, 0
|
||||
wallFuelCorrection = scalar, S16, 72, "mg", 0.01, 0
|
||||
revolutionCounterSinceStart = scalar, U16, 74, "", 1, 0
|
||||
deltaTps = scalar, S16, 76, "ratio", 0.01, 0
|
||||
canReadCounter = scalar, U16, 78, "", 1, 0
|
||||
tpsAccelFuel = scalar, S16, 80, "ms", 0.0033333333333333335, 0
|
||||
ignitionAdvance = scalar, S16, 82, "deg", 0.02, 0
|
||||
sparkDwellValue = scalar, U16, 84, "ms", 0.0033333333333333335, 0
|
||||
coilDutyCycle = scalar, U16, 86, "%", 0.01, 0
|
||||
idleAirValvePosition = scalar, U16, 88, "%", 0.01, 0
|
||||
etbTarget = scalar, S16, 90, "%", 0.01, 0
|
||||
etb1DutyCycle = scalar, S16, 92, "%", 0.01, 0
|
||||
etb1Error = scalar, S16, 94, "%", 0.01, 0
|
||||
fuelTankLevel = scalar, S16, 96, "%", 0.01, 0
|
||||
totalFuelConsumption = scalar, U16, 98, "grams", 1, 0
|
||||
fuelFlowRate = scalar, U16, 100, "gram/s", 0.005, 0
|
||||
veTableYAxis = scalar, U16, 102, "%", 0.01, 0
|
||||
afrTableYAxis = scalar, U16, 104, "%", 0.01, 0
|
||||
knockLevel = scalar, F32, 108, "Volts", 1, 0
|
||||
seconds = scalar, U32, 112, "sec", 1, 0
|
||||
engineMode = scalar, U32, 116, "em", 1, 0
|
||||
|
|
@ -4501,7 +4500,6 @@ entry = injectorLagMs, "fuel: injector lag", float, "%.3f"
|
|||
entry = iatCorrection, "fuel: IAT correction", float, "%.3f"
|
||||
entry = cltCorrection, "fuel: CLT correction", float, "%.3f"
|
||||
entry = baroCorrection, "fuel: Barometric pressure correction", float, "%.3f"
|
||||
entry = currentEnginePhase, "Engine Phase", int, "%d"
|
||||
entry = wallFuelAmount, "fuel: wall amount", float, "%.3f"
|
||||
entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f"
|
||||
entry = revolutionCounterSinceStart, "revolutionCounterSinceStart", int, "%d"
|
||||
|
|
@ -4847,7 +4845,7 @@ entry = mapVvt_MAP_AT_SPECIAL_POINT, "mapVvt_MAP_AT_SPECIAL_POINT", float, "%.3
|
|||
entry = mapVvt_MAP_AT_DIFF, "mapVvt_MAP_AT_DIFF", float, "%.3f"
|
||||
entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d"
|
||||
entry = mapVvt_map_peak, "mapVvt_map_peak", int, "%d"
|
||||
entry = currentEngineDecodedPhase, "Engine Phase2", int, "%d"
|
||||
entry = currentEngineDecodedPhase, "Engine Phase", int, "%d"
|
||||
entry = totalRevolutionCounter, "Crank revolution counter", int, "%d"
|
||||
entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f"
|
||||
entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f"
|
||||
|
|
|
|||
|
|
@ -86,7 +86,7 @@ enable2ndByteCanID = false
|
|||
; name = scalar, type, offset, units, scale, translate, lo, hi, digits
|
||||
|
||||
; CONFIG_DEFINITION_START
|
||||
; this section was generated automatically by rusEFI tool ConfigDefinition.jar based on gen_config.sh integration/rusefi_config.txt Thu Sep 01 03:56:31 UTC 2022
|
||||
; this section was generated automatically by rusEFI tool ConfigDefinition.jar based on gen_config.sh integration/rusefi_config.txt Thu Sep 01 04:18:44 UTC 2022
|
||||
|
||||
pageSize = 21300
|
||||
page = 1
|
||||
|
|
@ -2192,25 +2192,24 @@ injectorLagMs = scalar, U16, 62, "ms", 0.0033333333333333335, 0
|
|||
iatCorrection = scalar, U16, 64, "%", 0.01, 0
|
||||
cltCorrection = scalar, U16, 66, "%", 0.01, 0
|
||||
baroCorrection = scalar, U16, 68, "%", 0.01, 0
|
||||
currentEnginePhase = scalar, U16, 70, "deg", 1, 0
|
||||
wallFuelAmount = scalar, U16, 72, "mg", 0.01, 0
|
||||
wallFuelCorrection = scalar, S16, 74, "mg", 0.01, 0
|
||||
revolutionCounterSinceStart = scalar, U16, 76, "", 1, 0
|
||||
deltaTps = scalar, S16, 78, "ratio", 0.01, 0
|
||||
canReadCounter = scalar, U16, 80, "", 1, 0
|
||||
tpsAccelFuel = scalar, S16, 82, "ms", 0.0033333333333333335, 0
|
||||
ignitionAdvance = scalar, S16, 84, "deg", 0.02, 0
|
||||
sparkDwellValue = scalar, U16, 86, "ms", 0.0033333333333333335, 0
|
||||
coilDutyCycle = scalar, U16, 88, "%", 0.01, 0
|
||||
idleAirValvePosition = scalar, U16, 90, "%", 0.01, 0
|
||||
etbTarget = scalar, S16, 92, "%", 0.01, 0
|
||||
etb1DutyCycle = scalar, S16, 94, "%", 0.01, 0
|
||||
etb1Error = scalar, S16, 96, "%", 0.01, 0
|
||||
fuelTankLevel = scalar, S16, 98, "%", 0.01, 0
|
||||
totalFuelConsumption = scalar, U16, 100, "grams", 1, 0
|
||||
fuelFlowRate = scalar, U16, 102, "gram/s", 0.005, 0
|
||||
veTableYAxis = scalar, U16, 104, "%", 0.01, 0
|
||||
afrTableYAxis = scalar, U16, 106, "%", 0.01, 0
|
||||
wallFuelAmount = scalar, U16, 70, "mg", 0.01, 0
|
||||
wallFuelCorrection = scalar, S16, 72, "mg", 0.01, 0
|
||||
revolutionCounterSinceStart = scalar, U16, 74, "", 1, 0
|
||||
deltaTps = scalar, S16, 76, "ratio", 0.01, 0
|
||||
canReadCounter = scalar, U16, 78, "", 1, 0
|
||||
tpsAccelFuel = scalar, S16, 80, "ms", 0.0033333333333333335, 0
|
||||
ignitionAdvance = scalar, S16, 82, "deg", 0.02, 0
|
||||
sparkDwellValue = scalar, U16, 84, "ms", 0.0033333333333333335, 0
|
||||
coilDutyCycle = scalar, U16, 86, "%", 0.01, 0
|
||||
idleAirValvePosition = scalar, U16, 88, "%", 0.01, 0
|
||||
etbTarget = scalar, S16, 90, "%", 0.01, 0
|
||||
etb1DutyCycle = scalar, S16, 92, "%", 0.01, 0
|
||||
etb1Error = scalar, S16, 94, "%", 0.01, 0
|
||||
fuelTankLevel = scalar, S16, 96, "%", 0.01, 0
|
||||
totalFuelConsumption = scalar, U16, 98, "grams", 1, 0
|
||||
fuelFlowRate = scalar, U16, 100, "gram/s", 0.005, 0
|
||||
veTableYAxis = scalar, U16, 102, "%", 0.01, 0
|
||||
afrTableYAxis = scalar, U16, 104, "%", 0.01, 0
|
||||
knockLevel = scalar, F32, 108, "Volts", 1, 0
|
||||
seconds = scalar, U32, 112, "sec", 1, 0
|
||||
engineMode = scalar, U32, 116, "em", 1, 0
|
||||
|
|
@ -4501,7 +4500,6 @@ entry = injectorLagMs, "fuel: injector lag", float, "%.3f"
|
|||
entry = iatCorrection, "fuel: IAT correction", float, "%.3f"
|
||||
entry = cltCorrection, "fuel: CLT correction", float, "%.3f"
|
||||
entry = baroCorrection, "fuel: Barometric pressure correction", float, "%.3f"
|
||||
entry = currentEnginePhase, "Engine Phase", int, "%d"
|
||||
entry = wallFuelAmount, "fuel: wall amount", float, "%.3f"
|
||||
entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f"
|
||||
entry = revolutionCounterSinceStart, "revolutionCounterSinceStart", int, "%d"
|
||||
|
|
@ -4847,7 +4845,7 @@ entry = mapVvt_MAP_AT_SPECIAL_POINT, "mapVvt_MAP_AT_SPECIAL_POINT", float, "%.3
|
|||
entry = mapVvt_MAP_AT_DIFF, "mapVvt_MAP_AT_DIFF", float, "%.3f"
|
||||
entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d"
|
||||
entry = mapVvt_map_peak, "mapVvt_map_peak", int, "%d"
|
||||
entry = currentEngineDecodedPhase, "Engine Phase2", int, "%d"
|
||||
entry = currentEngineDecodedPhase, "Engine Phase", int, "%d"
|
||||
entry = totalRevolutionCounter, "Crank revolution counter", int, "%d"
|
||||
entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f"
|
||||
entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f"
|
||||
|
|
|
|||
|
|
@ -86,7 +86,7 @@ enable2ndByteCanID = false
|
|||
; name = scalar, type, offset, units, scale, translate, lo, hi, digits
|
||||
|
||||
; CONFIG_DEFINITION_START
|
||||
; this section was generated automatically by rusEFI tool ConfigDefinition.jar based on gen_config.sh integration/rusefi_config.txt Thu Sep 01 03:56:12 UTC 2022
|
||||
; this section was generated automatically by rusEFI tool ConfigDefinition.jar based on gen_config.sh integration/rusefi_config.txt Thu Sep 01 04:18:27 UTC 2022
|
||||
|
||||
pageSize = 21300
|
||||
page = 1
|
||||
|
|
@ -2192,25 +2192,24 @@ injectorLagMs = scalar, U16, 62, "ms", 0.0033333333333333335, 0
|
|||
iatCorrection = scalar, U16, 64, "%", 0.01, 0
|
||||
cltCorrection = scalar, U16, 66, "%", 0.01, 0
|
||||
baroCorrection = scalar, U16, 68, "%", 0.01, 0
|
||||
currentEnginePhase = scalar, U16, 70, "deg", 1, 0
|
||||
wallFuelAmount = scalar, U16, 72, "mg", 0.01, 0
|
||||
wallFuelCorrection = scalar, S16, 74, "mg", 0.01, 0
|
||||
revolutionCounterSinceStart = scalar, U16, 76, "", 1, 0
|
||||
deltaTps = scalar, S16, 78, "ratio", 0.01, 0
|
||||
canReadCounter = scalar, U16, 80, "", 1, 0
|
||||
tpsAccelFuel = scalar, S16, 82, "ms", 0.0033333333333333335, 0
|
||||
ignitionAdvance = scalar, S16, 84, "deg", 0.02, 0
|
||||
sparkDwellValue = scalar, U16, 86, "ms", 0.0033333333333333335, 0
|
||||
coilDutyCycle = scalar, U16, 88, "%", 0.01, 0
|
||||
idleAirValvePosition = scalar, U16, 90, "%", 0.01, 0
|
||||
etbTarget = scalar, S16, 92, "%", 0.01, 0
|
||||
etb1DutyCycle = scalar, S16, 94, "%", 0.01, 0
|
||||
etb1Error = scalar, S16, 96, "%", 0.01, 0
|
||||
fuelTankLevel = scalar, S16, 98, "%", 0.01, 0
|
||||
totalFuelConsumption = scalar, U16, 100, "grams", 1, 0
|
||||
fuelFlowRate = scalar, U16, 102, "gram/s", 0.005, 0
|
||||
veTableYAxis = scalar, U16, 104, "%", 0.01, 0
|
||||
afrTableYAxis = scalar, U16, 106, "%", 0.01, 0
|
||||
wallFuelAmount = scalar, U16, 70, "mg", 0.01, 0
|
||||
wallFuelCorrection = scalar, S16, 72, "mg", 0.01, 0
|
||||
revolutionCounterSinceStart = scalar, U16, 74, "", 1, 0
|
||||
deltaTps = scalar, S16, 76, "ratio", 0.01, 0
|
||||
canReadCounter = scalar, U16, 78, "", 1, 0
|
||||
tpsAccelFuel = scalar, S16, 80, "ms", 0.0033333333333333335, 0
|
||||
ignitionAdvance = scalar, S16, 82, "deg", 0.02, 0
|
||||
sparkDwellValue = scalar, U16, 84, "ms", 0.0033333333333333335, 0
|
||||
coilDutyCycle = scalar, U16, 86, "%", 0.01, 0
|
||||
idleAirValvePosition = scalar, U16, 88, "%", 0.01, 0
|
||||
etbTarget = scalar, S16, 90, "%", 0.01, 0
|
||||
etb1DutyCycle = scalar, S16, 92, "%", 0.01, 0
|
||||
etb1Error = scalar, S16, 94, "%", 0.01, 0
|
||||
fuelTankLevel = scalar, S16, 96, "%", 0.01, 0
|
||||
totalFuelConsumption = scalar, U16, 98, "grams", 1, 0
|
||||
fuelFlowRate = scalar, U16, 100, "gram/s", 0.005, 0
|
||||
veTableYAxis = scalar, U16, 102, "%", 0.01, 0
|
||||
afrTableYAxis = scalar, U16, 104, "%", 0.01, 0
|
||||
knockLevel = scalar, F32, 108, "Volts", 1, 0
|
||||
seconds = scalar, U32, 112, "sec", 1, 0
|
||||
engineMode = scalar, U32, 116, "em", 1, 0
|
||||
|
|
@ -4501,7 +4500,6 @@ entry = injectorLagMs, "fuel: injector lag", float, "%.3f"
|
|||
entry = iatCorrection, "fuel: IAT correction", float, "%.3f"
|
||||
entry = cltCorrection, "fuel: CLT correction", float, "%.3f"
|
||||
entry = baroCorrection, "fuel: Barometric pressure correction", float, "%.3f"
|
||||
entry = currentEnginePhase, "Engine Phase", int, "%d"
|
||||
entry = wallFuelAmount, "fuel: wall amount", float, "%.3f"
|
||||
entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f"
|
||||
entry = revolutionCounterSinceStart, "revolutionCounterSinceStart", int, "%d"
|
||||
|
|
@ -4847,7 +4845,7 @@ entry = mapVvt_MAP_AT_SPECIAL_POINT, "mapVvt_MAP_AT_SPECIAL_POINT", float, "%.3
|
|||
entry = mapVvt_MAP_AT_DIFF, "mapVvt_MAP_AT_DIFF", float, "%.3f"
|
||||
entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d"
|
||||
entry = mapVvt_map_peak, "mapVvt_map_peak", int, "%d"
|
||||
entry = currentEngineDecodedPhase, "Engine Phase2", int, "%d"
|
||||
entry = currentEngineDecodedPhase, "Engine Phase", int, "%d"
|
||||
entry = totalRevolutionCounter, "Crank revolution counter", int, "%d"
|
||||
entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f"
|
||||
entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f"
|
||||
|
|
|
|||
|
|
@ -86,7 +86,7 @@ enable2ndByteCanID = false
|
|||
; name = scalar, type, offset, units, scale, translate, lo, hi, digits
|
||||
|
||||
; CONFIG_DEFINITION_START
|
||||
; this section was generated automatically by rusEFI tool ConfigDefinition.jar based on hellen_cypress_gen_config.bat integration/rusefi_config.txt Thu Sep 01 03:55:37 UTC 2022
|
||||
; this section was generated automatically by rusEFI tool ConfigDefinition.jar based on hellen_cypress_gen_config.bat integration/rusefi_config.txt Thu Sep 01 04:17:57 UTC 2022
|
||||
|
||||
pageSize = 21300
|
||||
page = 1
|
||||
|
|
@ -2192,25 +2192,24 @@ injectorLagMs = scalar, U16, 62, "ms", 0.0033333333333333335, 0
|
|||
iatCorrection = scalar, U16, 64, "%", 0.01, 0
|
||||
cltCorrection = scalar, U16, 66, "%", 0.01, 0
|
||||
baroCorrection = scalar, U16, 68, "%", 0.01, 0
|
||||
currentEnginePhase = scalar, U16, 70, "deg", 1, 0
|
||||
wallFuelAmount = scalar, U16, 72, "mg", 0.01, 0
|
||||
wallFuelCorrection = scalar, S16, 74, "mg", 0.01, 0
|
||||
revolutionCounterSinceStart = scalar, U16, 76, "", 1, 0
|
||||
deltaTps = scalar, S16, 78, "ratio", 0.01, 0
|
||||
canReadCounter = scalar, U16, 80, "", 1, 0
|
||||
tpsAccelFuel = scalar, S16, 82, "ms", 0.0033333333333333335, 0
|
||||
ignitionAdvance = scalar, S16, 84, "deg", 0.02, 0
|
||||
sparkDwellValue = scalar, U16, 86, "ms", 0.0033333333333333335, 0
|
||||
coilDutyCycle = scalar, U16, 88, "%", 0.01, 0
|
||||
idleAirValvePosition = scalar, U16, 90, "%", 0.01, 0
|
||||
etbTarget = scalar, S16, 92, "%", 0.01, 0
|
||||
etb1DutyCycle = scalar, S16, 94, "%", 0.01, 0
|
||||
etb1Error = scalar, S16, 96, "%", 0.01, 0
|
||||
fuelTankLevel = scalar, S16, 98, "%", 0.01, 0
|
||||
totalFuelConsumption = scalar, U16, 100, "grams", 1, 0
|
||||
fuelFlowRate = scalar, U16, 102, "gram/s", 0.005, 0
|
||||
veTableYAxis = scalar, U16, 104, "%", 0.01, 0
|
||||
afrTableYAxis = scalar, U16, 106, "%", 0.01, 0
|
||||
wallFuelAmount = scalar, U16, 70, "mg", 0.01, 0
|
||||
wallFuelCorrection = scalar, S16, 72, "mg", 0.01, 0
|
||||
revolutionCounterSinceStart = scalar, U16, 74, "", 1, 0
|
||||
deltaTps = scalar, S16, 76, "ratio", 0.01, 0
|
||||
canReadCounter = scalar, U16, 78, "", 1, 0
|
||||
tpsAccelFuel = scalar, S16, 80, "ms", 0.0033333333333333335, 0
|
||||
ignitionAdvance = scalar, S16, 82, "deg", 0.02, 0
|
||||
sparkDwellValue = scalar, U16, 84, "ms", 0.0033333333333333335, 0
|
||||
coilDutyCycle = scalar, U16, 86, "%", 0.01, 0
|
||||
idleAirValvePosition = scalar, U16, 88, "%", 0.01, 0
|
||||
etbTarget = scalar, S16, 90, "%", 0.01, 0
|
||||
etb1DutyCycle = scalar, S16, 92, "%", 0.01, 0
|
||||
etb1Error = scalar, S16, 94, "%", 0.01, 0
|
||||
fuelTankLevel = scalar, S16, 96, "%", 0.01, 0
|
||||
totalFuelConsumption = scalar, U16, 98, "grams", 1, 0
|
||||
fuelFlowRate = scalar, U16, 100, "gram/s", 0.005, 0
|
||||
veTableYAxis = scalar, U16, 102, "%", 0.01, 0
|
||||
afrTableYAxis = scalar, U16, 104, "%", 0.01, 0
|
||||
knockLevel = scalar, F32, 108, "Volts", 1, 0
|
||||
seconds = scalar, U32, 112, "sec", 1, 0
|
||||
engineMode = scalar, U32, 116, "em", 1, 0
|
||||
|
|
@ -4501,7 +4500,6 @@ entry = injectorLagMs, "fuel: injector lag", float, "%.3f"
|
|||
entry = iatCorrection, "fuel: IAT correction", float, "%.3f"
|
||||
entry = cltCorrection, "fuel: CLT correction", float, "%.3f"
|
||||
entry = baroCorrection, "fuel: Barometric pressure correction", float, "%.3f"
|
||||
entry = currentEnginePhase, "Engine Phase", int, "%d"
|
||||
entry = wallFuelAmount, "fuel: wall amount", float, "%.3f"
|
||||
entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f"
|
||||
entry = revolutionCounterSinceStart, "revolutionCounterSinceStart", int, "%d"
|
||||
|
|
@ -4847,7 +4845,7 @@ entry = mapVvt_MAP_AT_SPECIAL_POINT, "mapVvt_MAP_AT_SPECIAL_POINT", float, "%.3
|
|||
entry = mapVvt_MAP_AT_DIFF, "mapVvt_MAP_AT_DIFF", float, "%.3f"
|
||||
entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d"
|
||||
entry = mapVvt_map_peak, "mapVvt_map_peak", int, "%d"
|
||||
entry = currentEngineDecodedPhase, "Engine Phase2", int, "%d"
|
||||
entry = currentEngineDecodedPhase, "Engine Phase", int, "%d"
|
||||
entry = totalRevolutionCounter, "Crank revolution counter", int, "%d"
|
||||
entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f"
|
||||
entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f"
|
||||
|
|
|
|||
|
|
@ -86,7 +86,7 @@ enable2ndByteCanID = false
|
|||
; name = scalar, type, offset, units, scale, translate, lo, hi, digits
|
||||
|
||||
; CONFIG_DEFINITION_START
|
||||
; this section was generated automatically by rusEFI tool ConfigDefinition.jar based on gen_config.sh integration/rusefi_config.txt Thu Sep 01 03:56:27 UTC 2022
|
||||
; this section was generated automatically by rusEFI tool ConfigDefinition.jar based on gen_config.sh integration/rusefi_config.txt Thu Sep 01 04:18:41 UTC 2022
|
||||
|
||||
pageSize = 21300
|
||||
page = 1
|
||||
|
|
@ -2192,25 +2192,24 @@ injectorLagMs = scalar, U16, 62, "ms", 0.0033333333333333335, 0
|
|||
iatCorrection = scalar, U16, 64, "%", 0.01, 0
|
||||
cltCorrection = scalar, U16, 66, "%", 0.01, 0
|
||||
baroCorrection = scalar, U16, 68, "%", 0.01, 0
|
||||
currentEnginePhase = scalar, U16, 70, "deg", 1, 0
