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Auto-generated configs and docs

This commit is contained in:
GitHub gen-configs Action 2022-09-01 04:18:59 +00:00
parent c63fb29aaf
commit 4f6f985d4f
39 changed files with 730 additions and 796 deletions
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3
firmware/console/binary/generated/data_logs.ini
View File

@ -58,7 +58,6 @@ entry = injectorLagMs, "fuel: injector lag", float, "%.3f"
entry = iatCorrection, "fuel: IAT correction", float, "%.3f" entry = iatCorrection, "fuel: IAT correction", float, "%.3f"
entry = cltCorrection, "fuel: CLT correction", float, "%.3f" entry = cltCorrection, "fuel: CLT correction", float, "%.3f"
entry = baroCorrection, "fuel: Barometric pressure 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 = wallFuelAmount, "fuel: wall amount", float, "%.3f"
entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f" entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f"
entry = revolutionCounterSinceStart, "revolutionCounterSinceStart", int, "%d" entry = revolutionCounterSinceStart, "revolutionCounterSinceStart", int, "%d"
@ -404,7 +403,7 @@ 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_DIFF, "mapVvt_MAP_AT_DIFF", float, "%.3f"
entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d" entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d"
entry = mapVvt_map_peak, "mapVvt_map_peak", 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 = totalRevolutionCounter, "Crank revolution counter", int, "%d"
entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f" entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f"
entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f" entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f"

2
firmware/console/binary/generated/gauges.ini
View File

@ -66,7 +66,6 @@ injectorLagMsGauge = injectorLagMs,"fuel: injector lag", "ms", 0.0,0.0, 0.0,0.0,
iatCorrectionGauge = iatCorrection,"fuel: IAT correction", "%", 0.0,0.0, 0.0,0.0, 0.0,0.0, 0,0 iatCorrectionGauge = iatCorrection,"fuel: IAT correction", "%", 0.0,0.0, 0.0,0.0, 0.0,0.0, 0,0
cltCorrectionGauge = cltCorrection,"fuel: CLT correction", "%", 0.0,0.0, 0.0,0.0, 0.0,0.0, 0,0 cltCorrectionGauge = cltCorrection,"fuel: CLT correction", "%", 0.0,0.0, 0.0,0.0, 0.0,0.0, 0,0
baroCorrectionGauge = baroCorrection,"fuel: Barometric pressure correction", "%", 0.0,0.0, 0.0,0.0, 0.0,0.0, 0,0 baroCorrectionGauge = baroCorrection,"fuel: Barometric pressure correction", "%", 0.0,0.0, 0.0,0.0, 0.0,0.0, 0,0
currentEnginePhaseGauge = currentEnginePhase,"Engine Phase", "deg", 0.0,0.0, 0.0,0.0, 0.0,0.0, 0,0
wallFuelAmountGauge = wallFuelAmount,"fuel: wall amount", "mg", 0.0,0.0, 0.0,0.0, 0.0,0.0, 0,0 wallFuelAmountGauge = wallFuelAmount,"fuel: wall amount", "mg", 0.0,0.0, 0.0,0.0, 0.0,0.0, 0,0
wallFuelCorrectionGauge = wallFuelCorrection,"fuel: wall correction", "mg", 0.0,0.0, 0.0,0.0, 0.0,0.0, 0,0 wallFuelCorrectionGauge = wallFuelCorrection,"fuel: wall correction", "mg", 0.0,0.0, 0.0,0.0, 0.0,0.0, 0,0
revolutionCounterSinceStartGauge = revolutionCounterSinceStart,"revolutionCounterSinceStart", "", 0.0,0.0, 0.0,0.0, 0.0,0.0, 0,0 revolutionCounterSinceStartGauge = revolutionCounterSinceStart,"revolutionCounterSinceStart", "", 0.0,0.0, 0.0,0.0, 0.0,0.0, 0,0
@ -85,6 +84,7 @@ totalFuelConsumptionGauge = totalFuelConsumption,"fuel: Total consumed", "grams"
fuelFlowRateGauge = fuelFlowRate,"fuel: Flow rate", "gram/s", 0.0,0.0, 0.0,0.0, 0.0,0.0, 0,0 fuelFlowRateGauge = fuelFlowRate,"fuel: Flow rate", "gram/s", 0.0,0.0, 0.0,0.0, 0.0,0.0, 0,0
veTableYAxisGauge = veTableYAxis,"veTableYAxis", "%", 0.0,0.0, 0.0,0.0, 0.0,0.0, 0,0 veTableYAxisGauge = veTableYAxis,"veTableYAxis", "%", 0.0,0.0, 0.0,0.0, 0.0,0.0, 0,0
afrTableYAxisGauge = afrTableYAxis,"afrTableYAxis", "%", 0.0,0.0, 0.0,0.0, 0.0,0.0, 0,0 afrTableYAxisGauge = afrTableYAxis,"afrTableYAxis", "%", 0.0,0.0, 0.0,0.0, 0.0,0.0, 0,0
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
knockLevelGauge = knockLevel,"knock: current level", "Volts", 0.0,0.0, 0.0,0.0, 0.0,0.0, 0,0 knockLevelGauge = knockLevel,"knock: current level", "Volts", 0.0,0.0, 0.0,0.0, 0.0,0.0, 0,0
secondsGauge = seconds,"Uptime", "sec", 0.0,0.0, 0.0,0.0, 0.0,0.0, 0,0 secondsGauge = seconds,"Uptime", "sec", 0.0,0.0, 0.0,0.0, 0.0,0.0, 0,0
engineModeGauge = engineMode,"Engine Mode", "em", 0.0,0.0, 0.0,0.0, 0.0,0.0, 0,0 engineModeGauge = engineMode,"Engine Mode", "em", 0.0,0.0, 0.0,0.0, 0.0,0.0, 0,0

37
firmware/console/binary/generated/output_channels.ini
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@ -66,25 +66,24 @@ injectorLagMs = scalar, U16, 62, "ms", 0.0033333333333333335, 0
iatCorrection = scalar, U16, 64, "%", 0.01, 0 iatCorrection = scalar, U16, 64, "%", 0.01, 0
cltCorrection = scalar, U16, 66, "%", 0.01, 0 cltCorrection = scalar, U16, 66, "%", 0.01, 0
baroCorrection = scalar, U16, 68, "%", 0.01, 0 baroCorrection = scalar, U16, 68, "%", 0.01, 0
currentEnginePhase = scalar, U16, 70, "deg", 1, 0 wallFuelAmount = scalar, U16, 70, "mg", 0.01, 0
wallFuelAmount = scalar, U16, 72, "mg", 0.01, 0 wallFuelCorrection = scalar, S16, 72, "mg", 0.01, 0
wallFuelCorrection = scalar, S16, 74, "mg", 0.01, 0 revolutionCounterSinceStart = scalar, U16, 74, "", 1, 0
revolutionCounterSinceStart = scalar, U16, 76, "", 1, 0 deltaTps = scalar, S16, 76, "ratio", 0.01, 0
deltaTps = scalar, S16, 78, "ratio", 0.01, 0 canReadCounter = scalar, U16, 78, "", 1, 0
canReadCounter = scalar, U16, 80, "", 1, 0 tpsAccelFuel = scalar, S16, 80, "ms", 0.0033333333333333335, 0
tpsAccelFuel = scalar, S16, 82, "ms", 0.0033333333333333335, 0 ignitionAdvance = scalar, S16, 82, "deg", 0.02, 0
ignitionAdvance = scalar, S16, 84, "deg", 0.02, 0 sparkDwellValue = scalar, U16, 84, "ms", 0.0033333333333333335, 0
sparkDwellValue = scalar, U16, 86, "ms", 0.0033333333333333335, 0 coilDutyCycle = scalar, U16, 86, "%", 0.01, 0
coilDutyCycle = scalar, U16, 88, "%", 0.01, 0 idleAirValvePosition = scalar, U16, 88, "%", 0.01, 0
idleAirValvePosition = scalar, U16, 90, "%", 0.01, 0 etbTarget = scalar, S16, 90, "%", 0.01, 0
etbTarget = scalar, S16, 92, "%", 0.01, 0 etb1DutyCycle = scalar, S16, 92, "%", 0.01, 0
etb1DutyCycle = scalar, S16, 94, "%", 0.01, 0 etb1Error = scalar, S16, 94, "%", 0.01, 0
etb1Error = scalar, S16, 96, "%", 0.01, 0 fuelTankLevel = scalar, S16, 96, "%", 0.01, 0
fuelTankLevel = scalar, S16, 98, "%", 0.01, 0 totalFuelConsumption = scalar, U16, 98, "grams", 1, 0
totalFuelConsumption = scalar, U16, 100, "grams", 1, 0 fuelFlowRate = scalar, U16, 100, "gram/s", 0.005, 0
fuelFlowRate = scalar, U16, 102, "gram/s", 0.005, 0 veTableYAxis = scalar, U16, 102, "%", 0.01, 0
veTableYAxis = scalar, U16, 104, "%", 0.01, 0 afrTableYAxis = scalar, U16, 104, "%", 0.01, 0
afrTableYAxis = scalar, U16, 106, "%", 0.01, 0
knockLevel = scalar, F32, 108, "Volts", 1, 0 knockLevel = scalar, F32, 108, "Volts", 1, 0
seconds = scalar, U32, 112, "sec", 1, 0 seconds = scalar, U32, 112, "sec", 1, 0
engineMode = scalar, U32, 116, "em", 1, 0 engineMode = scalar, U32, 116, "em", 1, 0

40
firmware/console/binary/generated/sensors.java
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@ -34,25 +34,25 @@ injectorLagMs("fuel: injector lag", SensorCategory.SENSOR_INPUTS, FieldType.INT1
iatCorrection("fuel: IAT correction", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 64, 0.01, 0.0, 0.0, "%"), iatCorrection("fuel: IAT correction", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 64, 0.01, 0.0, 0.0, "%"),
cltCorrection("fuel: CLT correction", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 66, 0.01, 0.0, 0.0, "%"), cltCorrection("fuel: CLT correction", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 66, 0.01, 0.0, 0.0, "%"),
baroCorrection("fuel: Barometric pressure correction", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 68, 0.01, 0.0, 0.0, "%"), baroCorrection("fuel: Barometric pressure correction", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 68, 0.01, 0.0, 0.0, "%"),
currentEnginePhase("Engine Phase", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 70, 1.0, 0.0, 0.0, "deg"), wallFuelAmount("fuel: wall amount", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 70, 0.01, 0.0, 0.0, "mg"),
wallFuelAmount("fuel: wall amount", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 72, 0.01, 0.0, 0.0, "mg"), wallFuelCorrection("fuel: wall correction", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 72, 0.01, 0.0, 0.0, "mg"),
wallFuelCorrection("fuel: wall correction", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 74, 0.01, 0.0, 0.0, "mg"), revolutionCounterSinceStart("revolutionCounterSinceStart", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 74, 1.0, 0.0, 0.0, ""),
revolutionCounterSinceStart("revolutionCounterSinceStart", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 76, 1.0, 0.0, 0.0, ""), deltaTps("fuel: TPS change", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 76, 0.01, 0.0, 0.0, "ratio"),
deltaTps("fuel: TPS change", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 78, 0.01, 0.0, 0.0, "ratio"), canReadCounter("canReadCounter", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 78, 1.0, 0.0, 0.0, ""),
canReadCounter("canReadCounter", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 80, 1.0, 0.0, 0.0, ""), tpsAccelFuel("fuel: TPS acceleration extra fuel ms", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 80, 0.0033333333333333335, 0.0, 0.0, "ms"),
tpsAccelFuel("fuel: TPS acceleration extra fuel ms", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 82, 0.0033333333333333335, 0.0, 0.0, "ms"), ignitionAdvance("timing", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 82, 0.02, 0.0, 0.0, "deg"),
ignitionAdvance("timing", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 84, 0.02, 0.0, 0.0, "deg"), sparkDwellValue("dwell: coil charge time", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 84, 0.0033333333333333335, 0.0, 0.0, "ms"),
sparkDwellValue("dwell: coil charge time", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 86, 0.0033333333333333335, 0.0, 0.0, "ms"), coilDutyCycle("dwell: coil duty cycle", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 86, 0.01, 0.0, 0.0, "%"),
coilDutyCycle("dwell: coil duty cycle", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 88, 0.01, 0.0, 0.0, "%"), idleAirValvePosition("Idle Air Valve", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 88, 0.01, 0.0, 0.0, "%"),
idleAirValvePosition("Idle Air Valve", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 90, 0.01, 0.0, 0.0, "%"), etbTarget("ETB Target", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 90, 0.01, 0.0, 0.0, "%"),
etbTarget("ETB Target", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 92, 0.01, 0.0, 0.0, "%"), etb1DutyCycle("ETB Duty", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 92, 0.01, 0.0, 0.0, "%"),
etb1DutyCycle("ETB Duty", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 94, 0.01, 0.0, 0.0, "%"), etb1Error("ETB Error", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 94, 0.01, 0.0, 0.0, "%"),
etb1Error("ETB Error", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 96, 0.01, 0.0, 0.0, "%"), fuelTankLevel("Fuel level", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 96, 0.01, 0.0, 0.0, "%"),
fuelTankLevel("Fuel level", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 98, 0.01, 0.0, 0.0, "%"), totalFuelConsumption("fuel: Total consumed", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 98, 1.0, 0.0, 0.0, "grams"),
totalFuelConsumption("fuel: Total consumed", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 100, 1.0, 0.0, 0.0, "grams"), fuelFlowRate("fuel: Flow rate", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 100, 0.005, 0.0, 0.0, "gram/s"),
fuelFlowRate("fuel: Flow rate", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 102, 0.005, 0.0, 0.0, "gram/s"), veTableYAxis("veTableYAxis", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 102, 0.01, 0.0, 0.0, "%"),
veTableYAxis("veTableYAxis", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 104, 0.01, 0.0, 0.0, "%"), afrTableYAxis("afrTableYAxis", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 104, 0.01, 0.0, 0.0, "%"),
afrTableYAxis("afrTableYAxis", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 106, 0.01, 0.0, 0.0, "%"), alignmentFill_at_106("need 4 byte alignment", SensorCategory.SENSOR_INPUTS, FieldType.INT8, 106, 1.0, -20.0, 100.0, "units"),
knockLevel("knock: current level", SensorCategory.SENSOR_INPUTS, FieldType.INT, 108, 1.0, 0.0, 0.0, "Volts"), knockLevel("knock: current level", SensorCategory.SENSOR_INPUTS, FieldType.INT, 108, 1.0, 0.0, 0.0, "Volts"),
seconds("Uptime", SensorCategory.SENSOR_INPUTS, FieldType.INT, 112, 1.0, 0.0, 0.0, "sec"), seconds("Uptime", SensorCategory.SENSOR_INPUTS, FieldType.INT, 112, 1.0, 0.0, 0.0, "sec"),
engineMode("Engine Mode", SensorCategory.SENSOR_INPUTS, FieldType.INT, 116, 1.0, 0.0, 0.0, "em"), engineMode("Engine Mode", SensorCategory.SENSOR_INPUTS, FieldType.INT, 116, 1.0, 0.0, 0.0, "em"),
@ -453,7 +453,7 @@ mapVvt_MAP_AT_SPECIAL_POINT("mapVvt_MAP_AT_SPECIAL_POINT", SensorCategory.SENSOR
mapVvt_MAP_AT_DIFF("mapVvt_MAP_AT_DIFF", SensorCategory.SENSOR_INPUTS, FieldType.INT, 1100, 1.0, -10000.0, 10000.0, ""), mapVvt_MAP_AT_DIFF("mapVvt_MAP_AT_DIFF", SensorCategory.SENSOR_INPUTS, FieldType.INT, 1100, 1.0, -10000.0, 10000.0, ""),
mapVvt_MAP_AT_CYCLE_COUNT("mapVvt_MAP_AT_CYCLE_COUNT", SensorCategory.SENSOR_INPUTS, FieldType.INT8, 1104, 1.0, -10000.0, 10000.0, ""), mapVvt_MAP_AT_CYCLE_COUNT("mapVvt_MAP_AT_CYCLE_COUNT", SensorCategory.SENSOR_INPUTS, FieldType.INT8, 1104, 1.0, -10000.0, 10000.0, ""),
mapVvt_map_peak("mapVvt_map_peak", SensorCategory.SENSOR_INPUTS, FieldType.INT8, 1105, 1.0, -10000.0, 10000.0, ""), mapVvt_map_peak("mapVvt_map_peak", SensorCategory.SENSOR_INPUTS, FieldType.INT8, 1105, 1.0, -10000.0, 10000.0, ""),
currentEngineDecodedPhase("Engine Phase2", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 1106, 1.0, 0.0, 0.0, "deg"), currentEngineDecodedPhase("Engine Phase", SensorCategory.SENSOR_INPUTS, FieldType.INT16, 1106, 1.0, 0.0, 0.0, "deg"),
totalRevolutionCounter("Crank revolution counter", SensorCategory.SENSOR_INPUTS, FieldType.INT, 1108, 1.0, -1.0, -1.0, ""), totalRevolutionCounter("Crank revolution counter", SensorCategory.SENSOR_INPUTS, FieldType.INT, 1108, 1.0, -1.0, -1.0, ""),
vvtSyncGapRatio("vvtSyncGapRatio", SensorCategory.SENSOR_INPUTS, FieldType.INT, 1112, 1.0, -10000.0, 10000.0, ""), vvtSyncGapRatio("vvtSyncGapRatio", SensorCategory.SENSOR_INPUTS, FieldType.INT, 1112, 1.0, -10000.0, 10000.0, ""),
vvtCurrentPosition("vvtCurrentPosition", SensorCategory.SENSOR_INPUTS, FieldType.INT, 1116, 1.0, -10000.0, 10000.0, ""), vvtCurrentPosition("vvtCurrentPosition", SensorCategory.SENSOR_INPUTS, FieldType.INT, 1116, 1.0, -10000.0, 10000.0, ""),

52
firmware/console/binary/output_channels_generated.h
View File

@ -1,4 +1,4 @@
// 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
// by class com.rusefi.output.CHeaderConsumer // by class com.rusefi.output.CHeaderConsumer
// begin // begin
#pragma once #pragma once
@ -342,114 +342,114 @@ struct output_channels_s {
* offset 68 * offset 68
*/ */
scaled_channel<uint16_t, 100, 1> baroCorrection = (uint16_t)0; scaled_channel<uint16_t, 100, 1> baroCorrection = (uint16_t)0;
/**
* Engine Phase
deg
* offset 70
*/
scaled_channel<uint16_t, 1, 1> unusedCurrentEnginePhase = (uint16_t)0;
/** /**
* @@GAUGE_NAME_FUEL_WALL_AMOUNT@@ * @@GAUGE_NAME_FUEL_WALL_AMOUNT@@
mg mg
* offset 72 * offset 70
*/ */
scaled_channel<uint16_t, 100, 1> wallFuelAmount = (uint16_t)0; scaled_channel<uint16_t, 100, 1> wallFuelAmount = (uint16_t)0;
/** /**
* @@GAUGE_NAME_FUEL_WALL_CORRECTION@@ * @@GAUGE_NAME_FUEL_WALL_CORRECTION@@
mg mg
* offset 74 * offset 72
*/ */
scaled_channel<int16_t, 100, 1> wallFuelCorrection = (int16_t)0; scaled_channel<int16_t, 100, 1> wallFuelCorrection = (int16_t)0;
/** /**
* offset 76 * offset 74
*/ */
uint16_t revolutionCounterSinceStart = (uint16_t)0; uint16_t revolutionCounterSinceStart = (uint16_t)0;
/** /**
* @@GAUGE_NAME_FUEL_TPS_ROC@@ * @@GAUGE_NAME_FUEL_TPS_ROC@@
ratio ratio
* offset 78 * offset 76
*/ */
scaled_channel<int16_t, 100, 1> deltaTps = (int16_t)0; scaled_channel<int16_t, 100, 1> deltaTps = (int16_t)0;
/** /**
* offset 80 * offset 78
*/ */
uint16_t canReadCounter = (uint16_t)0; uint16_t canReadCounter = (uint16_t)0;
/** /**
* @@GAUGE_NAME_FUEL_TPS_EXTRA@@ * @@GAUGE_NAME_FUEL_TPS_EXTRA@@
ms ms
* offset 82 * offset 80
*/ */
scaled_channel<int16_t, 300, 1> tpsAccelFuel = (int16_t)0; scaled_channel<int16_t, 300, 1> tpsAccelFuel = (int16_t)0;
/** /**
* @@GAUGE_NAME_TIMING_ADVANCE@@ * @@GAUGE_NAME_TIMING_ADVANCE@@
deg deg
* offset 84 * offset 82
*/ */
scaled_channel<int16_t, 50, 1> ignitionAdvance = (int16_t)0; scaled_channel<int16_t, 50, 1> ignitionAdvance = (int16_t)0;
/** /**
* @@GAUGE_COIL_DWELL_TIME@@ * @@GAUGE_COIL_DWELL_TIME@@
ms ms
* offset 86 * offset 84
*/ */
scaled_channel<uint16_t, 300, 1> sparkDwellValue = (uint16_t)0; scaled_channel<uint16_t, 300, 1> sparkDwellValue = (uint16_t)0;
/** /**
* @@GAUGE_NAME_DWELL_DUTY@@ * @@GAUGE_NAME_DWELL_DUTY@@
% %
* offset 88 * offset 86
*/ */
scaled_channel<uint16_t, 100, 1> coilDutyCycle = (uint16_t)0; scaled_channel<uint16_t, 100, 1> coilDutyCycle = (uint16_t)0;
/** /**
* @@GAUGE_NAME_IAC@@ * @@GAUGE_NAME_IAC@@
% %
* offset 90 * offset 88
*/ */
scaled_channel<uint16_t, 100, 1> idleAirValvePosition = (uint16_t)0; scaled_channel<uint16_t, 100, 1> idleAirValvePosition = (uint16_t)0;
/** /**
* ETB Target * ETB Target
% %
* offset 92 * offset 90
*/ */
scaled_channel<int16_t, 100, 1> etbTarget = (int16_t)0; scaled_channel<int16_t, 100, 1> etbTarget = (int16_t)0;
/** /**
* @@GAUGE_NAME_ETB_DUTY@@ * @@GAUGE_NAME_ETB_DUTY@@
% %
* offset 94 * offset 92
*/ */
scaled_channel<int16_t, 100, 1> etb1DutyCycle = (int16_t)0; scaled_channel<int16_t, 100, 1> etb1DutyCycle = (int16_t)0;
/** /**
* ETB Error * ETB Error
% %
* offset 96 * offset 94
*/ */
scaled_channel<int16_t, 100, 1> etb1Error = (int16_t)0; scaled_channel<int16_t, 100, 1> etb1Error = (int16_t)0;
/** /**
* Fuel level * Fuel level
% %
* offset 98 * offset 96
*/ */
scaled_channel<int16_t, 100, 1> fuelTankLevel = (int16_t)0; scaled_channel<int16_t, 100, 1> fuelTankLevel = (int16_t)0;
/** /**
* @@GAUGE_NAME_FUEL_CONSUMPTION@@ * @@GAUGE_NAME_FUEL_CONSUMPTION@@
grams grams
* offset 100 * offset 98
*/ */
scaled_channel<uint16_t, 1, 1> totalFuelConsumption = (uint16_t)0; scaled_channel<uint16_t, 1, 1> totalFuelConsumption = (uint16_t)0;
/** /**
* @@GAUGE_NAME_FUEL_FLOW@@ * @@GAUGE_NAME_FUEL_FLOW@@
gram/s gram/s
* offset 102 * offset 100
*/ */
scaled_channel<uint16_t, 200, 1> fuelFlowRate = (uint16_t)0; scaled_channel<uint16_t, 200, 1> fuelFlowRate = (uint16_t)0;
/** /**
% %
* offset 104 * offset 102
*/ */
scaled_channel<uint16_t, 100, 1> veTableYAxis = (uint16_t)0; scaled_channel<uint16_t, 100, 1> veTableYAxis = (uint16_t)0;
/** /**
% %
* offset 106 * offset 104
*/ */
scaled_channel<uint16_t, 100, 1> afrTableYAxis = (uint16_t)0; scaled_channel<uint16_t, 100, 1> afrTableYAxis = (uint16_t)0;
/**
* need 4 byte alignment
units
* offset 106
*/
uint8_t alignmentFill_at_106[2];
/** /**
* @@GAUGE_NAME_KNOCK_LEVEL@@ * @@GAUGE_NAME_KNOCK_LEVEL@@
Volts Volts
@ -1318,4 +1318,4 @@ struct output_channels_s {
static_assert(sizeof(output_channels_s) == 756); static_assert(sizeof(output_channels_s) == 756);
// end // 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