|
||||
wallFuelAmount = scalar, U16, 72, "mg", 0.01, 0
|
||||
wallFuelCorrection = scalar, S16, 74, "mg", 0.01, 0
|
||||
revolutionCounterSinceStart = scalar, U16, 76, "", 1, 0
|
||||
deltaTps = scalar, S16, 78, "ratio", 0.01, 0
|
||||
canReadCounter = scalar, U16, 80, "", 1, 0
|
||||
tpsAccelFuel = scalar, S16, 82, "ms", 0.0033333333333333335, 0
|
||||
ignitionAdvance = scalar, S16, 84, "deg", 0.02, 0
|
||||
sparkDwellValue = scalar, U16, 86, "ms", 0.0033333333333333335, 0
|
||||
coilDutyCycle = scalar, U16, 88, "%", 0.01, 0
|
||||
idleAirValvePosition = scalar, U16, 90, "%", 0.01, 0
|
||||
etbTarget = scalar, S16, 92, "%", 0.01, 0
|
||||
etb1DutyCycle = scalar, S16, 94, "%", 0.01, 0
|
||||
etb1Error = scalar, S16, 96, "%", 0.01, 0
|
||||
fuelTankLevel = scalar, S16, 98, "%", 0.01, 0
|
||||
totalFuelConsumption = scalar, U16, 100, "grams", 1, 0
|
||||
fuelFlowRate = scalar, U16, 102, "gram/s", 0.005, 0
|
||||
veTableYAxis = scalar, U16, 104, "%", 0.01, 0
|
||||
afrTableYAxis = scalar, U16, 106, "%", 0.01, 0
|
||||
wallFuelAmount = scalar, U16, 70, "mg", 0.01, 0
|
||||
wallFuelCorrection = scalar, S16, 72, "mg", 0.01, 0
|
||||
revolutionCounterSinceStart = scalar, U16, 74, "", 1, 0
|
||||
deltaTps = scalar, S16, 76, "ratio", 0.01, 0
|
||||
canReadCounter = scalar, U16, 78, "", 1, 0
|
||||
tpsAccelFuel = scalar, S16, 80, "ms", 0.0033333333333333335, 0
|
||||
ignitionAdvance = scalar, S16, 82, "deg", 0.02, 0
|
||||
sparkDwellValue = scalar, U16, 84, "ms", 0.0033333333333333335, 0
|
||||
coilDutyCycle = scalar, U16, 86, "%", 0.01, 0
|
||||
idleAirValvePosition = scalar, U16, 88, "%", 0.01, 0
|
||||
etbTarget = scalar, S16, 90, "%", 0.01, 0
|
||||
etb1DutyCycle = scalar, S16, 92, "%", 0.01, 0
|
||||
etb1Error = scalar, S16, 94, "%", 0.01, 0
|
||||
fuelTankLevel = scalar, S16, 96, "%", 0.01, 0
|
||||
totalFuelConsumption = scalar, U16, 98, "grams", 1, 0
|
||||
fuelFlowRate = scalar, U16, 100, "gram/s", 0.005, 0
|
||||
veTableYAxis = scalar, U16, 102, "%", 0.01, 0
|
||||
afrTableYAxis = scalar, U16, 104, "%", 0.01, 0
|
||||
knockLevel = scalar, F32, 108, "Volts", 1, 0
|
||||
seconds = scalar, U32, 112, "sec", 1, 0
|
||||
engineMode = scalar, U32, 116, "em", 1, 0
|
||||
|
|
@ -4501,7 +4500,6 @@ entry = injectorLagMs, "fuel: injector lag", float, "%.3f"
|
|||
entry = iatCorrection, "fuel: IAT correction", float, "%.3f"
|
||||
entry = cltCorrection, "fuel: CLT correction", float, "%.3f"
|
||||
entry = baroCorrection, "fuel: Barometric pressure correction", float, "%.3f"
|
||||
entry = currentEnginePhase, "Engine Phase", int, "%d"
|
||||
entry = wallFuelAmount, "fuel: wall amount", float, "%.3f"
|
||||
entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f"
|
||||
entry = revolutionCounterSinceStart, "revolutionCounterSinceStart", int, "%d"
|
||||
|
|
@ -4847,7 +4845,7 @@ entry = mapVvt_MAP_AT_SPECIAL_POINT, "mapVvt_MAP_AT_SPECIAL_POINT", float, "%.3
|
|||
entry = mapVvt_MAP_AT_DIFF, "mapVvt_MAP_AT_DIFF", float, "%.3f"
|
||||
entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d"
|
||||
entry = mapVvt_map_peak, "mapVvt_map_peak", int, "%d"
|
||||
entry = currentEngineDecodedPhase, "Engine Phase2", int, "%d"
|
||||
entry = currentEngineDecodedPhase, "Engine Phase", int, "%d"
|
||||
entry = totalRevolutionCounter, "Crank revolution counter", int, "%d"
|
||||
entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f"
|
||||
entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f"
|
||||
|
|
|
|||
|
|
@ -86,7 +86,7 @@ enable2ndByteCanID = false
|
|||
; name = scalar, type, offset, units, scale, translate, lo, hi, digits
|
||||
|
||||
; CONFIG_DEFINITION_START
|
||||
; this section was generated automatically by rusEFI tool ConfigDefinition.jar based on gen_config.sh integration/rusefi_config.txt Thu Sep 01 03:56:29 UTC 2022
|
||||
; this section was generated automatically by rusEFI tool ConfigDefinition.jar based on gen_config.sh integration/rusefi_config.txt Thu Sep 01 04:18:42 UTC 2022
|
||||
|
||||
pageSize = 21300
|
||||
page = 1
|
||||
|
|
@ -2192,25 +2192,24 @@ injectorLagMs = scalar, U16, 62, "ms", 0.0033333333333333335, 0
|
|||
iatCorrection = scalar, U16, 64, "%", 0.01, 0
|
||||
cltCorrection = scalar, U16, 66, "%", 0.01, 0
|
||||
baroCorrection = scalar, U16, 68, "%", 0.01, 0
|
||||
currentEnginePhase = scalar, U16, 70, "deg", 1, 0
|
||||
wallFuelAmount = scalar, U16, 72, "mg", 0.01, 0
|
||||
wallFuelCorrection = scalar, S16, 74, "mg", 0.01, 0
|
||||
revolutionCounterSinceStart = scalar, U16, 76, "", 1, 0
|
||||
deltaTps = scalar, S16, 78, "ratio", 0.01, 0
|
||||
canReadCounter = scalar, U16, 80, "", 1, 0
|
||||
tpsAccelFuel = scalar, S16, 82, "ms", 0.0033333333333333335, 0
|
||||
ignitionAdvance = scalar, S16, 84, "deg", 0.02, 0
|
||||
sparkDwellValue = scalar, U16, 86, "ms", 0.0033333333333333335, 0
|
||||
coilDutyCycle = scalar, U16, 88, "%", 0.01, 0
|
||||
idleAirValvePosition = scalar, U16, 90, "%", 0.01, 0
|
||||
etbTarget = scalar, S16, 92, "%", 0.01, 0
|
||||
etb1DutyCycle = scalar, S16, 94, "%", 0.01, 0
|
||||
etb1Error = scalar, S16, 96, "%", 0.01, 0
|
||||
fuelTankLevel = scalar, S16, 98, "%", 0.01, 0
|
||||
totalFuelConsumption = scalar, U16, 100, "grams", 1, 0
|
||||
fuelFlowRate = scalar, U16, 102, "gram/s", 0.005, 0
|
||||
veTableYAxis = scalar, U16, 104, "%", 0.01, 0
|
||||
afrTableYAxis = scalar, U16, 106, "%", 0.01, 0
|
||||
wallFuelAmount = scalar, U16, 70, "mg", 0.01, 0
|
||||
wallFuelCorrection = scalar, S16, 72, "mg", 0.01, 0
|
||||
revolutionCounterSinceStart = scalar, U16, 74, "", 1, 0
|
||||
deltaTps = scalar, S16, 76, "ratio", 0.01, 0
|
||||
canReadCounter = scalar, U16, 78, "", 1, 0
|
||||
tpsAccelFuel = scalar, S16, 80, "ms", 0.0033333333333333335, 0
|
||||
ignitionAdvance = scalar, S16, 82, "deg", 0.02, 0
|
||||
sparkDwellValue = scalar, U16, 84, "ms", 0.0033333333333333335, 0
|
||||
coilDutyCycle = scalar, U16, 86, "%", 0.01, 0
|
||||
idleAirValvePosition = scalar, U16, 88, "%", 0.01, 0
|
||||
etbTarget = scalar, S16, 90, "%", 0.01, 0
|
||||
etb1DutyCycle = scalar, S16, 92, "%", 0.01, 0
|
||||
etb1Error = scalar, S16, 94, "%", 0.01, 0
|
||||
fuelTankLevel = scalar, S16, 96, "%", 0.01, 0
|
||||
totalFuelConsumption = scalar, U16, 98, "grams", 1, 0
|
||||
fuelFlowRate = scalar, U16, 100, "gram/s", 0.005, 0
|
||||
veTableYAxis = scalar, U16, 102, "%", 0.01, 0
|
||||
afrTableYAxis = scalar, U16, 104, "%", 0.01, 0
|
||||
knockLevel = scalar, F32, 108, "Volts", 1, 0
|
||||
seconds = scalar, U32, 112, "sec", 1, 0
|
||||
engineMode = scalar, U32, 116, "em", 1, 0
|
||||
|
|
@ -4501,7 +4500,6 @@ entry = injectorLagMs, "fuel: injector lag", float, "%.3f"
|
|||
entry = iatCorrection, "fuel: IAT correction", float, "%.3f"
|
||||
entry = cltCorrection, "fuel: CLT correction", float, "%.3f"
|
||||
entry = baroCorrection, "fuel: Barometric pressure correction", float, "%.3f"
|
||||
entry = currentEnginePhase, "Engine Phase", int, "%d"
|
||||
entry = wallFuelAmount, "fuel: wall amount", float, "%.3f"
|
||||
entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f"
|
||||
entry = revolutionCounterSinceStart, "revolutionCounterSinceStart", int, "%d"
|
||||
|
|
@ -4847,7 +4845,7 @@ entry = mapVvt_MAP_AT_SPECIAL_POINT, "mapVvt_MAP_AT_SPECIAL_POINT", float, "%.3
|
|||
entry = mapVvt_MAP_AT_DIFF, "mapVvt_MAP_AT_DIFF", float, "%.3f"
|
||||
entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d"
|
||||
entry = mapVvt_map_peak, "mapVvt_map_peak", int, "%d"
|
||||
entry = currentEngineDecodedPhase, "Engine Phase2", int, "%d"
|
||||
entry = currentEngineDecodedPhase, "Engine Phase", int, "%d"
|
||||
entry = totalRevolutionCounter, "Crank revolution counter", int, "%d"
|
||||
entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f"
|
||||
entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f"
|
||||
|
|
|
|||
|
|
@ -86,7 +86,7 @@ enable2ndByteCanID = false
|
|||
; name = scalar, type, offset, units, scale, translate, lo, hi, digits
|
||||
|
||||
; CONFIG_DEFINITION_START
|
||||
; this section was generated automatically by rusEFI tool ConfigDefinition.jar based on gen_config.sh integration/rusefi_config.txt Thu Sep 01 03:56:16 UTC 2022
|
||||
; this section was generated automatically by rusEFI tool ConfigDefinition.jar based on gen_config.sh integration/rusefi_config.txt Thu Sep 01 04:18:30 UTC 2022
|
||||
|
||||
pageSize = 21300
|
||||
page = 1
|
||||
|
|
@ -2192,25 +2192,24 @@ injectorLagMs = scalar, U16, 62, "ms", 0.0033333333333333335, 0
|
|||
iatCorrection = scalar, U16, 64, "%", 0.01, 0
|
||||
cltCorrection = scalar, U16, 66, "%", 0.01, 0
|
||||
baroCorrection = scalar, U16, 68, "%", 0.01, 0
|
||||
currentEnginePhase = scalar, U16, 70, "deg", 1, 0
|
||||
wallFuelAmount = scalar, U16, 72, "mg", 0.01, 0
|
||||
wallFuelCorrection = scalar, S16, 74, "mg", 0.01, 0
|
||||
revolutionCounterSinceStart = scalar, U16, 76, "", 1, 0
|
||||
deltaTps = scalar, S16, 78, "ratio", 0.01, 0
|
||||
canReadCounter = scalar, U16, 80, "", 1, 0
|
||||
tpsAccelFuel = scalar, S16, 82, "ms", 0.0033333333333333335, 0
|
||||
ignitionAdvance = scalar, S16, 84, "deg", 0.02, 0
|
||||
sparkDwellValue = scalar, U16, 86, "ms", 0.0033333333333333335, 0
|
||||
coilDutyCycle = scalar, U16, 88, "%", 0.01, 0
|
||||
idleAirValvePosition = scalar, U16, 90, "%", 0.01, 0
|
||||
etbTarget = scalar, S16, 92, "%", 0.01, 0
|
||||
etb1DutyCycle = scalar, S16, 94, "%", 0.01, 0
|
||||
etb1Error = scalar, S16, 96, "%", 0.01, 0
|
||||
fuelTankLevel = scalar, S16, 98, "%", 0.01, 0
|
||||
totalFuelConsumption = scalar, U16, 100, "grams", 1, 0
|
||||
fuelFlowRate = scalar, U16, 102, "gram/s", 0.005, 0
|
||||
veTableYAxis = scalar, U16, 104, "%", 0.01, 0
|
||||
afrTableYAxis = scalar, U16, 106, "%", 0.01, 0
|
||||
wallFuelAmount = scalar, U16, 70, "mg", 0.01, 0
|
||||
wallFuelCorrection = scalar, S16, 72, "mg", 0.01, 0
|
||||
revolutionCounterSinceStart = scalar, U16, 74, "", 1, 0
|
||||
deltaTps = scalar, S16, 76, "ratio", 0.01, 0
|
||||
canReadCounter = scalar, U16, 78, "", 1, 0
|
||||
tpsAccelFuel = scalar, S16, 80, "ms", 0.0033333333333333335, 0
|
||||
ignitionAdvance = scalar, S16, 82, "deg", 0.02, 0
|
||||
sparkDwellValue = scalar, U16, 84, "ms", 0.0033333333333333335, 0
|
||||
coilDutyCycle = scalar, U16, 86, "%", 0.01, 0
|
||||
idleAirValvePosition = scalar, U16, 88, "%", 0.01, 0
|
||||
etbTarget = scalar, S16, 90, "%", 0.01, 0
|
||||
etb1DutyCycle = scalar, S16, 92, "%", 0.01, 0
|
||||
etb1Error = scalar, S16, 94, "%", 0.01, 0
|
||||
fuelTankLevel = scalar, S16, 96, "%", 0.01, 0
|
||||
totalFuelConsumption = scalar, U16, 98, "grams", 1, 0
|
||||
fuelFlowRate = scalar, U16, 100, "gram/s", 0.005, 0
|
||||
veTableYAxis = scalar, U16, 102, "%", 0.01, 0
|
||||
afrTableYAxis = scalar, U16, 104, "%", 0.01, 0
|
||||
knockLevel = scalar, F32, 108, "Volts", 1, 0
|
||||
seconds = scalar, U32, 112, "sec", 1, 0
|
||||
engineMode = scalar, U32, 116, "em", 1, 0
|
||||
|
|
@ -4501,7 +4500,6 @@ entry = injectorLagMs, "fuel: injector lag", float, "%.3f"
|
|||
entry = iatCorrection, "fuel: IAT correction", float, "%.3f"
|
||||
entry = cltCorrection, "fuel: CLT correction", float, "%.3f"
|
||||
entry = baroCorrection, "fuel: Barometric pressure correction", float, "%.3f"
|
||||
entry = currentEnginePhase, "Engine Phase", int, "%d"
|
||||
entry = wallFuelAmount, "fuel: wall amount", float, "%.3f"
|
||||
entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f"
|
||||
entry = revolutionCounterSinceStart, "revolutionCounterSinceStart", int, "%d"
|
||||
|
|
@ -4847,7 +4845,7 @@ entry = mapVvt_MAP_AT_SPECIAL_POINT, "mapVvt_MAP_AT_SPECIAL_POINT", float, "%.3
|
|||
entry = mapVvt_MAP_AT_DIFF, "mapVvt_MAP_AT_DIFF", float, "%.3f"
|
||||
entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d"
|
||||
entry = mapVvt_map_peak, "mapVvt_map_peak", int, "%d"
|
||||
entry = currentEngineDecodedPhase, "Engine Phase2", int, "%d"
|
||||
entry = currentEngineDecodedPhase, "Engine Phase", int, "%d"
|
||||
entry = totalRevolutionCounter, "Crank revolution counter", int, "%d"
|
||||
entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f"
|
||||
entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f"
|
||||
|
|
|
|||
|
|
@ -86,7 +86,7 @@ enable2ndByteCanID = false
|
|||
; name = scalar, type, offset, units, scale, translate, lo, hi, digits
|
||||
|
||||
; CONFIG_DEFINITION_START
|
||||
; this section was generated automatically by rusEFI tool ConfigDefinition.jar based on gen_config.sh integration/rusefi_config.txt Thu Sep 01 03:55:44 UTC 2022
|
||||
; this section was generated automatically by rusEFI tool ConfigDefinition.jar based on gen_config.sh integration/rusefi_config.txt Thu Sep 01 04:18:03 UTC 2022
|
||||
|
||||
pageSize = 21300
|
||||
page = 1
|
||||
|
|
@ -2192,25 +2192,24 @@ injectorLagMs = scalar, U16, 62, "ms", 0.0033333333333333335, 0
|
|||
iatCorrection = scalar, U16, 64, "%", 0.01, 0
|
||||
cltCorrection = scalar, U16, 66, "%", 0.01, 0
|
||||
baroCorrection = scalar, U16, 68, "%", 0.01, 0
|
||||
currentEnginePhase = scalar, U16, 70, "deg", 1, 0
|
||||
wallFuelAmount = scalar, U16, 72, "mg", 0.01, 0
|
||||
wallFuelCorrection = scalar, S16, 74, "mg", 0.01, 0
|
||||
revolutionCounterSinceStart = scalar, U16, 76, "", 1, 0
|
||||
deltaTps = scalar, S16, 78, "ratio", 0.01, 0
|
||||
canReadCounter = scalar, U16, 80, "", 1, 0
|
||||
tpsAccelFuel = scalar, S16, 82, "ms", 0.0033333333333333335, 0
|
||||
ignitionAdvance = scalar, S16, 84, "deg", 0.02, 0
|
||||
sparkDwellValue = scalar, U16, 86, "ms", 0.0033333333333333335, 0
|
||||
coilDutyCycle = scalar, U16, 88, "%", 0.01, 0
|
||||
idleAirValvePosition = scalar, U16, 90, "%", 0.01, 0
|
||||
etbTarget = scalar, S16, 92, "%", 0.01, 0
|
||||
etb1DutyCycle = scalar, S16, 94, "%", 0.01, 0
|
||||
etb1Error = scalar, S16, 96, "%", 0.01, 0
|
||||
fuelTankLevel = scalar, S16, 98, "%", 0.01, 0
|
||||
totalFuelConsumption = scalar, U16, 100, "grams", 1, 0
|
||||
fuelFlowRate = scalar, U16, 102, "gram/s", 0.005, 0
|
||||
veTableYAxis = scalar, U16, 104, "%", 0.01, 0
|
||||
afrTableYAxis = scalar, U16, 106, "%", 0.01, 0
|
||||
wallFuelAmount = scalar, U16, 70, "mg", 0.01, 0
|
||||
wallFuelCorrection = scalar, S16, 72, "mg", 0.01, 0
|
||||
revolutionCounterSinceStart = scalar, U16, 74, "", 1, 0
|
||||
deltaTps = scalar, S16, 76, "ratio", 0.01, 0
|
||||
canReadCounter = scalar, U16, 78, "", 1, 0
|
||||
tpsAccelFuel = scalar, S16, 80, "ms", 0.0033333333333333335, 0
|
||||
ignitionAdvance = scalar, S16, 82, "deg", 0.02, 0
|
||||
sparkDwellValue = scalar, U16, 84, "ms", 0.0033333333333333335, 0
|
||||
coilDutyCycle = scalar, U16, 86, "%", 0.01, 0
|
||||
idleAirValvePosition = scalar, U16, 88, "%", 0.01, 0
|
||||
etbTarget = scalar, S16, 90, "%", 0.01, 0
|
||||
etb1DutyCycle = scalar, S16, 92, "%", 0.01, 0
|
||||
etb1Error = scalar, S16, 94, "%", 0.01, 0
|
||||
fuelTankLevel = scalar, S16, 96, "%", 0.01, 0
|
||||
totalFuelConsumption = scalar, U16, 98, "grams", 1, 0
|
||||
fuelFlowRate = scalar, U16, 100, "gram/s", 0.005, 0
|
||||
veTableYAxis = scalar, U16, 102, "%", 0.01, 0
|
||||
afrTableYAxis = scalar, U16, 104, "%", 0.01, 0
|
||||
knockLevel = scalar, F32, 108, "Volts", 1, 0
|
||||
seconds = scalar, U32, 112, "sec", 1, 0
|
||||
engineMode = scalar, U32, 116, "em", 1, 0
|
||||
|
|
@ -4501,7 +4500,6 @@ entry = injectorLagMs, "fuel: injector lag", float, "%.3f"
|
|||
entry = iatCorrection, "fuel: IAT correction", float, "%.3f"
|
||||
entry = cltCorrection, "fuel: CLT correction", float, "%.3f"
|
||||
entry = baroCorrection, "fuel: Barometric pressure correction", float, "%.3f"
|
||||
entry = currentEnginePhase, "Engine Phase", int, "%d"
|
||||
entry = wallFuelAmount, "fuel: wall amount", float, "%.3f"
|
||||
entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f"
|
||||
entry = revolutionCounterSinceStart, "revolutionCounterSinceStart", int, "%d"
|
||||
|
|
@ -4847,7 +4845,7 @@ entry = mapVvt_MAP_AT_SPECIAL_POINT, "mapVvt_MAP_AT_SPECIAL_POINT", float, "%.3
|
|||
entry = mapVvt_MAP_AT_DIFF, "mapVvt_MAP_AT_DIFF", float, "%.3f"
|
||||
entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d"
|
||||
entry = mapVvt_map_peak, "mapVvt_map_peak", int, "%d"
|
||||
entry = currentEngineDecodedPhase, "Engine Phase2", int, "%d"
|
||||
entry = currentEngineDecodedPhase, "Engine Phase", int, "%d"
|
||||