6
firmware/controllers/trigger/trigger_central_generated.h
View File

@ -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 // by class com.rusefi.output.CHeaderConsumer
// begin // begin
#pragma once #pragma once
@ -32,7 +32,7 @@ struct trigger_central_s {
*/ */
uint8_t mapVvt_map_peak = (uint8_t)0; uint8_t mapVvt_map_peak = (uint8_t)0;
/** /**
* Engine Phase2 * Engine Phase
deg deg
* offset 38 * offset 38
*/ */
@ -41,4 +41,4 @@ struct trigger_central_s {
static_assert(sizeof(trigger_central_s) == 40); static_assert(sizeof(trigger_central_s) == 40);
// end // 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

42
firmware/tunerstudio/generated/rusefi.ini
View File

@ -86,7 +86,7 @@ enable2ndByteCanID = false
; name = scalar, type, offset, units, scale, translate, lo, hi, digits ; name = scalar, type, offset, units, scale, translate, lo, hi, digits
; CONFIG_DEFINITION_START ; 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 pageSize = 21300
page = 1 page = 1
@ -2192,25 +2192,24 @@ injectorLagMs = scalar, U16, 62, "ms", 0.0033333333333333335, 0
iatCorrection = scalar, U16, 64, "%", 0.01, 0 iatCorrection = scalar, U16, 64, "%", 0.01, 0
cltCorrection = scalar, U16, 66, "%", 0.01, 0 cltCorrection = scalar, U16, 66, "%", 0.01, 0
baroCorrection = scalar, U16, 68, "%", 0.01, 0 baroCorrection = scalar, U16, 68, "%", 0.01, 0
currentEnginePhase = scalar, U16, 70, "deg", 1, 0 wallFuelAmount = scalar, U16, 70, "mg", 0.01, 0
wallFuelAmount = scalar, U16, 72, "mg", 0.01, 0 wallFuelCorrection = scalar, S16, 72, "mg", 0.01, 0
wallFuelCorrection = scalar, S16, 74, "mg", 0.01, 0 revolutionCounterSinceStart = scalar, U16, 74, "", 1, 0
revolutionCounterSinceStart = scalar, U16, 76, "", 1, 0 deltaTps = scalar, S16, 76, "ratio", 0.01, 0
deltaTps = scalar, S16, 78, "ratio", 0.01, 0 canReadCounter = scalar, U16, 78, "", 1, 0
canReadCounter = scalar, U16, 80, "", 1, 0 tpsAccelFuel = scalar, S16, 80, "ms", 0.0033333333333333335, 0
tpsAccelFuel = scalar, S16, 82, "ms", 0.0033333333333333335, 0 ignitionAdvance = scalar, S16, 82, "deg", 0.02, 0
ignitionAdvance = scalar, S16, 84, "deg", 0.02, 0 sparkDwellValue = scalar, U16, 84, "ms", 0.0033333333333333335, 0
sparkDwellValue = scalar, U16, 86, "ms", 0.0033333333333333335, 0 coilDutyCycle = scalar, U16, 86, "%", 0.01, 0
coilDutyCycle = scalar, U16, 88, "%", 0.01, 0 idleAirValvePosition = scalar, U16, 88, "%", 0.01, 0
idleAirValvePosition = scalar, U16, 90, "%", 0.01, 0 etbTarget = scalar, S16, 90, "%", 0.01, 0
etbTarget = scalar, S16, 92, "%", 0.01, 0 etb1DutyCycle = scalar, S16, 92, "%", 0.01, 0
etb1DutyCycle = scalar, S16, 94, "%", 0.01, 0 etb1Error = scalar, S16, 94, "%", 0.01, 0
etb1Error = scalar, S16, 96, "%", 0.01, 0 fuelTankLevel = scalar, S16, 96, "%", 0.01, 0
fuelTankLevel = scalar, S16, 98, "%", 0.01, 0 totalFuelConsumption = scalar, U16, 98, "grams", 1, 0
totalFuelConsumption = scalar, U16, 100, "grams", 1, 0 fuelFlowRate = scalar, U16, 100, "gram/s", 0.005, 0
fuelFlowRate = scalar, U16, 102, "gram/s", 0.005, 0 veTableYAxis = scalar, U16, 102, "%", 0.01, 0
veTableYAxis = scalar, U16, 104, "%", 0.01, 0 afrTableYAxis = scalar, U16, 104, "%", 0.01, 0
afrTableYAxis = scalar, U16, 106, "%", 0.01, 0
knockLevel = scalar, F32, 108, "Volts", 1, 0 knockLevel = scalar, F32, 108, "Volts", 1, 0
seconds = scalar, U32, 112, "sec", 1, 0 seconds = scalar, U32, 112, "sec", 1, 0
engineMode = scalar, U32, 116, "em", 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 = iatCorrection, "fuel: IAT correction", float, "%.3f"
entry = cltCorrection, "fuel: CLT correction", float, "%.3f" entry = cltCorrection, "fuel: CLT correction", float, "%.3f"
entry = baroCorrection, "fuel: Barometric pressure 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 = wallFuelAmount, "fuel: wall amount", float, "%.3f"
entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f" entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f"
entry = revolutionCounterSinceStart, "revolutionCounterSinceStart", int, "%d" 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_DIFF, "mapVvt_MAP_AT_DIFF", float, "%.3f"
entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d" entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d"
entry = mapVvt_map_peak, "mapVvt_map_peak", 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 = totalRevolutionCounter, "Crank revolution counter", int, "%d"
entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f" entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f"
entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f" entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f"

42
firmware/tunerstudio/generated/rusefi_48way.ini
View File

@ -86,7 +86,7 @@ enable2ndByteCanID = false
; name = scalar, type, offset, units, scale, translate, lo, hi, digits ; name = scalar, type, offset, units, scale, translate, lo, hi, digits
; CONFIG_DEFINITION_START ; 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 pageSize = 21300
page = 1 page = 1
@ -2192,25 +2192,24 @@ injectorLagMs = scalar, U16, 62, "ms", 0.0033333333333333335, 0
iatCorrection = scalar, U16, 64, "%", 0.01, 0 iatCorrection = scalar, U16, 64, "%", 0.01, 0
cltCorrection = scalar, U16, 66, "%", 0.01, 0 cltCorrection = scalar, U16, 66, "%", 0.01, 0
baroCorrection = scalar, U16, 68, "%", 0.01, 0 baroCorrection = scalar, U16, 68, "%", 0.01, 0
currentEnginePhase = scalar, U16, 70, "deg", 1, 0 wallFuelAmount = scalar, U16, 70, "mg", 0.01, 0
wallFuelAmount = scalar, U16, 72, "mg", 0.01, 0 wallFuelCorrection = scalar, S16, 72, "mg", 0.01, 0
wallFuelCorrection = scalar, S16, 74, "mg", 0.01, 0 revolutionCounterSinceStart = scalar, U16, 74, "", 1, 0
revolutionCounterSinceStart = scalar, U16, 76, "", 1, 0 deltaTps = scalar, S16, 76, "ratio", 0.01, 0
deltaTps = scalar, S16, 78, "ratio", 0.01, 0 canReadCounter = scalar, U16, 78, "", 1, 0
canReadCounter = scalar, U16, 80, "", 1, 0 tpsAccelFuel = scalar, S16, 80, "ms", 0.0033333333333333335, 0
tpsAccelFuel = scalar, S16, 82, "ms", 0.0033333333333333335, 0 ignitionAdvance = scalar, S16, 82, "deg", 0.02, 0
ignitionAdvance = scalar, S16, 84, "deg", 0.02, 0 sparkDwellValue = scalar, U16, 84, "ms", 0.0033333333333333335, 0
sparkDwellValue = scalar, U16, 86, "ms", 0.0033333333333333335, 0 coilDutyCycle = scalar, U16, 86, "%", 0.01, 0
coilDutyCycle = scalar, U16, 88, "%", 0.01, 0 idleAirValvePosition = scalar, U16, 88, "%", 0.01, 0
idleAirValvePosition = scalar, U16, 90, "%", 0.01, 0 etbTarget = scalar, S16, 90, "%", 0.01, 0
etbTarget = scalar, S16, 92, "%", 0.01, 0 etb1DutyCycle = scalar, S16, 92, "%", 0.01, 0
etb1DutyCycle = scalar, S16, 94, "%", 0.01, 0 etb1Error = scalar, S16, 94, "%", 0.01, 0
etb1Error = scalar, S16, 96, "%", 0.01, 0 fuelTankLevel = scalar, S16, 96, "%", 0.01, 0
fuelTankLevel = scalar, S16, 98, "%", 0.01, 0 totalFuelConsumption = scalar, U16, 98, "grams", 1, 0
totalFuelConsumption = scalar, U16, 100, "grams", 1, 0 fuelFlowRate = scalar, U16, 100, "gram/s", 0.005, 0
fuelFlowRate = scalar, U16, 102, "gram/s", 0.005, 0 veTableYAxis = scalar, U16, 102, "%", 0.01, 0
veTableYAxis = scalar, U16, 104, "%", 0.01, 0 afrTableYAxis = scalar, U16, 104, "%", 0.01, 0
afrTableYAxis = scalar, U16, 106, "%", 0.01, 0
knockLevel = scalar, F32, 108, "Volts", 1, 0 knockLevel = scalar, F32, 108, "Volts", 1, 0
seconds = scalar, U32, 112, "sec", 1, 0 seconds = scalar, U32, 112, "sec", 1, 0
engineMode = scalar, U32, 116, "em", 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 = iatCorrection, "fuel: IAT correction", float, "%.3f"
entry = cltCorrection, "fuel: CLT correction", float, "%.3f" entry = cltCorrection, "fuel: CLT correction", float, "%.3f"
entry = baroCorrection, "fuel: Barometric pressure 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 = wallFuelAmount, "fuel: wall amount", float, "%.3f"
entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f" entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f"
entry = revolutionCounterSinceStart, "revolutionCounterSinceStart", int, "%d" 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_DIFF, "mapVvt_MAP_AT_DIFF", float, "%.3f"
entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d" entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d"
entry = mapVvt_map_peak, "mapVvt_map_peak", 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 = totalRevolutionCounter, "Crank revolution counter", int, "%d"
entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f" entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f"
entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f" entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f"

42
firmware/tunerstudio/generated/rusefi_alphax-2chan.ini
View File

@ -86,7 +86,7 @@ enable2ndByteCanID = false
; name = scalar, type, offset, units, scale, translate, lo, hi, digits ; name = scalar, type, offset, units, scale, translate, lo, hi, digits
; CONFIG_DEFINITION_START ; 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 pageSize = 21300
page = 1 page = 1
@ -2192,25 +2192,24 @@ injectorLagMs = scalar, U16, 62, "ms", 0.0033333333333333335, 0
iatCorrection = scalar, U16, 64, "%", 0.01, 0 iatCorrection = scalar, U16, 64, "%", 0.01, 0
cltCorrection = scalar, U16, 66, "%", 0.01, 0 cltCorrection = scalar, U16, 66, "%", 0.01, 0
baroCorrection = scalar, U16, 68, "%", 0.01, 0 baroCorrection = scalar, U16, 68, "%", 0.01, 0
currentEnginePhase = scalar, U16, 70, "deg", 1, 0 wallFuelAmount = scalar, U16, 70, "mg", 0.01, 0
wallFuelAmount = scalar, U16, 72, "mg", 0.01, 0 wallFuelCorrection = scalar, S16, 72, "mg", 0.01, 0
wallFuelCorrection = scalar, S16, 74, "mg", 0.01, 0 revolutionCounterSinceStart = scalar, U16, 74, "", 1, 0
revolutionCounterSinceStart = scalar, U16, 76, "", 1, 0 deltaTps = scalar, S16, 76, "ratio", 0.01, 0
deltaTps = scalar, S16, 78, "ratio", 0.01, 0 canReadCounter = scalar, U16, 78, "", 1, 0
canReadCounter = scalar, U16, 80, "", 1, 0 tpsAccelFuel = scalar, S16, 80, "ms", 0.0033333333333333335, 0
tpsAccelFuel = scalar, S16, 82, "ms", 0.0033333333333333335, 0 ignitionAdvance = scalar, S16, 82, "deg", 0.02, 0
ignitionAdvance = scalar, S16, 84, "deg", 0.02, 0 sparkDwellValue = scalar, U16, 84, "ms", 0.0033333333333333335, 0
sparkDwellValue = scalar, U16, 86, "ms", 0.0033333333333333335, 0 coilDutyCycle = scalar, U16, 86, "%", 0.01, 0
coilDutyCycle = scalar, U16, 88, "%", 0.01, 0 idleAirValvePosition = scalar, U16, 88, "%", 0.01, 0
idleAirValvePosition = scalar, U16, 90, "%", 0.01, 0 etbTarget = scalar, S16, 90, "%", 0.01, 0
etbTarget = scalar, S16, 92, "%", 0.01, 0 etb1DutyCycle = scalar, S16, 92, "%", 0.01, 0
etb1DutyCycle = scalar, S16, 94, "%", 0.01, 0 etb1Error = scalar, S16, 94, "%", 0.01, 0
etb1Error = scalar, S16, 96, "%", 0.01, 0 fuelTankLevel = scalar, S16, 96, "%", 0.01, 0
fuelTankLevel = scalar, S16, 98, "%", 0.01, 0 totalFuelConsumption = scalar, U16, 98, "grams", 1, 0
totalFuelConsumption = scalar, U16, 100, "grams", 1, 0 fuelFlowRate = scalar, U16, 100, "gram/s", 0.005, 0
fuelFlowRate = scalar, U16, 102, "gram/s", 0.005, 0 veTableYAxis = scalar, U16, 102, "%", 0.01, 0
veTableYAxis = scalar, U16, 104, "%", 0.01, 0 afrTableYAxis = scalar, U16, 104, "%", 0.01, 0
afrTableYAxis = scalar, U16, 106, "%", 0.01, 0
knockLevel = scalar, F32, 108, "Volts", 1, 0 knockLevel = scalar, F32, 108, "Volts", 1, 0
seconds = scalar, U32, 112, "sec", 1, 0 seconds = scalar, U32, 112, "sec", 1, 0
engineMode = scalar, U32, 116, "em", 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 = iatCorrection, "fuel: IAT correction", float, "%.3f"
entry = cltCorrection, "fuel: CLT correction", float, "%.3f" entry = cltCorrection, "fuel: CLT correction", float, "%.3f"
entry = baroCorrection, "fuel: Barometric pressure 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 = wallFuelAmount, "fuel: wall amount", float, "%.3f"
entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f" entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f"
entry = revolutionCounterSinceStart, "revolutionCounterSinceStart", int, "%d" 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_DIFF, "mapVvt_MAP_AT_DIFF", float, "%.3f"
entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d" entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d"
entry = mapVvt_map_peak, "mapVvt_map_peak", 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 = totalRevolutionCounter, "Crank revolution counter", int, "%d"
entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f" entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f"
entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f" entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f"

42
firmware/tunerstudio/generated/rusefi_alphax-4chan.ini
View File

@ -86,7 +86,7 @@ enable2ndByteCanID = false
; name = scalar, type, offset, units, scale, translate, lo, hi, digits ; name = scalar, type, offset, units, scale, translate, lo, hi, digits
; CONFIG_DEFINITION_START ; 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 pageSize = 21300
page = 1 page = 1
@ -2192,25 +2192,24 @@ injectorLagMs = scalar, U16, 62, "ms", 0.0033333333333333335, 0
iatCorrection = scalar, U16, 64, "%", 0.01, 0 iatCorrection = scalar, U16, 64, "%", 0.01, 0
cltCorrection = scalar, U16, 66, "%", 0.01, 0 cltCorrection = scalar, U16, 66, "%", 0.01, 0
baroCorrection = scalar, U16, 68, "%", 0.01, 0 baroCorrection = scalar, U16, 68, "%", 0.01, 0
currentEnginePhase = scalar, U16, 70, "deg", 1, 0 wallFuelAmount = scalar, U16, 70, "mg", 0.01, 0
wallFuelAmount = scalar, U16, 72, "mg", 0.01, 0 wallFuelCorrection = scalar, S16, 72, "mg", 0.01, 0
wallFuelCorrection = scalar, S16, 74, "mg", 0.01, 0 revolutionCounterSinceStart = scalar, U16, 74, "", 1, 0
revolutionCounterSinceStart = scalar, U16, 76, "", 1, 0 deltaTps = scalar, S16, 76, "ratio", 0.01, 0
deltaTps = scalar, S16, 78, "ratio", 0.01, 0 canReadCounter = scalar, U16, 78, "", 1, 0
canReadCounter = scalar, U16, 80, "", 1, 0 tpsAccelFuel = scalar, S16, 80, "ms", 0.0033333333333333335, 0
tpsAccelFuel = scalar, S16, 82, "ms", 0.0033333333333333335, 0 ignitionAdvance = scalar, S16, 82, "deg", 0.02, 0
ignitionAdvance = scalar, S16, 84, "deg", 0.02, 0 sparkDwellValue = scalar, U16, 84, "ms", 0.0033333333333333335, 0
sparkDwellValue = scalar, U16, 86, "ms", 0.0033333333333333335, 0 coilDutyCycle = scalar, U16, 86, "%", 0.01, 0
coilDutyCycle = scalar, U16, 88, "%", 0.01, 0 idleAirValvePosition = scalar, U16, 88, "%", 0.01, 0
idleAirValvePosition = scalar, U16, 90, "%", 0.01, 0 etbTarget = scalar, S16, 90, "%", 0.01, 0
etbTarget = scalar, S16, 92, "%", 0.01, 0 etb1DutyCycle = scalar, S16, 92, "%", 0.01, 0
etb1DutyCycle = scalar, S16, 94, "%", 0.01, 0 etb1Error = scalar, S16, 94, "%", 0.01, 0
etb1Error = scalar, S16, 96, "%", 0.01, 0 fuelTankLevel = scalar, S16, 96, "%", 0.01, 0
fuelTankLevel = scalar, S16, 98, "%", 0.01, 0 totalFuelConsumption = scalar, U16, 98, "grams", 1, 0
totalFuelConsumption = scalar, U16, 100, "grams", 1, 0 fuelFlowRate = scalar, U16, 100, "gram/s", 0.005, 0
fuelFlowRate = scalar, U16, 102, "gram/s", 0.005, 0 veTableYAxis = scalar, U16, 102, "%", 0.01, 0
veTableYAxis = scalar, U16, 104, "%", 0.01, 0 afrTableYAxis = scalar, U16, 104, "%", 0.01, 0
afrTableYAxis = scalar, U16, 106, "%", 0.01, 0
knockLevel = scalar, F32, 108, "Volts", 1, 0 knockLevel = scalar, F32, 108, "Volts", 1, 0
seconds = scalar, U32, 112, "sec", 1, 0 seconds = scalar, U32, 112, "sec", 1, 0
engineMode = scalar, U32, 116, "em", 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 = iatCorrection, "fuel: IAT correction", float, "%.3f"
entry = cltCorrection, "fuel: CLT correction", float, "%.3f" entry = cltCorrection, "fuel: CLT correction", float, "%.3f"
entry = baroCorrection, "fuel: Barometric pressure 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 = wallFuelAmount, "fuel: wall amount", float, "%.3f"
entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f" entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f"
entry = revolutionCounterSinceStart, "revolutionCounterSinceStart", int, "%d" 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_DIFF, "mapVvt_MAP_AT_DIFF", float, "%.3f"
entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d" entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d"
entry = mapVvt_map_peak, "mapVvt_map_peak", 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 = totalRevolutionCounter, "Crank revolution counter", int, "%d"
entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f" entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f"
entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f" entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f"