entry = totalRevolutionCounter, "Crank revolution counter", int, "%d"
|
||||
entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f"
|
||||
entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f"
|
||||
|
|
|
|||
|
|
@ -86,7 +86,7 @@ enable2ndByteCanID = false
|
|||
; name = scalar, type, offset, units, scale, translate, lo, hi, digits
|
||||
|
||||
; CONFIG_DEFINITION_START
|
||||
; this section was generated automatically by rusEFI tool ConfigDefinition.jar based on gen_config.sh integration/rusefi_config.txt Thu Sep 01 03:56:02 UTC 2022
|
||||
; this section was generated automatically by rusEFI tool ConfigDefinition.jar based on gen_config.sh integration/rusefi_config.txt Thu Sep 01 04:18:19 UTC 2022
|
||||
|
||||
pageSize = 21300
|
||||
page = 1
|
||||
|
|
@ -2192,25 +2192,24 @@ injectorLagMs = scalar, U16, 62, "ms", 0.0033333333333333335, 0
|
|||
iatCorrection = scalar, U16, 64, "%", 0.01, 0
|
||||
cltCorrection = scalar, U16, 66, "%", 0.01, 0
|
||||
baroCorrection = scalar, U16, 68, "%", 0.01, 0
|
||||
currentEnginePhase = scalar, U16, 70, "deg", 1, 0
|
||||
wallFuelAmount = scalar, U16, 72, "mg", 0.01, 0
|
||||
wallFuelCorrection = scalar, S16, 74, "mg", 0.01, 0
|
||||
revolutionCounterSinceStart = scalar, U16, 76, "", 1, 0
|
||||
deltaTps = scalar, S16, 78, "ratio", 0.01, 0
|
||||
canReadCounter = scalar, U16, 80, "", 1, 0
|
||||
tpsAccelFuel = scalar, S16, 82, "ms", 0.0033333333333333335, 0
|
||||
ignitionAdvance = scalar, S16, 84, "deg", 0.02, 0
|
||||
sparkDwellValue = scalar, U16, 86, "ms", 0.0033333333333333335, 0
|
||||
coilDutyCycle = scalar, U16, 88, "%", 0.01, 0
|
||||
idleAirValvePosition = scalar, U16, 90, "%", 0.01, 0
|
||||
etbTarget = scalar, S16, 92, "%", 0.01, 0
|
||||
etb1DutyCycle = scalar, S16, 94, "%", 0.01, 0
|
||||
etb1Error = scalar, S16, 96, "%", 0.01, 0
|
||||
fuelTankLevel = scalar, S16, 98, "%", 0.01, 0
|
||||
totalFuelConsumption = scalar, U16, 100, "grams", 1, 0
|
||||
fuelFlowRate = scalar, U16, 102, "gram/s", 0.005, 0
|
||||
veTableYAxis = scalar, U16, 104, "%", 0.01, 0
|
||||
afrTableYAxis = scalar, U16, 106, "%", 0.01, 0
|
||||
wallFuelAmount = scalar, U16, 70, "mg", 0.01, 0
|
||||
wallFuelCorrection = scalar, S16, 72, "mg", 0.01, 0
|
||||
revolutionCounterSinceStart = scalar, U16, 74, "", 1, 0
|
||||
deltaTps = scalar, S16, 76, "ratio", 0.01, 0
|
||||
canReadCounter = scalar, U16, 78, "", 1, 0
|
||||
tpsAccelFuel = scalar, S16, 80, "ms", 0.0033333333333333335, 0
|
||||
ignitionAdvance = scalar, S16, 82, "deg", 0.02, 0
|
||||
sparkDwellValue = scalar, U16, 84, "ms", 0.0033333333333333335, 0
|
||||
coilDutyCycle = scalar, U16, 86, "%", 0.01, 0
|
||||
idleAirValvePosition = scalar, U16, 88, "%", 0.01, 0
|
||||
etbTarget = scalar, S16, 90, "%", 0.01, 0
|
||||
etb1DutyCycle = scalar, S16, 92, "%", 0.01, 0
|
||||
etb1Error = scalar, S16, 94, "%", 0.01, 0
|
||||
fuelTankLevel = scalar, S16, 96, "%", 0.01, 0
|
||||
totalFuelConsumption = scalar, U16, 98, "grams", 1, 0
|
||||
fuelFlowRate = scalar, U16, 100, "gram/s", 0.005, 0
|
||||
veTableYAxis = scalar, U16, 102, "%", 0.01, 0
|
||||
afrTableYAxis = scalar, U16, 104, "%", 0.01, 0
|
||||
knockLevel = scalar, F32, 108, "Volts", 1, 0
|
||||
seconds = scalar, U32, 112, "sec", 1, 0
|
||||
engineMode = scalar, U32, 116, "em", 1, 0
|
||||
|
|
@ -4501,7 +4500,6 @@ entry = injectorLagMs, "fuel: injector lag", float, "%.3f"
|
|||
entry = iatCorrection, "fuel: IAT correction", float, "%.3f"
|
||||
entry = cltCorrection, "fuel: CLT correction", float, "%.3f"
|
||||
entry = baroCorrection, "fuel: Barometric pressure correction", float, "%.3f"
|
||||
entry = currentEnginePhase, "Engine Phase", int, "%d"
|
||||
entry = wallFuelAmount, "fuel: wall amount", float, "%.3f"
|
||||
entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f"
|
||||
entry = revolutionCounterSinceStart, "revolutionCounterSinceStart", int, "%d"
|
||||
|
|
@ -4847,7 +4845,7 @@ entry = mapVvt_MAP_AT_SPECIAL_POINT, "mapVvt_MAP_AT_SPECIAL_POINT", float, "%.3
|
|||
entry = mapVvt_MAP_AT_DIFF, "mapVvt_MAP_AT_DIFF", float, "%.3f"
|
||||
entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d"
|
||||
entry = mapVvt_map_peak, "mapVvt_map_peak", int, "%d"
|
||||
entry = currentEngineDecodedPhase, "Engine Phase2", int, "%d"
|
||||
entry = currentEngineDecodedPhase, "Engine Phase", int, "%d"
|
||||
entry = totalRevolutionCounter, "Crank revolution counter", int, "%d"
|
||||
entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f"
|
||||
entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f"
|
||||
|
|
|
|||
|
|
@ -86,7 +86,7 @@ enable2ndByteCanID = false
|
|||
; name = scalar, type, offset, units, scale, translate, lo, hi, digits
|
||||
|
||||
; CONFIG_DEFINITION_START
|
||||
; this section was generated automatically by rusEFI tool ConfigDefinition.jar based on gen_config.sh integration/rusefi_config.txt Thu Sep 01 03:56:00 UTC 2022
|
||||
; this section was generated automatically by rusEFI tool ConfigDefinition.jar based on gen_config.sh integration/rusefi_config.txt Thu Sep 01 04:18:17 UTC 2022
|
||||
|
||||
pageSize = 21300
|
||||
page = 1
|
||||
|
|
@ -2192,25 +2192,24 @@ injectorLagMs = scalar, U16, 62, "ms", 0.0033333333333333335, 0
|
|||
iatCorrection = scalar, U16, 64, "%", 0.01, 0
|
||||
cltCorrection = scalar, U16, 66, "%", 0.01, 0
|
||||
baroCorrection = scalar, U16, 68, "%", 0.01, 0
|
||||
currentEnginePhase = scalar, U16, 70, "deg", 1, 0
|
||||
wallFuelAmount = scalar, U16, 72, "mg", 0.01, 0
|
||||
wallFuelCorrection = scalar, S16, 74, "mg", 0.01, 0
|
||||
revolutionCounterSinceStart = scalar, U16, 76, "", 1, 0
|
||||
deltaTps = scalar, S16, 78, "ratio", 0.01, 0
|
||||
canReadCounter = scalar, U16, 80, "", 1, 0
|
||||
tpsAccelFuel = scalar, S16, 82, "ms", 0.0033333333333333335, 0
|
||||
ignitionAdvance = scalar, S16, 84, "deg", 0.02, 0
|
||||
sparkDwellValue = scalar, U16, 86, "ms", 0.0033333333333333335, 0
|
||||
coilDutyCycle = scalar, U16, 88, "%", 0.01, 0
|
||||
idleAirValvePosition = scalar, U16, 90, "%", 0.01, 0
|
||||
etbTarget = scalar, S16, 92, "%", 0.01, 0
|
||||
etb1DutyCycle = scalar, S16, 94, "%", 0.01, 0
|
||||
etb1Error = scalar, S16, 96, "%", 0.01, 0
|
||||
fuelTankLevel = scalar, S16, 98, "%", 0.01, 0
|
||||
totalFuelConsumption = scalar, U16, 100, "grams", 1, 0
|
||||
fuelFlowRate = scalar, U16, 102, "gram/s", 0.005, 0
|
||||
veTableYAxis = scalar, U16, 104, "%", 0.01, 0
|
||||
afrTableYAxis = scalar, U16, 106, "%", 0.01, 0
|
||||
wallFuelAmount = scalar, U16, 70, "mg", 0.01, 0
|
||||
wallFuelCorrection = scalar, S16, 72, "mg", 0.01, 0
|
||||
revolutionCounterSinceStart = scalar, U16, 74, "", 1, 0
|
||||
deltaTps = scalar, S16, 76, "ratio", 0.01, 0
|
||||
canReadCounter = scalar, U16, 78, "", 1, 0
|
||||
tpsAccelFuel = scalar, S16, 80, "ms", 0.0033333333333333335, 0
|
||||
ignitionAdvance = scalar, S16, 82, "deg", 0.02, 0
|
||||
sparkDwellValue = scalar, U16, 84, "ms", 0.0033333333333333335, 0
|
||||
coilDutyCycle = scalar, U16, 86, "%", 0.01, 0
|
||||
idleAirValvePosition = scalar, U16, 88, "%", 0.01, 0
|
||||
etbTarget = scalar, S16, 90, "%", 0.01, 0
|
||||
etb1DutyCycle = scalar, S16, 92, "%", 0.01, 0
|
||||
etb1Error = scalar, S16, 94, "%", 0.01, 0
|
||||
fuelTankLevel = scalar, S16, 96, "%", 0.01, 0
|
||||
totalFuelConsumption = scalar, U16, 98, "grams", 1, 0
|
||||
fuelFlowRate = scalar, U16, 100, "gram/s", 0.005, 0
|
||||
veTableYAxis = scalar, U16, 102, "%", 0.01, 0
|
||||
afrTableYAxis = scalar, U16, 104, "%", 0.01, 0
|
||||
knockLevel = scalar, F32, 108, "Volts", 1, 0
|
||||
seconds = scalar, U32, 112, "sec", 1, 0
|
||||
engineMode = scalar, U32, 116, "em", 1, 0
|
||||
|
|
@ -4501,7 +4500,6 @@ entry = injectorLagMs, "fuel: injector lag", float, "%.3f"
|
|||
entry = iatCorrection, "fuel: IAT correction", float, "%.3f"
|
||||
entry = cltCorrection, "fuel: CLT correction", float, "%.3f"
|
||||
entry = baroCorrection, "fuel: Barometric pressure correction", float, "%.3f"
|
||||
entry = currentEnginePhase, "Engine Phase", int, "%d"
|
||||
entry = wallFuelAmount, "fuel: wall amount", float, "%.3f"
|
||||
entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f"
|
||||
entry = revolutionCounterSinceStart, "revolutionCounterSinceStart", int, "%d"
|
||||
|
|
@ -4847,7 +4845,7 @@ entry = mapVvt_MAP_AT_SPECIAL_POINT, "mapVvt_MAP_AT_SPECIAL_POINT", float, "%.3
|
|||
entry = mapVvt_MAP_AT_DIFF, "mapVvt_MAP_AT_DIFF", float, "%.3f"
|
||||
entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d"
|
||||
entry = mapVvt_map_peak, "mapVvt_map_peak", int, "%d"
|
||||
entry = currentEngineDecodedPhase, "Engine Phase2", int, "%d"
|
||||
entry = currentEngineDecodedPhase, "Engine Phase", int, "%d"
|
||||
entry = totalRevolutionCounter, "Crank revolution counter", int, "%d"
|
||||
entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f"
|
||||
entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f"
|
||||
|
|
|
|||
|
|
@ -86,7 +86,7 @@ enable2ndByteCanID = false
|
|||
; name = scalar, type, offset, units, scale, translate, lo, hi, digits
|
||||
|
||||
; CONFIG_DEFINITION_START
|
||||
; this section was generated automatically by rusEFI tool ConfigDefinition.jar based on gen_config.sh integration/rusefi_config.txt Thu Sep 01 03:55:50 UTC 2022
|
||||
; this section was generated automatically by rusEFI tool ConfigDefinition.jar based on gen_config.sh integration/rusefi_config.txt Thu Sep 01 04:18:08 UTC 2022
|
||||
|
||||
pageSize = 21300
|
||||
page = 1
|
||||
|
|
@ -2192,25 +2192,24 @@ injectorLagMs = scalar, U16, 62, "ms", 0.0033333333333333335, 0
|
|||
iatCorrection = scalar, U16, 64, "%", 0.01, 0
|
||||
cltCorrection = scalar, U16, 66, "%", 0.01, 0
|
||||
baroCorrection = scalar, U16, 68, "%", 0.01, 0
|
||||
currentEnginePhase = scalar, U16, 70, "deg", 1, 0
|
||||
wallFuelAmount = scalar, U16, 72, "mg", 0.01, 0
|
||||
wallFuelCorrection = scalar, S16, 74, "mg", 0.01, 0
|
||||
revolutionCounterSinceStart = scalar, U16, 76, "", 1, 0
|
||||
deltaTps = scalar, S16, 78, "ratio", 0.01, 0
|
||||
canReadCounter = scalar, U16, 80, "", 1, 0
|
||||
tpsAccelFuel = scalar, S16, 82, "ms", 0.0033333333333333335, 0
|
||||
ignitionAdvance = scalar, S16, 84, "deg", 0.02, 0
|
||||
sparkDwellValue = scalar, U16, 86, "ms", 0.0033333333333333335, 0
|
||||
coilDutyCycle = scalar, U16, 88, "%", 0.01, 0
|
||||
idleAirValvePosition = scalar, U16, 90, "%", 0.01, 0
|
||||
etbTarget = scalar, S16, 92, "%", 0.01, 0
|
||||
etb1DutyCycle = scalar, S16, 94, "%", 0.01, 0
|
||||
etb1Error = scalar, S16, 96, "%", 0.01, 0
|
||||
fuelTankLevel = scalar, S16, 98, "%", 0.01, 0
|
||||
totalFuelConsumption = scalar, U16, 100, "grams", 1, 0
|
||||
fuelFlowRate = scalar, U16, 102, "gram/s", 0.005, 0
|
||||
veTableYAxis = scalar, U16, 104, "%", 0.01, 0
|
||||
afrTableYAxis = scalar, U16, 106, "%", 0.01, 0
|
||||
wallFuelAmount = scalar, U16, 70, "mg", 0.01, 0
|
||||
wallFuelCorrection = scalar, S16, 72, "mg", 0.01, 0
|
||||
revolutionCounterSinceStart = scalar, U16, 74, "", 1, 0
|
||||
deltaTps = scalar, S16, 76, "ratio", 0.01, 0
|
||||
canReadCounter = scalar, U16, 78, "", 1, 0
|
||||
tpsAccelFuel = scalar, S16, 80, "ms", 0.0033333333333333335, 0
|
||||
ignitionAdvance = scalar, S16, 82, "deg", 0.02, 0
|
||||
sparkDwellValue = scalar, U16, 84, "ms", 0.0033333333333333335, 0
|
||||
coilDutyCycle = scalar, U16, 86, "%", 0.01, 0
|
||||
idleAirValvePosition = scalar, U16, 88, "%", 0.01, 0
|
||||
etbTarget = scalar, S16, 90, "%", 0.01, 0
|
||||
etb1DutyCycle = scalar, S16, 92, "%", 0.01, 0
|
||||
etb1Error = scalar, S16, 94, "%", 0.01, 0
|
||||
fuelTankLevel = scalar, S16, 96, "%", 0.01, 0
|
||||
totalFuelConsumption = scalar, U16, 98, "grams", 1, 0
|
||||
fuelFlowRate = scalar, U16, 100, "gram/s", 0.005, 0
|
||||
veTableYAxis = scalar, U16, 102, "%", 0.01, 0
|
||||
afrTableYAxis = scalar, U16, 104, "%", 0.01, 0
|
||||
knockLevel = scalar, F32, 108, "Volts", 1, 0
|
||||
seconds = scalar, U32, 112, "sec", 1, 0
|
||||
engineMode = scalar, U32, 116, "em", 1, 0
|
||||
|
|
@ -4501,7 +4500,6 @@ entry = injectorLagMs, "fuel: injector lag", float, "%.3f"
|
|||
entry = iatCorrection, "fuel: IAT correction", float, "%.3f"
|
||||
entry = cltCorrection, "fuel: CLT correction", float, "%.3f"
|
||||
entry = baroCorrection, "fuel: Barometric pressure correction", float, "%.3f"
|
||||
entry = currentEnginePhase, "Engine Phase", int, "%d"
|
||||
entry = wallFuelAmount, "fuel: wall amount", float, "%.3f"
|
||||
entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f"
|
||||
entry = revolutionCounterSinceStart, "revolutionCounterSinceStart", int, "%d"
|
||||
|
|
@ -4847,7 +4845,7 @@ entry = mapVvt_MAP_AT_SPECIAL_POINT, "mapVvt_MAP_AT_SPECIAL_POINT", float, "%.3
|
|||
entry = mapVvt_MAP_AT_DIFF, "mapVvt_MAP_AT_DIFF", float, "%.3f"
|
||||
entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d"
|
||||
entry = mapVvt_map_peak, "mapVvt_map_peak", int, "%d"
|
||||
entry = currentEngineDecodedPhase, "Engine Phase2", int, "%d"
|
||||
entry = currentEngineDecodedPhase, "Engine Phase", int, "%d"
|
||||
entry = totalRevolutionCounter, "Crank revolution counter", int, "%d"
|
||||
entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f"
|
||||
entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f"
|
||||
|
|
|
|||
|
|
@ -86,7 +86,7 @@ enable2ndByteCanID = false
|
|||
; name = scalar, type, offset, units, scale, translate, lo, hi, digits
|
||||
|
||||
; CONFIG_DEFINITION_START
|
||||
; this section was generated automatically by rusEFI tool ConfigDefinition.jar based on gen_config.sh integration/rusefi_config.txt Thu Sep 01 03:55:48 UTC 2022
|
||||
; this section was generated automatically by rusEFI tool ConfigDefinition.jar based on gen_config.sh integration/rusefi_config.txt Thu Sep 01 04:18:07 UTC 2022
|
||||
|
||||
pageSize = 21300
|
||||
page = 1
|
||||
|
|
@ -2192,25 +2192,24 @@ injectorLagMs = scalar, U16, 62, "ms", 0.0033333333333333335, 0
|
|||
iatCorrection = scalar, U16, 64, "%", 0.01, 0
|
||||
cltCorrection = scalar, U16, 66, "%", 0.01, 0
|
||||
baroCorrection = scalar, U16, 68, "%", 0.01, 0
|
||||
currentEnginePhase = scalar, U16, 70, "deg", 1, 0
|
||||
wallFuelAmount = scalar, U16, 72, "mg", 0.01, 0
|
||||
wallFuelCorrection = scalar, S16, 74, "mg", 0.01, 0
|
||||
revolutionCounterSinceStart = scalar, U16, 76, "", 1, 0
|
||||
deltaTps = scalar, S16, 78, "ratio", 0.01, 0
|
||||
canReadCounter = scalar, U16, 80, "", 1, 0
|
||||
tpsAccelFuel = scalar, S16, 82, "ms", 0.0033333333333333335, 0
|
||||
ignitionAdvance = scalar, S16, 84, "deg", 0.02, 0
|
||||
sparkDwellValue = scalar, U16, 86, "ms", 0.0033333333333333335, 0
|
||||
coilDutyCycle = scalar, U16, 88, "%", 0.01, 0
|
||||
idleAirValvePosition = scalar, U16, 90, "%", 0.01, 0
|
||||
etbTarget = scalar, S16, 92, "%", 0.01, 0
|
||||
etb1DutyCycle = scalar, S16, 94, "%", 0.01, 0
|
||||
etb1Error = scalar, S16, 96, "%", 0.01, 0
|
||||
fuelTankLevel = scalar, S16, 98, "%", 0.01, 0
|
||||
totalFuelConsumption = scalar, U16, 100, "grams", 1, 0
|
||||
fuelFlowRate = scalar, U16, 102, "gram/s", 0.005, 0
|
||||
veTableYAxis = scalar, U16, 104, "%", 0.01, 0
|
||||
afrTableYAxis = scalar, U16, 106, "%", 0.01, 0
|
||||
wallFuelAmount = scalar, U16, 70, "mg", 0.01, 0
|
||||
wallFuelCorrection = scalar, S16, 72, "mg", 0.01, 0
|
||||
revolutionCounterSinceStart = scalar, U16, 74, "", 1, 0
|
||||
deltaTps = scalar, S16, 76, "ratio", 0.01, 0
|
||||
canReadCounter = scalar, U16, 78, "", 1, 0
|
||||
tpsAccelFuel = scalar, S16, 80, "ms", 0.0033333333333333335, 0
|
||||
ignitionAdvance = scalar, S16, 82, "deg", 0.02, 0
|
||||
sparkDwellValue = scalar, U16, 84, "ms", 0.0033333333333333335, 0
|
||||
coilDutyCycle = scalar, U16, 86, "%", 0.01, 0
|
||||
idleAirValvePosition = scalar, U16, 88, "%", 0.01, 0
|
||||
etbTarget = scalar, S16, 90, "%", 0.01, 0
|
||||
etb1DutyCycle = scalar, S16, 92, "%", 0.01, 0
|
||||
etb1Error = scalar, S16, 94, "%", 0.01, 0
|
||||
fuelTankLevel = scalar, S16, 96, "%", 0.01, 0
|
||||
totalFuelConsumption = scalar, U16, 98, "grams", 1, 0
|
||||
fuelFlowRate = scalar, U16, 100, "gram/s", 0.005, 0
|
||||
veTableYAxis = scalar, U16, 102, "%", 0.01, 0
|
||||
afrTableYAxis = scalar, U16, 104, "%", 0.01, 0
|
||||
knockLevel = scalar, F32, 108, "Volts", 1, 0
|
||||
seconds = scalar, U32, 112, "sec", 1, 0
|
||||
engineMode = scalar, U32, 116, "em", 1, 0