42
firmware/tunerstudio/generated/rusefi_atlas.ini
View File

@ -86,7 +86,7 @@ enable2ndByteCanID = false
; name = scalar, type, offset, units, scale, translate, lo, hi, digits ; name = scalar, type, offset, units, scale, translate, lo, hi, digits
; CONFIG_DEFINITION_START ; 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 pageSize = 21300
page = 1 page = 1
@ -2192,25 +2192,24 @@ injectorLagMs = scalar, U16, 62, "ms", 0.0033333333333333335, 0
iatCorrection = scalar, U16, 64, "%", 0.01, 0 iatCorrection = scalar, U16, 64, "%", 0.01, 0
cltCorrection = scalar, U16, 66, "%", 0.01, 0 cltCorrection = scalar, U16, 66, "%", 0.01, 0
baroCorrection = scalar, U16, 68, "%", 0.01, 0 baroCorrection = scalar, U16, 68, "%", 0.01, 0
currentEnginePhase = scalar, U16, 70, "deg", 1, 0 wallFuelAmount = scalar, U16, 70, "mg", 0.01, 0
wallFuelAmount = scalar, U16, 72, "mg", 0.01, 0 wallFuelCorrection = scalar, S16, 72, "mg", 0.01, 0
wallFuelCorrection = scalar, S16, 74, "mg", 0.01, 0 revolutionCounterSinceStart = scalar, U16, 74, "", 1, 0
revolutionCounterSinceStart = scalar, U16, 76, "", 1, 0 deltaTps = scalar, S16, 76, "ratio", 0.01, 0
deltaTps = scalar, S16, 78, "ratio", 0.01, 0 canReadCounter = scalar, U16, 78, "", 1, 0
canReadCounter = scalar, U16, 80, "", 1, 0 tpsAccelFuel = scalar, S16, 80, "ms", 0.0033333333333333335, 0
tpsAccelFuel = scalar, S16, 82, "ms", 0.0033333333333333335, 0 ignitionAdvance = scalar, S16, 82, "deg", 0.02, 0
ignitionAdvance = scalar, S16, 84, "deg", 0.02, 0 sparkDwellValue = scalar, U16, 84, "ms", 0.0033333333333333335, 0
sparkDwellValue = scalar, U16, 86, "ms", 0.0033333333333333335, 0 coilDutyCycle = scalar, U16, 86, "%", 0.01, 0
coilDutyCycle = scalar, U16, 88, "%", 0.01, 0 idleAirValvePosition = scalar, U16, 88, "%", 0.01, 0
idleAirValvePosition = scalar, U16, 90, "%", 0.01, 0 etbTarget = scalar, S16, 90, "%", 0.01, 0
etbTarget = scalar, S16, 92, "%", 0.01, 0 etb1DutyCycle = scalar, S16, 92, "%", 0.01, 0
etb1DutyCycle = scalar, S16, 94, "%", 0.01, 0 etb1Error = scalar, S16, 94, "%", 0.01, 0
etb1Error = scalar, S16, 96, "%", 0.01, 0 fuelTankLevel = scalar, S16, 96, "%", 0.01, 0
fuelTankLevel = scalar, S16, 98, "%", 0.01, 0 totalFuelConsumption = scalar, U16, 98, "grams", 1, 0
totalFuelConsumption = scalar, U16, 100, "grams", 1, 0 fuelFlowRate = scalar, U16, 100, "gram/s", 0.005, 0
fuelFlowRate = scalar, U16, 102, "gram/s", 0.005, 0 veTableYAxis = scalar, U16, 102, "%", 0.01, 0
veTableYAxis = scalar, U16, 104, "%", 0.01, 0 afrTableYAxis = scalar, U16, 104, "%", 0.01, 0
afrTableYAxis = scalar, U16, 106, "%", 0.01, 0
knockLevel = scalar, F32, 108, "Volts", 1, 0 knockLevel = scalar, F32, 108, "Volts", 1, 0
seconds = scalar, U32, 112, "sec", 1, 0 seconds = scalar, U32, 112, "sec", 1, 0
engineMode = scalar, U32, 116, "em", 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 = iatCorrection, "fuel: IAT correction", float, "%.3f"
entry = cltCorrection, "fuel: CLT correction", float, "%.3f" entry = cltCorrection, "fuel: CLT correction", float, "%.3f"
entry = baroCorrection, "fuel: Barometric pressure 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 = wallFuelAmount, "fuel: wall amount", float, "%.3f"
entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f" entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f"
entry = revolutionCounterSinceStart, "revolutionCounterSinceStart", int, "%d" 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_DIFF, "mapVvt_MAP_AT_DIFF", float, "%.3f"
entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d" entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d"
entry = mapVvt_map_peak, "mapVvt_map_peak", 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 = totalRevolutionCounter, "Crank revolution counter", int, "%d"
entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f" entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f"
entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f" entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f"

42
firmware/tunerstudio/generated/rusefi_core8.ini
View File

@ -86,7 +86,7 @@ enable2ndByteCanID = false
; name = scalar, type, offset, units, scale, translate, lo, hi, digits ; name = scalar, type, offset, units, scale, translate, lo, hi, digits
; CONFIG_DEFINITION_START ; 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 pageSize = 21300
page = 1 page = 1
@ -2192,25 +2192,24 @@ injectorLagMs = scalar, U16, 62, "ms", 0.0033333333333333335, 0
iatCorrection = scalar, U16, 64, "%", 0.01, 0 iatCorrection = scalar, U16, 64, "%", 0.01, 0
cltCorrection = scalar, U16, 66, "%", 0.01, 0 cltCorrection = scalar, U16, 66, "%", 0.01, 0
baroCorrection = scalar, U16, 68, "%", 0.01, 0 baroCorrection = scalar, U16, 68, "%", 0.01, 0
currentEnginePhase = scalar, U16, 70, "deg", 1, 0 wallFuelAmount = scalar, U16, 70, "mg", 0.01, 0
wallFuelAmount = scalar, U16, 72, "mg", 0.01, 0 wallFuelCorrection = scalar, S16, 72, "mg", 0.01, 0
wallFuelCorrection = scalar, S16, 74, "mg", 0.01, 0 revolutionCounterSinceStart = scalar, U16, 74, "", 1, 0
revolutionCounterSinceStart = scalar, U16, 76, "", 1, 0 deltaTps = scalar, S16, 76, "ratio", 0.01, 0
deltaTps = scalar, S16, 78, "ratio", 0.01, 0 canReadCounter = scalar, U16, 78, "", 1, 0
canReadCounter = scalar, U16, 80, "", 1, 0 tpsAccelFuel = scalar, S16, 80, "ms", 0.0033333333333333335, 0
tpsAccelFuel = scalar, S16, 82, "ms", 0.0033333333333333335, 0 ignitionAdvance = scalar, S16, 82, "deg", 0.02, 0
ignitionAdvance = scalar, S16, 84, "deg", 0.02, 0 sparkDwellValue = scalar, U16, 84, "ms", 0.0033333333333333335, 0
sparkDwellValue = scalar, U16, 86, "ms", 0.0033333333333333335, 0 coilDutyCycle = scalar, U16, 86, "%", 0.01, 0
coilDutyCycle = scalar, U16, 88, "%", 0.01, 0 idleAirValvePosition = scalar, U16, 88, "%", 0.01, 0
idleAirValvePosition = scalar, U16, 90, "%", 0.01, 0 etbTarget = scalar, S16, 90, "%", 0.01, 0
etbTarget = scalar, S16, 92, "%", 0.01, 0 etb1DutyCycle = scalar, S16, 92, "%", 0.01, 0
etb1DutyCycle = scalar, S16, 94, "%", 0.01, 0 etb1Error = scalar, S16, 94, "%", 0.01, 0
etb1Error = scalar, S16, 96, "%", 0.01, 0 fuelTankLevel = scalar, S16, 96, "%", 0.01, 0
fuelTankLevel = scalar, S16, 98, "%", 0.01, 0 totalFuelConsumption = scalar, U16, 98, "grams", 1, 0
totalFuelConsumption = scalar, U16, 100, "grams", 1, 0 fuelFlowRate = scalar, U16, 100, "gram/s", 0.005, 0
fuelFlowRate = scalar, U16, 102, "gram/s", 0.005, 0 veTableYAxis = scalar, U16, 102, "%", 0.01, 0
veTableYAxis = scalar, U16, 104, "%", 0.01, 0 afrTableYAxis = scalar, U16, 104, "%", 0.01, 0
afrTableYAxis = scalar, U16, 106, "%", 0.01, 0
knockLevel = scalar, F32, 108, "Volts", 1, 0 knockLevel = scalar, F32, 108, "Volts", 1, 0
seconds = scalar, U32, 112, "sec", 1, 0 seconds = scalar, U32, 112, "sec", 1, 0
engineMode = scalar, U32, 116, "em", 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 = iatCorrection, "fuel: IAT correction", float, "%.3f"
entry = cltCorrection, "fuel: CLT correction", float, "%.3f" entry = cltCorrection, "fuel: CLT correction", float, "%.3f"
entry = baroCorrection, "fuel: Barometric pressure 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 = wallFuelAmount, "fuel: wall amount", float, "%.3f"
entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f" entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f"
entry = revolutionCounterSinceStart, "revolutionCounterSinceStart", int, "%d" 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_DIFF, "mapVvt_MAP_AT_DIFF", float, "%.3f"
entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d" entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d"
entry = mapVvt_map_peak, "mapVvt_map_peak", 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 = totalRevolutionCounter, "Crank revolution counter", int, "%d"
entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f" entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f"
entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f" entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f"

42
firmware/tunerstudio/generated/rusefi_cypress.ini
View File

@ -86,7 +86,7 @@ enable2ndByteCanID = false
; name = scalar, type, offset, units, scale, translate, lo, hi, digits ; name = scalar, type, offset, units, scale, translate, lo, hi, digits
; CONFIG_DEFINITION_START ; 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 pageSize = 21300
page = 1 page = 1
@ -2192,25 +2192,24 @@ injectorLagMs = scalar, U16, 62, "ms", 0.0033333333333333335, 0
iatCorrection = scalar, U16, 64, "%", 0.01, 0 iatCorrection = scalar, U16, 64, "%", 0.01, 0
cltCorrection = scalar, U16, 66, "%", 0.01, 0 cltCorrection = scalar, U16, 66, "%", 0.01, 0
baroCorrection = scalar, U16, 68, "%", 0.01, 0 baroCorrection = scalar, U16, 68, "%", 0.01, 0
currentEnginePhase = scalar, U16, 70, "deg", 1, 0 wallFuelAmount = scalar, U16, 70, "mg", 0.01, 0
wallFuelAmount = scalar, U16, 72, "mg", 0.01, 0 wallFuelCorrection = scalar, S16, 72, "mg", 0.01, 0
wallFuelCorrection = scalar, S16, 74, "mg", 0.01, 0 revolutionCounterSinceStart = scalar, U16, 74, "", 1, 0
revolutionCounterSinceStart = scalar, U16, 76, "", 1, 0 deltaTps = scalar, S16, 76, "ratio", 0.01, 0
deltaTps = scalar, S16, 78, "ratio", 0.01, 0 canReadCounter = scalar, U16, 78, "", 1, 0
canReadCounter = scalar, U16, 80, "", 1, 0 tpsAccelFuel = scalar, S16, 80, "ms", 0.0033333333333333335, 0
tpsAccelFuel = scalar, S16, 82, "ms", 0.0033333333333333335, 0 ignitionAdvance = scalar, S16, 82, "deg", 0.02, 0
ignitionAdvance = scalar, S16, 84, "deg", 0.02, 0 sparkDwellValue = scalar, U16, 84, "ms", 0.0033333333333333335, 0
sparkDwellValue = scalar, U16, 86, "ms", 0.0033333333333333335, 0 coilDutyCycle = scalar, U16, 86, "%", 0.01, 0
coilDutyCycle = scalar, U16, 88, "%", 0.01, 0 idleAirValvePosition = scalar, U16, 88, "%", 0.01, 0
idleAirValvePosition = scalar, U16, 90, "%", 0.01, 0 etbTarget = scalar, S16, 90, "%", 0.01, 0
etbTarget = scalar, S16, 92, "%", 0.01, 0 etb1DutyCycle = scalar, S16, 92, "%", 0.01, 0
etb1DutyCycle = scalar, S16, 94, "%", 0.01, 0 etb1Error = scalar, S16, 94, "%", 0.01, 0
etb1Error = scalar, S16, 96, "%", 0.01, 0 fuelTankLevel = scalar, S16, 96, "%", 0.01, 0
fuelTankLevel = scalar, S16, 98, "%", 0.01, 0 totalFuelConsumption = scalar, U16, 98, "grams", 1, 0
totalFuelConsumption = scalar, U16, 100, "grams", 1, 0 fuelFlowRate = scalar, U16, 100, "gram/s", 0.005, 0
fuelFlowRate = scalar, U16, 102, "gram/s", 0.005, 0 veTableYAxis = scalar, U16, 102, "%", 0.01, 0
veTableYAxis = scalar, U16, 104, "%", 0.01, 0 afrTableYAxis = scalar, U16, 104, "%", 0.01, 0
afrTableYAxis = scalar, U16, 106, "%", 0.01, 0
knockLevel = scalar, F32, 108, "Volts", 1, 0 knockLevel = scalar, F32, 108, "Volts", 1, 0
seconds = scalar, U32, 112, "sec", 1, 0 seconds = scalar, U32, 112, "sec", 1, 0
engineMode = scalar, U32, 116, "em", 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 = iatCorrection, "fuel: IAT correction", float, "%.3f"
entry = cltCorrection, "fuel: CLT correction", float, "%.3f" entry = cltCorrection, "fuel: CLT correction", float, "%.3f"
entry = baroCorrection, "fuel: Barometric pressure 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 = wallFuelAmount, "fuel: wall amount", float, "%.3f"
entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f" entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f"
entry = revolutionCounterSinceStart, "revolutionCounterSinceStart", int, "%d" 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_DIFF, "mapVvt_MAP_AT_DIFF", float, "%.3f"
entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d" entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d"
entry = mapVvt_map_peak, "mapVvt_map_peak", 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 = totalRevolutionCounter, "Crank revolution counter", int, "%d"
entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f" entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f"
entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f" entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f"

42
firmware/tunerstudio/generated/rusefi_f407-discovery.ini
View File

@ -86,7 +86,7 @@ enable2ndByteCanID = false
; name = scalar, type, offset, units, scale, translate, lo, hi, digits ; name = scalar, type, offset, units, scale, translate, lo, hi, digits
; CONFIG_DEFINITION_START ; 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 pageSize = 21300
page = 1 page = 1
@ -2192,25 +2192,24 @@ injectorLagMs = scalar, U16, 62, "ms", 0.0033333333333333335, 0
iatCorrection = scalar, U16, 64, "%", 0.01, 0 iatCorrection = scalar, U16, 64, "%", 0.01, 0
cltCorrection = scalar, U16, 66, "%", 0.01, 0 cltCorrection = scalar, U16, 66, "%", 0.01, 0
baroCorrection = scalar, U16, 68, "%", 0.01, 0 baroCorrection = scalar, U16, 68, "%", 0.01, 0
currentEnginePhase = scalar, U16, 70, "deg", 1, 0 wallFuelAmount = scalar, U16, 70, "mg", 0.01, 0
wallFuelAmount = scalar, U16, 72, "mg", 0.01, 0 wallFuelCorrection = scalar, S16, 72, "mg", 0.01, 0
wallFuelCorrection = scalar, S16, 74, "mg", 0.01, 0 revolutionCounterSinceStart = scalar, U16, 74, "", 1, 0
revolutionCounterSinceStart = scalar, U16, 76, "", 1, 0 deltaTps = scalar, S16, 76, "ratio", 0.01, 0
deltaTps = scalar, S16, 78, "ratio", 0.01, 0 canReadCounter = scalar, U16, 78, "", 1, 0
canReadCounter = scalar, U16, 80, "", 1, 0 tpsAccelFuel = scalar, S16, 80, "ms", 0.0033333333333333335, 0
tpsAccelFuel = scalar, S16, 82, "ms", 0.0033333333333333335, 0 ignitionAdvance = scalar, S16, 82, "deg", 0.02, 0
ignitionAdvance = scalar, S16, 84, "deg", 0.02, 0 sparkDwellValue = scalar, U16, 84, "ms", 0.0033333333333333335, 0
sparkDwellValue = scalar, U16, 86, "ms", 0.0033333333333333335, 0 coilDutyCycle = scalar, U16, 86, "%", 0.01, 0
coilDutyCycle = scalar, U16, 88, "%", 0.01, 0 idleAirValvePosition = scalar, U16, 88, "%", 0.01, 0
idleAirValvePosition = scalar, U16, 90, "%", 0.01, 0 etbTarget = scalar, S16, 90, "%", 0.01, 0
etbTarget = scalar, S16, 92, "%", 0.01, 0 etb1DutyCycle = scalar, S16, 92, "%", 0.01, 0
etb1DutyCycle = scalar, S16, 94, "%", 0.01, 0 etb1Error = scalar, S16, 94, "%", 0.01, 0
etb1Error = scalar, S16, 96, "%", 0.01, 0 fuelTankLevel = scalar, S16, 96, "%", 0.01, 0
fuelTankLevel = scalar, S16, 98, "%", 0.01, 0 totalFuelConsumption = scalar, U16, 98, "grams", 1, 0
totalFuelConsumption = scalar, U16, 100, "grams", 1, 0 fuelFlowRate = scalar, U16, 100, "gram/s", 0.005, 0
fuelFlowRate = scalar, U16, 102, "gram/s", 0.005, 0 veTableYAxis = scalar, U16, 102, "%", 0.01, 0
veTableYAxis = scalar, U16, 104, "%", 0.01, 0 afrTableYAxis = scalar, U16, 104, "%", 0.01, 0
afrTableYAxis = scalar, U16, 106, "%", 0.01, 0
knockLevel = scalar, F32, 108, "Volts", 1, 0 knockLevel = scalar, F32, 108, "Volts", 1, 0
seconds = scalar, U32, 112, "sec", 1, 0 seconds = scalar, U32, 112, "sec", 1, 0
engineMode = scalar, U32, 116, "em", 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 = iatCorrection, "fuel: IAT correction", float, "%.3f"
entry = cltCorrection, "fuel: CLT correction", float, "%.3f" entry = cltCorrection, "fuel: CLT correction", float, "%.3f"
entry = baroCorrection, "fuel: Barometric pressure 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 = wallFuelAmount, "fuel: wall amount", float, "%.3f"
entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f" entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f"
entry = revolutionCounterSinceStart, "revolutionCounterSinceStart", int, "%d" 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_DIFF, "mapVvt_MAP_AT_DIFF", float, "%.3f"
entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d" entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d"
entry = mapVvt_map_peak, "mapVvt_map_peak", 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 = totalRevolutionCounter, "Crank revolution counter", int, "%d"
entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f" entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f"
entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f" entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f"

42
firmware/tunerstudio/generated/rusefi_f429-discovery.ini
View File

@ -86,7 +86,7 @@ enable2ndByteCanID = false
; name = scalar, type, offset, units, scale, translate, lo, hi, digits ; name = scalar, type, offset, units, scale, translate, lo, hi, digits
; CONFIG_DEFINITION_START ; 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 pageSize = 21300
page = 1 page = 1
@ -2192,25 +2192,24 @@ injectorLagMs = scalar, U16, 62, "ms", 0.0033333333333333335, 0
iatCorrection = scalar, U16, 64, "%", 0.01, 0 iatCorrection = scalar, U16, 64, "%", 0.01, 0
cltCorrection = scalar, U16, 66, "%", 0.01, 0 cltCorrection = scalar, U16, 66, "%", 0.01, 0
baroCorrection = scalar, U16, 68, "%", 0.01, 0 baroCorrection = scalar, U16, 68, "%", 0.01, 0
currentEnginePhase = scalar, U16, 70, "deg", 1, 0 wallFuelAmount = scalar, U16, 70, "mg", 0.01, 0
wallFuelAmount = scalar, U16, 72, "mg", 0.01, 0 wallFuelCorrection = scalar, S16, 72, "mg", 0.01, 0
wallFuelCorrection = scalar, S16, 74, "mg", 0.01, 0 revolutionCounterSinceStart = scalar, U16, 74, "", 1, 0
revolutionCounterSinceStart = scalar, U16, 76, "", 1, 0 deltaTps = scalar, S16, 76, "ratio", 0.01, 0
deltaTps = scalar, S16, 78, "ratio", 0.01, 0 canReadCounter = scalar, U16, 78, "", 1, 0
canReadCounter = scalar, U16, 80, "", 1, 0 tpsAccelFuel = scalar, S16, 80, "ms", 0.0033333333333333335, 0
tpsAccelFuel = scalar, S16, 82, "ms", 0.0033333333333333335, 0 ignitionAdvance = scalar, S16, 82, "deg", 0.02, 0
ignitionAdvance = scalar, S16, 84, "deg", 0.02, 0 sparkDwellValue = scalar, U16, 84, "ms", 0.0033333333333333335, 0
sparkDwellValue = scalar, U16, 86, "ms", 0.0033333333333333335, 0 coilDutyCycle = scalar, U16, 86, "%", 0.01, 0
coilDutyCycle = scalar, U16, 88, "%", 0.01, 0 idleAirValvePosition = scalar, U16, 88, "%", 0.01, 0
idleAirValvePosition = scalar, U16, 90, "%", 0.01, 0 etbTarget = scalar, S16, 90, "%", 0.01, 0
etbTarget = scalar, S16, 92, "%", 0.01, 0 etb1DutyCycle = scalar, S16, 92, "%", 0.01, 0
etb1DutyCycle = scalar, S16, 94, "%", 0.01, 0 etb1Error = scalar, S16, 94, "%", 0.01, 0
etb1Error = scalar, S16, 96, "%", 0.01, 0 fuelTankLevel = scalar, S16, 96, "%", 0.01, 0
fuelTankLevel = scalar, S16, 98, "%", 0.01, 0 totalFuelConsumption = scalar, U16, 98, "grams", 1, 0
totalFuelConsumption = scalar, U16, 100, "grams", 1, 0 fuelFlowRate = scalar, U16, 100, "gram/s", 0.005, 0
fuelFlowRate = scalar, U16, 102, "gram/s", 0.005, 0 veTableYAxis = scalar, U16, 102, "%", 0.01, 0
veTableYAxis = scalar, U16, 104, "%", 0.01, 0 afrTableYAxis = scalar, U16, 104, "%", 0.01, 0
afrTableYAxis = scalar, U16, 106, "%", 0.01, 0
knockLevel = scalar, F32, 108, "Volts", 1, 0 knockLevel = scalar, F32, 108, "Volts", 1, 0
seconds = scalar, U32, 112, "sec", 1, 0 seconds = scalar, U32, 112, "sec", 1, 0
engineMode = scalar, U32, 116, "em", 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 = iatCorrection, "fuel: IAT correction", float, "%.3f"
entry = cltCorrection, "fuel: CLT correction", float, "%.3f" entry = cltCorrection, "fuel: CLT correction", float, "%.3f"
entry = baroCorrection, "fuel: Barometric pressure 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 = wallFuelAmount, "fuel: wall amount", float, "%.3f"
entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f" entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f"
entry = revolutionCounterSinceStart, "revolutionCounterSinceStart", int, "%d" 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_DIFF, "mapVvt_MAP_AT_DIFF", float, "%.3f"
entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d" entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d"
entry = mapVvt_map_peak, "mapVvt_map_peak", 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 = totalRevolutionCounter, "Crank revolution counter", int, "%d"
entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f" entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f"
entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f" entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f"

42
firmware/tunerstudio/generated/rusefi_frankenso_na6.ini
View File

@ -86,7 +86,7 @@ enable2ndByteCanID = false
; name = scalar, type, offset, units, scale, translate, lo, hi, digits ; name = scalar, type, offset, units, scale, translate, lo, hi, digits
; CONFIG_DEFINITION_START ; 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 pageSize = 21300
page = 1 page = 1
@ -2192,25 +2192,24 @@ injectorLagMs = scalar, U16, 62, "ms", 0.0033333333333333335, 0
iatCorrection = scalar, U16, 64, "%", 0.01, 0 iatCorrection = scalar, U16, 64, "%", 0.01, 0
cltCorrection = scalar, U16, 66, "%", 0.01, 0 cltCorrection = scalar, U16, 66, "%", 0.01, 0
baroCorrection = scalar, U16, 68, "%", 0.01, 0 baroCorrection = scalar, U16, 68, "%", 0.01, 0
currentEnginePhase = scalar, U16, 70, "deg", 1, 0 wallFuelAmount = scalar, U16, 70, "mg", 0.01, 0
wallFuelAmount = scalar, U16, 72, "mg", 0.01, 0 wallFuelCorrection = scalar, S16, 72, "mg", 0.01, 0
wallFuelCorrection = scalar, S16, 74, "mg", 0.01, 0 revolutionCounterSinceStart = scalar, U16, 74, "", 1, 0
revolutionCounterSinceStart = scalar, U16, 76, "", 1, 0 deltaTps = scalar, S16, 76, "ratio", 0.01, 0
deltaTps = scalar, S16, 78, "ratio", 0.01, 0 canReadCounter = scalar, U16, 78, "", 1, 0
canReadCounter = scalar, U16, 80, "", 1, 0 tpsAccelFuel = scalar, S16, 80, "ms", 0.0033333333333333335, 0
tpsAccelFuel = scalar, S16, 82, "ms", 0.0033333333333333335, 0 ignitionAdvance = scalar, S16, 82, "deg", 0.02, 0
ignitionAdvance = scalar, S16, 84, "deg", 0.02, 0 sparkDwellValue = scalar, U16, 84, "ms", 0.0033333333333333335, 0
sparkDwellValue = scalar, U16, 86, "ms", 0.0033333333333333335, 0 coilDutyCycle = scalar, U16, 86, "%", 0.01, 0
coilDutyCycle = scalar, U16, 88, "%", 0.01, 0 idleAirValvePosition = scalar, U16, 88, "%", 0.01, 0
idleAirValvePosition = scalar, U16, 90, "%", 0.01, 0 etbTarget = scalar, S16, 90, "%", 0.01, 0
etbTarget = scalar, S16, 92, "%", 0.01, 0 etb1DutyCycle = scalar, S16, 92, "%", 0.01, 0
etb1DutyCycle = scalar, S16, 94, "%", 0.01, 0 etb1Error = scalar, S16, 94, "%", 0.01, 0
etb1Error = scalar, S16, 96, "%", 0.01, 0 fuelTankLevel = scalar, S16, 96, "%", 0.01, 0
fuelTankLevel = scalar, S16, 98, "%", 0.01, 0 totalFuelConsumption = scalar, U16, 98, "grams", 1, 0
totalFuelConsumption = scalar, U16, 100, "grams", 1, 0 fuelFlowRate = scalar, U16, 100, "gram/s", 0.005, 0
fuelFlowRate = scalar, U16, 102, "gram/s", 0.005, 0 veTableYAxis = scalar, U16, 102, "%", 0.01, 0
veTableYAxis = scalar, U16, 104, "%", 0.01, 0 afrTableYAxis = scalar, U16, 104, "%", 0.01, 0
afrTableYAxis = scalar, U16, 106, "%", 0.01, 0
knockLevel = scalar, F32, 108, "Volts", 1, 0 knockLevel = scalar, F32, 108, "Volts", 1, 0
seconds = scalar, U32, 112, "sec", 1, 0 seconds = scalar, U32, 112, "sec", 1, 0
engineMode = scalar, U32, 116, "em", 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 = iatCorrection, "fuel: IAT correction", float, "%.3f"
entry = cltCorrection, "fuel: CLT correction", float, "%.3f" entry = cltCorrection, "fuel: CLT correction", float, "%.3f"
entry = baroCorrection, "fuel: Barometric pressure 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 = wallFuelAmount, "fuel: wall amount", float, "%.3f"
entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f" entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f"
entry = revolutionCounterSinceStart, "revolutionCounterSinceStart", int, "%d" 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_DIFF, "mapVvt_MAP_AT_DIFF", float, "%.3f"
entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d" entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d"
entry = mapVvt_map_peak, "mapVvt_map_peak", 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 = totalRevolutionCounter, "Crank revolution counter", int, "%d"
entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f" entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f"
entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f" entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f"

42
firmware/tunerstudio/generated/rusefi_harley81.ini
View File

@ -86,7 +86,7 @@ enable2ndByteCanID = false
; name = scalar, type, offset, units, scale, translate, lo, hi, digits ; name = scalar, type, offset, units, scale, translate, lo, hi, digits
; CONFIG_DEFINITION_START ; 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 pageSize = 21300
page = 1 page = 1
@ -2192,25 +2192,24 @@ injectorLagMs = scalar, U16, 62, "ms", 0.0033333333333333335, 0
iatCorrection = scalar, U16, 64, "%", 0.01, 0 iatCorrection = scalar, U16, 64, "%", 0.01, 0
cltCorrection = scalar, U16, 66, "%", 0.01, 0 cltCorrection = scalar, U16, 66, "%", 0.01, 0
baroCorrection = scalar, U16, 68, "%", 0.01, 0 baroCorrection = scalar, U16, 68, "%", 0.01, 0
currentEnginePhase = scalar, U16, 70, "deg", 1, 0 wallFuelAmount = scalar, U16, 70, "mg", 0.01, 0
wallFuelAmount = scalar, U16, 72, "mg", 0.01, 0 wallFuelCorrection = scalar, S16, 72, "mg", 0.01, 0
wallFuelCorrection = scalar, S16, 74, "mg", 0.01, 0 revolutionCounterSinceStart = scalar, U16, 74, "", 1, 0
revolutionCounterSinceStart = scalar, U16, 76, "", 1, 0 deltaTps = scalar, S16, 76, "ratio", 0.01, 0
deltaTps = scalar, S16, 78, "ratio", 0.01, 0 canReadCounter = scalar, U16, 78, "", 1, 0
canReadCounter = scalar, U16, 80, "", 1, 0 tpsAccelFuel = scalar, S16, 80, "ms", 0.0033333333333333335, 0
tpsAccelFuel = scalar, S16, 82, "ms", 0.0033333333333333335, 0 ignitionAdvance = scalar, S16, 82, "deg", 0.02, 0
ignitionAdvance = scalar, S16, 84, "deg", 0.02, 0 sparkDwellValue = scalar, U16, 84, "ms", 0.0033333333333333335, 0
sparkDwellValue = scalar, U16, 86, "ms", 0.0033333333333333335, 0 coilDutyCycle = scalar, U16, 86, "%", 0.01, 0
coilDutyCycle = scalar, U16, 88, "%", 0.01, 0 idleAirValvePosition = scalar, U16, 88, "%", 0.01, 0
idleAirValvePosition = scalar, U16, 90, "%", 0.01, 0 etbTarget = scalar, S16, 90, "%", 0.01, 0
etbTarget = scalar, S16, 92, "%", 0.01, 0 etb1DutyCycle = scalar, S16, 92, "%", 0.01, 0
etb1DutyCycle = scalar, S16, 94, "%", 0.01, 0 etb1Error = scalar, S16, 94, "%", 0.01, 0
etb1Error = scalar, S16, 96, "%", 0.01, 0 fuelTankLevel = scalar, S16, 96, "%", 0.01, 0
fuelTankLevel = scalar, S16, 98, "%", 0.01, 0 totalFuelConsumption = scalar, U16, 98, "grams", 1, 0
totalFuelConsumption = scalar, U16, 100, "grams", 1, 0 fuelFlowRate = scalar, U16, 100, "gram/s", 0.005, 0
fuelFlowRate = scalar, U16, 102, "gram/s", 0.005, 0 veTableYAxis = scalar, U16, 102, "%", 0.01, 0
veTableYAxis = scalar, U16, 104, "%", 0.01, 0 afrTableYAxis = scalar, U16, 104, "%", 0.01, 0
afrTableYAxis = scalar, U16, 106, "%", 0.01, 0
knockLevel = scalar, F32, 108, "Volts", 1, 0 knockLevel = scalar, F32, 108, "Volts", 1, 0
seconds = scalar, U32, 112, "sec", 1, 0 seconds = scalar, U32, 112, "sec", 1, 0
engineMode = scalar, U32, 116, "em", 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 = iatCorrection, "fuel: IAT correction", float, "%.3f"
entry = cltCorrection, "fuel: CLT correction", float, "%.3f" entry = cltCorrection, "fuel: CLT correction", float, "%.3f"
entry = baroCorrection, "fuel: Barometric pressure 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 = wallFuelAmount, "fuel: wall amount", float, "%.3f"
entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f" entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f"
entry = revolutionCounterSinceStart, "revolutionCounterSinceStart", int, "%d" 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_DIFF, "mapVvt_MAP_AT_DIFF", float, "%.3f"
entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d" entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d"
entry = mapVvt_map_peak, "mapVvt_map_peak", 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 = totalRevolutionCounter, "Crank revolution counter", int, "%d"
entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f" entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f"
entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f" entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f"

42
firmware/tunerstudio/generated/rusefi_hellen-gm-e67.ini
View File

@ -86,7 +86,7 @@ enable2ndByteCanID = false
; name = scalar, type, offset, units, scale, translate, lo, hi, digits ; name = scalar, type, offset, units, scale, translate, lo, hi, digits
; CONFIG_DEFINITION_START ; 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 pageSize = 21300
page = 1 page = 1
@ -2192,25 +2192,24 @@ injectorLagMs = scalar, U16, 62, "ms", 0.0033333333333333335, 0
iatCorrection = scalar, U16, 64, "%", 0.01, 0 iatCorrection = scalar, U16, 64, "%", 0.01, 0
cltCorrection = scalar, U16, 66, "%", 0.01, 0 cltCorrection = scalar, U16, 66, "%", 0.01, 0
baroCorrection = scalar, U16, 68, "%", 0.01, 0 baroCorrection = scalar, U16, 68, "%", 0.01, 0
currentEnginePhase = scalar, U16, 70, "deg", 1, 0 wallFuelAmount = scalar, U16, 70, "mg", 0.01, 0
wallFuelAmount = scalar, U16, 72, "mg", 0.01, 0 wallFuelCorrection = scalar, S16, 72, "mg", 0.01, 0
wallFuelCorrection = scalar, S16, 74, "mg", 0.01, 0 revolutionCounterSinceStart = scalar, U16, 74, "", 1, 0
revolutionCounterSinceStart = scalar, U16, 76, "", 1, 0 deltaTps = scalar, S16, 76, "ratio", 0.01, 0
deltaTps = scalar, S16, 78, "ratio", 0.01, 0 canReadCounter = scalar, U16, 78, "", 1, 0
canReadCounter = scalar, U16, 80, "", 1, 0 tpsAccelFuel = scalar, S16, 80, "ms", 0.0033333333333333335, 0
tpsAccelFuel = scalar, S16, 82, "ms", 0.0033333333333333335, 0 ignitionAdvance = scalar, S16, 82, "deg", 0.02, 0
ignitionAdvance = scalar, S16, 84, "deg", 0.02, 0 sparkDwellValue = scalar, U16, 84, "ms", 0.0033333333333333335, 0
sparkDwellValue = scalar, U16, 86, "ms", 0.0033333333333333335, 0 coilDutyCycle = scalar, U16, 86, "%", 0.01, 0
coilDutyCycle = scalar, U16, 88, "%", 0.01, 0 idleAirValvePosition = scalar, U16, 88, "%", 0.01, 0
idleAirValvePosition = scalar, U16, 90, "%", 0.01, 0 etbTarget = scalar, S16, 90, "%", 0.01, 0
etbTarget = scalar, S16, 92, "%", 0.01, 0 etb1DutyCycle = scalar, S16, 92, "%", 0.01, 0
etb1DutyCycle = scalar, S16, 94, "%", 0.01, 0 etb1Error = scalar, S16, 94, "%", 0.01, 0
etb1Error = scalar, S16, 96, "%", 0.01, 0 fuelTankLevel = scalar, S16, 96, "%", 0.01, 0
fuelTankLevel = scalar, S16, 98, "%", 0.01, 0 totalFuelConsumption = scalar, U16, 98, "grams", 1, 0
totalFuelConsumption = scalar, U16, 100, "grams", 1, 0 fuelFlowRate = scalar, U16, 100, "gram/s", 0.005, 0
fuelFlowRate = scalar, U16, 102, "gram/s", 0.005, 0 veTableYAxis = scalar, U16, 102, "%", 0.01, 0
veTableYAxis = scalar, U16, 104, "%", 0.01, 0 afrTableYAxis = scalar, U16, 104, "%", 0.01, 0
afrTableYAxis = scalar, U16, 106, "%", 0.01, 0
knockLevel = scalar, F32, 108, "Volts", 1, 0 knockLevel = scalar, F32, 108, "Volts", 1, 0
seconds = scalar, U32, 112, "sec", 1, 0 seconds = scalar, U32, 112, "sec", 1, 0
engineMode = scalar, U32, 116, "em", 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 = iatCorrection, "fuel: IAT correction", float, "%.3f"
entry = cltCorrection, "fuel: CLT correction", float, "%.3f" entry = cltCorrection, "fuel: CLT correction", float, "%.3f"
entry = baroCorrection, "fuel: Barometric pressure 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 = wallFuelAmount, "fuel: wall amount", float, "%.3f"
entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f" entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f"
entry = revolutionCounterSinceStart, "revolutionCounterSinceStart", int, "%d" 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_DIFF, "mapVvt_MAP_AT_DIFF", float, "%.3f"
entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d" entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d"
entry = mapVvt_map_peak, "mapVvt_map_peak", 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 = totalRevolutionCounter, "Crank revolution counter", int, "%d"
entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f" entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f"
entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f" entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f"

42
firmware/tunerstudio/generated/rusefi_hellen-nb1.ini
View File

@ -86,7 +86,7 @@ enable2ndByteCanID = false
; name = scalar, type, offset, units, scale, translate, lo, hi, digits ; name = scalar, type, offset, units, scale, translate, lo, hi, digits
; CONFIG_DEFINITION_START ; 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 pageSize = 21300
page = 1 page = 1
@ -2192,25 +2192,24 @@ injectorLagMs = scalar, U16, 62, "ms", 0.0033333333333333335, 0
iatCorrection = scalar, U16, 64, "%", 0.01, 0 iatCorrection = scalar, U16, 64, "%", 0.01, 0
cltCorrection = scalar, U16, 66, "%", 0.01, 0 cltCorrection = scalar, U16, 66, "%", 0.01, 0
baroCorrection = scalar, U16, 68, "%", 0.01, 0 baroCorrection = scalar, U16, 68, "%", 0.01, 0
currentEnginePhase = scalar, U16, 70, "deg", 1, 0 wallFuelAmount = scalar, U16, 70, "mg", 0.01, 0
wallFuelAmount = scalar, U16, 72, "mg", 0.01, 0 wallFuelCorrection = scalar, S16, 72, "mg", 0.01, 0
wallFuelCorrection = scalar, S16, 74, "mg", 0.01, 0 revolutionCounterSinceStart = scalar, U16, 74, "", 1, 0
revolutionCounterSinceStart = scalar, U16, 76, "", 1, 0 deltaTps = scalar, S16, 76, "ratio", 0.01, 0
deltaTps = scalar, S16, 78, "ratio", 0.01, 0 canReadCounter = scalar, U16, 78, "", 1, 0
canReadCounter = scalar, U16, 80, "", 1, 0 tpsAccelFuel = scalar, S16, 80, "ms", 0.0033333333333333335, 0
tpsAccelFuel = scalar, S16, 82, "ms", 0.0033333333333333335, 0 ignitionAdvance = scalar, S16, 82, "deg", 0.02, 0
ignitionAdvance = scalar, S16, 84, "deg", 0.02, 0 sparkDwellValue = scalar, U16, 84, "ms", 0.0033333333333333335, 0
sparkDwellValue = scalar, U16, 86, "ms", 0.0033333333333333335, 0 coilDutyCycle = scalar, U16, 86, "%", 0.01, 0
coilDutyCycle = scalar, U16, 88, "%", 0.01, 0 idleAirValvePosition = scalar, U16, 88, "%", 0.01, 0
idleAirValvePosition = scalar, U16, 90, "%", 0.01, 0 etbTarget = scalar, S16, 90, "%", 0.01, 0
etbTarget = scalar, S16, 92, "%", 0.01, 0 etb1DutyCycle = scalar, S16, 92, "%", 0.01, 0
etb1DutyCycle = scalar, S16, 94, "%", 0.01, 0 etb1Error = scalar, S16, 94, "%", 0.01, 0
etb1Error = scalar, S16, 96, "%", 0.01, 0 fuelTankLevel = scalar, S16, 96, "%", 0.01, 0
fuelTankLevel = scalar, S16, 98, "%", 0.01, 0 totalFuelConsumption = scalar, U16, 98, "grams", 1, 0
totalFuelConsumption = scalar, U16, 100, "grams", 1, 0 fuelFlowRate = scalar, U16, 100, "gram/s", 0.005, 0
fuelFlowRate = scalar, U16, 102, "gram/s", 0.005, 0 veTableYAxis = scalar, U16, 102, "%", 0.01, 0
veTableYAxis = scalar, U16, 104, "%", 0.01, 0 afrTableYAxis = scalar, U16, 104, "%", 0.01, 0
afrTableYAxis = scalar, U16, 106, "%", 0.01, 0
knockLevel = scalar, F32, 108, "Volts", 1, 0 knockLevel = scalar, F32, 108, "Volts", 1, 0
seconds = scalar, U32, 112, "sec", 1, 0 seconds = scalar, U32, 112, "sec", 1, 0
engineMode = scalar, U32, 116, "em", 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 = iatCorrection, "fuel: IAT correction", float, "%.3f"
entry = cltCorrection, "fuel: CLT correction", float, "%.3f" entry = cltCorrection, "fuel: CLT correction", float, "%.3f"
entry = baroCorrection, "fuel: Barometric pressure 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 = wallFuelAmount, "fuel: wall amount", float, "%.3f"
entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f" entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f"
entry = revolutionCounterSinceStart, "revolutionCounterSinceStart", int, "%d" 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_DIFF, "mapVvt_MAP_AT_DIFF", float, "%.3f"
entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d" entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d"
entry = mapVvt_map_peak, "mapVvt_map_peak", 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 = totalRevolutionCounter, "Crank revolution counter", int, "%d"
entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f" entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f"
entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f" entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f"