|
||||
|
|
@ -4501,7 +4500,6 @@ entry = injectorLagMs, "fuel: injector lag", float, "%.3f"
|
|||
entry = iatCorrection, "fuel: IAT correction", float, "%.3f"
|
||||
entry = cltCorrection, "fuel: CLT correction", float, "%.3f"
|
||||
entry = baroCorrection, "fuel: Barometric pressure correction", float, "%.3f"
|
||||
entry = currentEnginePhase, "Engine Phase", int, "%d"
|
||||
entry = wallFuelAmount, "fuel: wall amount", float, "%.3f"
|
||||
entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f"
|
||||
entry = revolutionCounterSinceStart, "revolutionCounterSinceStart", int, "%d"
|
||||
|
|
@ -4847,7 +4845,7 @@ entry = mapVvt_MAP_AT_SPECIAL_POINT, "mapVvt_MAP_AT_SPECIAL_POINT", float, "%.3
|
|||
entry = mapVvt_MAP_AT_DIFF, "mapVvt_MAP_AT_DIFF", float, "%.3f"
|
||||
entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d"
|
||||
entry = mapVvt_map_peak, "mapVvt_map_peak", int, "%d"
|
||||
entry = currentEngineDecodedPhase, "Engine Phase2", int, "%d"
|
||||
entry = currentEngineDecodedPhase, "Engine Phase", int, "%d"
|
||||
entry = totalRevolutionCounter, "Crank revolution counter", int, "%d"
|
||||
entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f"
|
||||
entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f"
|
||||
|
|
|
|||
|
|
@ -86,7 +86,7 @@ enable2ndByteCanID = false
|
|||
; name = scalar, type, offset, units, scale, translate, lo, hi, digits
|
||||
|
||||
; CONFIG_DEFINITION_START
|
||||
; this section was generated automatically by rusEFI tool ConfigDefinition.jar based on gen_config.sh integration/rusefi_config.txt Thu Sep 01 03:55:46 UTC 2022
|
||||
; this section was generated automatically by rusEFI tool ConfigDefinition.jar based on gen_config.sh integration/rusefi_config.txt Thu Sep 01 04:18:05 UTC 2022
|
||||
|
||||
pageSize = 21300
|
||||
page = 1
|
||||
|
|
@ -2192,25 +2192,24 @@ injectorLagMs = scalar, U16, 62, "ms", 0.0033333333333333335, 0
|
|||
iatCorrection = scalar, U16, 64, "%", 0.01, 0
|
||||
cltCorrection = scalar, U16, 66, "%", 0.01, 0
|
||||
baroCorrection = scalar, U16, 68, "%", 0.01, 0
|
||||
currentEnginePhase = scalar, U16, 70, "deg", 1, 0
|
||||
wallFuelAmount = scalar, U16, 72, "mg", 0.01, 0
|
||||
wallFuelCorrection = scalar, S16, 74, "mg", 0.01, 0
|
||||
revolutionCounterSinceStart = scalar, U16, 76, "", 1, 0
|
||||
deltaTps = scalar, S16, 78, "ratio", 0.01, 0
|
||||
canReadCounter = scalar, U16, 80, "", 1, 0
|
||||
tpsAccelFuel = scalar, S16, 82, "ms", 0.0033333333333333335, 0
|
||||
ignitionAdvance = scalar, S16, 84, "deg", 0.02, 0
|
||||
sparkDwellValue = scalar, U16, 86, "ms", 0.0033333333333333335, 0
|
||||
coilDutyCycle = scalar, U16, 88, "%", 0.01, 0
|
||||
idleAirValvePosition = scalar, U16, 90, "%", 0.01, 0
|
||||
etbTarget = scalar, S16, 92, "%", 0.01, 0
|
||||
etb1DutyCycle = scalar, S16, 94, "%", 0.01, 0
|
||||
etb1Error = scalar, S16, 96, "%", 0.01, 0
|
||||
fuelTankLevel = scalar, S16, 98, "%", 0.01, 0
|
||||
totalFuelConsumption = scalar, U16, 100, "grams", 1, 0
|
||||
fuelFlowRate = scalar, U16, 102, "gram/s", 0.005, 0
|
||||
veTableYAxis = scalar, U16, 104, "%", 0.01, 0
|
||||
afrTableYAxis = scalar, U16, 106, "%", 0.01, 0
|
||||
wallFuelAmount = scalar, U16, 70, "mg", 0.01, 0
|
||||
wallFuelCorrection = scalar, S16, 72, "mg", 0.01, 0
|
||||
revolutionCounterSinceStart = scalar, U16, 74, "", 1, 0
|
||||
deltaTps = scalar, S16, 76, "ratio", 0.01, 0
|
||||
canReadCounter = scalar, U16, 78, "", 1, 0
|
||||
tpsAccelFuel = scalar, S16, 80, "ms", 0.0033333333333333335, 0
|
||||
ignitionAdvance = scalar, S16, 82, "deg", 0.02, 0
|
||||
sparkDwellValue = scalar, U16, 84, "ms", 0.0033333333333333335, 0
|
||||
coilDutyCycle = scalar, U16, 86, "%", 0.01, 0
|
||||
idleAirValvePosition = scalar, U16, 88, "%", 0.01, 0
|
||||
etbTarget = scalar, S16, 90, "%", 0.01, 0
|
||||
etb1DutyCycle = scalar, S16, 92, "%", 0.01, 0
|
||||
etb1Error = scalar, S16, 94, "%", 0.01, 0
|
||||
fuelTankLevel = scalar, S16, 96, "%", 0.01, 0
|
||||
totalFuelConsumption = scalar, U16, 98, "grams", 1, 0
|
||||
fuelFlowRate = scalar, U16, 100, "gram/s", 0.005, 0
|
||||
veTableYAxis = scalar, U16, 102, "%", 0.01, 0
|
||||
afrTableYAxis = scalar, U16, 104, "%", 0.01, 0
|
||||
knockLevel = scalar, F32, 108, "Volts", 1, 0
|
||||
seconds = scalar, U32, 112, "sec", 1, 0
|
||||
engineMode = scalar, U32, 116, "em", 1, 0
|
||||
|
|
@ -4501,7 +4500,6 @@ entry = injectorLagMs, "fuel: injector lag", float, "%.3f"
|
|||
entry = iatCorrection, "fuel: IAT correction", float, "%.3f"
|
||||
entry = cltCorrection, "fuel: CLT correction", float, "%.3f"
|
||||
entry = baroCorrection, "fuel: Barometric pressure correction", float, "%.3f"
|
||||
entry = currentEnginePhase, "Engine Phase", int, "%d"
|
||||
entry = wallFuelAmount, "fuel: wall amount", float, "%.3f"
|
||||
entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f"
|
||||
entry = revolutionCounterSinceStart, "revolutionCounterSinceStart", int, "%d"
|
||||
|
|
@ -4847,7 +4845,7 @@ entry = mapVvt_MAP_AT_SPECIAL_POINT, "mapVvt_MAP_AT_SPECIAL_POINT", float, "%.3
|
|||
entry = mapVvt_MAP_AT_DIFF, "mapVvt_MAP_AT_DIFF", float, "%.3f"
|
||||
entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d"
|
||||
entry = mapVvt_map_peak, "mapVvt_map_peak", int, "%d"
|
||||
entry = currentEngineDecodedPhase, "Engine Phase2", int, "%d"
|
||||
entry = currentEngineDecodedPhase, "Engine Phase", int, "%d"
|
||||
entry = totalRevolutionCounter, "Crank revolution counter", int, "%d"
|
||||
entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f"
|
||||
entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f"
|
||||
|
|
|
|||
|
|
@ -86,7 +86,7 @@ enable2ndByteCanID = false
|
|||
; name = scalar, type, offset, units, scale, translate, lo, hi, digits
|
||||
|
||||
; CONFIG_DEFINITION_START
|
||||
; this section was generated automatically by rusEFI tool ConfigDefinition.jar based on gen_config.sh integration/rusefi_config.txt Thu Sep 01 03:55:52 UTC 2022
|
||||
; this section was generated automatically by rusEFI tool ConfigDefinition.jar based on gen_config.sh integration/rusefi_config.txt Thu Sep 01 04:18:10 UTC 2022
|
||||
|
||||
pageSize = 21300
|
||||
page = 1
|
||||
|
|
@ -2192,25 +2192,24 @@ injectorLagMs = scalar, U16, 62, "ms", 0.0033333333333333335, 0
|
|||
iatCorrection = scalar, U16, 64, "%", 0.01, 0
|
||||
cltCorrection = scalar, U16, 66, "%", 0.01, 0
|
||||
baroCorrection = scalar, U16, 68, "%", 0.01, 0
|
||||
currentEnginePhase = scalar, U16, 70, "deg", 1, 0
|
||||
wallFuelAmount = scalar, U16, 72, "mg", 0.01, 0
|
||||
wallFuelCorrection = scalar, S16, 74, "mg", 0.01, 0
|
||||
revolutionCounterSinceStart = scalar, U16, 76, "", 1, 0
|
||||
deltaTps = scalar, S16, 78, "ratio", 0.01, 0
|
||||
canReadCounter = scalar, U16, 80, "", 1, 0
|
||||
tpsAccelFuel = scalar, S16, 82, "ms", 0.0033333333333333335, 0
|
||||
ignitionAdvance = scalar, S16, 84, "deg", 0.02, 0
|
||||
sparkDwellValue = scalar, U16, 86, "ms", 0.0033333333333333335, 0
|
||||
coilDutyCycle = scalar, U16, 88, "%", 0.01, 0
|
||||
idleAirValvePosition = scalar, U16, 90, "%", 0.01, 0
|
||||
etbTarget = scalar, S16, 92, "%", 0.01, 0
|
||||
etb1DutyCycle = scalar, S16, 94, "%", 0.01, 0
|
||||
etb1Error = scalar, S16, 96, "%", 0.01, 0
|
||||
fuelTankLevel = scalar, S16, 98, "%", 0.01, 0
|
||||
totalFuelConsumption = scalar, U16, 100, "grams", 1, 0
|
||||
fuelFlowRate = scalar, U16, 102, "gram/s", 0.005, 0
|
||||
veTableYAxis = scalar, U16, 104, "%", 0.01, 0
|
||||
afrTableYAxis = scalar, U16, 106, "%", 0.01, 0
|
||||
wallFuelAmount = scalar, U16, 70, "mg", 0.01, 0
|
||||
wallFuelCorrection = scalar, S16, 72, "mg", 0.01, 0
|
||||
revolutionCounterSinceStart = scalar, U16, 74, "", 1, 0
|
||||
deltaTps = scalar, S16, 76, "ratio", 0.01, 0
|
||||
canReadCounter = scalar, U16, 78, "", 1, 0
|
||||
tpsAccelFuel = scalar, S16, 80, "ms", 0.0033333333333333335, 0
|
||||
ignitionAdvance = scalar, S16, 82, "deg", 0.02, 0
|
||||
sparkDwellValue = scalar, U16, 84, "ms", 0.0033333333333333335, 0
|
||||
coilDutyCycle = scalar, U16, 86, "%", 0.01, 0
|
||||
idleAirValvePosition = scalar, U16, 88, "%", 0.01, 0
|
||||
etbTarget = scalar, S16, 90, "%", 0.01, 0
|
||||
etb1DutyCycle = scalar, S16, 92, "%", 0.01, 0
|
||||
etb1Error = scalar, S16, 94, "%", 0.01, 0
|
||||
fuelTankLevel = scalar, S16, 96, "%", 0.01, 0
|
||||
totalFuelConsumption = scalar, U16, 98, "grams", 1, 0
|
||||
fuelFlowRate = scalar, U16, 100, "gram/s", 0.005, 0
|
||||
veTableYAxis = scalar, U16, 102, "%", 0.01, 0
|
||||
afrTableYAxis = scalar, U16, 104, "%", 0.01, 0
|
||||
knockLevel = scalar, F32, 108, "Volts", 1, 0
|
||||
seconds = scalar, U32, 112, "sec", 1, 0
|
||||
engineMode = scalar, U32, 116, "em", 1, 0
|
||||
|
|
@ -4501,7 +4500,6 @@ entry = injectorLagMs, "fuel: injector lag", float, "%.3f"
|
|||
entry = iatCorrection, "fuel: IAT correction", float, "%.3f"
|
||||
entry = cltCorrection, "fuel: CLT correction", float, "%.3f"
|
||||
entry = baroCorrection, "fuel: Barometric pressure correction", float, "%.3f"
|
||||
entry = currentEnginePhase, "Engine Phase", int, "%d"
|
||||
entry = wallFuelAmount, "fuel: wall amount", float, "%.3f"
|
||||
entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f"
|
||||
entry = revolutionCounterSinceStart, "revolutionCounterSinceStart", int, "%d"
|
||||
|
|
@ -4847,7 +4845,7 @@ entry = mapVvt_MAP_AT_SPECIAL_POINT, "mapVvt_MAP_AT_SPECIAL_POINT", float, "%.3
|
|||
entry = mapVvt_MAP_AT_DIFF, "mapVvt_MAP_AT_DIFF", float, "%.3f"
|
||||
entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d"
|
||||
entry = mapVvt_map_peak, "mapVvt_map_peak", int, "%d"
|
||||
entry = currentEngineDecodedPhase, "Engine Phase2", int, "%d"
|
||||
entry = currentEngineDecodedPhase, "Engine Phase", int, "%d"
|
||||
entry = totalRevolutionCounter, "Crank revolution counter", int, "%d"
|
||||
entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f"
|
||||
entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f"
|
||||
|
|
|
|||
|
|
@ -86,7 +86,7 @@ enable2ndByteCanID = false
|
|||
; name = scalar, type, offset, units, scale, translate, lo, hi, digits
|
||||
|
||||
; CONFIG_DEFINITION_START
|
||||
; this section was generated automatically by rusEFI tool ConfigDefinition.jar based on gen_config.sh integration/rusefi_config.txt Thu Sep 01 03:55:56 UTC 2022
|
||||
; this section was generated automatically by rusEFI tool ConfigDefinition.jar based on gen_config.sh integration/rusefi_config.txt Thu Sep 01 04:18:13 UTC 2022
|
||||
|
||||
pageSize = 21300
|
||||
page = 1
|
||||
|
|
@ -2192,25 +2192,24 @@ injectorLagMs = scalar, U16, 62, "ms", 0.0033333333333333335, 0
|
|||
iatCorrection = scalar, U16, 64, "%", 0.01, 0
|
||||
cltCorrection = scalar, U16, 66, "%", 0.01, 0
|
||||
baroCorrection = scalar, U16, 68, "%", 0.01, 0
|
||||
currentEnginePhase = scalar, U16, 70, "deg", 1, 0
|
||||
wallFuelAmount = scalar, U16, 72, "mg", 0.01, 0
|
||||
wallFuelCorrection = scalar, S16, 74, "mg", 0.01, 0
|
||||
revolutionCounterSinceStart = scalar, U16, 76, "", 1, 0
|
||||
deltaTps = scalar, S16, 78, "ratio", 0.01, 0
|
||||
canReadCounter = scalar, U16, 80, "", 1, 0
|
||||
tpsAccelFuel = scalar, S16, 82, "ms", 0.0033333333333333335, 0
|
||||
ignitionAdvance = scalar, S16, 84, "deg", 0.02, 0
|
||||
sparkDwellValue = scalar, U16, 86, "ms", 0.0033333333333333335, 0
|
||||
coilDutyCycle = scalar, U16, 88, "%", 0.01, 0
|
||||
idleAirValvePosition = scalar, U16, 90, "%", 0.01, 0
|
||||
etbTarget = scalar, S16, 92, "%", 0.01, 0
|
||||
etb1DutyCycle = scalar, S16, 94, "%", 0.01, 0
|
||||
etb1Error = scalar, S16, 96, "%", 0.01, 0
|
||||
fuelTankLevel = scalar, S16, 98, "%", 0.01, 0
|
||||
totalFuelConsumption = scalar, U16, 100, "grams", 1, 0
|
||||
fuelFlowRate = scalar, U16, 102, "gram/s", 0.005, 0
|
||||
veTableYAxis = scalar, U16, 104, "%", 0.01, 0
|
||||
afrTableYAxis = scalar, U16, 106, "%", 0.01, 0
|
||||
wallFuelAmount = scalar, U16, 70, "mg", 0.01, 0
|
||||
wallFuelCorrection = scalar, S16, 72, "mg", 0.01, 0
|
||||
revolutionCounterSinceStart = scalar, U16, 74, "", 1, 0
|
||||
deltaTps = scalar, S16, 76, "ratio", 0.01, 0
|
||||
canReadCounter = scalar, U16, 78, "", 1, 0
|
||||
tpsAccelFuel = scalar, S16, 80, "ms", 0.0033333333333333335, 0
|
||||
ignitionAdvance = scalar, S16, 82, "deg", 0.02, 0
|
||||
sparkDwellValue = scalar, U16, 84, "ms", 0.0033333333333333335, 0
|
||||
coilDutyCycle = scalar, U16, 86, "%", 0.01, 0
|
||||
idleAirValvePosition = scalar, U16, 88, "%", 0.01, 0
|
||||
etbTarget = scalar, S16, 90, "%", 0.01, 0
|
||||
etb1DutyCycle = scalar, S16, 92, "%", 0.01, 0
|
||||
etb1Error = scalar, S16, 94, "%", 0.01, 0
|
||||
fuelTankLevel = scalar, S16, 96, "%", 0.01, 0
|
||||
totalFuelConsumption = scalar, U16, 98, "grams", 1, 0
|
||||
fuelFlowRate = scalar, U16, 100, "gram/s", 0.005, 0
|
||||
veTableYAxis = scalar, U16, 102, "%", 0.01, 0
|
||||
afrTableYAxis = scalar, U16, 104, "%", 0.01, 0
|
||||
knockLevel = scalar, F32, 108, "Volts", 1, 0
|
||||
seconds = scalar, U32, 112, "sec", 1, 0
|
||||
engineMode = scalar, U32, 116, "em", 1, 0
|
||||
|
|
@ -4501,7 +4500,6 @@ entry = injectorLagMs, "fuel: injector lag", float, "%.3f"
|
|||
entry = iatCorrection, "fuel: IAT correction", float, "%.3f"
|
||||
entry = cltCorrection, "fuel: CLT correction", float, "%.3f"
|
||||
entry = baroCorrection, "fuel: Barometric pressure correction", float, "%.3f"
|
||||
entry = currentEnginePhase, "Engine Phase", int, "%d"
|
||||
entry = wallFuelAmount, "fuel: wall amount", float, "%.3f"
|
||||
entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f"
|
||||
entry = revolutionCounterSinceStart, "revolutionCounterSinceStart", int, "%d"
|
||||
|
|
@ -4847,7 +4845,7 @@ entry = mapVvt_MAP_AT_SPECIAL_POINT, "mapVvt_MAP_AT_SPECIAL_POINT", float, "%.3
|
|||
entry = mapVvt_MAP_AT_DIFF, "mapVvt_MAP_AT_DIFF", float, "%.3f"
|
||||
entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d"
|
||||
entry = mapVvt_map_peak, "mapVvt_map_peak", int, "%d"
|
||||
entry = currentEngineDecodedPhase, "Engine Phase2", int, "%d"
|
||||
entry = currentEngineDecodedPhase, "Engine Phase", int, "%d"
|
||||
entry = totalRevolutionCounter, "Crank revolution counter", int, "%d"
|
||||
entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f"
|
||||
entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f"
|
||||
|
|
|
|||
|
|
@ -86,7 +86,7 @@ enable2ndByteCanID = false
|
|||
; name = scalar, type, offset, units, scale, translate, lo, hi, digits
|
||||
|
||||
; CONFIG_DEFINITION_START
|
||||
; this section was generated automatically by rusEFI tool ConfigDefinition.jar based on gen_config.sh integration/rusefi_config.txt Thu Sep 01 03:55:58 UTC 2022
|
||||
; this section was generated automatically by rusEFI tool ConfigDefinition.jar based on gen_config.sh integration/rusefi_config.txt Thu Sep 01 04:18:15 UTC 2022
|
||||
|
||||
pageSize = 21300
|
||||
page = 1
|
||||
|
|
@ -2192,25 +2192,24 @@ injectorLagMs = scalar, U16, 62, "ms", 0.0033333333333333335, 0
|
|||
iatCorrection = scalar, U16, 64, "%", 0.01, 0
|
||||
cltCorrection = scalar, U16, 66, "%", 0.01, 0
|
||||
baroCorrection = scalar, U16, 68, "%", 0.01, 0
|
||||
currentEnginePhase = scalar, U16, 70, "deg", 1, 0
|
||||
wallFuelAmount = scalar, U16, 72, "mg", 0.01, 0
|
||||
wallFuelCorrection = scalar, S16, 74, "mg", 0.01, 0
|
||||
revolutionCounterSinceStart = scalar, U16, 76, "", 1, 0
|
||||
deltaTps = scalar, S16, 78, "ratio", 0.01, 0
|
||||
canReadCounter = scalar, U16, 80, "", 1, 0
|
||||
tpsAccelFuel = scalar, S16, 82, "ms", 0.0033333333333333335, 0
|
||||
ignitionAdvance = scalar, S16, 84, "deg", 0.02, 0
|
||||
sparkDwellValue = scalar, U16, 86, "ms", 0.0033333333333333335, 0
|
||||
coilDutyCycle = scalar, U16, 88, "%", 0.01, 0
|
||||
idleAirValvePosition = scalar, U16, 90, "%", 0.01, 0
|
||||
etbTarget = scalar, S16, 92, "%", 0.01, 0
|
||||
etb1DutyCycle = scalar, S16, 94, "%", 0.01, 0
|
||||
etb1Error = scalar, S16, 96, "%", 0.01, 0
|
||||
fuelTankLevel = scalar, S16, 98, "%", 0.01, 0
|
||||
totalFuelConsumption = scalar, U16, 100, "grams", 1, 0
|
||||
fuelFlowRate = scalar, U16, 102, "gram/s", 0.005, 0
|
||||
veTableYAxis = scalar, U16, 104, "%", 0.01, 0
|
||||
afrTableYAxis = scalar, U16, 106, "%", 0.01, 0
|
||||
wallFuelAmount = scalar, U16, 70, "mg", 0.01, 0
|
||||
wallFuelCorrection = scalar, S16, 72, "mg", 0.01, 0