42
firmware/tunerstudio/generated/rusefi_hellen121nissan.ini
View File

@ -86,7 +86,7 @@ enable2ndByteCanID = false
; name = scalar, type, offset, units, scale, translate, lo, hi, digits ; name = scalar, type, offset, units, scale, translate, lo, hi, digits
; CONFIG_DEFINITION_START ; 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 pageSize = 21300
page = 1 page = 1
@ -2192,25 +2192,24 @@ injectorLagMs = scalar, U16, 62, "ms", 0.0033333333333333335, 0
iatCorrection = scalar, U16, 64, "%", 0.01, 0 iatCorrection = scalar, U16, 64, "%", 0.01, 0
cltCorrection = scalar, U16, 66, "%", 0.01, 0 cltCorrection = scalar, U16, 66, "%", 0.01, 0
baroCorrection = scalar, U16, 68, "%", 0.01, 0 baroCorrection = scalar, U16, 68, "%", 0.01, 0
currentEnginePhase = scalar, U16, 70, "deg", 1, 0 wallFuelAmount = scalar, U16, 70, "mg", 0.01, 0
wallFuelAmount = scalar, U16, 72, "mg", 0.01, 0 wallFuelCorrection = scalar, S16, 72, "mg", 0.01, 0
wallFuelCorrection = scalar, S16, 74, "mg", 0.01, 0 revolutionCounterSinceStart = scalar, U16, 74, "", 1, 0
revolutionCounterSinceStart = scalar, U16, 76, "", 1, 0 deltaTps = scalar, S16, 76, "ratio", 0.01, 0
deltaTps = scalar, S16, 78, "ratio", 0.01, 0 canReadCounter = scalar, U16, 78, "", 1, 0
canReadCounter = scalar, U16, 80, "", 1, 0 tpsAccelFuel = scalar, S16, 80, "ms", 0.0033333333333333335, 0
tpsAccelFuel = scalar, S16, 82, "ms", 0.0033333333333333335, 0 ignitionAdvance = scalar, S16, 82, "deg", 0.02, 0
ignitionAdvance = scalar, S16, 84, "deg", 0.02, 0 sparkDwellValue = scalar, U16, 84, "ms", 0.0033333333333333335, 0
sparkDwellValue = scalar, U16, 86, "ms", 0.0033333333333333335, 0 coilDutyCycle = scalar, U16, 86, "%", 0.01, 0
coilDutyCycle = scalar, U16, 88, "%", 0.01, 0 idleAirValvePosition = scalar, U16, 88, "%", 0.01, 0
idleAirValvePosition = scalar, U16, 90, "%", 0.01, 0 etbTarget = scalar, S16, 90, "%", 0.01, 0
etbTarget = scalar, S16, 92, "%", 0.01, 0 etb1DutyCycle = scalar, S16, 92, "%", 0.01, 0
etb1DutyCycle = scalar, S16, 94, "%", 0.01, 0 etb1Error = scalar, S16, 94, "%", 0.01, 0
etb1Error = scalar, S16, 96, "%", 0.01, 0 fuelTankLevel = scalar, S16, 96, "%", 0.01, 0
fuelTankLevel = scalar, S16, 98, "%", 0.01, 0 totalFuelConsumption = scalar, U16, 98, "grams", 1, 0
totalFuelConsumption = scalar, U16, 100, "grams", 1, 0 fuelFlowRate = scalar, U16, 100, "gram/s", 0.005, 0
fuelFlowRate = scalar, U16, 102, "gram/s", 0.005, 0 veTableYAxis = scalar, U16, 102, "%", 0.01, 0
veTableYAxis = scalar, U16, 104, "%", 0.01, 0 afrTableYAxis = scalar, U16, 104, "%", 0.01, 0
afrTableYAxis = scalar, U16, 106, "%", 0.01, 0
knockLevel = scalar, F32, 108, "Volts", 1, 0 knockLevel = scalar, F32, 108, "Volts", 1, 0
seconds = scalar, U32, 112, "sec", 1, 0 seconds = scalar, U32, 112, "sec", 1, 0
engineMode = scalar, U32, 116, "em", 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 = iatCorrection, "fuel: IAT correction", float, "%.3f"
entry = cltCorrection, "fuel: CLT correction", float, "%.3f" entry = cltCorrection, "fuel: CLT correction", float, "%.3f"
entry = baroCorrection, "fuel: Barometric pressure 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 = wallFuelAmount, "fuel: wall amount", float, "%.3f"
entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f" entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f"
entry = revolutionCounterSinceStart, "revolutionCounterSinceStart", int, "%d" 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_DIFF, "mapVvt_MAP_AT_DIFF", float, "%.3f"
entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d" entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d"
entry = mapVvt_map_peak, "mapVvt_map_peak", 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 = totalRevolutionCounter, "Crank revolution counter", int, "%d"
entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f" entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f"
entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f" entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f"

42
firmware/tunerstudio/generated/rusefi_hellen121vag.ini
View File

@ -86,7 +86,7 @@ enable2ndByteCanID = false
; name = scalar, type, offset, units, scale, translate, lo, hi, digits ; name = scalar, type, offset, units, scale, translate, lo, hi, digits
; CONFIG_DEFINITION_START ; 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 pageSize = 21300
page = 1 page = 1
@ -2192,25 +2192,24 @@ injectorLagMs = scalar, U16, 62, "ms", 0.0033333333333333335, 0
iatCorrection = scalar, U16, 64, "%", 0.01, 0 iatCorrection = scalar, U16, 64, "%", 0.01, 0
cltCorrection = scalar, U16, 66, "%", 0.01, 0 cltCorrection = scalar, U16, 66, "%", 0.01, 0
baroCorrection = scalar, U16, 68, "%", 0.01, 0 baroCorrection = scalar, U16, 68, "%", 0.01, 0
currentEnginePhase = scalar, U16, 70, "deg", 1, 0 wallFuelAmount = scalar, U16, 70, "mg", 0.01, 0
wallFuelAmount = scalar, U16, 72, "mg", 0.01, 0 wallFuelCorrection = scalar, S16, 72, "mg", 0.01, 0
wallFuelCorrection = scalar, S16, 74, "mg", 0.01, 0 revolutionCounterSinceStart = scalar, U16, 74, "", 1, 0
revolutionCounterSinceStart = scalar, U16, 76, "", 1, 0 deltaTps = scalar, S16, 76, "ratio", 0.01, 0
deltaTps = scalar, S16, 78, "ratio", 0.01, 0 canReadCounter = scalar, U16, 78, "", 1, 0
canReadCounter = scalar, U16, 80, "", 1, 0 tpsAccelFuel = scalar, S16, 80, "ms", 0.0033333333333333335, 0
tpsAccelFuel = scalar, S16, 82, "ms", 0.0033333333333333335, 0 ignitionAdvance = scalar, S16, 82, "deg", 0.02, 0
ignitionAdvance = scalar, S16, 84, "deg", 0.02, 0 sparkDwellValue = scalar, U16, 84, "ms", 0.0033333333333333335, 0
sparkDwellValue = scalar, U16, 86, "ms", 0.0033333333333333335, 0 coilDutyCycle = scalar, U16, 86, "%", 0.01, 0
coilDutyCycle = scalar, U16, 88, "%", 0.01, 0 idleAirValvePosition = scalar, U16, 88, "%", 0.01, 0
idleAirValvePosition = scalar, U16, 90, "%", 0.01, 0 etbTarget = scalar, S16, 90, "%", 0.01, 0
etbTarget = scalar, S16, 92, "%", 0.01, 0 etb1DutyCycle = scalar, S16, 92, "%", 0.01, 0
etb1DutyCycle = scalar, S16, 94, "%", 0.01, 0 etb1Error = scalar, S16, 94, "%", 0.01, 0
etb1Error = scalar, S16, 96, "%", 0.01, 0 fuelTankLevel = scalar, S16, 96, "%", 0.01, 0
fuelTankLevel = scalar, S16, 98, "%", 0.01, 0 totalFuelConsumption = scalar, U16, 98, "grams", 1, 0
totalFuelConsumption = scalar, U16, 100, "grams", 1, 0 fuelFlowRate = scalar, U16, 100, "gram/s", 0.005, 0
fuelFlowRate = scalar, U16, 102, "gram/s", 0.005, 0 veTableYAxis = scalar, U16, 102, "%", 0.01, 0
veTableYAxis = scalar, U16, 104, "%", 0.01, 0 afrTableYAxis = scalar, U16, 104, "%", 0.01, 0
afrTableYAxis = scalar, U16, 106, "%", 0.01, 0
knockLevel = scalar, F32, 108, "Volts", 1, 0 knockLevel = scalar, F32, 108, "Volts", 1, 0
seconds = scalar, U32, 112, "sec", 1, 0 seconds = scalar, U32, 112, "sec", 1, 0
engineMode = scalar, U32, 116, "em", 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 = iatCorrection, "fuel: IAT correction", float, "%.3f"
entry = cltCorrection, "fuel: CLT correction", float, "%.3f" entry = cltCorrection, "fuel: CLT correction", float, "%.3f"
entry = baroCorrection, "fuel: Barometric pressure 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 = wallFuelAmount, "fuel: wall amount", float, "%.3f"
entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f" entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f"
entry = revolutionCounterSinceStart, "revolutionCounterSinceStart", int, "%d" 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_DIFF, "mapVvt_MAP_AT_DIFF", float, "%.3f"
entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d" entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d"
entry = mapVvt_map_peak, "mapVvt_map_peak", 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 = totalRevolutionCounter, "Crank revolution counter", int, "%d"
entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f" entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f"
entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f" entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f"

42
firmware/tunerstudio/generated/rusefi_hellen128mercedes.ini
View File

@ -86,7 +86,7 @@ enable2ndByteCanID = false
; name = scalar, type, offset, units, scale, translate, lo, hi, digits ; name = scalar, type, offset, units, scale, translate, lo, hi, digits
; CONFIG_DEFINITION_START ; 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 pageSize = 21300
page = 1 page = 1
@ -2192,25 +2192,24 @@ injectorLagMs = scalar, U16, 62, "ms", 0.0033333333333333335, 0
iatCorrection = scalar, U16, 64, "%", 0.01, 0 iatCorrection = scalar, U16, 64, "%", 0.01, 0
cltCorrection = scalar, U16, 66, "%", 0.01, 0 cltCorrection = scalar, U16, 66, "%", 0.01, 0
baroCorrection = scalar, U16, 68, "%", 0.01, 0 baroCorrection = scalar, U16, 68, "%", 0.01, 0
currentEnginePhase = scalar, U16, 70, "deg", 1, 0 wallFuelAmount = scalar, U16, 70, "mg", 0.01, 0
wallFuelAmount = scalar, U16, 72, "mg", 0.01, 0 wallFuelCorrection = scalar, S16, 72, "mg", 0.01, 0
wallFuelCorrection = scalar, S16, 74, "mg", 0.01, 0 revolutionCounterSinceStart = scalar, U16, 74, "", 1, 0
revolutionCounterSinceStart = scalar, U16, 76, "", 1, 0 deltaTps = scalar, S16, 76, "ratio", 0.01, 0
deltaTps = scalar, S16, 78, "ratio", 0.01, 0 canReadCounter = scalar, U16, 78, "", 1, 0
canReadCounter = scalar, U16, 80, "", 1, 0 tpsAccelFuel = scalar, S16, 80, "ms", 0.0033333333333333335, 0
tpsAccelFuel = scalar, S16, 82, "ms", 0.0033333333333333335, 0 ignitionAdvance = scalar, S16, 82, "deg", 0.02, 0
ignitionAdvance = scalar, S16, 84, "deg", 0.02, 0 sparkDwellValue = scalar, U16, 84, "ms", 0.0033333333333333335, 0
sparkDwellValue = scalar, U16, 86, "ms", 0.0033333333333333335, 0 coilDutyCycle = scalar, U16, 86, "%", 0.01, 0
coilDutyCycle = scalar, U16, 88, "%", 0.01, 0 idleAirValvePosition = scalar, U16, 88, "%", 0.01, 0
idleAirValvePosition = scalar, U16, 90, "%", 0.01, 0 etbTarget = scalar, S16, 90, "%", 0.01, 0
etbTarget = scalar, S16, 92, "%", 0.01, 0 etb1DutyCycle = scalar, S16, 92, "%", 0.01, 0
etb1DutyCycle = scalar, S16, 94, "%", 0.01, 0 etb1Error = scalar, S16, 94, "%", 0.01, 0
etb1Error = scalar, S16, 96, "%", 0.01, 0 fuelTankLevel = scalar, S16, 96, "%", 0.01, 0
fuelTankLevel = scalar, S16, 98, "%", 0.01, 0 totalFuelConsumption = scalar, U16, 98, "grams", 1, 0
totalFuelConsumption = scalar, U16, 100, "grams", 1, 0 fuelFlowRate = scalar, U16, 100, "gram/s", 0.005, 0
fuelFlowRate = scalar, U16, 102, "gram/s", 0.005, 0 veTableYAxis = scalar, U16, 102, "%", 0.01, 0
veTableYAxis = scalar, U16, 104, "%", 0.01, 0 afrTableYAxis = scalar, U16, 104, "%", 0.01, 0
afrTableYAxis = scalar, U16, 106, "%", 0.01, 0
knockLevel = scalar, F32, 108, "Volts", 1, 0 knockLevel = scalar, F32, 108, "Volts", 1, 0
seconds = scalar, U32, 112, "sec", 1, 0 seconds = scalar, U32, 112, "sec", 1, 0
engineMode = scalar, U32, 116, "em", 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 = iatCorrection, "fuel: IAT correction", float, "%.3f"
entry = cltCorrection, "fuel: CLT correction", float, "%.3f" entry = cltCorrection, "fuel: CLT correction", float, "%.3f"
entry = baroCorrection, "fuel: Barometric pressure 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 = wallFuelAmount, "fuel: wall amount", float, "%.3f"
entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f" entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f"
entry = revolutionCounterSinceStart, "revolutionCounterSinceStart", int, "%d" 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_DIFF, "mapVvt_MAP_AT_DIFF", float, "%.3f"
entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d" entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d"
entry = mapVvt_map_peak, "mapVvt_map_peak", 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 = totalRevolutionCounter, "Crank revolution counter", int, "%d"
entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f" entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f"
entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f" entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f"

42
firmware/tunerstudio/generated/rusefi_hellen154hyundai.ini
View File

@ -86,7 +86,7 @@ enable2ndByteCanID = false
; name = scalar, type, offset, units, scale, translate, lo, hi, digits ; name = scalar, type, offset, units, scale, translate, lo, hi, digits
; CONFIG_DEFINITION_START ; 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 pageSize = 21300
page = 1 page = 1
@ -2192,25 +2192,24 @@ injectorLagMs = scalar, U16, 62, "ms", 0.0033333333333333335, 0
iatCorrection = scalar, U16, 64, "%", 0.01, 0 iatCorrection = scalar, U16, 64, "%", 0.01, 0
cltCorrection = scalar, U16, 66, "%", 0.01, 0 cltCorrection = scalar, U16, 66, "%", 0.01, 0
baroCorrection = scalar, U16, 68, "%", 0.01, 0 baroCorrection = scalar, U16, 68, "%", 0.01, 0
currentEnginePhase = scalar, U16, 70, "deg", 1, 0 wallFuelAmount = scalar, U16, 70, "mg", 0.01, 0
wallFuelAmount = scalar, U16, 72, "mg", 0.01, 0 wallFuelCorrection = scalar, S16, 72, "mg", 0.01, 0
wallFuelCorrection = scalar, S16, 74, "mg", 0.01, 0 revolutionCounterSinceStart = scalar, U16, 74, "", 1, 0
revolutionCounterSinceStart = scalar, U16, 76, "", 1, 0 deltaTps = scalar, S16, 76, "ratio", 0.01, 0
deltaTps = scalar, S16, 78, "ratio", 0.01, 0 canReadCounter = scalar, U16, 78, "", 1, 0
canReadCounter = scalar, U16, 80, "", 1, 0 tpsAccelFuel = scalar, S16, 80, "ms", 0.0033333333333333335, 0
tpsAccelFuel = scalar, S16, 82, "ms", 0.0033333333333333335, 0 ignitionAdvance = scalar, S16, 82, "deg", 0.02, 0
ignitionAdvance = scalar, S16, 84, "deg", 0.02, 0 sparkDwellValue = scalar, U16, 84, "ms", 0.0033333333333333335, 0
sparkDwellValue = scalar, U16, 86, "ms", 0.0033333333333333335, 0 coilDutyCycle = scalar, U16, 86, "%", 0.01, 0
coilDutyCycle = scalar, U16, 88, "%", 0.01, 0 idleAirValvePosition = scalar, U16, 88, "%", 0.01, 0
idleAirValvePosition = scalar, U16, 90, "%", 0.01, 0 etbTarget = scalar, S16, 90, "%", 0.01, 0
etbTarget = scalar, S16, 92, "%", 0.01, 0 etb1DutyCycle = scalar, S16, 92, "%", 0.01, 0
etb1DutyCycle = scalar, S16, 94, "%", 0.01, 0 etb1Error = scalar, S16, 94, "%", 0.01, 0
etb1Error = scalar, S16, 96, "%", 0.01, 0 fuelTankLevel = scalar, S16, 96, "%", 0.01, 0
fuelTankLevel = scalar, S16, 98, "%", 0.01, 0 totalFuelConsumption = scalar, U16, 98, "grams", 1, 0
totalFuelConsumption = scalar, U16, 100, "grams", 1, 0 fuelFlowRate = scalar, U16, 100, "gram/s", 0.005, 0
fuelFlowRate = scalar, U16, 102, "gram/s", 0.005, 0 veTableYAxis = scalar, U16, 102, "%", 0.01, 0
veTableYAxis = scalar, U16, 104, "%", 0.01, 0 afrTableYAxis = scalar, U16, 104, "%", 0.01, 0
afrTableYAxis = scalar, U16, 106, "%", 0.01, 0
knockLevel = scalar, F32, 108, "Volts", 1, 0 knockLevel = scalar, F32, 108, "Volts", 1, 0
seconds = scalar, U32, 112, "sec", 1, 0 seconds = scalar, U32, 112, "sec", 1, 0
engineMode = scalar, U32, 116, "em", 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 = iatCorrection, "fuel: IAT correction", float, "%.3f"
entry = cltCorrection, "fuel: CLT correction", float, "%.3f" entry = cltCorrection, "fuel: CLT correction", float, "%.3f"
entry = baroCorrection, "fuel: Barometric pressure 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 = wallFuelAmount, "fuel: wall amount", float, "%.3f"
entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f" entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f"
entry = revolutionCounterSinceStart, "revolutionCounterSinceStart", int, "%d" 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_DIFF, "mapVvt_MAP_AT_DIFF", float, "%.3f"
entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d" entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d"
entry = mapVvt_map_peak, "mapVvt_map_peak", 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 = totalRevolutionCounter, "Crank revolution counter", int, "%d"
entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f" entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f"
entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f" entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f"

42
firmware/tunerstudio/generated/rusefi_hellen72.ini
View File

@ -86,7 +86,7 @@ enable2ndByteCanID = false
; name = scalar, type, offset, units, scale, translate, lo, hi, digits ; name = scalar, type, offset, units, scale, translate, lo, hi, digits
; CONFIG_DEFINITION_START ; 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 pageSize = 21300
page = 1 page = 1
@ -2192,25 +2192,24 @@ injectorLagMs = scalar, U16, 62, "ms", 0.0033333333333333335, 0
iatCorrection = scalar, U16, 64, "%", 0.01, 0 iatCorrection = scalar, U16, 64, "%", 0.01, 0
cltCorrection = scalar, U16, 66, "%", 0.01, 0 cltCorrection = scalar, U16, 66, "%", 0.01, 0
baroCorrection = scalar, U16, 68, "%", 0.01, 0 baroCorrection = scalar, U16, 68, "%", 0.01, 0
currentEnginePhase = scalar, U16, 70, "deg", 1, 0 wallFuelAmount = scalar, U16, 70, "mg", 0.01, 0
wallFuelAmount = scalar, U16, 72, "mg", 0.01, 0 wallFuelCorrection = scalar, S16, 72, "mg", 0.01, 0
wallFuelCorrection = scalar, S16, 74, "mg", 0.01, 0 revolutionCounterSinceStart = scalar, U16, 74, "", 1, 0
revolutionCounterSinceStart = scalar, U16, 76, "", 1, 0 deltaTps = scalar, S16, 76, "ratio", 0.01, 0
deltaTps = scalar, S16, 78, "ratio", 0.01, 0 canReadCounter = scalar, U16, 78, "", 1, 0
canReadCounter = scalar, U16, 80, "", 1, 0 tpsAccelFuel = scalar, S16, 80, "ms", 0.0033333333333333335, 0
tpsAccelFuel = scalar, S16, 82, "ms", 0.0033333333333333335, 0 ignitionAdvance = scalar, S16, 82, "deg", 0.02, 0
ignitionAdvance = scalar, S16, 84, "deg", 0.02, 0 sparkDwellValue = scalar, U16, 84, "ms", 0.0033333333333333335, 0
sparkDwellValue = scalar, U16, 86, "ms", 0.0033333333333333335, 0 coilDutyCycle = scalar, U16, 86, "%", 0.01, 0
coilDutyCycle = scalar, U16, 88, "%", 0.01, 0 idleAirValvePosition = scalar, U16, 88, "%", 0.01, 0
idleAirValvePosition = scalar, U16, 90, "%", 0.01, 0 etbTarget = scalar, S16, 90, "%", 0.01, 0
etbTarget = scalar, S16, 92, "%", 0.01, 0 etb1DutyCycle = scalar, S16, 92, "%", 0.01, 0
etb1DutyCycle = scalar, S16, 94, "%", 0.01, 0 etb1Error = scalar, S16, 94, "%", 0.01, 0
etb1Error = scalar, S16, 96, "%", 0.01, 0 fuelTankLevel = scalar, S16, 96, "%", 0.01, 0
fuelTankLevel = scalar, S16, 98, "%", 0.01, 0 totalFuelConsumption = scalar, U16, 98, "grams", 1, 0
totalFuelConsumption = scalar, U16, 100, "grams", 1, 0 fuelFlowRate = scalar, U16, 100, "gram/s", 0.005, 0
fuelFlowRate = scalar, U16, 102, "gram/s", 0.005, 0 veTableYAxis = scalar, U16, 102, "%", 0.01, 0
veTableYAxis = scalar, U16, 104, "%", 0.01, 0 afrTableYAxis = scalar, U16, 104, "%", 0.01, 0
afrTableYAxis = scalar, U16, 106, "%", 0.01, 0
knockLevel = scalar, F32, 108, "Volts", 1, 0 knockLevel = scalar, F32, 108, "Volts", 1, 0
seconds = scalar, U32, 112, "sec", 1, 0 seconds = scalar, U32, 112, "sec", 1, 0
engineMode = scalar, U32, 116, "em", 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 = iatCorrection, "fuel: IAT correction", float, "%.3f"
entry = cltCorrection, "fuel: CLT correction", float, "%.3f" entry = cltCorrection, "fuel: CLT correction", float, "%.3f"
entry = baroCorrection, "fuel: Barometric pressure 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 = wallFuelAmount, "fuel: wall amount", float, "%.3f"
entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f" entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f"
entry = revolutionCounterSinceStart, "revolutionCounterSinceStart", int, "%d" 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_DIFF, "mapVvt_MAP_AT_DIFF", float, "%.3f"
entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d" entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d"
entry = mapVvt_map_peak, "mapVvt_map_peak", 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 = totalRevolutionCounter, "Crank revolution counter", int, "%d"
entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f" entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f"
entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f" entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f"

42
firmware/tunerstudio/generated/rusefi_hellen81.ini
View File

@ -86,7 +86,7 @@ enable2ndByteCanID = false
; name = scalar, type, offset, units, scale, translate, lo, hi, digits ; name = scalar, type, offset, units, scale, translate, lo, hi, digits
; CONFIG_DEFINITION_START ; 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 pageSize = 21300
page = 1 page = 1
@ -2192,25 +2192,24 @@ injectorLagMs = scalar, U16, 62, "ms", 0.0033333333333333335, 0
iatCorrection = scalar, U16, 64, "%", 0.01, 0 iatCorrection = scalar, U16, 64, "%", 0.01, 0
cltCorrection = scalar, U16, 66, "%", 0.01, 0 cltCorrection = scalar, U16, 66, "%", 0.01, 0
baroCorrection = scalar, U16, 68, "%", 0.01, 0 baroCorrection = scalar, U16, 68, "%", 0.01, 0
currentEnginePhase = scalar, U16, 70, "deg", 1, 0 wallFuelAmount = scalar, U16, 70, "mg", 0.01, 0
wallFuelAmount = scalar, U16, 72, "mg", 0.01, 0 wallFuelCorrection = scalar, S16, 72, "mg", 0.01, 0
wallFuelCorrection = scalar, S16, 74, "mg", 0.01, 0 revolutionCounterSinceStart = scalar, U16, 74, "", 1, 0
revolutionCounterSinceStart = scalar, U16, 76, "", 1, 0 deltaTps = scalar, S16, 76, "ratio", 0.01, 0
deltaTps = scalar, S16, 78, "ratio", 0.01, 0 canReadCounter = scalar, U16, 78, "", 1, 0
canReadCounter = scalar, U16, 80, "", 1, 0 tpsAccelFuel = scalar, S16, 80, "ms", 0.0033333333333333335, 0
tpsAccelFuel = scalar, S16, 82, "ms", 0.0033333333333333335, 0 ignitionAdvance = scalar, S16, 82, "deg", 0.02, 0
ignitionAdvance = scalar, S16, 84, "deg", 0.02, 0 sparkDwellValue = scalar, U16, 84, "ms", 0.0033333333333333335, 0
sparkDwellValue = scalar, U16, 86, "ms", 0.0033333333333333335, 0 coilDutyCycle = scalar, U16, 86, "%", 0.01, 0
coilDutyCycle = scalar, U16, 88, "%", 0.01, 0 idleAirValvePosition = scalar, U16, 88, "%", 0.01, 0
idleAirValvePosition = scalar, U16, 90, "%", 0.01, 0 etbTarget = scalar, S16, 90, "%", 0.01, 0
etbTarget = scalar, S16, 92, "%", 0.01, 0 etb1DutyCycle = scalar, S16, 92, "%", 0.01, 0
etb1DutyCycle = scalar, S16, 94, "%", 0.01, 0 etb1Error = scalar, S16, 94, "%", 0.01, 0
etb1Error = scalar, S16, 96, "%", 0.01, 0 fuelTankLevel = scalar, S16, 96, "%", 0.01, 0
fuelTankLevel = scalar, S16, 98, "%", 0.01, 0 totalFuelConsumption = scalar, U16, 98, "grams", 1, 0
totalFuelConsumption = scalar, U16, 100, "grams", 1, 0 fuelFlowRate = scalar, U16, 100, "gram/s", 0.005, 0
fuelFlowRate = scalar, U16, 102, "gram/s", 0.005, 0 veTableYAxis = scalar, U16, 102, "%", 0.01, 0
veTableYAxis = scalar, U16, 104, "%", 0.01, 0 afrTableYAxis = scalar, U16, 104, "%", 0.01, 0
afrTableYAxis = scalar, U16, 106, "%", 0.01, 0
knockLevel = scalar, F32, 108, "Volts", 1, 0 knockLevel = scalar, F32, 108, "Volts", 1, 0
seconds = scalar, U32, 112, "sec", 1, 0 seconds = scalar, U32, 112, "sec", 1, 0
engineMode = scalar, U32, 116, "em", 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 = iatCorrection, "fuel: IAT correction", float, "%.3f"
entry = cltCorrection, "fuel: CLT correction", float, "%.3f" entry = cltCorrection, "fuel: CLT correction", float, "%.3f"
entry = baroCorrection, "fuel: Barometric pressure 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 = wallFuelAmount, "fuel: wall amount", float, "%.3f"
entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f" entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f"
entry = revolutionCounterSinceStart, "revolutionCounterSinceStart", int, "%d" 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_DIFF, "mapVvt_MAP_AT_DIFF", float, "%.3f"
entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d" entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d"
entry = mapVvt_map_peak, "mapVvt_map_peak", 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 = totalRevolutionCounter, "Crank revolution counter", int, "%d"
entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f" entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f"
entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f" entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f"

42
firmware/tunerstudio/generated/rusefi_hellen88bmw.ini
View File

@ -86,7 +86,7 @@ enable2ndByteCanID = false
; name = scalar, type, offset, units, scale, translate, lo, hi, digits ; name = scalar, type, offset, units, scale, translate, lo, hi, digits
; CONFIG_DEFINITION_START ; 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 pageSize = 21300
page = 1 page = 1
@ -2192,25 +2192,24 @@ injectorLagMs = scalar, U16, 62, "ms", 0.0033333333333333335, 0
iatCorrection = scalar, U16, 64, "%", 0.01, 0 iatCorrection = scalar, U16, 64, "%", 0.01, 0
cltCorrection = scalar, U16, 66, "%", 0.01, 0 cltCorrection = scalar, U16, 66, "%", 0.01, 0
baroCorrection = scalar, U16, 68, "%", 0.01, 0 baroCorrection = scalar, U16, 68, "%", 0.01, 0
currentEnginePhase = scalar, U16, 70, "deg", 1, 0 wallFuelAmount = scalar, U16, 70, "mg", 0.01, 0
wallFuelAmount = scalar, U16, 72, "mg", 0.01, 0 wallFuelCorrection = scalar, S16, 72, "mg", 0.01, 0
wallFuelCorrection = scalar, S16, 74, "mg", 0.01, 0 revolutionCounterSinceStart = scalar, U16, 74, "", 1, 0
revolutionCounterSinceStart = scalar, U16, 76, "", 1, 0 deltaTps = scalar, S16, 76, "ratio", 0.01, 0
deltaTps = scalar, S16, 78, "ratio", 0.01, 0 canReadCounter = scalar, U16, 78, "", 1, 0
canReadCounter = scalar, U16, 80, "", 1, 0 tpsAccelFuel = scalar, S16, 80, "ms", 0.0033333333333333335, 0
tpsAccelFuel = scalar, S16, 82, "ms", 0.0033333333333333335, 0 ignitionAdvance = scalar, S16, 82, "deg", 0.02, 0
ignitionAdvance = scalar, S16, 84, "deg", 0.02, 0 sparkDwellValue = scalar, U16, 84, "ms", 0.0033333333333333335, 0
sparkDwellValue = scalar, U16, 86, "ms", 0.0033333333333333335, 0 coilDutyCycle = scalar, U16, 86, "%", 0.01, 0
coilDutyCycle = scalar, U16, 88, "%", 0.01, 0 idleAirValvePosition = scalar, U16, 88, "%", 0.01, 0
idleAirValvePosition = scalar, U16, 90, "%", 0.01, 0 etbTarget = scalar, S16, 90, "%", 0.01, 0
etbTarget = scalar, S16, 92, "%", 0.01, 0 etb1DutyCycle = scalar, S16, 92, "%", 0.01, 0
etb1DutyCycle = scalar, S16, 94, "%", 0.01, 0 etb1Error = scalar, S16, 94, "%", 0.01, 0
etb1Error = scalar, S16, 96, "%", 0.01, 0 fuelTankLevel = scalar, S16, 96, "%", 0.01, 0
fuelTankLevel = scalar, S16, 98, "%", 0.01, 0 totalFuelConsumption = scalar, U16, 98, "grams", 1, 0
totalFuelConsumption = scalar, U16, 100, "grams", 1, 0 fuelFlowRate = scalar, U16, 100, "gram/s", 0.005, 0
fuelFlowRate = scalar, U16, 102, "gram/s", 0.005, 0 veTableYAxis = scalar, U16, 102, "%", 0.01, 0
veTableYAxis = scalar, U16, 104, "%", 0.01, 0 afrTableYAxis = scalar, U16, 104, "%", 0.01, 0
afrTableYAxis = scalar, U16, 106, "%", 0.01, 0
knockLevel = scalar, F32, 108, "Volts", 1, 0 knockLevel = scalar, F32, 108, "Volts", 1, 0
seconds = scalar, U32, 112, "sec", 1, 0 seconds = scalar, U32, 112, "sec", 1, 0
engineMode = scalar, U32, 116, "em", 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 = iatCorrection, "fuel: IAT correction", float, "%.3f"
entry = cltCorrection, "fuel: CLT correction", float, "%.3f" entry = cltCorrection, "fuel: CLT correction", float, "%.3f"
entry = baroCorrection, "fuel: Barometric pressure 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 = wallFuelAmount, "fuel: wall amount", float, "%.3f"
entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f" entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f"
entry = revolutionCounterSinceStart, "revolutionCounterSinceStart", int, "%d" 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_DIFF, "mapVvt_MAP_AT_DIFF", float, "%.3f"
entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d" entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d"
entry = mapVvt_map_peak, "mapVvt_map_peak", 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 = totalRevolutionCounter, "Crank revolution counter", int, "%d"
entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f" entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f"
entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f" entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f"

42
firmware/tunerstudio/generated/rusefi_hellenNA6.ini
View File

@ -86,7 +86,7 @@ enable2ndByteCanID = false
; name = scalar, type, offset, units, scale, translate, lo, hi, digits ; name = scalar, type, offset, units, scale, translate, lo, hi, digits
; CONFIG_DEFINITION_START ; 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 pageSize = 21300
page = 1 page = 1
@ -2192,25 +2192,24 @@ injectorLagMs = scalar, U16, 62, "ms", 0.0033333333333333335, 0
iatCorrection = scalar, U16, 64, "%", 0.01, 0 iatCorrection = scalar, U16, 64, "%", 0.01, 0
cltCorrection = scalar, U16, 66, "%", 0.01, 0 cltCorrection = scalar, U16, 66, "%", 0.01, 0
baroCorrection = scalar, U16, 68, "%", 0.01, 0 baroCorrection = scalar, U16, 68, "%", 0.01, 0
currentEnginePhase = scalar, U16, 70, "deg", 1, 0 wallFuelAmount = scalar, U16, 70, "mg", 0.01, 0
wallFuelAmount = scalar, U16, 72, "mg", 0.01, 0 wallFuelCorrection = scalar, S16, 72, "mg", 0.01, 0
wallFuelCorrection = scalar, S16, 74, "mg", 0.01, 0 revolutionCounterSinceStart = scalar, U16, 74, "", 1, 0
revolutionCounterSinceStart = scalar, U16, 76, "", 1, 0 deltaTps = scalar, S16, 76, "ratio", 0.01, 0
deltaTps = scalar, S16, 78, "ratio", 0.01, 0 canReadCounter = scalar, U16, 78, "", 1, 0
canReadCounter = scalar, U16, 80, "", 1, 0 tpsAccelFuel = scalar, S16, 80, "ms", 0.0033333333333333335, 0
tpsAccelFuel = scalar, S16, 82, "ms", 0.0033333333333333335, 0 ignitionAdvance = scalar, S16, 82, "deg", 0.02, 0
ignitionAdvance = scalar, S16, 84, "deg", 0.02, 0 sparkDwellValue = scalar, U16, 84, "ms", 0.0033333333333333335, 0
sparkDwellValue = scalar, U16, 86, "ms", 0.0033333333333333335, 0 coilDutyCycle = scalar, U16, 86, "%", 0.01, 0
coilDutyCycle = scalar, U16, 88, "%", 0.01, 0 idleAirValvePosition = scalar, U16, 88, "%", 0.01, 0
idleAirValvePosition = scalar, U16, 90, "%", 0.01, 0 etbTarget = scalar, S16, 90, "%", 0.01, 0
etbTarget = scalar, S16, 92, "%", 0.01, 0 etb1DutyCycle = scalar, S16, 92, "%", 0.01, 0
etb1DutyCycle = scalar, S16, 94, "%", 0.01, 0 etb1Error = scalar, S16, 94, "%", 0.01, 0
etb1Error = scalar, S16, 96, "%", 0.01, 0 fuelTankLevel = scalar, S16, 96, "%", 0.01, 0
fuelTankLevel = scalar, S16, 98, "%", 0.01, 0 totalFuelConsumption = scalar, U16, 98, "grams", 1, 0
totalFuelConsumption = scalar, U16, 100, "grams", 1, 0 fuelFlowRate = scalar, U16, 100, "gram/s", 0.005, 0
fuelFlowRate = scalar, U16, 102, "gram/s", 0.005, 0 veTableYAxis = scalar, U16, 102, "%", 0.01, 0
veTableYAxis = scalar, U16, 104, "%", 0.01, 0 afrTableYAxis = scalar, U16, 104, "%", 0.01, 0
afrTableYAxis = scalar, U16, 106, "%", 0.01, 0
knockLevel = scalar, F32, 108, "Volts", 1, 0 knockLevel = scalar, F32, 108, "Volts", 1, 0
seconds = scalar, U32, 112, "sec", 1, 0 seconds = scalar, U32, 112, "sec", 1, 0
engineMode = scalar, U32, 116, "em", 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 = iatCorrection, "fuel: IAT correction", float, "%.3f"
entry = cltCorrection, "fuel: CLT correction", float, "%.3f" entry = cltCorrection, "fuel: CLT correction", float, "%.3f"
entry = baroCorrection, "fuel: Barometric pressure 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 = wallFuelAmount, "fuel: wall amount", float, "%.3f"
entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f" entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f"
entry = revolutionCounterSinceStart, "revolutionCounterSinceStart", int, "%d" 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_DIFF, "mapVvt_MAP_AT_DIFF", float, "%.3f"
entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d" entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d"
entry = mapVvt_map_peak, "mapVvt_map_peak", 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 = totalRevolutionCounter, "Crank revolution counter", int, "%d"
entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f" entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f"
entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f" entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f"

42
firmware/tunerstudio/generated/rusefi_hellenNA8_96.ini
View File

@ -86,7 +86,7 @@ enable2ndByteCanID = false
; name = scalar, type, offset, units, scale, translate, lo, hi, digits ; name = scalar, type, offset, units, scale, translate, lo, hi, digits
; CONFIG_DEFINITION_START ; 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 pageSize = 21300
page = 1 page = 1
@ -2192,25 +2192,24 @@ injectorLagMs = scalar, U16, 62, "ms", 0.0033333333333333335, 0
iatCorrection = scalar, U16, 64, "%", 0.01, 0 iatCorrection = scalar, U16, 64, "%", 0.01, 0
cltCorrection = scalar, U16, 66, "%", 0.01, 0 cltCorrection = scalar, U16, 66, "%", 0.01, 0
baroCorrection = scalar, U16, 68, "%", 0.01, 0 baroCorrection = scalar, U16, 68, "%", 0.01, 0
currentEnginePhase = scalar, U16, 70, "deg", 1, 0 wallFuelAmount = scalar, U16, 70, "mg", 0.01, 0
wallFuelAmount = scalar, U16, 72, "mg", 0.01, 0 wallFuelCorrection = scalar, S16, 72, "mg", 0.01, 0
wallFuelCorrection = scalar, S16, 74, "mg", 0.01, 0 revolutionCounterSinceStart = scalar, U16, 74, "", 1, 0
revolutionCounterSinceStart = scalar, U16, 76, "", 1, 0 deltaTps = scalar, S16, 76, "ratio", 0.01, 0
deltaTps = scalar, S16, 78, "ratio", 0.01, 0 canReadCounter = scalar, U16, 78, "", 1, 0
canReadCounter = scalar, U16, 80, "", 1, 0 tpsAccelFuel = scalar, S16, 80, "ms", 0.0033333333333333335, 0
tpsAccelFuel = scalar, S16, 82, "ms", 0.0033333333333333335, 0 ignitionAdvance = scalar, S16, 82, "deg", 0.02, 0
ignitionAdvance = scalar, S16, 84, "deg", 0.02, 0 sparkDwellValue = scalar, U16, 84, "ms", 0.0033333333333333335, 0
sparkDwellValue = scalar, U16, 86, "ms", 0.0033333333333333335, 0 coilDutyCycle = scalar, U16, 86, "%", 0.01, 0
coilDutyCycle = scalar, U16, 88, "%", 0.01, 0 idleAirValvePosition = scalar, U16, 88, "%", 0.01, 0
idleAirValvePosition = scalar, U16, 90, "%", 0.01, 0 etbTarget = scalar, S16, 90, "%", 0.01, 0
etbTarget = scalar, S16, 92, "%", 0.01, 0 etb1DutyCycle = scalar, S16, 92, "%", 0.01, 0
etb1DutyCycle = scalar, S16, 94, "%", 0.01, 0 etb1Error = scalar, S16, 94, "%", 0.01, 0
etb1Error = scalar, S16, 96, "%", 0.01, 0 fuelTankLevel = scalar, S16, 96, "%", 0.01, 0
fuelTankLevel = scalar, S16, 98, "%", 0.01, 0 totalFuelConsumption = scalar, U16, 98, "grams", 1, 0
totalFuelConsumption = scalar, U16, 100, "grams", 1, 0 fuelFlowRate = scalar, U16, 100, "gram/s", 0.005, 0
fuelFlowRate = scalar, U16, 102, "gram/s", 0.005, 0 veTableYAxis = scalar, U16, 102, "%", 0.01, 0
veTableYAxis = scalar, U16, 104, "%", 0.01, 0 afrTableYAxis = scalar, U16, 104, "%", 0.01, 0
afrTableYAxis = scalar, U16, 106, "%", 0.01, 0
knockLevel = scalar, F32, 108, "Volts", 1, 0 knockLevel = scalar, F32, 108, "Volts", 1, 0
seconds = scalar, U32, 112, "sec", 1, 0 seconds = scalar, U32, 112, "sec", 1, 0
engineMode = scalar, U32, 116, "em", 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 = iatCorrection, "fuel: IAT correction", float, "%.3f"
entry = cltCorrection, "fuel: CLT correction", float, "%.3f" entry = cltCorrection, "fuel: CLT correction", float, "%.3f"
entry = baroCorrection, "fuel: Barometric pressure 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 = wallFuelAmount, "fuel: wall amount", float, "%.3f"
entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f" entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f"
entry = revolutionCounterSinceStart, "revolutionCounterSinceStart", int, "%d" 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_DIFF, "mapVvt_MAP_AT_DIFF", float, "%.3f"
entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d" entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d"
entry = mapVvt_map_peak, "mapVvt_map_peak", 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 = totalRevolutionCounter, "Crank revolution counter", int, "%d"
entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f" entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f"
entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f" entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f"