|
||||
revolutionCounterSinceStart = scalar, U16, 74, "", 1, 0
|
||||
deltaTps = scalar, S16, 76, "ratio", 0.01, 0
|
||||
canReadCounter = scalar, U16, 78, "", 1, 0
|
||||
tpsAccelFuel = scalar, S16, 80, "ms", 0.0033333333333333335, 0
|
||||
ignitionAdvance = scalar, S16, 82, "deg", 0.02, 0
|
||||
sparkDwellValue = scalar, U16, 84, "ms", 0.0033333333333333335, 0
|
||||
coilDutyCycle = scalar, U16, 86, "%", 0.01, 0
|
||||
idleAirValvePosition = scalar, U16, 88, "%", 0.01, 0
|
||||
etbTarget = scalar, S16, 90, "%", 0.01, 0
|
||||
etb1DutyCycle = scalar, S16, 92, "%", 0.01, 0
|
||||
etb1Error = scalar, S16, 94, "%", 0.01, 0
|
||||
fuelTankLevel = scalar, S16, 96, "%", 0.01, 0
|
||||
totalFuelConsumption = scalar, U16, 98, "grams", 1, 0
|
||||
fuelFlowRate = scalar, U16, 100, "gram/s", 0.005, 0
|
||||
veTableYAxis = scalar, U16, 102, "%", 0.01, 0
|
||||
afrTableYAxis = scalar, U16, 104, "%", 0.01, 0
|
||||
knockLevel = scalar, F32, 108, "Volts", 1, 0
|
||||
seconds = scalar, U32, 112, "sec", 1, 0
|
||||
engineMode = scalar, U32, 116, "em", 1, 0
|
||||
|
|
@ -4501,7 +4500,6 @@ entry = injectorLagMs, "fuel: injector lag", float, "%.3f"
|
|||
entry = iatCorrection, "fuel: IAT correction", float, "%.3f"
|
||||
entry = cltCorrection, "fuel: CLT correction", float, "%.3f"
|
||||
entry = baroCorrection, "fuel: Barometric pressure correction", float, "%.3f"
|
||||
entry = currentEnginePhase, "Engine Phase", int, "%d"
|
||||
entry = wallFuelAmount, "fuel: wall amount", float, "%.3f"
|
||||
entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f"
|
||||
entry = revolutionCounterSinceStart, "revolutionCounterSinceStart", int, "%d"
|
||||
|
|
@ -4847,7 +4845,7 @@ entry = mapVvt_MAP_AT_SPECIAL_POINT, "mapVvt_MAP_AT_SPECIAL_POINT", float, "%.3
|
|||
entry = mapVvt_MAP_AT_DIFF, "mapVvt_MAP_AT_DIFF", float, "%.3f"
|
||||
entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d"
|
||||
entry = mapVvt_map_peak, "mapVvt_map_peak", int, "%d"
|
||||
entry = currentEngineDecodedPhase, "Engine Phase2", int, "%d"
|
||||
entry = currentEngineDecodedPhase, "Engine Phase", int, "%d"
|
||||
entry = totalRevolutionCounter, "Crank revolution counter", int, "%d"
|
||||
entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f"
|
||||
entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f"
|
||||
|
|
|
|||
|
|
@ -86,7 +86,7 @@ enable2ndByteCanID = false
|
|||
; name = scalar, type, offset, units, scale, translate, lo, hi, digits
|
||||
|
||||
; CONFIG_DEFINITION_START
|
||||
; this section was generated automatically by rusEFI tool ConfigDefinition.jar based on gen_config.sh integration/rusefi_config.txt Thu Sep 01 03:55:54 UTC 2022
|
||||
; this section was generated automatically by rusEFI tool ConfigDefinition.jar based on gen_config.sh integration/rusefi_config.txt Thu Sep 01 04:18:12 UTC 2022
|
||||
|
||||
pageSize = 21300
|
||||
page = 1
|
||||
|
|
@ -2192,25 +2192,24 @@ injectorLagMs = scalar, U16, 62, "ms", 0.0033333333333333335, 0
|
|||
iatCorrection = scalar, U16, 64, "%", 0.01, 0
|
||||
cltCorrection = scalar, U16, 66, "%", 0.01, 0
|
||||
baroCorrection = scalar, U16, 68, "%", 0.01, 0
|
||||
currentEnginePhase = scalar, U16, 70, "deg", 1, 0
|
||||
wallFuelAmount = scalar, U16, 72, "mg", 0.01, 0
|
||||
wallFuelCorrection = scalar, S16, 74, "mg", 0.01, 0
|
||||
revolutionCounterSinceStart = scalar, U16, 76, "", 1, 0
|
||||
deltaTps = scalar, S16, 78, "ratio", 0.01, 0
|
||||
canReadCounter = scalar, U16, 80, "", 1, 0
|
||||
tpsAccelFuel = scalar, S16, 82, "ms", 0.0033333333333333335, 0
|
||||
ignitionAdvance = scalar, S16, 84, "deg", 0.02, 0
|
||||
sparkDwellValue = scalar, U16, 86, "ms", 0.0033333333333333335, 0
|
||||
coilDutyCycle = scalar, U16, 88, "%", 0.01, 0
|
||||
idleAirValvePosition = scalar, U16, 90, "%", 0.01, 0
|
||||
etbTarget = scalar, S16, 92, "%", 0.01, 0
|
||||
etb1DutyCycle = scalar, S16, 94, "%", 0.01, 0
|
||||
etb1Error = scalar, S16, 96, "%", 0.01, 0
|
||||
fuelTankLevel = scalar, S16, 98, "%", 0.01, 0
|
||||
totalFuelConsumption = scalar, U16, 100, "grams", 1, 0
|
||||
fuelFlowRate = scalar, U16, 102, "gram/s", 0.005, 0
|
||||
veTableYAxis = scalar, U16, 104, "%", 0.01, 0
|
||||
afrTableYAxis = scalar, U16, 106, "%", 0.01, 0
|
||||
wallFuelAmount = scalar, U16, 70, "mg", 0.01, 0
|
||||
wallFuelCorrection = scalar, S16, 72, "mg", 0.01, 0
|
||||
revolutionCounterSinceStart = scalar, U16, 74, "", 1, 0
|
||||
deltaTps = scalar, S16, 76, "ratio", 0.01, 0
|
||||
canReadCounter = scalar, U16, 78, "", 1, 0
|
||||
tpsAccelFuel = scalar, S16, 80, "ms", 0.0033333333333333335, 0
|
||||
ignitionAdvance = scalar, S16, 82, "deg", 0.02, 0
|
||||
sparkDwellValue = scalar, U16, 84, "ms", 0.0033333333333333335, 0
|
||||
coilDutyCycle = scalar, U16, 86, "%", 0.01, 0
|
||||
idleAirValvePosition = scalar, U16, 88, "%", 0.01, 0
|
||||
etbTarget = scalar, S16, 90, "%", 0.01, 0
|
||||
etb1DutyCycle = scalar, S16, 92, "%", 0.01, 0
|
||||
etb1Error = scalar, S16, 94, "%", 0.01, 0
|
||||
fuelTankLevel = scalar, S16, 96, "%", 0.01, 0
|
||||
totalFuelConsumption = scalar, U16, 98, "grams", 1, 0
|
||||
fuelFlowRate = scalar, U16, 100, "gram/s", 0.005, 0
|
||||
veTableYAxis = scalar, U16, 102, "%", 0.01, 0
|
||||
afrTableYAxis = scalar, U16, 104, "%", 0.01, 0
|
||||
knockLevel = scalar, F32, 108, "Volts", 1, 0
|
||||
seconds = scalar, U32, 112, "sec", 1, 0
|
||||
engineMode = scalar, U32, 116, "em", 1, 0
|
||||
|
|
@ -4501,7 +4500,6 @@ entry = injectorLagMs, "fuel: injector lag", float, "%.3f"
|
|||
entry = iatCorrection, "fuel: IAT correction", float, "%.3f"
|
||||
entry = cltCorrection, "fuel: CLT correction", float, "%.3f"
|
||||
entry = baroCorrection, "fuel: Barometric pressure correction", float, "%.3f"
|
||||
entry = currentEnginePhase, "Engine Phase", int, "%d"
|
||||
entry = wallFuelAmount, "fuel: wall amount", float, "%.3f"
|
||||
entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f"
|
||||
entry = revolutionCounterSinceStart, "revolutionCounterSinceStart", int, "%d"
|
||||
|
|
@ -4847,7 +4845,7 @@ entry = mapVvt_MAP_AT_SPECIAL_POINT, "mapVvt_MAP_AT_SPECIAL_POINT", float, "%.3
|
|||
entry = mapVvt_MAP_AT_DIFF, "mapVvt_MAP_AT_DIFF", float, "%.3f"
|
||||
entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d"
|
||||
entry = mapVvt_map_peak, "mapVvt_map_peak", int, "%d"
|
||||
entry = currentEngineDecodedPhase, "Engine Phase2", int, "%d"
|
||||
entry = currentEngineDecodedPhase, "Engine Phase", int, "%d"
|
||||
entry = totalRevolutionCounter, "Crank revolution counter", int, "%d"
|
||||
entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f"
|
||||
entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f"
|
||||
|
|
|
|||
|
|
@ -86,7 +86,7 @@ enable2ndByteCanID = false
|
|||
; name = scalar, type, offset, units, scale, translate, lo, hi, digits
|
||||
|
||||
; CONFIG_DEFINITION_START
|
||||
; this section was generated automatically by rusEFI tool ConfigDefinition.jar based on gen_config.sh integration/rusefi_config.txt Thu Sep 01 03:56:04 UTC 2022
|
||||
; this section was generated automatically by rusEFI tool ConfigDefinition.jar based on gen_config.sh integration/rusefi_config.txt Thu Sep 01 04:18:20 UTC 2022
|
||||
|
||||
pageSize = 21300
|
||||
page = 1
|
||||
|
|
@ -2192,25 +2192,24 @@ injectorLagMs = scalar, U16, 62, "ms", 0.0033333333333333335, 0
|
|||
iatCorrection = scalar, U16, 64, "%", 0.01, 0
|
||||
cltCorrection = scalar, U16, 66, "%", 0.01, 0
|
||||
baroCorrection = scalar, U16, 68, "%", 0.01, 0
|
||||
currentEnginePhase = scalar, U16, 70, "deg", 1, 0
|
||||
wallFuelAmount = scalar, U16, 72, "mg", 0.01, 0
|
||||
wallFuelCorrection = scalar, S16, 74, "mg", 0.01, 0
|
||||
revolutionCounterSinceStart = scalar, U16, 76, "", 1, 0
|
||||
deltaTps = scalar, S16, 78, "ratio", 0.01, 0
|
||||
canReadCounter = scalar, U16, 80, "", 1, 0
|
||||
tpsAccelFuel = scalar, S16, 82, "ms", 0.0033333333333333335, 0
|
||||
ignitionAdvance = scalar, S16, 84, "deg", 0.02, 0
|
||||
sparkDwellValue = scalar, U16, 86, "ms", 0.0033333333333333335, 0
|
||||
coilDutyCycle = scalar, U16, 88, "%", 0.01, 0
|
||||
idleAirValvePosition = scalar, U16, 90, "%", 0.01, 0
|
||||
etbTarget = scalar, S16, 92, "%", 0.01, 0
|
||||
etb1DutyCycle = scalar, S16, 94, "%", 0.01, 0
|
||||
etb1Error = scalar, S16, 96, "%", 0.01, 0
|
||||
fuelTankLevel = scalar, S16, 98, "%", 0.01, 0
|
||||
totalFuelConsumption = scalar, U16, 100, "grams", 1, 0
|
||||
fuelFlowRate = scalar, U16, 102, "gram/s", 0.005, 0
|
||||
veTableYAxis = scalar, U16, 104, "%", 0.01, 0
|
||||
afrTableYAxis = scalar, U16, 106, "%", 0.01, 0
|
||||
wallFuelAmount = scalar, U16, 70, "mg", 0.01, 0
|
||||
wallFuelCorrection = scalar, S16, 72, "mg", 0.01, 0
|
||||
revolutionCounterSinceStart = scalar, U16, 74, "", 1, 0
|
||||
deltaTps = scalar, S16, 76, "ratio", 0.01, 0
|
||||
canReadCounter = scalar, U16, 78, "", 1, 0
|
||||
tpsAccelFuel = scalar, S16, 80, "ms", 0.0033333333333333335, 0
|
||||
ignitionAdvance = scalar, S16, 82, "deg", 0.02, 0
|
||||
sparkDwellValue = scalar, U16, 84, "ms", 0.0033333333333333335, 0
|
||||
coilDutyCycle = scalar, U16, 86, "%", 0.01, 0
|
||||
idleAirValvePosition = scalar, U16, 88, "%", 0.01, 0
|
||||
etbTarget = scalar, S16, 90, "%", 0.01, 0
|
||||
etb1DutyCycle = scalar, S16, 92, "%", 0.01, 0
|
||||
etb1Error = scalar, S16, 94, "%", 0.01, 0
|
||||
fuelTankLevel = scalar, S16, 96, "%", 0.01, 0
|
||||
totalFuelConsumption = scalar, U16, 98, "grams", 1, 0
|
||||
fuelFlowRate = scalar, U16, 100, "gram/s", 0.005, 0
|
||||
veTableYAxis = scalar, U16, 102, "%", 0.01, 0
|
||||
afrTableYAxis = scalar, U16, 104, "%", 0.01, 0
|
||||
knockLevel = scalar, F32, 108, "Volts", 1, 0
|
||||
seconds = scalar, U32, 112, "sec", 1, 0
|
||||
engineMode = scalar, U32, 116, "em", 1, 0
|
||||
|
|
@ -4501,7 +4500,6 @@ entry = injectorLagMs, "fuel: injector lag", float, "%.3f"
|
|||
entry = iatCorrection, "fuel: IAT correction", float, "%.3f"
|
||||
entry = cltCorrection, "fuel: CLT correction", float, "%.3f"
|
||||
entry = baroCorrection, "fuel: Barometric pressure correction", float, "%.3f"
|
||||
entry = currentEnginePhase, "Engine Phase", int, "%d"
|
||||
entry = wallFuelAmount, "fuel: wall amount", float, "%.3f"
|
||||
entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f"
|
||||
entry = revolutionCounterSinceStart, "revolutionCounterSinceStart", int, "%d"
|
||||
|
|
@ -4847,7 +4845,7 @@ entry = mapVvt_MAP_AT_SPECIAL_POINT, "mapVvt_MAP_AT_SPECIAL_POINT", float, "%.3
|
|||
entry = mapVvt_MAP_AT_DIFF, "mapVvt_MAP_AT_DIFF", float, "%.3f"
|
||||
entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d"
|
||||
entry = mapVvt_map_peak, "mapVvt_map_peak", int, "%d"
|
||||
entry = currentEngineDecodedPhase, "Engine Phase2", int, "%d"
|
||||
entry = currentEngineDecodedPhase, "Engine Phase", int, "%d"
|
||||
entry = totalRevolutionCounter, "Crank revolution counter", int, "%d"
|
||||
entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f"
|
||||
entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f"
|
||||
|
|
|
|||
|
|
@ -86,7 +86,7 @@ enable2ndByteCanID = false
|
|||
; name = scalar, type, offset, units, scale, translate, lo, hi, digits
|
||||
|
||||
; CONFIG_DEFINITION_START
|
||||
; this section was generated automatically by rusEFI tool ConfigDefinition.jar based on gen_config.sh integration/rusefi_config.txt Thu Sep 01 03:56:06 UTC 2022
|
||||
; this section was generated automatically by rusEFI tool ConfigDefinition.jar based on gen_config.sh integration/rusefi_config.txt Thu Sep 01 04:18:22 UTC 2022
|
||||
|
||||
pageSize = 21300
|
||||
page = 1
|
||||
|
|
@ -2192,25 +2192,24 @@ injectorLagMs = scalar, U16, 62, "ms", 0.0033333333333333335, 0
|
|||
iatCorrection = scalar, U16, 64, "%", 0.01, 0
|
||||
cltCorrection = scalar, U16, 66, "%", 0.01, 0
|
||||
baroCorrection = scalar, U16, 68, "%", 0.01, 0
|
||||
currentEnginePhase = scalar, U16, 70, "deg", 1, 0
|
||||
wallFuelAmount = scalar, U16, 72, "mg", 0.01, 0
|
||||
wallFuelCorrection = scalar, S16, 74, "mg", 0.01, 0
|
||||
revolutionCounterSinceStart = scalar, U16, 76, "", 1, 0
|
||||
deltaTps = scalar, S16, 78, "ratio", 0.01, 0
|
||||
canReadCounter = scalar, U16, 80, "", 1, 0
|
||||
tpsAccelFuel = scalar, S16, 82, "ms", 0.0033333333333333335, 0
|
||||
ignitionAdvance = scalar, S16, 84, "deg", 0.02, 0
|
||||
sparkDwellValue = scalar, U16, 86, "ms", 0.0033333333333333335, 0
|
||||
coilDutyCycle = scalar, U16, 88, "%", 0.01, 0
|
||||
idleAirValvePosition = scalar, U16, 90, "%", 0.01, 0
|
||||
etbTarget = scalar, S16, 92, "%", 0.01, 0
|
||||
etb1DutyCycle = scalar, S16, 94, "%", 0.01, 0
|
||||
etb1Error = scalar, S16, 96, "%", 0.01, 0
|
||||
fuelTankLevel = scalar, S16, 98, "%", 0.01, 0
|
||||
totalFuelConsumption = scalar, U16, 100, "grams", 1, 0
|
||||
fuelFlowRate = scalar, U16, 102, "gram/s", 0.005, 0
|
||||
veTableYAxis = scalar, U16, 104, "%", 0.01, 0
|
||||
afrTableYAxis = scalar, U16, 106, "%", 0.01, 0
|
||||
wallFuelAmount = scalar, U16, 70, "mg", 0.01, 0
|
||||
wallFuelCorrection = scalar, S16, 72, "mg", 0.01, 0
|
||||
revolutionCounterSinceStart = scalar, U16, 74, "", 1, 0
|
||||
deltaTps = scalar, S16, 76, "ratio", 0.01, 0
|
||||
canReadCounter = scalar, U16, 78, "", 1, 0
|
||||
tpsAccelFuel = scalar, S16, 80, "ms", 0.0033333333333333335, 0
|
||||
ignitionAdvance = scalar, S16, 82, "deg", 0.02, 0
|
||||
sparkDwellValue = scalar, U16, 84, "ms", 0.0033333333333333335, 0
|
||||
coilDutyCycle = scalar, U16, 86, "%", 0.01, 0
|
||||
idleAirValvePosition = scalar, U16, 88, "%", 0.01, 0
|
||||
etbTarget = scalar, S16, 90, "%", 0.01, 0
|
||||
etb1DutyCycle = scalar, S16, 92, "%", 0.01, 0
|
||||
etb1Error = scalar, S16, 94, "%", 0.01, 0
|
||||
fuelTankLevel = scalar, S16, 96, "%", 0.01, 0
|
||||
totalFuelConsumption = scalar, U16, 98, "grams", 1, 0
|
||||
fuelFlowRate = scalar, U16, 100, "gram/s", 0.005, 0
|
||||
veTableYAxis = scalar, U16, 102, "%", 0.01, 0
|
||||
afrTableYAxis = scalar, U16, 104, "%", 0.01, 0
|
||||
knockLevel = scalar, F32, 108, "Volts", 1, 0
|
||||
seconds = scalar, U32, 112, "sec", 1, 0
|
||||
engineMode = scalar, U32, 116, "em", 1, 0
|
||||
|
|
@ -4501,7 +4500,6 @@ entry = injectorLagMs, "fuel: injector lag", float, "%.3f"
|
|||
entry = iatCorrection, "fuel: IAT correction", float, "%.3f"
|
||||
entry = cltCorrection, "fuel: CLT correction", float, "%.3f"
|
||||
entry = baroCorrection, "fuel: Barometric pressure correction", float, "%.3f"
|
||||
entry = currentEnginePhase, "Engine Phase", int, "%d"
|
||||
entry = wallFuelAmount, "fuel: wall amount", float, "%.3f"
|
||||
entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f"
|
||||
entry = revolutionCounterSinceStart, "revolutionCounterSinceStart", int, "%d"
|
||||
|
|
@ -4847,7 +4845,7 @@ entry = mapVvt_MAP_AT_SPECIAL_POINT, "mapVvt_MAP_AT_SPECIAL_POINT", float, "%.3
|
|||
entry = mapVvt_MAP_AT_DIFF, "mapVvt_MAP_AT_DIFF", float, "%.3f"
|
||||
entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d"
|
||||
entry = mapVvt_map_peak, "mapVvt_map_peak", int, "%d"
|
||||
entry = currentEngineDecodedPhase, "Engine Phase2", int, "%d"
|
||||
entry = currentEngineDecodedPhase, "Engine Phase", int, "%d"
|
||||
entry = totalRevolutionCounter, "Crank revolution counter", int, "%d"
|
||||
entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f"
|
||||
entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f"
|
||||
|
|
|
|||
|
|
@ -86,7 +86,7 @@ enable2ndByteCanID = false
|
|||
; name = scalar, type, offset, units, scale, translate, lo, hi, digits
|
||||
|
||||
; CONFIG_DEFINITION_START
|
||||
; this section was generated automatically by rusEFI tool ConfigDefinition.jar based on kinetis_gen_config.bat integration/rusefi_config.txt Thu Sep 01 03:55:35 UTC 2022
|
||||
; this section was generated automatically by rusEFI tool ConfigDefinition.jar based on kinetis_gen_config.bat integration/rusefi_config.txt Thu Sep 01 04:17:55 UTC 2022
|
||||
|
||||
pageSize = 21300
|
||||
page = 1
|
||||
|
|
@ -2192,25 +2192,24 @@ injectorLagMs = scalar, U16, 62, "ms", 0.0033333333333333335, 0
|
|||
iatCorrection = scalar, U16, 64, "%", 0.01, 0
|
||||
cltCorrection = scalar, U16, 66, "%", 0.01, 0
|
||||
baroCorrection = scalar, U16, 68, "%", 0.01, 0
|
||||
currentEnginePhase = scalar, U16, 70, "deg", 1, 0
|
||||
wallFuelAmount = scalar, U16, 72, "mg", 0.01, 0
|