42
firmware/tunerstudio/generated/rusefi_kin.ini
View File

@ -86,7 +86,7 @@ enable2ndByteCanID = false
; name = scalar, type, offset, units, scale, translate, lo, hi, digits ; name = scalar, type, offset, units, scale, translate, lo, hi, digits
; CONFIG_DEFINITION_START ; 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 pageSize = 21300
page = 1 page = 1
@ -2192,25 +2192,24 @@ injectorLagMs = scalar, U16, 62, "ms", 0.0033333333333333335, 0
iatCorrection = scalar, U16, 64, "%", 0.01, 0 iatCorrection = scalar, U16, 64, "%", 0.01, 0
cltCorrection = scalar, U16, 66, "%", 0.01, 0 cltCorrection = scalar, U16, 66, "%", 0.01, 0
baroCorrection = scalar, U16, 68, "%", 0.01, 0 baroCorrection = scalar, U16, 68, "%", 0.01, 0
currentEnginePhase = scalar, U16, 70, "deg", 1, 0 wallFuelAmount = scalar, U16, 70, "mg", 0.01, 0
wallFuelAmount = scalar, U16, 72, "mg", 0.01, 0 wallFuelCorrection = scalar, S16, 72, "mg", 0.01, 0
wallFuelCorrection = scalar, S16, 74, "mg", 0.01, 0 revolutionCounterSinceStart = scalar, U16, 74, "", 1, 0
revolutionCounterSinceStart = scalar, U16, 76, "", 1, 0 deltaTps = scalar, S16, 76, "ratio", 0.01, 0
deltaTps = scalar, S16, 78, "ratio", 0.01, 0 canReadCounter = scalar, U16, 78, "", 1, 0
canReadCounter = scalar, U16, 80, "", 1, 0 tpsAccelFuel = scalar, S16, 80, "ms", 0.0033333333333333335, 0
tpsAccelFuel = scalar, S16, 82, "ms", 0.0033333333333333335, 0 ignitionAdvance = scalar, S16, 82, "deg", 0.02, 0
ignitionAdvance = scalar, S16, 84, "deg", 0.02, 0 sparkDwellValue = scalar, U16, 84, "ms", 0.0033333333333333335, 0
sparkDwellValue = scalar, U16, 86, "ms", 0.0033333333333333335, 0 coilDutyCycle = scalar, U16, 86, "%", 0.01, 0
coilDutyCycle = scalar, U16, 88, "%", 0.01, 0 idleAirValvePosition = scalar, U16, 88, "%", 0.01, 0
idleAirValvePosition = scalar, U16, 90, "%", 0.01, 0 etbTarget = scalar, S16, 90, "%", 0.01, 0
etbTarget = scalar, S16, 92, "%", 0.01, 0 etb1DutyCycle = scalar, S16, 92, "%", 0.01, 0
etb1DutyCycle = scalar, S16, 94, "%", 0.01, 0 etb1Error = scalar, S16, 94, "%", 0.01, 0
etb1Error = scalar, S16, 96, "%", 0.01, 0 fuelTankLevel = scalar, S16, 96, "%", 0.01, 0
fuelTankLevel = scalar, S16, 98, "%", 0.01, 0 totalFuelConsumption = scalar, U16, 98, "grams", 1, 0
totalFuelConsumption = scalar, U16, 100, "grams", 1, 0 fuelFlowRate = scalar, U16, 100, "gram/s", 0.005, 0
fuelFlowRate = scalar, U16, 102, "gram/s", 0.005, 0 veTableYAxis = scalar, U16, 102, "%", 0.01, 0
veTableYAxis = scalar, U16, 104, "%", 0.01, 0 afrTableYAxis = scalar, U16, 104, "%", 0.01, 0
afrTableYAxis = scalar, U16, 106, "%", 0.01, 0
knockLevel = scalar, F32, 108, "Volts", 1, 0 knockLevel = scalar, F32, 108, "Volts", 1, 0
seconds = scalar, U32, 112, "sec", 1, 0 seconds = scalar, U32, 112, "sec", 1, 0
engineMode = scalar, U32, 116, "em", 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 = iatCorrection, "fuel: IAT correction", float, "%.3f"
entry = cltCorrection, "fuel: CLT correction", float, "%.3f" entry = cltCorrection, "fuel: CLT correction", float, "%.3f"
entry = baroCorrection, "fuel: Barometric pressure 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 = wallFuelAmount, "fuel: wall amount", float, "%.3f"
entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f" entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f"
entry = revolutionCounterSinceStart, "revolutionCounterSinceStart", int, "%d" 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_DIFF, "mapVvt_MAP_AT_DIFF", float, "%.3f"
entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d" entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d"
entry = mapVvt_map_peak, "mapVvt_map_peak", 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 = totalRevolutionCounter, "Crank revolution counter", int, "%d"
entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f" entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f"
entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f" entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f"

42
firmware/tunerstudio/generated/rusefi_mre_f4.ini
View File

@ -86,7 +86,7 @@ enable2ndByteCanID = false
; name = scalar, type, offset, units, scale, translate, lo, hi, digits ; name = scalar, type, offset, units, scale, translate, lo, hi, digits
; CONFIG_DEFINITION_START ; 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 pageSize = 21300
page = 1 page = 1
@ -2192,25 +2192,24 @@ injectorLagMs = scalar, U16, 62, "ms", 0.0033333333333333335, 0
iatCorrection = scalar, U16, 64, "%", 0.01, 0 iatCorrection = scalar, U16, 64, "%", 0.01, 0
cltCorrection = scalar, U16, 66, "%", 0.01, 0 cltCorrection = scalar, U16, 66, "%", 0.01, 0
baroCorrection = scalar, U16, 68, "%", 0.01, 0 baroCorrection = scalar, U16, 68, "%", 0.01, 0
currentEnginePhase = scalar, U16, 70, "deg", 1, 0 wallFuelAmount = scalar, U16, 70, "mg", 0.01, 0
wallFuelAmount = scalar, U16, 72, "mg", 0.01, 0 wallFuelCorrection = scalar, S16, 72, "mg", 0.01, 0
wallFuelCorrection = scalar, S16, 74, "mg", 0.01, 0 revolutionCounterSinceStart = scalar, U16, 74, "", 1, 0
revolutionCounterSinceStart = scalar, U16, 76, "", 1, 0 deltaTps = scalar, S16, 76, "ratio", 0.01, 0
deltaTps = scalar, S16, 78, "ratio", 0.01, 0 canReadCounter = scalar, U16, 78, "", 1, 0
canReadCounter = scalar, U16, 80, "", 1, 0 tpsAccelFuel = scalar, S16, 80, "ms", 0.0033333333333333335, 0
tpsAccelFuel = scalar, S16, 82, "ms", 0.0033333333333333335, 0 ignitionAdvance = scalar, S16, 82, "deg", 0.02, 0
ignitionAdvance = scalar, S16, 84, "deg", 0.02, 0 sparkDwellValue = scalar, U16, 84, "ms", 0.0033333333333333335, 0
sparkDwellValue = scalar, U16, 86, "ms", 0.0033333333333333335, 0 coilDutyCycle = scalar, U16, 86, "%", 0.01, 0
coilDutyCycle = scalar, U16, 88, "%", 0.01, 0 idleAirValvePosition = scalar, U16, 88, "%", 0.01, 0
idleAirValvePosition = scalar, U16, 90, "%", 0.01, 0 etbTarget = scalar, S16, 90, "%", 0.01, 0
etbTarget = scalar, S16, 92, "%", 0.01, 0 etb1DutyCycle = scalar, S16, 92, "%", 0.01, 0
etb1DutyCycle = scalar, S16, 94, "%", 0.01, 0 etb1Error = scalar, S16, 94, "%", 0.01, 0
etb1Error = scalar, S16, 96, "%", 0.01, 0 fuelTankLevel = scalar, S16, 96, "%", 0.01, 0
fuelTankLevel = scalar, S16, 98, "%", 0.01, 0 totalFuelConsumption = scalar, U16, 98, "grams", 1, 0
totalFuelConsumption = scalar, U16, 100, "grams", 1, 0 fuelFlowRate = scalar, U16, 100, "gram/s", 0.005, 0
fuelFlowRate = scalar, U16, 102, "gram/s", 0.005, 0 veTableYAxis = scalar, U16, 102, "%", 0.01, 0
veTableYAxis = scalar, U16, 104, "%", 0.01, 0 afrTableYAxis = scalar, U16, 104, "%", 0.01, 0
afrTableYAxis = scalar, U16, 106, "%", 0.01, 0
knockLevel = scalar, F32, 108, "Volts", 1, 0 knockLevel = scalar, F32, 108, "Volts", 1, 0
seconds = scalar, U32, 112, "sec", 1, 0 seconds = scalar, U32, 112, "sec", 1, 0
engineMode = scalar, U32, 116, "em", 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 = iatCorrection, "fuel: IAT correction", float, "%.3f"
entry = cltCorrection, "fuel: CLT correction", float, "%.3f" entry = cltCorrection, "fuel: CLT correction", float, "%.3f"
entry = baroCorrection, "fuel: Barometric pressure 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 = wallFuelAmount, "fuel: wall amount", float, "%.3f"
entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f" entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f"
entry = revolutionCounterSinceStart, "revolutionCounterSinceStart", int, "%d" 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_DIFF, "mapVvt_MAP_AT_DIFF", float, "%.3f"
entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d" entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d"
entry = mapVvt_map_peak, "mapVvt_map_peak", 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 = totalRevolutionCounter, "Crank revolution counter", int, "%d"
entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f" entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f"
entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f" entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f"

42
firmware/tunerstudio/generated/rusefi_mre_f7.ini
View File

@ -86,7 +86,7 @@ enable2ndByteCanID = false
; name = scalar, type, offset, units, scale, translate, lo, hi, digits ; name = scalar, type, offset, units, scale, translate, lo, hi, digits
; CONFIG_DEFINITION_START ; 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 pageSize = 21300
page = 1 page = 1
@ -2192,25 +2192,24 @@ injectorLagMs = scalar, U16, 62, "ms", 0.0033333333333333335, 0
iatCorrection = scalar, U16, 64, "%", 0.01, 0 iatCorrection = scalar, U16, 64, "%", 0.01, 0
cltCorrection = scalar, U16, 66, "%", 0.01, 0 cltCorrection = scalar, U16, 66, "%", 0.01, 0
baroCorrection = scalar, U16, 68, "%", 0.01, 0 baroCorrection = scalar, U16, 68, "%", 0.01, 0
currentEnginePhase = scalar, U16, 70, "deg", 1, 0 wallFuelAmount = scalar, U16, 70, "mg", 0.01, 0
wallFuelAmount = scalar, U16, 72, "mg", 0.01, 0 wallFuelCorrection = scalar, S16, 72, "mg", 0.01, 0
wallFuelCorrection = scalar, S16, 74, "mg", 0.01, 0 revolutionCounterSinceStart = scalar, U16, 74, "", 1, 0
revolutionCounterSinceStart = scalar, U16, 76, "", 1, 0 deltaTps = scalar, S16, 76, "ratio", 0.01, 0
deltaTps = scalar, S16, 78, "ratio", 0.01, 0 canReadCounter = scalar, U16, 78, "", 1, 0
canReadCounter = scalar, U16, 80, "", 1, 0 tpsAccelFuel = scalar, S16, 80, "ms", 0.0033333333333333335, 0
tpsAccelFuel = scalar, S16, 82, "ms", 0.0033333333333333335, 0 ignitionAdvance = scalar, S16, 82, "deg", 0.02, 0
ignitionAdvance = scalar, S16, 84, "deg", 0.02, 0 sparkDwellValue = scalar, U16, 84, "ms", 0.0033333333333333335, 0
sparkDwellValue = scalar, U16, 86, "ms", 0.0033333333333333335, 0 coilDutyCycle = scalar, U16, 86, "%", 0.01, 0
coilDutyCycle = scalar, U16, 88, "%", 0.01, 0 idleAirValvePosition = scalar, U16, 88, "%", 0.01, 0
idleAirValvePosition = scalar, U16, 90, "%", 0.01, 0 etbTarget = scalar, S16, 90, "%", 0.01, 0
etbTarget = scalar, S16, 92, "%", 0.01, 0 etb1DutyCycle = scalar, S16, 92, "%", 0.01, 0
etb1DutyCycle = scalar, S16, 94, "%", 0.01, 0 etb1Error = scalar, S16, 94, "%", 0.01, 0
etb1Error = scalar, S16, 96, "%", 0.01, 0 fuelTankLevel = scalar, S16, 96, "%", 0.01, 0
fuelTankLevel = scalar, S16, 98, "%", 0.01, 0 totalFuelConsumption = scalar, U16, 98, "grams", 1, 0
totalFuelConsumption = scalar, U16, 100, "grams", 1, 0 fuelFlowRate = scalar, U16, 100, "gram/s", 0.005, 0
fuelFlowRate = scalar, U16, 102, "gram/s", 0.005, 0 veTableYAxis = scalar, U16, 102, "%", 0.01, 0
veTableYAxis = scalar, U16, 104, "%", 0.01, 0 afrTableYAxis = scalar, U16, 104, "%", 0.01, 0
afrTableYAxis = scalar, U16, 106, "%", 0.01, 0
knockLevel = scalar, F32, 108, "Volts", 1, 0 knockLevel = scalar, F32, 108, "Volts", 1, 0
seconds = scalar, U32, 112, "sec", 1, 0 seconds = scalar, U32, 112, "sec", 1, 0
engineMode = scalar, U32, 116, "em", 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 = iatCorrection, "fuel: IAT correction", float, "%.3f"
entry = cltCorrection, "fuel: CLT correction", float, "%.3f" entry = cltCorrection, "fuel: CLT correction", float, "%.3f"
entry = baroCorrection, "fuel: Barometric pressure 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 = wallFuelAmount, "fuel: wall amount", float, "%.3f"
entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f" entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f"
entry = revolutionCounterSinceStart, "revolutionCounterSinceStart", int, "%d" 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_DIFF, "mapVvt_MAP_AT_DIFF", float, "%.3f"
entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d" entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d"
entry = mapVvt_map_peak, "mapVvt_map_peak", 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 = totalRevolutionCounter, "Crank revolution counter", int, "%d"
entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f" entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f"
entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f" entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f"

42
firmware/tunerstudio/generated/rusefi_prometheus_405.ini
View File

@ -86,7 +86,7 @@ enable2ndByteCanID = false
; name = scalar, type, offset, units, scale, translate, lo, hi, digits ; name = scalar, type, offset, units, scale, translate, lo, hi, digits
; CONFIG_DEFINITION_START ; 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 pageSize = 21300
page = 1 page = 1
@ -2192,25 +2192,24 @@ injectorLagMs = scalar, U16, 62, "ms", 0.0033333333333333335, 0
iatCorrection = scalar, U16, 64, "%", 0.01, 0 iatCorrection = scalar, U16, 64, "%", 0.01, 0
cltCorrection = scalar, U16, 66, "%", 0.01, 0 cltCorrection = scalar, U16, 66, "%", 0.01, 0
baroCorrection = scalar, U16, 68, "%", 0.01, 0 baroCorrection = scalar, U16, 68, "%", 0.01, 0
currentEnginePhase = scalar, U16, 70, "deg", 1, 0 wallFuelAmount = scalar, U16, 70, "mg", 0.01, 0
wallFuelAmount = scalar, U16, 72, "mg", 0.01, 0 wallFuelCorrection = scalar, S16, 72, "mg", 0.01, 0
wallFuelCorrection = scalar, S16, 74, "mg", 0.01, 0 revolutionCounterSinceStart = scalar, U16, 74, "", 1, 0
revolutionCounterSinceStart = scalar, U16, 76, "", 1, 0 deltaTps = scalar, S16, 76, "ratio", 0.01, 0
deltaTps = scalar, S16, 78, "ratio", 0.01, 0 canReadCounter = scalar, U16, 78, "", 1, 0
canReadCounter = scalar, U16, 80, "", 1, 0 tpsAccelFuel = scalar, S16, 80, "ms", 0.0033333333333333335, 0
tpsAccelFuel = scalar, S16, 82, "ms", 0.0033333333333333335, 0 ignitionAdvance = scalar, S16, 82, "deg", 0.02, 0
ignitionAdvance = scalar, S16, 84, "deg", 0.02, 0 sparkDwellValue = scalar, U16, 84, "ms", 0.0033333333333333335, 0
sparkDwellValue = scalar, U16, 86, "ms", 0.0033333333333333335, 0 coilDutyCycle = scalar, U16, 86, "%", 0.01, 0
coilDutyCycle = scalar, U16, 88, "%", 0.01, 0 idleAirValvePosition = scalar, U16, 88, "%", 0.01, 0
idleAirValvePosition = scalar, U16, 90, "%", 0.01, 0 etbTarget = scalar, S16, 90, "%", 0.01, 0
etbTarget = scalar, S16, 92, "%", 0.01, 0 etb1DutyCycle = scalar, S16, 92, "%", 0.01, 0
etb1DutyCycle = scalar, S16, 94, "%", 0.01, 0 etb1Error = scalar, S16, 94, "%", 0.01, 0
etb1Error = scalar, S16, 96, "%", 0.01, 0 fuelTankLevel = scalar, S16, 96, "%", 0.01, 0
fuelTankLevel = scalar, S16, 98, "%", 0.01, 0 totalFuelConsumption = scalar, U16, 98, "grams", 1, 0
totalFuelConsumption = scalar, U16, 100, "grams", 1, 0 fuelFlowRate = scalar, U16, 100, "gram/s", 0.005, 0
fuelFlowRate = scalar, U16, 102, "gram/s", 0.005, 0 veTableYAxis = scalar, U16, 102, "%", 0.01, 0
veTableYAxis = scalar, U16, 104, "%", 0.01, 0 afrTableYAxis = scalar, U16, 104, "%", 0.01, 0
afrTableYAxis = scalar, U16, 106, "%", 0.01, 0
knockLevel = scalar, F32, 108, "Volts", 1, 0 knockLevel = scalar, F32, 108, "Volts", 1, 0
seconds = scalar, U32, 112, "sec", 1, 0 seconds = scalar, U32, 112, "sec", 1, 0
engineMode = scalar, U32, 116, "em", 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 = iatCorrection, "fuel: IAT correction", float, "%.3f"
entry = cltCorrection, "fuel: CLT correction", float, "%.3f" entry = cltCorrection, "fuel: CLT correction", float, "%.3f"
entry = baroCorrection, "fuel: Barometric pressure 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 = wallFuelAmount, "fuel: wall amount", float, "%.3f"
entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f" entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f"
entry = revolutionCounterSinceStart, "revolutionCounterSinceStart", int, "%d" 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_DIFF, "mapVvt_MAP_AT_DIFF", float, "%.3f"
entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d" entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d"
entry = mapVvt_map_peak, "mapVvt_map_peak", 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 = totalRevolutionCounter, "Crank revolution counter", int, "%d"
entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f" entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f"
entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f" entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f"

42
firmware/tunerstudio/generated/rusefi_prometheus_469.ini
View File

@ -86,7 +86,7 @@ enable2ndByteCanID = false
; name = scalar, type, offset, units, scale, translate, lo, hi, digits ; name = scalar, type, offset, units, scale, translate, lo, hi, digits
; CONFIG_DEFINITION_START ; 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 pageSize = 21300
page = 1 page = 1
@ -2192,25 +2192,24 @@ injectorLagMs = scalar, U16, 62, "ms", 0.0033333333333333335, 0
iatCorrection = scalar, U16, 64, "%", 0.01, 0 iatCorrection = scalar, U16, 64, "%", 0.01, 0
cltCorrection = scalar, U16, 66, "%", 0.01, 0 cltCorrection = scalar, U16, 66, "%", 0.01, 0
baroCorrection = scalar, U16, 68, "%", 0.01, 0 baroCorrection = scalar, U16, 68, "%", 0.01, 0
currentEnginePhase = scalar, U16, 70, "deg", 1, 0 wallFuelAmount = scalar, U16, 70, "mg", 0.01, 0
wallFuelAmount = scalar, U16, 72, "mg", 0.01, 0 wallFuelCorrection = scalar, S16, 72, "mg", 0.01, 0
wallFuelCorrection = scalar, S16, 74, "mg", 0.01, 0 revolutionCounterSinceStart = scalar, U16, 74, "", 1, 0
revolutionCounterSinceStart = scalar, U16, 76, "", 1, 0 deltaTps = scalar, S16, 76, "ratio", 0.01, 0
deltaTps = scalar, S16, 78, "ratio", 0.01, 0 canReadCounter = scalar, U16, 78, "", 1, 0
canReadCounter = scalar, U16, 80, "", 1, 0 tpsAccelFuel = scalar, S16, 80, "ms", 0.0033333333333333335, 0
tpsAccelFuel = scalar, S16, 82, "ms", 0.0033333333333333335, 0 ignitionAdvance = scalar, S16, 82, "deg", 0.02, 0
ignitionAdvance = scalar, S16, 84, "deg", 0.02, 0 sparkDwellValue = scalar, U16, 84, "ms", 0.0033333333333333335, 0
sparkDwellValue = scalar, U16, 86, "ms", 0.0033333333333333335, 0 coilDutyCycle = scalar, U16, 86, "%", 0.01, 0
coilDutyCycle = scalar, U16, 88, "%", 0.01, 0 idleAirValvePosition = scalar, U16, 88, "%", 0.01, 0
idleAirValvePosition = scalar, U16, 90, "%", 0.01, 0 etbTarget = scalar, S16, 90, "%", 0.01, 0
etbTarget = scalar, S16, 92, "%", 0.01, 0 etb1DutyCycle = scalar, S16, 92, "%", 0.01, 0
etb1DutyCycle = scalar, S16, 94, "%", 0.01, 0 etb1Error = scalar, S16, 94, "%", 0.01, 0
etb1Error = scalar, S16, 96, "%", 0.01, 0 fuelTankLevel = scalar, S16, 96, "%", 0.01, 0
fuelTankLevel = scalar, S16, 98, "%", 0.01, 0 totalFuelConsumption = scalar, U16, 98, "grams", 1, 0
totalFuelConsumption = scalar, U16, 100, "grams", 1, 0 fuelFlowRate = scalar, U16, 100, "gram/s", 0.005, 0
fuelFlowRate = scalar, U16, 102, "gram/s", 0.005, 0 veTableYAxis = scalar, U16, 102, "%", 0.01, 0
veTableYAxis = scalar, U16, 104, "%", 0.01, 0 afrTableYAxis = scalar, U16, 104, "%", 0.01, 0
afrTableYAxis = scalar, U16, 106, "%", 0.01, 0
knockLevel = scalar, F32, 108, "Volts", 1, 0 knockLevel = scalar, F32, 108, "Volts", 1, 0
seconds = scalar, U32, 112, "sec", 1, 0 seconds = scalar, U32, 112, "sec", 1, 0
engineMode = scalar, U32, 116, "em", 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 = iatCorrection, "fuel: IAT correction", float, "%.3f"
entry = cltCorrection, "fuel: CLT correction", float, "%.3f" entry = cltCorrection, "fuel: CLT correction", float, "%.3f"
entry = baroCorrection, "fuel: Barometric pressure 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 = wallFuelAmount, "fuel: wall amount", float, "%.3f"
entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f" entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f"
entry = revolutionCounterSinceStart, "revolutionCounterSinceStart", int, "%d" 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_DIFF, "mapVvt_MAP_AT_DIFF", float, "%.3f"
entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d" entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d"
entry = mapVvt_map_peak, "mapVvt_map_peak", 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 = totalRevolutionCounter, "Crank revolution counter", int, "%d"
entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f" entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f"
entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f" entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f"