||||
wallFuelCorrection = scalar, S16, 74, "mg", 0.01, 0
|
||||
revolutionCounterSinceStart = scalar, U16, 76, "", 1, 0
|
||||
deltaTps = scalar, S16, 78, "ratio", 0.01, 0
|
||||
canReadCounter = scalar, U16, 80, "", 1, 0
|
||||
tpsAccelFuel = scalar, S16, 82, "ms", 0.0033333333333333335, 0
|
||||
ignitionAdvance = scalar, S16, 84, "deg", 0.02, 0
|
||||
sparkDwellValue = scalar, U16, 86, "ms", 0.0033333333333333335, 0
|
||||
coilDutyCycle = scalar, U16, 88, "%", 0.01, 0
|
||||
idleAirValvePosition = scalar, U16, 90, "%", 0.01, 0
|
||||
etbTarget = scalar, S16, 92, "%", 0.01, 0
|
||||
etb1DutyCycle = scalar, S16, 94, "%", 0.01, 0
|
||||
etb1Error = scalar, S16, 96, "%", 0.01, 0
|
||||
fuelTankLevel = scalar, S16, 98, "%", 0.01, 0
|
||||
totalFuelConsumption = scalar, U16, 100, "grams", 1, 0
|
||||
fuelFlowRate = scalar, U16, 102, "gram/s", 0.005, 0
|
||||
veTableYAxis = scalar, U16, 104, "%", 0.01, 0
|
||||
afrTableYAxis = scalar, U16, 106, "%", 0.01, 0
|
||||
wallFuelAmount = scalar, U16, 70, "mg", 0.01, 0
|
||||
wallFuelCorrection = scalar, S16, 72, "mg", 0.01, 0
|
||||
revolutionCounterSinceStart = scalar, U16, 74, "", 1, 0
|
||||
deltaTps = scalar, S16, 76, "ratio", 0.01, 0
|
||||
canReadCounter = scalar, U16, 78, "", 1, 0
|
||||
tpsAccelFuel = scalar, S16, 80, "ms", 0.0033333333333333335, 0
|
||||
ignitionAdvance = scalar, S16, 82, "deg", 0.02, 0
|
||||
sparkDwellValue = scalar, U16, 84, "ms", 0.0033333333333333335, 0
|
||||
coilDutyCycle = scalar, U16, 86, "%", 0.01, 0
|
||||
idleAirValvePosition = scalar, U16, 88, "%", 0.01, 0
|
||||
etbTarget = scalar, S16, 90, "%", 0.01, 0
|
||||
etb1DutyCycle = scalar, S16, 92, "%", 0.01, 0
|
||||
etb1Error = scalar, S16, 94, "%", 0.01, 0
|
||||
fuelTankLevel = scalar, S16, 96, "%", 0.01, 0
|
||||
totalFuelConsumption = scalar, U16, 98, "grams", 1, 0
|
||||
fuelFlowRate = scalar, U16, 100, "gram/s", 0.005, 0
|
||||
veTableYAxis = scalar, U16, 102, "%", 0.01, 0
|
||||
afrTableYAxis = scalar, U16, 104, "%", 0.01, 0
|
||||
knockLevel = scalar, F32, 108, "Volts", 1, 0
|
||||
seconds = scalar, U32, 112, "sec", 1, 0
|
||||
engineMode = scalar, U32, 116, "em", 1, 0
|
||||
|
|
@ -4501,7 +4500,6 @@ entry = injectorLagMs, "fuel: injector lag", float, "%.3f"
|
|||
entry = iatCorrection, "fuel: IAT correction", float, "%.3f"
|
||||
entry = cltCorrection, "fuel: CLT correction", float, "%.3f"
|
||||
entry = baroCorrection, "fuel: Barometric pressure correction", float, "%.3f"
|
||||
entry = currentEnginePhase, "Engine Phase", int, "%d"
|
||||
entry = wallFuelAmount, "fuel: wall amount", float, "%.3f"
|
||||
entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f"
|
||||
entry = revolutionCounterSinceStart, "revolutionCounterSinceStart", int, "%d"
|
||||
|
|
@ -4847,7 +4845,7 @@ entry = mapVvt_MAP_AT_SPECIAL_POINT, "mapVvt_MAP_AT_SPECIAL_POINT", float, "%.3
|
|||
entry = mapVvt_MAP_AT_DIFF, "mapVvt_MAP_AT_DIFF", float, "%.3f"
|
||||
entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d"
|
||||
entry = mapVvt_map_peak, "mapVvt_map_peak", int, "%d"
|
||||
entry = currentEngineDecodedPhase, "Engine Phase2", int, "%d"
|
||||
entry = currentEngineDecodedPhase, "Engine Phase", int, "%d"
|
||||
entry = totalRevolutionCounter, "Crank revolution counter", int, "%d"
|
||||
entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f"
|
||||
entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f"
|
||||
|
|
|
|||
|
|
@ -86,7 +86,7 @@ enable2ndByteCanID = false
|
|||
; name = scalar, type, offset, units, scale, translate, lo, hi, digits
|
||||
|
||||
; CONFIG_DEFINITION_START
|
||||
; this section was generated automatically by rusEFI tool ConfigDefinition.jar based on gen_config.sh integration/rusefi_config.txt Thu Sep 01 03:56:10 UTC 2022
|
||||
; this section was generated automatically by rusEFI tool ConfigDefinition.jar based on gen_config.sh integration/rusefi_config.txt Thu Sep 01 04:18:25 UTC 2022
|
||||
|
||||
pageSize = 21300
|
||||
page = 1
|
||||
|
|
@ -2192,25 +2192,24 @@ injectorLagMs = scalar, U16, 62, "ms", 0.0033333333333333335, 0
|
|||
iatCorrection = scalar, U16, 64, "%", 0.01, 0
|
||||
cltCorrection = scalar, U16, 66, "%", 0.01, 0
|
||||
baroCorrection = scalar, U16, 68, "%", 0.01, 0
|
||||
currentEnginePhase = scalar, U16, 70, "deg", 1, 0
|
||||
wallFuelAmount = scalar, U16, 72, "mg", 0.01, 0
|
||||
wallFuelCorrection = scalar, S16, 74, "mg", 0.01, 0
|
||||
revolutionCounterSinceStart = scalar, U16, 76, "", 1, 0
|
||||
deltaTps = scalar, S16, 78, "ratio", 0.01, 0
|
||||
canReadCounter = scalar, U16, 80, "", 1, 0
|
||||
tpsAccelFuel = scalar, S16, 82, "ms", 0.0033333333333333335, 0
|
||||
ignitionAdvance = scalar, S16, 84, "deg", 0.02, 0
|
||||
sparkDwellValue = scalar, U16, 86, "ms", 0.0033333333333333335, 0
|
||||
coilDutyCycle = scalar, U16, 88, "%", 0.01, 0
|
||||
idleAirValvePosition = scalar, U16, 90, "%", 0.01, 0
|
||||
etbTarget = scalar, S16, 92, "%", 0.01, 0
|
||||
etb1DutyCycle = scalar, S16, 94, "%", 0.01, 0
|
||||
etb1Error = scalar, S16, 96, "%", 0.01, 0
|
||||
fuelTankLevel = scalar, S16, 98, "%", 0.01, 0
|
||||
totalFuelConsumption = scalar, U16, 100, "grams", 1, 0
|
||||
fuelFlowRate = scalar, U16, 102, "gram/s", 0.005, 0
|
||||
veTableYAxis = scalar, U16, 104, "%", 0.01, 0
|
||||
afrTableYAxis = scalar, U16, 106, "%", 0.01, 0
|
||||
wallFuelAmount = scalar, U16, 70, "mg", 0.01, 0
|
||||
wallFuelCorrection = scalar, S16, 72, "mg", 0.01, 0
|
||||
revolutionCounterSinceStart = scalar, U16, 74, "", 1, 0
|
||||
deltaTps = scalar, S16, 76, "ratio", 0.01, 0
|
||||
canReadCounter = scalar, U16, 78, "", 1, 0
|
||||
tpsAccelFuel = scalar, S16, 80, "ms", 0.0033333333333333335, 0
|
||||
ignitionAdvance = scalar, S16, 82, "deg", 0.02, 0
|
||||
sparkDwellValue = scalar, U16, 84, "ms", 0.0033333333333333335, 0
|
||||
coilDutyCycle = scalar, U16, 86, "%", 0.01, 0
|
||||
idleAirValvePosition = scalar, U16, 88, "%", 0.01, 0
|
||||
etbTarget = scalar, S16, 90, "%", 0.01, 0
|
||||
etb1DutyCycle = scalar, S16, 92, "%", 0.01, 0
|
||||
etb1Error = scalar, S16, 94, "%", 0.01, 0
|
||||
fuelTankLevel = scalar, S16, 96, "%", 0.01, 0
|
||||
totalFuelConsumption = scalar, U16, 98, "grams", 1, 0
|
||||
fuelFlowRate = scalar, U16, 100, "gram/s", 0.005, 0
|
||||
veTableYAxis = scalar, U16, 102, "%", 0.01, 0
|
||||
afrTableYAxis = scalar, U16, 104, "%", 0.01, 0
|
||||
knockLevel = scalar, F32, 108, "Volts", 1, 0
|
||||
seconds = scalar, U32, 112, "sec", 1, 0
|
||||
engineMode = scalar, U32, 116, "em", 1, 0
|
||||
|
|
@ -4501,7 +4500,6 @@ entry = injectorLagMs, "fuel: injector lag", float, "%.3f"
|
|||
entry = iatCorrection, "fuel: IAT correction", float, "%.3f"
|
||||
entry = cltCorrection, "fuel: CLT correction", float, "%.3f"
|
||||
entry = baroCorrection, "fuel: Barometric pressure correction", float, "%.3f"
|
||||
entry = currentEnginePhase, "Engine Phase", int, "%d"
|
||||
entry = wallFuelAmount, "fuel: wall amount", float, "%.3f"
|
||||
entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f"
|
||||
entry = revolutionCounterSinceStart, "revolutionCounterSinceStart", int, "%d"
|
||||
|
|
@ -4847,7 +4845,7 @@ entry = mapVvt_MAP_AT_SPECIAL_POINT, "mapVvt_MAP_AT_SPECIAL_POINT", float, "%.3
|
|||
entry = mapVvt_MAP_AT_DIFF, "mapVvt_MAP_AT_DIFF", float, "%.3f"
|
||||
entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d"
|
||||
entry = mapVvt_map_peak, "mapVvt_map_peak", int, "%d"
|
||||
entry = currentEngineDecodedPhase, "Engine Phase2", int, "%d"
|
||||
entry = currentEngineDecodedPhase, "Engine Phase", int, "%d"
|
||||
entry = totalRevolutionCounter, "Crank revolution counter", int, "%d"
|
||||
entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f"
|
||||
entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f"
|
||||
|
|
|
|||
|
|
@ -86,7 +86,7 @@ enable2ndByteCanID = false
|
|||
; name = scalar, type, offset, units, scale, translate, lo, hi, digits
|
||||
|
||||
; CONFIG_DEFINITION_START
|
||||
; this section was generated automatically by rusEFI tool ConfigDefinition.jar based on gen_config.sh integration/rusefi_config.txt Thu Sep 01 03:56:08 UTC 2022
|
||||
; this section was generated automatically by rusEFI tool ConfigDefinition.jar based on gen_config.sh integration/rusefi_config.txt Thu Sep 01 04:18:24 UTC 2022
|
||||
|
||||
pageSize = 21300
|
||||
page = 1
|
||||
|
|
@ -2192,25 +2192,24 @@ injectorLagMs = scalar, U16, 62, "ms", 0.0033333333333333335, 0
|
|||
iatCorrection = scalar, U16, 64, "%", 0.01, 0
|
||||
cltCorrection = scalar, U16, 66, "%", 0.01, 0
|
||||
baroCorrection = scalar, U16, 68, "%", 0.01, 0
|
||||
currentEnginePhase = scalar, U16, 70, "deg", 1, 0
|
||||
wallFuelAmount = scalar, U16, 72, "mg", 0.01, 0
|
||||
wallFuelCorrection = scalar, S16, 74, "mg", 0.01, 0
|
||||
revolutionCounterSinceStart = scalar, U16, 76, "", 1, 0
|
||||
deltaTps = scalar, S16, 78, "ratio", 0.01, 0
|
||||
canReadCounter = scalar, U16, 80, "", 1, 0
|
||||
tpsAccelFuel = scalar, S16, 82, "ms", 0.0033333333333333335, 0
|
||||
ignitionAdvance = scalar, S16, 84, "deg", 0.02, 0
|
||||
sparkDwellValue = scalar, U16, 86, "ms", 0.0033333333333333335, 0
|
||||
coilDutyCycle = scalar, U16, 88, "%", 0.01, 0
|
||||
idleAirValvePosition = scalar, U16, 90, "%", 0.01, 0
|
||||
etbTarget = scalar, S16, 92, "%", 0.01, 0
|
||||
etb1DutyCycle = scalar, S16, 94, "%", 0.01, 0
|
||||
etb1Error = scalar, S16, 96, "%", 0.01, 0
|
||||
fuelTankLevel = scalar, S16, 98, "%", 0.01, 0
|
||||
totalFuelConsumption = scalar, U16, 100, "grams", 1, 0
|
||||
fuelFlowRate = scalar, U16, 102, "gram/s", 0.005, 0
|
||||
veTableYAxis = scalar, U16, 104, "%", 0.01, 0
|
||||
afrTableYAxis = scalar, U16, 106, "%", 0.01, 0
|
||||
wallFuelAmount = scalar, U16, 70, "mg", 0.01, 0
|
||||
wallFuelCorrection = scalar, S16, 72, "mg", 0.01, 0
|
||||
revolutionCounterSinceStart = scalar, U16, 74, "", 1, 0
|
||||
deltaTps = scalar, S16, 76, "ratio", 0.01, 0
|
||||
canReadCounter = scalar, U16, 78, "", 1, 0
|
||||
tpsAccelFuel = scalar, S16, 80, "ms", 0.0033333333333333335, 0
|
||||
ignitionAdvance = scalar, S16, 82, "deg", 0.02, 0
|
||||
sparkDwellValue = scalar, U16, 84, "ms", 0.0033333333333333335, 0
|
||||
coilDutyCycle = scalar, U16, 86, "%", 0.01, 0
|
||||
idleAirValvePosition = scalar, U16, 88, "%", 0.01, 0
|
||||
etbTarget = scalar, S16, 90, "%", 0.01, 0
|
||||
etb1DutyCycle = scalar, S16, 92, "%", 0.01, 0
|
||||
etb1Error = scalar, S16, 94, "%", 0.01, 0
|
||||
fuelTankLevel = scalar, S16, 96, "%", 0.01, 0
|
||||
totalFuelConsumption = scalar, U16, 98, "grams", 1, 0
|
||||
fuelFlowRate = scalar, U16, 100, "gram/s", 0.005, 0
|
||||
veTableYAxis = scalar, U16, 102, "%", 0.01, 0
|
||||
afrTableYAxis = scalar, U16, 104, "%", 0.01, 0
|
||||
knockLevel = scalar, F32, 108, "Volts", 1, 0
|
||||
seconds = scalar, U32, 112, "sec", 1, 0
|
||||
engineMode = scalar, U32, 116, "em", 1, 0
|
||||
|
|
@ -4501,7 +4500,6 @@ entry = injectorLagMs, "fuel: injector lag", float, "%.3f"
|
|||
entry = iatCorrection, "fuel: IAT correction", float, "%.3f"
|
||||
entry = cltCorrection, "fuel: CLT correction", float, "%.3f"
|
||||
entry = baroCorrection, "fuel: Barometric pressure correction", float, "%.3f"
|
||||
entry = currentEnginePhase, "Engine Phase", int, "%d"
|
||||
entry = wallFuelAmount, "fuel: wall amount", float, "%.3f"
|
||||
entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f"
|
||||
entry = revolutionCounterSinceStart, "revolutionCounterSinceStart", int, "%d"
|
||||
|
|
@ -4847,7 +4845,7 @@ entry = mapVvt_MAP_AT_SPECIAL_POINT, "mapVvt_MAP_AT_SPECIAL_POINT", float, "%.3
|
|||
entry = mapVvt_MAP_AT_DIFF, "mapVvt_MAP_AT_DIFF", float, "%.3f"
|
||||
entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d"
|
||||
entry = mapVvt_map_peak, "mapVvt_map_peak", int, "%d"
|
||||
entry = currentEngineDecodedPhase, "Engine Phase2", int, "%d"
|
||||
entry = currentEngineDecodedPhase, "Engine Phase", int, "%d"
|
||||
entry = totalRevolutionCounter, "Crank revolution counter", int, "%d"
|
||||
entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f"
|
||||
entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f"
|
||||
|
|
|
|||
|
|
@ -86,7 +86,7 @@ enable2ndByteCanID = false
|
|||
; name = scalar, type, offset, units, scale, translate, lo, hi, digits
|
||||
|
||||
; CONFIG_DEFINITION_START
|
||||
; this section was generated automatically by rusEFI tool ConfigDefinition.jar based on gen_config.sh integration/rusefi_config.txt Thu Sep 01 03:56:20 UTC 2022
|
||||
; this section was generated automatically by rusEFI tool ConfigDefinition.jar based on gen_config.sh integration/rusefi_config.txt Thu Sep 01 04:18:34 UTC 2022
|
||||
|
||||
pageSize = 21300
|
||||
page = 1
|
||||
|
|
@ -2192,25 +2192,24 @@ injectorLagMs = scalar, U16, 62, "ms", 0.0033333333333333335, 0
|
|||
iatCorrection = scalar, U16, 64, "%", 0.01, 0
|
||||
cltCorrection = scalar, U16, 66, "%", 0.01, 0
|
||||
baroCorrection = scalar, U16, 68, "%", 0.01, 0
|
||||
currentEnginePhase = scalar, U16, 70, "deg", 1, 0
|
||||
wallFuelAmount = scalar, U16, 72, "mg", 0.01, 0
|
||||
wallFuelCorrection = scalar, S16, 74, "mg", 0.01, 0
|
||||
revolutionCounterSinceStart = scalar, U16, 76, "", 1, 0
|
||||
deltaTps = scalar, S16, 78, "ratio", 0.01, 0
|
||||
canReadCounter = scalar, U16, 80, "", 1, 0
|
||||
tpsAccelFuel = scalar, S16, 82, "ms", 0.0033333333333333335, 0
|
||||
ignitionAdvance = scalar, S16, 84, "deg", 0.02, 0
|
||||
sparkDwellValue = scalar, U16, 86, "ms", 0.0033333333333333335, 0
|
||||
coilDutyCycle = scalar, U16, 88, "%", 0.01, 0
|
||||
idleAirValvePosition = scalar, U16, 90, "%", 0.01, 0
|
||||
etbTarget = scalar, S16, 92, "%", 0.01, 0
|
||||
etb1DutyCycle = scalar, S16, 94, "%", 0.01, 0
|
||||
etb1Error = scalar, S16, 96, "%", 0.01, 0
|
||||
fuelTankLevel = scalar, S16, 98, "%", 0.01, 0
|
||||
totalFuelConsumption = scalar, U16, 100, "grams", 1, 0
|
||||
fuelFlowRate = scalar, U16, 102, "gram/s", 0.005, 0
|
||||
veTableYAxis = scalar, U16, 104, "%", 0.01, 0
|
||||
afrTableYAxis = scalar, U16, 106, "%", 0.01, 0
|
||||
wallFuelAmount = scalar, U16, 70, "mg", 0.01, 0
|
||||
wallFuelCorrection = scalar, S16, 72, "mg", 0.01, 0
|
||||
revolutionCounterSinceStart = scalar, U16, 74, "", 1, 0
|
||||
deltaTps = scalar, S16, 76, "ratio", 0.01, 0
|
||||
canReadCounter = scalar, U16, 78, "", 1, 0
|
||||
tpsAccelFuel = scalar, S16, 80, "ms", 0.0033333333333333335, 0
|
||||
ignitionAdvance = scalar, S16, 82, "deg", 0.02, 0
|
||||
sparkDwellValue = scalar, U16, 84, "ms", 0.0033333333333333335, 0
|
||||
coilDutyCycle = scalar, U16, 86, "%", 0.01, 0
|
||||
idleAirValvePosition = scalar, U16, 88, "%", 0.01, 0
|
||||
etbTarget = scalar, S16, 90, "%", 0.01, 0
|
||||
etb1DutyCycle = scalar, S16, 92, "%", 0.01, 0
|
||||
etb1Error = scalar, S16, 94, "%", 0.01, 0
|
||||
fuelTankLevel = scalar, S16, 96, "%", 0.01, 0
|
||||
totalFuelConsumption = scalar, U16, 98, "grams", 1, 0
|
||||
fuelFlowRate = scalar, U16, 100, "gram/s", 0.005, 0
|
||||
veTableYAxis = scalar, U16, 102, "%", 0.01, 0
|
||||
afrTableYAxis = scalar, U16, 104, "%", 0.01, 0
|
||||
knockLevel = scalar, F32, 108, "Volts", 1, 0
|
||||
seconds = scalar, U32, 112, "sec", 1, 0
|
||||
engineMode = scalar, U32, 116, "em", 1, 0
|
||||
|
|
@ -4501,7 +4500,6 @@ entry = injectorLagMs, "fuel: injector lag", float, "%.3f"
|
|||
entry = iatCorrection, "fuel: IAT correction", float, "%.3f"
|
||||
entry = cltCorrection, "fuel: CLT correction", float, "%.3f"
|
||||
entry = baroCorrection, "fuel: Barometric pressure correction", float, "%.3f"
|
||||
entry = currentEnginePhase, "Engine Phase", int, "%d"
|
||||
entry = wallFuelAmount, "fuel: wall amount", float, "%.3f"
|
||||
entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f"
|
||||
entry = revolutionCounterSinceStart, "revolutionCounterSinceStart", int, "%d"
|
||||
|
|
@ -4847,7 +4845,7 @@ entry = mapVvt_MAP_AT_SPECIAL_POINT, "mapVvt_MAP_AT_SPECIAL_POINT", float, "%.3
|
|||
entry = mapVvt_MAP_AT_DIFF, "mapVvt_MAP_AT_DIFF", float, "%.3f"
|
||||
entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d"
|
||||
entry = mapVvt_map_peak, "mapVvt_map_peak", int, "%d"
|
||||
entry = currentEngineDecodedPhase, "Engine Phase2", int, "%d"
|
||||
entry = currentEngineDecodedPhase, "Engine Phase", int, "%d"
|
||||
entry = totalRevolutionCounter, "Crank revolution counter", int, "%d"
|
||||
entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f"
|
||||
entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f"
|
||||
|
|
|
|||
|
|
@ -86,7 +86,7 @@ enable2ndByteCanID = false
|
|||
; name = scalar, type, offset, units, scale, translate, lo, hi, digits
|
||||
|
||||
; CONFIG_DEFINITION_START
|
||||
; this section was generated automatically by rusEFI tool ConfigDefinition.jar based on gen_config.sh integration/rusefi_config.txt Thu Sep 01 03:56:18 UTC 2022
|
||||
; this section was generated automatically by rusEFI tool ConfigDefinition.jar based on gen_config.sh integration/rusefi_config.txt Thu Sep 01 04:18:32 UTC 2022
|
||||
|
||||
pageSize = 21300
|
||||
page = 1
|
||||
|
|
@ -2192,25 +2192,24 @@ injectorLagMs = scalar, U16, 62, "ms", 0.0033333333333333335, 0
|
|||
iatCorrection = scalar, U16, 64, "%", 0.01, 0
|
||||
cltCorrection = scalar, U16, 66, "%", 0.01, 0
|
||||
baroCorrection = scalar, U16, 68, "%", 0.01, 0
|
||||
currentEnginePhase = scalar, U16, 70, "deg", 1, 0
|
||||
wallFuelAmount = scalar, U16, 72, "mg", 0.01, 0
|
||||
wallFuelCorrection = scalar, S16, 74, "mg", 0.01, 0
|
||||
revolutionCounterSinceStart = scalar, U16, 76, "", 1, 0
|
||||
deltaTps = scalar, S16, 78, "ratio", 0.01, 0
|
||||
canReadCounter = scalar, U16, 80, "", 1, 0
|
||||
tpsAccelFuel = scalar, S16, 82, "ms", 0.0033333333333333335, 0
|
||||
ignitionAdvance = scalar, S16, 84, "deg", 0.02, 0
|
||||
sparkDwellValue = scalar, U16, 86, "ms", 0.0033333333333333335, 0
|
||||
coilDutyCycle = scalar, U16, 88, "%", 0.01, 0
|
||||
idleAirValvePosition = scalar, U16, 90, "%", 0.01, 0
|
||||
etbTarget = scalar, S16, 92, "%", 0.01, 0
|
||||
etb1DutyCycle = scalar, S16, 94, "%", 0.01, 0
|
||||
etb1Error = scalar, S16, 96, "%", 0.01, 0
|
||||
fuelTankLevel = scalar, S16, 98, "%", 0.01, 0
|
||||
totalFuelConsumption = scalar, U16, 100, "grams", 1, 0
|
||||
fuelFlowRate = scalar, U16, 102, "gram/s", 0.005, 0
|
||||
veTableYAxis = scalar, U16, 104, "%", 0.01, 0
|
||||
afrTableYAxis = scalar, U16, 106, "%", 0.01, 0
|
||||
wallFuelAmount = scalar, U16, 70, "mg", 0.01, 0
|
||||
wallFuelCorrection = scalar, S16, 72, "mg", 0.01, 0
|
||||
revolutionCounterSinceStart = scalar, U16, 74, "", 1, 0
|
||||
deltaTps = scalar, S16, 76, "ratio", 0.01, 0
|
||||
canReadCounter = scalar, U16, 78, "", 1, 0
|
||||
tpsAccelFuel = scalar, S16, 80, "ms", 0.0033333333333333335, 0
|
||||
ignitionAdvance = scalar, S16, 82, "deg", 0.02, 0
|
||||
sparkDwellValue = scalar, U16, 84, "ms", 0.0033333333333333335, 0
|
||||
coilDutyCycle = scalar, U16, 86, "%", 0.01, 0
|
||||
idleAirValvePosition = scalar, U16, 88, "%", 0.01, 0
|
||||
etbTarget = scalar, S16, 90, "%", 0.01, 0
|
||||
etb1DutyCycle = scalar, S16, 92, "%", 0.01, 0
|
||||
etb1Error = scalar, S16, 94, "%", 0.01, 0
|
||||
fuelTankLevel = scalar, S16, 96, "%", 0.01, 0
|
||||
totalFuelConsumption = scalar, U16, 98, "grams", 1, 0
|
||||
fuelFlowRate = scalar, U16, 100, "gram/s", 0.005, 0
|
||||
veTableYAxis = scalar, U16, 102, "%", 0.01, 0
|
||||
afrTableYAxis = scalar, U16, 104, "%", 0.01, 0
|
||||
knockLevel = scalar, F32, 108, "Volts", 1, 0
|
||||
seconds = scalar, U32, 112, "sec", 1, 0
|
||||
engineMode = scalar, U32, 116, "em", 1, 0
|
||||
|
|
@ -4501,7 +4500,6 @@ entry = injectorLagMs, "fuel: injector lag", float, "%.3f"
|
|||
entry = iatCorrection, "fuel: IAT correction", float, "%.3f"
|
||||
entry = cltCorrection, "fuel: CLT correction", float, "%.3f"
|
||||
entry = baroCorrection, "fuel: Barometric pressure correction", float, "%.3f"
|
||||
entry = currentEnginePhase, "Engine Phase", int, "%d"
|
||||
entry = wallFuelAmount, "fuel: wall amount", float, "%.3f"
|
||||
entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f"
|
||||
entry = revolutionCounterSinceStart, "revolutionCounterSinceStart", int, "%d"
|
||||
|
|
@ -4847,7 +4845,7 @@ entry = mapVvt_MAP_AT_SPECIAL_POINT, "mapVvt_MAP_AT_SPECIAL_POINT", float, "%.3
|
|||
entry = mapVvt_MAP_AT_DIFF, "mapVvt_MAP_AT_DIFF", float, "%.3f"
|
||||
entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d"
|
||||
entry = mapVvt_map_peak, "mapVvt_map_peak", int, "%d"
|
||||
entry = currentEngineDecodedPhase, "Engine Phase2", int, "%d"
|
||||
entry = currentEngineDecodedPhase, "Engine Phase", int, "%d"
|
||||
entry = totalRevolutionCounter, "Crank revolution counter", int, "%d"
|
||||
entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f"
|
||||
entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f"
|
||||
|
|
|
|||
|
|
@ -86,7 +86,7 @@ enable2ndByteCanID = false
|
|||
; name = scalar, type, offset, units, scale, translate, lo, hi, digits
|
||||
|
||||
; CONFIG_DEFINITION_START
|
||||
; this section was generated automatically by rusEFI tool ConfigDefinition.jar based on gen_config.sh integration/rusefi_config.txt Thu Sep 01 03:56:24 UTC 2022
|
||||
; this section was generated automatically by rusEFI tool ConfigDefinition.jar based on gen_config.sh integration/rusefi_config.txt Thu Sep 01 04:18:37 UTC 2022
|
||||
|
||||
pageSize = 21300
|
||||
page = 1
|
||||
|
|
@ -2192,25 +2192,24 @@ injectorLagMs = scalar, U16, 62, "ms", 0.0033333333333333335, 0
|
|||
iatCorrection = scalar, U16, 64, "%", 0.01, 0
|
||||
cltCorrection = scalar, U16, 66, "%", 0.01, 0
|
||||
baroCorrection = scalar, U16, 68, "%", 0.01, 0
|
||||
currentEnginePhase = scalar, U16, 70, "deg", 1, 0
|
||||
wallFuelAmount = scalar, U16, 72, "mg", 0.01, 0
|
||||
wallFuelCorrection = scalar, S16, 74, "mg", 0.01, 0
|
||||
revolutionCounterSinceStart = scalar, U16, 76, "", 1, 0
|
||||
deltaTps = scalar, S16, 78, "ratio", 0.01, 0
|
||||
canReadCounter = scalar, U16, 80, "", 1, 0
|
||||
tpsAccelFuel = scalar, S16, 82, "ms", 0.0033333333333333335, 0
|
||||
ignitionAdvance = scalar, S16, 84, "deg", 0.02, 0
|
||||
sparkDwellValue = scalar, U16, 86, "ms", 0.0033333333333333335, 0
|
||||
coilDutyCycle = scalar, U16, 88, "%", 0.01, 0
|
||||
idleAirValvePosition = scalar, U16, 90, "%", 0.01, 0
|
||||
etbTarget = scalar, S16, 92, "%", 0.01, 0
|
||||
etb1DutyCycle = scalar, S16, 94, "%", 0.01, 0
|
||||
etb1Error = scalar, S16, 96, "%", 0.01, 0
|
||||
fuelTankLevel = scalar, S16, 98, "%", 0.01, 0
|
||||
totalFuelConsumption = scalar, U16, 100, "grams", 1, 0
|
||||
fuelFlowRate = scalar, U16, 102, "gram/s", 0.005, 0
|
||||
veTableYAxis = scalar, U16, 104, "%", 0.01, 0
|
||||
afrTableYAxis = scalar, U16, 106, "%", 0.01, 0
|
||||
wallFuelAmount = scalar, U16, 70, "mg", 0.01, 0
|
||||
wallFuelCorrection = scalar, S16, 72, "mg", 0.01, 0
|
||||
revolutionCounterSinceStart = scalar, U16, 74, "", 1, 0
|
||||
deltaTps = scalar, S16, 76, "ratio", 0.01, 0
|
||||
canReadCounter = scalar, U16, 78, "", 1, 0
|
||||
tpsAccelFuel = scalar, S16, 80, "ms", 0.0033333333333333335, 0
|
||||
ignitionAdvance = scalar, S16, 82, "deg", 0.02, 0
|
||||
sparkDwellValue = scalar, U16, 84, "ms", 0.0033333333333333335, 0
|
||||
coilDutyCycle = scalar, U16, 86, "%", 0.01, 0
|
||||
idleAirValvePosition = scalar, U16, 88, "%", 0.01, 0
|
||||
etbTarget = scalar, S16, 90, "%", 0.01, 0
|
||||
etb1DutyCycle = scalar, S16, 92, "%", 0.01, 0
|
||||
etb1Error = scalar, S16, 94, "%", 0.01, 0
|
||||
fuelTankLevel = scalar, S16, 96, "%", 0.01, 0
|
||||
totalFuelConsumption = scalar, U16, 98, "grams", 1, 0
|
||||
fuelFlowRate = scalar, U16, 100, "gram/s", 0.005, 0
|
||||
veTableYAxis = scalar, U16, 102, "%", 0.01, 0
|
||||
afrTableYAxis = scalar, U16, 104, "%", 0.01, 0
|
||||
knockLevel = scalar, F32, 108, "Volts", 1, 0
|
||||
seconds = scalar, U32, 112, "sec", 1, 0
|
||||
engineMode = scalar, U32, 116, "em", 1, 0
|
||||
|
|
@ -4501,7 +4500,6 @@ entry = injectorLagMs, "fuel: injector lag", float, "%.3f"
|
|||
entry = iatCorrection, "fuel: IAT correction", float, "%.3f"
|
||||
entry = cltCorrection, "fuel: CLT correction", float, "%.3f"
|
||||
entry = baroCorrection, "fuel: Barometric pressure correction", float, "%.3f"
|
||||
entry = currentEnginePhase, "Engine Phase", int, "%d"
|
||||
entry = wallFuelAmount, "fuel: wall amount", float, "%.3f"
|
||||
entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f"
|
||||
entry = revolutionCounterSinceStart, "revolutionCounterSinceStart", int, "%d"
|
||||
|
|
@ -4847,7 +4845,7 @@ entry = mapVvt_MAP_AT_SPECIAL_POINT, "mapVvt_MAP_AT_SPECIAL_POINT", float, "%.3
|
|||
entry = mapVvt_MAP_AT_DIFF, "mapVvt_MAP_AT_DIFF", float, "%.3f"
|
||||
entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d"
|
||||
entry = mapVvt_map_peak, "mapVvt_map_peak", int, "%d"
|
||||
entry = currentEngineDecodedPhase, "Engine Phase2", int, "%d"
|
||||
entry = currentEngineDecodedPhase, "Engine Phase", int, "%d"
|
||||
entry = totalRevolutionCounter, "Crank revolution counter", int, "%d"
|
||||
entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f"
|
||||
entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f"
|
||||
|
|
|
|||
|
|
@ -86,7 +86,7 @@ enable2ndByteCanID = false
|
|||
; name = scalar, type, offset, units, scale, translate, lo, hi, digits
|
||||
|
||||
; CONFIG_DEFINITION_START
|
||||
; this section was generated automatically by rusEFI tool ConfigDefinition.jar based on gen_config.sh integration/rusefi_config.txt Thu Sep 01 03:56:21 UTC 2022
|
||||
; this section was generated automatically by rusEFI tool ConfigDefinition.jar based on gen_config.sh integration/rusefi_config.txt Thu Sep 01 04:18:35 UTC 2022
|
||||
|
||||
pageSize = 21300
|
||||
page = 1
|
||||
|
|
@ -2192,25 +2192,24 @@ injectorLagMs = scalar, U16, 62, "ms", 0.0033333333333333335, 0
|
|||
iatCorrection = scalar, U16, 64, "%", 0.01, 0
|
||||
cltCorrection = scalar, U16, 66, "%", 0.01, 0
|
||||
baroCorrection = scalar, U16, 68, "%", 0.01, 0
|
||||
currentEnginePhase = scalar, U16, 70, "deg", 1, 0
|
||||
wallFuelAmount = scalar, U16, 72, "mg", 0.01, 0
|
||||
wallFuelCorrection = scalar, S16, 74, "mg", 0.01, 0
|
||||
revolutionCounterSinceStart = scalar, U16, 76, "", 1, 0
|
||||
deltaTps = scalar, S16, 78, "ratio", 0.01, 0
|
||||
canReadCounter = scalar, U16, 80, "", 1, 0
|
||||
tpsAccelFuel = scalar, S16, 82, "ms", 0.0033333333333333335, 0
|
||||
ignitionAdvance = scalar, S16, 84, "deg", 0.02, 0
|
||||
sparkDwellValue = scalar, U16, 86, "ms", 0.0033333333333333335, 0
|
||||
coilDutyCycle = scalar, U16, 88, "%", 0.01, 0
|
||||
idleAirValvePosition = scalar, U16, 90, "%", 0.01, 0
|
||||
etbTarget = scalar, S16, 92, "%", 0.01, 0
|
||||
etb1DutyCycle = scalar, S16, 94, "%", 0.01, 0
|
||||
etb1Error = scalar, S16, 96, "%", 0.01, 0
|
||||
fuelTankLevel = scalar, S16, 98, "%", 0.01, 0
|
||||
totalFuelConsumption = scalar, U16, 100, "grams", 1, 0
|
||||
fuelFlowRate = scalar, U16, 102, "gram/s", 0.005, 0
|
||||
veTableYAxis = scalar, U16, 104, "%", 0.01, 0
|
||||
afrTableYAxis = scalar, U16, 106, "%", 0.01, 0
|
||||
wallFuelAmount = scalar, U16, 70, "mg", 0.01, 0
|
||||
wallFuelCorrection = scalar, S16, 72, "mg", 0.01, 0
|
||||
revolutionCounterSinceStart = scalar, U16, 74, "", 1, 0
|
||||
deltaTps = scalar, S16, 76, "ratio", 0.01, 0
|
||||
canReadCounter = scalar, U16, 78, "", 1, 0
|
||||
tpsAccelFuel = scalar, S16, 80, "ms", 0.0033333333333333335, 0
|
||||
ignitionAdvance = scalar, S16, 82, "deg", 0.02, 0
|
||||
sparkDwellValue = scalar, U16, 84, "ms", 0.0033333333333333335, 0
|
||||
coilDutyCycle = scalar, U16, 86, "%", 0.01, 0
|
||||
idleAirValvePosition = scalar, U16, 88, "%", 0.01, 0
|
||||
etbTarget = scalar, S16, 90, "%", 0.01, 0
|
||||
etb1DutyCycle = scalar, S16, 92, "%", 0.01, 0
|
||||
etb1Error = scalar, S16, 94, "%", 0.01, 0
|
||||
fuelTankLevel = scalar, S16, 96, "%", 0.01, 0
|
||||
totalFuelConsumption = scalar, U16, 98, "grams", 1, 0
|
||||
fuelFlowRate = scalar, U16, 100, "gram/s", 0.005, 0
|
||||
veTableYAxis = scalar, U16, 102, "%", 0.01, 0
|
||||
afrTableYAxis = scalar, U16, 104, "%", 0.01, 0
|
||||
knockLevel = scalar, F32, 108, "Volts", 1, 0
|
||||
seconds = scalar, U32, 112, "sec", 1, 0
|
||||
engineMode = scalar, U32, 116, "em", 1, 0
|
||||
|
|
@ -4501,7 +4500,6 @@ entry = injectorLagMs, "fuel: injector lag", float, "%.3f"
|
|||
entry = iatCorrection, "fuel: IAT correction", float, "%.3f"
|
||||
entry = cltCorrection, "fuel: CLT correction", float, "%.3f"
|
||||
entry = baroCorrection, "fuel: Barometric pressure correction", float, "%.3f"
|
||||
entry = currentEnginePhase, "Engine Phase", int, "%d"
|
||||
entry = wallFuelAmount, "fuel: wall amount", float, "%.3f"
|
||||
entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f"
|
||||
entry = revolutionCounterSinceStart, "revolutionCounterSinceStart", int, "%d"
|
||||
|
|
@ -4847,7 +4845,7 @@ entry = mapVvt_MAP_AT_SPECIAL_POINT, "mapVvt_MAP_AT_SPECIAL_POINT", float, "%.3
|
|||
entry = mapVvt_MAP_AT_DIFF, "mapVvt_MAP_AT_DIFF", float, "%.3f"
|
||||
entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d"
|
||||
entry = mapVvt_map_peak, "mapVvt_map_peak", int, "%d"
|
||||
entry = currentEngineDecodedPhase, "Engine Phase2", int, "%d"
|
||||
entry = currentEngineDecodedPhase, "Engine Phase", int, "%d"
|
||||
entry = totalRevolutionCounter, "Crank revolution counter", int, "%d"
|
||||
entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f"
|
||||
entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f"
|
||||
|
|
|
|||
|
|
@ -86,7 +86,7 @@ enable2ndByteCanID = false
|
|||
; name = scalar, type, offset, units, scale, translate, lo, hi, digits
|
||||
|
||||
; CONFIG_DEFINITION_START
|
||||
; this section was generated automatically by rusEFI tool ConfigDefinition.jar based on gen_config.sh integration/rusefi_config.txt Thu Sep 01 03:56:25 UTC 2022
|
||||
; this section was generated automatically by rusEFI tool ConfigDefinition.jar based on gen_config.sh integration/rusefi_config.txt Thu Sep 01 04:18:39 UTC 2022
|
||||
|
||||
pageSize = 21300
|
||||
page = 1
|
||||
|
|
@ -2192,25 +2192,24 @@ injectorLagMs = scalar, U16, 62, "ms", 0.0033333333333333335, 0
|
|||
iatCorrection = scalar, U16, 64, "%", 0.01, 0
|
||||
cltCorrection = scalar, U16, 66, "%", 0.01, 0
|
||||
baroCorrection = scalar, U16, 68, "%", 0.01, 0
|
||||
currentEnginePhase = scalar, U16, 70, "deg", 1, 0
|
||||
wallFuelAmount = scalar, U16, 72, "mg", 0.01, 0
|
||||
wallFuelCorrection = scalar, S16, 74, "mg", 0.01, 0
|
||||
revolutionCounterSinceStart = scalar, U16, 76, "", 1, 0
|
||||
deltaTps = scalar, S16, 78, "ratio", 0.01, 0
|
||||
canReadCounter = scalar, U16, 80, "", 1, 0
|
||||
tpsAccelFuel = scalar, S16, 82, "ms", 0.0033333333333333335, 0
|
||||
ignitionAdvance = scalar, S16, 84, "deg", 0.02, 0
|
||||
sparkDwellValue = scalar, U16, 86, "ms", 0.0033333333333333335, 0
|
||||
coilDutyCycle = scalar, U16, 88, "%", 0.01, 0
|
||||
idleAirValvePosition = scalar, U16, 90, "%", 0.01, 0
|
||||
etbTarget = scalar, S16, 92, "%", 0.01, 0
|
||||
etb1DutyCycle = scalar, S16, 94, "%", 0.01, 0
|
||||
etb1Error = scalar, S16, 96, "%", 0.01, 0
|
||||
fuelTankLevel = scalar, S16, 98, "%", 0.01, 0
|
||||
totalFuelConsumption = scalar, U16, 100, "grams", 1, 0
|
||||
fuelFlowRate = scalar, U16, 102, "gram/s", 0.005, 0
|
||||
veTableYAxis = scalar, U16, 104, "%", 0.01, 0
|
||||
afrTableYAxis = scalar, U16, 106, "%", 0.01, 0
|
||||
wallFuelAmount = scalar, U16, 70, "mg", 0.01, 0
|
||||
wallFuelCorrection = scalar, S16, 72, "mg", 0.01, 0
|
||||
revolutionCounterSinceStart = scalar, U16, 74, "", 1, 0
|
||||
deltaTps = scalar, S16, 76, "ratio", 0.01, 0
|
||||
canReadCounter = scalar, U16, 78, "", 1, 0
|
||||
tpsAccelFuel = scalar, S16, 80, "ms", 0.0033333333333333335, 0
|
||||
ignitionAdvance = scalar, S16, 82, "deg", 0.02, 0
|
||||
sparkDwellValue = scalar, U16, 84, "ms", 0.0033333333333333335, 0
|
||||
coilDutyCycle = scalar, U16, 86, "%", 0.01, 0
|
||||
idleAirValvePosition = scalar, U16, 88, "%", 0.01, 0
|
||||
etbTarget = scalar, S16, 90, "%", 0.01, 0
|
||||
etb1DutyCycle = scalar, S16, 92, "%", 0.01, 0
|
||||
etb1Error = scalar, S16, 94, "%", 0.01, 0
|
||||
fuelTankLevel = scalar, S16, 96, "%", 0.01, 0
|
||||
totalFuelConsumption = scalar, U16, 98, "grams", 1, 0
|
||||
fuelFlowRate = scalar, U16, 100, "gram/s", 0.005, 0
|
||||
veTableYAxis = scalar, U16, 102, "%", 0.01, 0
|
||||
afrTableYAxis = scalar, U16, 104, "%", 0.01, 0
|
||||
knockLevel = scalar, F32, 108, "Volts", 1, 0
|
||||
seconds = scalar, U32, 112, "sec", 1, 0
|
||||
engineMode = scalar, U32, 116, "em", 1, 0
|
||||
|
|
@ -4501,7 +4500,6 @@ entry = injectorLagMs, "fuel: injector lag", float, "%.3f"
|
|||
entry = iatCorrection, "fuel: IAT correction", float, "%.3f"
|
||||
entry = cltCorrection, "fuel: CLT correction", float, "%.3f"
|
||||
entry = baroCorrection, "fuel: Barometric pressure correction", float, "%.3f"
|
||||
entry = currentEnginePhase, "Engine Phase", int, "%d"
|
||||
entry = wallFuelAmount, "fuel: wall amount", float, "%.3f"
|
||||
entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f"
|
||||
entry = revolutionCounterSinceStart, "revolutionCounterSinceStart", int, "%d"
|
||||
|
|
@ -4847,7 +4845,7 @@ entry = mapVvt_MAP_AT_SPECIAL_POINT, "mapVvt_MAP_AT_SPECIAL_POINT", float, "%.3
|
|||
entry = mapVvt_MAP_AT_DIFF, "mapVvt_MAP_AT_DIFF", float, "%.3f"
|
||||
entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d"
|
||||
entry = mapVvt_map_peak, "mapVvt_map_peak", int, "%d"
|
||||
entry = currentEngineDecodedPhase, "Engine Phase2", int, "%d"
|
||||
entry = currentEngineDecodedPhase, "Engine Phase", int, "%d"
|
||||
entry = totalRevolutionCounter, "Crank revolution counter", int, "%d"
|
||||
entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f"
|
||||
entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f"
|
||||
|
|
|
|||
|
|
@ -86,7 +86,7 @@ enable2ndByteCanID = false
|
|||
; name = scalar, type, offset, units, scale, translate, lo, hi, digits
|
||||
|
||||
; CONFIG_DEFINITION_START
|
||||
; this section was generated automatically by rusEFI tool ConfigDefinition.jar based on config/boards/subaru_eg33/config/gen_subaru_config.sh integration/rusefi_config.txt Thu Sep 01 03:55:39 UTC 2022
|
||||
; this section was generated automatically by rusEFI tool ConfigDefinition.jar based on config/boards/subaru_eg33/config/gen_subaru_config.sh integration/rusefi_config.txt Thu Sep 01 04:17:58 UTC 2022
|
||||
|
||||
pageSize = 21300
|
||||
page = 1
|
||||
|
|
@ -2192,25 +2192,24 @@ injectorLagMs = scalar, U16, 62, "ms", 0.0033333333333333335, 0
|
|||
iatCorrection = scalar, U16, 64, "%", 0.01, 0
|
||||
cltCorrection = scalar, U16, 66, "%", 0.01, 0
|
||||
baroCorrection = scalar, U16, 68, "%", 0.01, 0
|
||||
currentEnginePhase = scalar, U16, 70, "deg", 1, 0
|
||||
wallFuelAmount = scalar, U16, 72, "mg", 0.01, 0
|
||||
wallFuelCorrection = scalar, S16, 74, "mg", 0.01, 0
|
||||
revolutionCounterSinceStart = scalar, U16, 76, "", 1, 0
|
||||
deltaTps = scalar, S16, 78, "ratio", 0.01, 0
|
||||
canReadCounter = scalar, U16, 80, "", 1, 0
|
||||
tpsAccelFuel = scalar, S16, 82, "ms", 0.0033333333333333335, 0
|
||||
ignitionAdvance = scalar, S16, 84, "deg", 0.02, 0
|
||||
sparkDwellValue = scalar, U16, 86, "ms", 0.0033333333333333335, 0
|
||||
coilDutyCycle = scalar, U16, 88, "%", 0.01, 0
|
||||
idleAirValvePosition = scalar, U16, 90, "%", 0.01, 0
|
||||
etbTarget = scalar, S16, 92, "%", 0.01, 0
|
||||
etb1DutyCycle = scalar, S16, 94, "%", 0.01, 0
|
||||
etb1Error = scalar, S16, 96, "%", 0.01, 0
|
||||
fuelTankLevel = scalar, S16, 98, "%", 0.01, 0
|
||||
totalFuelConsumption = scalar, U16, 100, "grams", 1, 0
|
||||
fuelFlowRate = scalar, U16, 102, "gram/s", 0.005, 0
|
||||
veTableYAxis = scalar, U16, 104, "%", 0.01, 0
|
||||
afrTableYAxis = scalar, U16, 106, "%", 0.01, 0
|
||||
wallFuelAmount = scalar, U16, 70, "mg", 0.01, 0
|
||||
wallFuelCorrection = scalar, S16, 72, "mg", 0.01, 0
|
||||
revolutionCounterSinceStart = scalar, U16, 74, "", 1, 0
|
||||
deltaTps = scalar, S16, 76, "ratio", 0.01, 0
|
||||
canReadCounter = scalar, U16, 78, "", 1, 0
|
||||
tpsAccelFuel = scalar, S16, 80, "ms", 0.0033333333333333335, 0
|
||||
ignitionAdvance = scalar, S16, 82, "deg", 0.02, 0
|
||||
sparkDwellValue = scalar, U16, 84, "ms", 0.0033333333333333335, 0
|
||||
coilDutyCycle = scalar, U16, 86, "%", 0.01, 0
|
||||
idleAirValvePosition = scalar, U16, 88, "%", 0.01, 0
|
||||
etbTarget = scalar, S16, 90, "%", 0.01, 0
|
||||
etb1DutyCycle = scalar, S16, 92, "%", 0.01, 0
|
||||
etb1Error = scalar, S16, 94, "%", 0.01, 0
|
||||
fuelTankLevel = scalar, S16, 96, "%", 0.01, 0
|
||||
totalFuelConsumption = scalar, U16, 98, "grams", 1, 0
|
||||
fuelFlowRate = scalar, U16, 100, "gram/s", 0.005, 0
|
||||
veTableYAxis = scalar, U16, 102, "%", 0.01, 0
|
||||
afrTableYAxis = scalar, U16, 104, "%", 0.01, 0
|
||||
knockLevel = scalar, F32, 108, "Volts", 1, 0
|
||||
seconds = scalar, U32, 112, "sec", 1, 0
|
||||
engineMode = scalar, U32, 116, "em", 1, 0
|
||||
|
|
@ -4501,7 +4500,6 @@ entry = injectorLagMs, "fuel: injector lag", float, "%.3f"
|
|||
entry = iatCorrection, "fuel: IAT correction", float, "%.3f"
|
||||
entry = cltCorrection, "fuel: CLT correction", float, "%.3f"
|
||||
entry = baroCorrection, "fuel: Barometric pressure correction", float, "%.3f"
|
||||
entry = currentEnginePhase, "Engine Phase", int, "%d"
|
||||
entry = wallFuelAmount, "fuel: wall amount", float, "%.3f"
|
||||
entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f"
|
||||
entry = revolutionCounterSinceStart, "revolutionCounterSinceStart", int, "%d"
|
||||
|
|
@ -4847,7 +4845,7 @@ entry = mapVvt_MAP_AT_SPECIAL_POINT, "mapVvt_MAP_AT_SPECIAL_POINT", float, "%.3
|
|||
entry = mapVvt_MAP_AT_DIFF, "mapVvt_MAP_AT_DIFF", float, "%.3f"
|
||||
entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d"
|
||||
entry = mapVvt_map_peak, "mapVvt_map_peak", int, "%d"
|
||||
entry = currentEngineDecodedPhase, "Engine Phase2", int, "%d"
|
||||
entry = currentEngineDecodedPhase, "Engine Phase", int, "%d"
|
||||
entry = totalRevolutionCounter, "Crank revolution counter", int, "%d"
|
||||
entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f"
|
||||
entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f"
|
||||
|
|
|
|||
|
|
@ -86,7 +86,7 @@ enable2ndByteCanID = false
|
|||
; name = scalar, type, offset, units, scale, translate, lo, hi, digits
|
||||
|
||||
; CONFIG_DEFINITION_START
|
||||
; this section was generated automatically by rusEFI tool ConfigDefinition.jar based on gen_config.sh integration/rusefi_config.txt Thu Sep 01 03:56:33 UTC 2022
|
||||
; this section was generated automatically by rusEFI tool ConfigDefinition.jar based on gen_config.sh integration/rusefi_config.txt Thu Sep 01 04:18:46 UTC 2022
|
||||
|
||||
pageSize = 21300
|
||||
page = 1
|
||||
|
|
@ -2192,25 +2192,24 @@ injectorLagMs = scalar, U16, 62, "ms", 0.0033333333333333335, 0
|
|||
iatCorrection = scalar, U16, 64, "%", 0.01, 0
|
||||
cltCorrection = scalar, U16, 66, "%", 0.01, 0
|
||||
baroCorrection = scalar, U16, 68, "%", 0.01, 0
|
||||
currentEnginePhase = scalar, U16, 70, "deg", 1, 0
|
||||
wallFuelAmount = scalar, U16, 72, "mg", 0.01, 0
|
||||
wallFuelCorrection = scalar, S16, 74, "mg", 0.01, 0
|
||||
revolutionCounterSinceStart = scalar, U16, 76, "", 1, 0
|
||||
deltaTps = scalar, S16, 78, "ratio", 0.01, 0
|
||||
canReadCounter = scalar, U16, 80, "", 1, 0
|
||||
tpsAccelFuel = scalar, S16, 82, "ms", 0.0033333333333333335, 0
|
||||
ignitionAdvance = scalar, S16, 84, "deg", 0.02, 0
|
||||
sparkDwellValue = scalar, U16, 86, "ms", 0.0033333333333333335, 0
|
||||
coilDutyCycle = scalar, U16, 88, "%", 0.01, 0
|
||||
idleAirValvePosition = scalar, U16, 90, "%", 0.01, 0
|
||||
etbTarget = scalar, S16, 92, "%", 0.01, 0
|
||||
etb1DutyCycle = scalar, S16, 94, "%", 0.01, 0
|
||||
etb1Error = scalar, S16, 96, "%", 0.01, 0
|
||||
fuelTankLevel = scalar, S16, 98, "%", 0.01, 0
|
||||
totalFuelConsumption = scalar, U16, 100, "grams", 1, 0
|
||||
fuelFlowRate = scalar, U16, 102, "gram/s", 0.005, 0
|
||||
veTableYAxis = scalar, U16, 104, "%", 0.01, 0
|
||||
afrTableYAxis = scalar, U16, 106, "%", 0.01, 0
|
||||
wallFuelAmount = scalar, U16, 70, "mg", 0.01, 0
|
||||
wallFuelCorrection = scalar, S16, 72, "mg", 0.01, 0
|
||||
revolutionCounterSinceStart = scalar, U16, 74, "", 1, 0
|
||||
deltaTps = scalar, S16, 76, "ratio", 0.01, 0
|
||||
canReadCounter = scalar, U16, 78, "", 1, 0
|
||||
tpsAccelFuel = scalar, S16, 80, "ms", 0.0033333333333333335, 0
|
||||
ignitionAdvance = scalar, S16, 82, "deg", 0.02, 0
|
||||
sparkDwellValue = scalar, U16, 84, "ms", 0.0033333333333333335, 0
|
||||
coilDutyCycle = scalar, U16, 86, "%", 0.01, 0
|
||||
idleAirValvePosition = scalar, U16, 88, "%", 0.01, 0
|
||||
etbTarget = scalar, S16, 90, "%", 0.01, 0
|
||||
etb1DutyCycle = scalar, S16, 92, "%", 0.01, 0
|
||||
etb1Error = scalar, S16, 94, "%", 0.01, 0
|
||||
fuelTankLevel = scalar, S16, 96, "%", 0.01, 0
|
||||
totalFuelConsumption = scalar, U16, 98, "grams", 1, 0
|
||||
fuelFlowRate = scalar, U16, 100, "gram/s", 0.005, 0
|
||||
veTableYAxis = scalar, U16, 102, "%", 0.01, 0
|
||||
afrTableYAxis = scalar, U16, 104, "%", 0.01, 0
|
||||
knockLevel = scalar, F32, 108, "Volts", 1, 0
|
||||
seconds = scalar, U32, 112, "sec", 1, 0
|
||||
engineMode = scalar, U32, 116, "em", 1, 0
|
||||
|
|
@ -4501,7 +4500,6 @@ entry = injectorLagMs, "fuel: injector lag", float, "%.3f"
|
|||
entry = iatCorrection, "fuel: IAT correction", float, "%.3f"
|
||||
entry = cltCorrection, "fuel: CLT correction", float, "%.3f"
|
||||
entry = baroCorrection, "fuel: Barometric pressure correction", float, "%.3f"
|
||||
entry = currentEnginePhase, "Engine Phase", int, "%d"
|
||||
entry = wallFuelAmount, "fuel: wall amount", float, "%.3f"
|
||||
entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f"
|
||||
entry = revolutionCounterSinceStart, "revolutionCounterSinceStart", int, "%d"
|
||||
|
|
@ -4847,7 +4845,7 @@ entry = mapVvt_MAP_AT_SPECIAL_POINT, "mapVvt_MAP_AT_SPECIAL_POINT", float, "%.3
|
|||
entry = mapVvt_MAP_AT_DIFF, "mapVvt_MAP_AT_DIFF", float, "%.3f"
|
||||
entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d"
|
||||
entry = mapVvt_map_peak, "mapVvt_map_peak", int, "%d"
|
||||
entry = currentEngineDecodedPhase, "Engine Phase2", int, "%d"
|
||||
entry = currentEngineDecodedPhase, "Engine Phase", int, "%d"
|
||||
entry = totalRevolutionCounter, "Crank revolution counter", int, "%d"
|
||||
entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f"
|
||||
entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f"
|
||||
|
|
|
|||
|
|
@ -1,6 +1,6 @@
|
|||
package com.rusefi.config.generated;
|
||||
|
||||
// this file was generated automatically by rusEFI tool ConfigDefinition.jar based on (unknown script) console/binary/output_channels.txt Mon Aug 29 12:19:32 UTC 2022
|
||||
// this file was generated automatically by rusEFI tool ConfigDefinition.jar based on (unknown script) console/binary/output_channels.txt Thu Sep 01 04:17:54 UTC 2022
|
||||
|
||||
// by class com.rusefi.output.FileJavaFieldsConsumer
|
||||
import com.rusefi.config.*;
|
||||
|
|
@ -455,25 +455,25 @@ public class TsOutputs {
|
|||
public static final Field IATCORRECTION = Field.create("IATCORRECTION", 64, FieldType.INT16).setScale(0.01);
|
||||
public static final Field CLTCORRECTION = Field.create("CLTCORRECTION", 66, FieldType.INT16).setScale(0.01);
|
||||
public static final Field BAROCORRECTION = Field.create("BAROCORRECTION", 68, FieldType.INT16).setScale(0.01);
|
||||
public static final Field CURRENTENGINEPHASE = Field.create("CURRENTENGINEPHASE", 70, FieldType.INT16).setScale(1.0);
|
||||
public static final Field WALLFUELAMOUNT = Field.create("WALLFUELAMOUNT", 72, FieldType.INT16).setScale(0.01);
|
||||
public static final Field WALLFUELCORRECTION = Field.create("WALLFUELCORRECTION", 74, FieldType.INT16).setScale(0.01);
|
||||
public static final Field REVOLUTIONCOUNTERSINCESTART = Field.create("REVOLUTIONCOUNTERSINCESTART", 76, FieldType.INT16).setScale(1.0);
|
||||
public static final Field DELTATPS = Field.create("DELTATPS", 78, FieldType.INT16).setScale(0.01);
|
||||
public static final Field CANREADCOUNTER = Field.create("CANREADCOUNTER", 80, FieldType.INT16).setScale(1.0);
|
||||
public static final Field TPSACCELFUEL = Field.create("TPSACCELFUEL", 82, FieldType.INT16).setScale(0.0033333333333333335);
|
||||
public static final Field IGNITIONADVANCE = Field.create("IGNITIONADVANCE", 84, FieldType.INT16).setScale(0.02);
|
||||
public static final Field SPARKDWELLVALUE = Field.create("SPARKDWELLVALUE", 86, FieldType.INT16).setScale(0.0033333333333333335);
|
||||
public static final Field COILDUTYCYCLE = Field.create("COILDUTYCYCLE", 88, FieldType.INT16).setScale(0.01);
|
||||
public static final Field IDLEAIRVALVEPOSITION = Field.create("IDLEAIRVALVEPOSITION", 90, FieldType.INT16).setScale(0.01);
|
||||
public static final Field ETBTARGET = Field.create("ETBTARGET", 92, FieldType.INT16).setScale(0.01);
|
||||
public static final Field ETB1DUTYCYCLE = Field.create("ETB1DUTYCYCLE", 94, FieldType.INT16).setScale(0.01);
|
||||
public static final Field ETB1ERROR = Field.create("ETB1ERROR", 96, FieldType.INT16).setScale(0.01);
|
||||
public static final Field FUELTANKLEVEL = Field.create("FUELTANKLEVEL", 98, FieldType.INT16).setScale(0.01);
|
||||
public static final Field TOTALFUELCONSUMPTION = Field.create("TOTALFUELCONSUMPTION", 100, FieldType.INT16).setScale(1.0);
|
||||
public static final Field FUELFLOWRATE = Field.create("FUELFLOWRATE", 102, FieldType.INT16).setScale(0.005);
|
||||
public static final Field VETABLEYAXIS = Field.create("VETABLEYAXIS", 104, FieldType.INT16).setScale(0.01);
|
||||
public static final Field AFRTABLEYAXIS = Field.create("AFRTABLEYAXIS", 106, FieldType.INT16).setScale(0.01);
|
||||
public static final Field WALLFUELAMOUNT = Field.create("WALLFUELAMOUNT", 70, FieldType.INT16).setScale(0.01);
|
||||
public static final Field WALLFUELCORRECTION = Field.create("WALLFUELCORRECTION", 72, FieldType.INT16).setScale(0.01);
|
||||
public static final Field REVOLUTIONCOUNTERSINCESTART = Field.create("REVOLUTIONCOUNTERSINCESTART", 74, FieldType.INT16).setScale(1.0);
|
||||
public static final Field DELTATPS = Field.create("DELTATPS", 76, FieldType.INT16).setScale(0.01);
|
||||
public static final Field CANREADCOUNTER = Field.create("CANREADCOUNTER", 78, FieldType.INT16).setScale(1.0);
|
||||
public static final Field TPSACCELFUEL = Field.create("TPSACCELFUEL", 80, FieldType.INT16).setScale(0.0033333333333333335);
|
||||
public static final Field IGNITIONADVANCE = Field.create("IGNITIONADVANCE", 82, FieldType.INT16).setScale(0.02);
|
||||
public static final Field SPARKDWELLVALUE = Field.create("SPARKDWELLVALUE", 84, FieldType.INT16).setScale(0.0033333333333333335);
|
||||
public static final Field COILDUTYCYCLE = Field.create("COILDUTYCYCLE", 86, FieldType.INT16).setScale(0.01);
|
||||
public static final Field IDLEAIRVALVEPOSITION = Field.create("IDLEAIRVALVEPOSITION", 88, FieldType.INT16).setScale(0.01);
|
||||
public static final Field ETBTARGET = Field.create("ETBTARGET", 90, FieldType.INT16).setScale(0.01);
|
||||
public static final Field ETB1DUTYCYCLE = Field.create("ETB1DUTYCYCLE", 92, FieldType.INT16).setScale(0.01);
|
||||
public static final Field ETB1ERROR = Field.create("ETB1ERROR", 94, FieldType.INT16).setScale(0.01);
|
||||
public static final Field FUELTANKLEVEL = Field.create("FUELTANKLEVEL", 96, FieldType.INT16).setScale(0.01);
|
||||
public static final Field TOTALFUELCONSUMPTION = Field.create("TOTALFUELCONSUMPTION", 98, FieldType.INT16).setScale(1.0);
|
||||
public static final Field FUELFLOWRATE = Field.create("FUELFLOWRATE", 100, FieldType.INT16).setScale(0.005);
|
||||
public static final Field VETABLEYAXIS = Field.create("VETABLEYAXIS", 102, FieldType.INT16).setScale(0.01);
|
||||
public static final Field AFRTABLEYAXIS = Field.create("AFRTABLEYAXIS", 104, FieldType.INT16).setScale(0.01);
|
||||
public static final Field ALIGNMENTFILL_AT_106 = Field.create("ALIGNMENTFILL_AT_106", 106, FieldType.INT8).setScale(1.0);
|
||||
public static final Field KNOCKLEVEL = Field.create("KNOCKLEVEL", 108, FieldType.FLOAT);
|
||||
public static final Field SECONDS = Field.create("SECONDS", 112, FieldType.INT).setScale(1.0);
|
||||
public static final Field ENGINEMODE = Field.create("ENGINEMODE", 116, FieldType.INT).setScale(1.0);
|
||||
|
|
@ -979,7 +979,6 @@ public class TsOutputs {
|
|||
IATCORRECTION,
|
||||
CLTCORRECTION,
|
||||
BAROCORRECTION,
|
||||
CURRENTENGINEPHASE,
|
||||
WALLFUELAMOUNT,
|
||||
WALLFUELCORRECTION,
|
||||
REVOLUTIONCOUNTERSINCESTART,
|
||||
|
|
@ -998,6 +997,7 @@ public class TsOutputs {
|
|||
FUELFLOWRATE,
|
||||
VETABLEYAXIS,
|
||||
AFRTABLEYAXIS,
|
||||
ALIGNMENTFILL_AT_106,
|
||||
KNOCKLEVEL,
|
||||
SECONDS,
|
||||
ENGINEMODE,
|
||||
|
|
|
|||
Loading…
Reference in New Issue