42
firmware/tunerstudio/generated/rusefi_proteus_f4.ini
View File

@ -86,7 +86,7 @@ enable2ndByteCanID = false
; name = scalar, type, offset, units, scale, translate, lo, hi, digits ; name = scalar, type, offset, units, scale, translate, lo, hi, digits
; CONFIG_DEFINITION_START ; 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 pageSize = 21300
page = 1 page = 1
@ -2192,25 +2192,24 @@ injectorLagMs = scalar, U16, 62, "ms", 0.0033333333333333335, 0
iatCorrection = scalar, U16, 64, "%", 0.01, 0 iatCorrection = scalar, U16, 64, "%", 0.01, 0
cltCorrection = scalar, U16, 66, "%", 0.01, 0 cltCorrection = scalar, U16, 66, "%", 0.01, 0
baroCorrection = scalar, U16, 68, "%", 0.01, 0 baroCorrection = scalar, U16, 68, "%", 0.01, 0
currentEnginePhase = scalar, U16, 70, "deg", 1, 0 wallFuelAmount = scalar, U16, 70, "mg", 0.01, 0
wallFuelAmount = scalar, U16, 72, "mg", 0.01, 0 wallFuelCorrection = scalar, S16, 72, "mg", 0.01, 0
wallFuelCorrection = scalar, S16, 74, "mg", 0.01, 0 revolutionCounterSinceStart = scalar, U16, 74, "", 1, 0
revolutionCounterSinceStart = scalar, U16, 76, "", 1, 0 deltaTps = scalar, S16, 76, "ratio", 0.01, 0
deltaTps = scalar, S16, 78, "ratio", 0.01, 0 canReadCounter = scalar, U16, 78, "", 1, 0
canReadCounter = scalar, U16, 80, "", 1, 0 tpsAccelFuel = scalar, S16, 80, "ms", 0.0033333333333333335, 0
tpsAccelFuel = scalar, S16, 82, "ms", 0.0033333333333333335, 0 ignitionAdvance = scalar, S16, 82, "deg", 0.02, 0
ignitionAdvance = scalar, S16, 84, "deg", 0.02, 0 sparkDwellValue = scalar, U16, 84, "ms", 0.0033333333333333335, 0
sparkDwellValue = scalar, U16, 86, "ms", 0.0033333333333333335, 0 coilDutyCycle = scalar, U16, 86, "%", 0.01, 0
coilDutyCycle = scalar, U16, 88, "%", 0.01, 0 idleAirValvePosition = scalar, U16, 88, "%", 0.01, 0
idleAirValvePosition = scalar, U16, 90, "%", 0.01, 0 etbTarget = scalar, S16, 90, "%", 0.01, 0
etbTarget = scalar, S16, 92, "%", 0.01, 0 etb1DutyCycle = scalar, S16, 92, "%", 0.01, 0
etb1DutyCycle = scalar, S16, 94, "%", 0.01, 0 etb1Error = scalar, S16, 94, "%", 0.01, 0
etb1Error = scalar, S16, 96, "%", 0.01, 0 fuelTankLevel = scalar, S16, 96, "%", 0.01, 0
fuelTankLevel = scalar, S16, 98, "%", 0.01, 0 totalFuelConsumption = scalar, U16, 98, "grams", 1, 0
totalFuelConsumption = scalar, U16, 100, "grams", 1, 0 fuelFlowRate = scalar, U16, 100, "gram/s", 0.005, 0
fuelFlowRate = scalar, U16, 102, "gram/s", 0.005, 0 veTableYAxis = scalar, U16, 102, "%", 0.01, 0
veTableYAxis = scalar, U16, 104, "%", 0.01, 0 afrTableYAxis = scalar, U16, 104, "%", 0.01, 0
afrTableYAxis = scalar, U16, 106, "%", 0.01, 0
knockLevel = scalar, F32, 108, "Volts", 1, 0 knockLevel = scalar, F32, 108, "Volts", 1, 0
seconds = scalar, U32, 112, "sec", 1, 0 seconds = scalar, U32, 112, "sec", 1, 0
engineMode = scalar, U32, 116, "em", 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 = iatCorrection, "fuel: IAT correction", float, "%.3f"
entry = cltCorrection, "fuel: CLT correction", float, "%.3f" entry = cltCorrection, "fuel: CLT correction", float, "%.3f"
entry = baroCorrection, "fuel: Barometric pressure 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 = wallFuelAmount, "fuel: wall amount", float, "%.3f"
entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f" entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f"
entry = revolutionCounterSinceStart, "revolutionCounterSinceStart", int, "%d" 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_DIFF, "mapVvt_MAP_AT_DIFF", float, "%.3f"
entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d" entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d"
entry = mapVvt_map_peak, "mapVvt_map_peak", 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 = totalRevolutionCounter, "Crank revolution counter", int, "%d"
entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f" entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f"
entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f" entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f"

42
firmware/tunerstudio/generated/rusefi_proteus_f7.ini
View File

@ -86,7 +86,7 @@ enable2ndByteCanID = false
; name = scalar, type, offset, units, scale, translate, lo, hi, digits ; name = scalar, type, offset, units, scale, translate, lo, hi, digits
; CONFIG_DEFINITION_START ; 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 pageSize = 21300
page = 1 page = 1
@ -2192,25 +2192,24 @@ injectorLagMs = scalar, U16, 62, "ms", 0.0033333333333333335, 0
iatCorrection = scalar, U16, 64, "%", 0.01, 0 iatCorrection = scalar, U16, 64, "%", 0.01, 0
cltCorrection = scalar, U16, 66, "%", 0.01, 0 cltCorrection = scalar, U16, 66, "%", 0.01, 0
baroCorrection = scalar, U16, 68, "%", 0.01, 0 baroCorrection = scalar, U16, 68, "%", 0.01, 0
currentEnginePhase = scalar, U16, 70, "deg", 1, 0 wallFuelAmount = scalar, U16, 70, "mg", 0.01, 0
wallFuelAmount = scalar, U16, 72, "mg", 0.01, 0 wallFuelCorrection = scalar, S16, 72, "mg", 0.01, 0
wallFuelCorrection = scalar, S16, 74, "mg", 0.01, 0 revolutionCounterSinceStart = scalar, U16, 74, "", 1, 0
revolutionCounterSinceStart = scalar, U16, 76, "", 1, 0 deltaTps = scalar, S16, 76, "ratio", 0.01, 0
deltaTps = scalar, S16, 78, "ratio", 0.01, 0 canReadCounter = scalar, U16, 78, "", 1, 0
canReadCounter = scalar, U16, 80, "", 1, 0 tpsAccelFuel = scalar, S16, 80, "ms", 0.0033333333333333335, 0
tpsAccelFuel = scalar, S16, 82, "ms", 0.0033333333333333335, 0 ignitionAdvance = scalar, S16, 82, "deg", 0.02, 0
ignitionAdvance = scalar, S16, 84, "deg", 0.02, 0 sparkDwellValue = scalar, U16, 84, "ms", 0.0033333333333333335, 0
sparkDwellValue = scalar, U16, 86, "ms", 0.0033333333333333335, 0 coilDutyCycle = scalar, U16, 86, "%", 0.01, 0
coilDutyCycle = scalar, U16, 88, "%", 0.01, 0 idleAirValvePosition = scalar, U16, 88, "%", 0.01, 0
idleAirValvePosition = scalar, U16, 90, "%", 0.01, 0 etbTarget = scalar, S16, 90, "%", 0.01, 0
etbTarget = scalar, S16, 92, "%", 0.01, 0 etb1DutyCycle = scalar, S16, 92, "%", 0.01, 0
etb1DutyCycle = scalar, S16, 94, "%", 0.01, 0 etb1Error = scalar, S16, 94, "%", 0.01, 0
etb1Error = scalar, S16, 96, "%", 0.01, 0 fuelTankLevel = scalar, S16, 96, "%", 0.01, 0
fuelTankLevel = scalar, S16, 98, "%", 0.01, 0 totalFuelConsumption = scalar, U16, 98, "grams", 1, 0
totalFuelConsumption = scalar, U16, 100, "grams", 1, 0 fuelFlowRate = scalar, U16, 100, "gram/s", 0.005, 0
fuelFlowRate = scalar, U16, 102, "gram/s", 0.005, 0 veTableYAxis = scalar, U16, 102, "%", 0.01, 0
veTableYAxis = scalar, U16, 104, "%", 0.01, 0 afrTableYAxis = scalar, U16, 104, "%", 0.01, 0
afrTableYAxis = scalar, U16, 106, "%", 0.01, 0
knockLevel = scalar, F32, 108, "Volts", 1, 0 knockLevel = scalar, F32, 108, "Volts", 1, 0
seconds = scalar, U32, 112, "sec", 1, 0 seconds = scalar, U32, 112, "sec", 1, 0
engineMode = scalar, U32, 116, "em", 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 = iatCorrection, "fuel: IAT correction", float, "%.3f"
entry = cltCorrection, "fuel: CLT correction", float, "%.3f" entry = cltCorrection, "fuel: CLT correction", float, "%.3f"
entry = baroCorrection, "fuel: Barometric pressure 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 = wallFuelAmount, "fuel: wall amount", float, "%.3f"
entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f" entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f"
entry = revolutionCounterSinceStart, "revolutionCounterSinceStart", int, "%d" 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_DIFF, "mapVvt_MAP_AT_DIFF", float, "%.3f"
entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d" entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d"
entry = mapVvt_map_peak, "mapVvt_map_peak", 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 = totalRevolutionCounter, "Crank revolution counter", int, "%d"
entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f" entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f"
entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f" entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f"

42
firmware/tunerstudio/generated/rusefi_proteus_h7.ini
View File

@ -86,7 +86,7 @@ enable2ndByteCanID = false
; name = scalar, type, offset, units, scale, translate, lo, hi, digits ; name = scalar, type, offset, units, scale, translate, lo, hi, digits
; CONFIG_DEFINITION_START ; 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 pageSize = 21300
page = 1 page = 1
@ -2192,25 +2192,24 @@ injectorLagMs = scalar, U16, 62, "ms", 0.0033333333333333335, 0
iatCorrection = scalar, U16, 64, "%", 0.01, 0 iatCorrection = scalar, U16, 64, "%", 0.01, 0
cltCorrection = scalar, U16, 66, "%", 0.01, 0 cltCorrection = scalar, U16, 66, "%", 0.01, 0
baroCorrection = scalar, U16, 68, "%", 0.01, 0 baroCorrection = scalar, U16, 68, "%", 0.01, 0
currentEnginePhase = scalar, U16, 70, "deg", 1, 0 wallFuelAmount = scalar, U16, 70, "mg", 0.01, 0
wallFuelAmount = scalar, U16, 72, "mg", 0.01, 0 wallFuelCorrection = scalar, S16, 72, "mg", 0.01, 0
wallFuelCorrection = scalar, S16, 74, "mg", 0.01, 0 revolutionCounterSinceStart = scalar, U16, 74, "", 1, 0
revolutionCounterSinceStart = scalar, U16, 76, "", 1, 0 deltaTps = scalar, S16, 76, "ratio", 0.01, 0
deltaTps = scalar, S16, 78, "ratio", 0.01, 0 canReadCounter = scalar, U16, 78, "", 1, 0
canReadCounter = scalar, U16, 80, "", 1, 0 tpsAccelFuel = scalar, S16, 80, "ms", 0.0033333333333333335, 0
tpsAccelFuel = scalar, S16, 82, "ms", 0.0033333333333333335, 0 ignitionAdvance = scalar, S16, 82, "deg", 0.02, 0
ignitionAdvance = scalar, S16, 84, "deg", 0.02, 0 sparkDwellValue = scalar, U16, 84, "ms", 0.0033333333333333335, 0
sparkDwellValue = scalar, U16, 86, "ms", 0.0033333333333333335, 0 coilDutyCycle = scalar, U16, 86, "%", 0.01, 0
coilDutyCycle = scalar, U16, 88, "%", 0.01, 0 idleAirValvePosition = scalar, U16, 88, "%", 0.01, 0
idleAirValvePosition = scalar, U16, 90, "%", 0.01, 0 etbTarget = scalar, S16, 90, "%", 0.01, 0
etbTarget = scalar, S16, 92, "%", 0.01, 0 etb1DutyCycle = scalar, S16, 92, "%", 0.01, 0
etb1DutyCycle = scalar, S16, 94, "%", 0.01, 0 etb1Error = scalar, S16, 94, "%", 0.01, 0
etb1Error = scalar, S16, 96, "%", 0.01, 0 fuelTankLevel = scalar, S16, 96, "%", 0.01, 0
fuelTankLevel = scalar, S16, 98, "%", 0.01, 0 totalFuelConsumption = scalar, U16, 98, "grams", 1, 0
totalFuelConsumption = scalar, U16, 100, "grams", 1, 0 fuelFlowRate = scalar, U16, 100, "gram/s", 0.005, 0
fuelFlowRate = scalar, U16, 102, "gram/s", 0.005, 0 veTableYAxis = scalar, U16, 102, "%", 0.01, 0
veTableYAxis = scalar, U16, 104, "%", 0.01, 0 afrTableYAxis = scalar, U16, 104, "%", 0.01, 0
afrTableYAxis = scalar, U16, 106, "%", 0.01, 0
knockLevel = scalar, F32, 108, "Volts", 1, 0 knockLevel = scalar, F32, 108, "Volts", 1, 0
seconds = scalar, U32, 112, "sec", 1, 0 seconds = scalar, U32, 112, "sec", 1, 0
engineMode = scalar, U32, 116, "em", 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 = iatCorrection, "fuel: IAT correction", float, "%.3f"
entry = cltCorrection, "fuel: CLT correction", float, "%.3f" entry = cltCorrection, "fuel: CLT correction", float, "%.3f"
entry = baroCorrection, "fuel: Barometric pressure 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 = wallFuelAmount, "fuel: wall amount", float, "%.3f"
entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f" entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f"
entry = revolutionCounterSinceStart, "revolutionCounterSinceStart", int, "%d" 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_DIFF, "mapVvt_MAP_AT_DIFF", float, "%.3f"
entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d" entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d"
entry = mapVvt_map_peak, "mapVvt_map_peak", 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 = totalRevolutionCounter, "Crank revolution counter", int, "%d"
entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f" entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f"
entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f" entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f"

42
firmware/tunerstudio/generated/rusefi_subaru_eg33_f7.ini
View File

@ -86,7 +86,7 @@ enable2ndByteCanID = false
; name = scalar, type, offset, units, scale, translate, lo, hi, digits ; name = scalar, type, offset, units, scale, translate, lo, hi, digits
; CONFIG_DEFINITION_START ; 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 pageSize = 21300
page = 1 page = 1
@ -2192,25 +2192,24 @@ injectorLagMs = scalar, U16, 62, "ms", 0.0033333333333333335, 0
iatCorrection = scalar, U16, 64, "%", 0.01, 0 iatCorrection = scalar, U16, 64, "%", 0.01, 0
cltCorrection = scalar, U16, 66, "%", 0.01, 0 cltCorrection = scalar, U16, 66, "%", 0.01, 0
baroCorrection = scalar, U16, 68, "%", 0.01, 0 baroCorrection = scalar, U16, 68, "%", 0.01, 0
currentEnginePhase = scalar, U16, 70, "deg", 1, 0 wallFuelAmount = scalar, U16, 70, "mg", 0.01, 0
wallFuelAmount = scalar, U16, 72, "mg", 0.01, 0 wallFuelCorrection = scalar, S16, 72, "mg", 0.01, 0
wallFuelCorrection = scalar, S16, 74, "mg", 0.01, 0 revolutionCounterSinceStart = scalar, U16, 74, "", 1, 0
revolutionCounterSinceStart = scalar, U16, 76, "", 1, 0 deltaTps = scalar, S16, 76, "ratio", 0.01, 0
deltaTps = scalar, S16, 78, "ratio", 0.01, 0 canReadCounter = scalar, U16, 78, "", 1, 0
canReadCounter = scalar, U16, 80, "", 1, 0 tpsAccelFuel = scalar, S16, 80, "ms", 0.0033333333333333335, 0
tpsAccelFuel = scalar, S16, 82, "ms", 0.0033333333333333335, 0 ignitionAdvance = scalar, S16, 82, "deg", 0.02, 0
ignitionAdvance = scalar, S16, 84, "deg", 0.02, 0 sparkDwellValue = scalar, U16, 84, "ms", 0.0033333333333333335, 0
sparkDwellValue = scalar, U16, 86, "ms", 0.0033333333333333335, 0 coilDutyCycle = scalar, U16, 86, "%", 0.01, 0
coilDutyCycle = scalar, U16, 88, "%", 0.01, 0 idleAirValvePosition = scalar, U16, 88, "%", 0.01, 0
idleAirValvePosition = scalar, U16, 90, "%", 0.01, 0 etbTarget = scalar, S16, 90, "%", 0.01, 0
etbTarget = scalar, S16, 92, "%", 0.01, 0 etb1DutyCycle = scalar, S16, 92, "%", 0.01, 0
etb1DutyCycle = scalar, S16, 94, "%", 0.01, 0 etb1Error = scalar, S16, 94, "%", 0.01, 0
etb1Error = scalar, S16, 96, "%", 0.01, 0 fuelTankLevel = scalar, S16, 96, "%", 0.01, 0
fuelTankLevel = scalar, S16, 98, "%", 0.01, 0 totalFuelConsumption = scalar, U16, 98, "grams", 1, 0
totalFuelConsumption = scalar, U16, 100, "grams", 1, 0 fuelFlowRate = scalar, U16, 100, "gram/s", 0.005, 0
fuelFlowRate = scalar, U16, 102, "gram/s", 0.005, 0 veTableYAxis = scalar, U16, 102, "%", 0.01, 0
veTableYAxis = scalar, U16, 104, "%", 0.01, 0 afrTableYAxis = scalar, U16, 104, "%", 0.01, 0
afrTableYAxis = scalar, U16, 106, "%", 0.01, 0
knockLevel = scalar, F32, 108, "Volts", 1, 0 knockLevel = scalar, F32, 108, "Volts", 1, 0
seconds = scalar, U32, 112, "sec", 1, 0 seconds = scalar, U32, 112, "sec", 1, 0
engineMode = scalar, U32, 116, "em", 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 = iatCorrection, "fuel: IAT correction", float, "%.3f"
entry = cltCorrection, "fuel: CLT correction", float, "%.3f" entry = cltCorrection, "fuel: CLT correction", float, "%.3f"
entry = baroCorrection, "fuel: Barometric pressure 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 = wallFuelAmount, "fuel: wall amount", float, "%.3f"
entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f" entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f"
entry = revolutionCounterSinceStart, "revolutionCounterSinceStart", int, "%d" 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_DIFF, "mapVvt_MAP_AT_DIFF", float, "%.3f"
entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d" entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d"
entry = mapVvt_map_peak, "mapVvt_map_peak", 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 = totalRevolutionCounter, "Crank revolution counter", int, "%d"
entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f" entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f"
entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f" entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f"

42
firmware/tunerstudio/generated/rusefi_tdg-pdm8.ini
View File

@ -86,7 +86,7 @@ enable2ndByteCanID = false
; name = scalar, type, offset, units, scale, translate, lo, hi, digits ; name = scalar, type, offset, units, scale, translate, lo, hi, digits
; CONFIG_DEFINITION_START ; 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 pageSize = 21300
page = 1 page = 1
@ -2192,25 +2192,24 @@ injectorLagMs = scalar, U16, 62, "ms", 0.0033333333333333335, 0
iatCorrection = scalar, U16, 64, "%", 0.01, 0 iatCorrection = scalar, U16, 64, "%", 0.01, 0
cltCorrection = scalar, U16, 66, "%", 0.01, 0 cltCorrection = scalar, U16, 66, "%", 0.01, 0
baroCorrection = scalar, U16, 68, "%", 0.01, 0 baroCorrection = scalar, U16, 68, "%", 0.01, 0
currentEnginePhase = scalar, U16, 70, "deg", 1, 0 wallFuelAmount = scalar, U16, 70, "mg", 0.01, 0
wallFuelAmount = scalar, U16, 72, "mg", 0.01, 0 wallFuelCorrection = scalar, S16, 72, "mg", 0.01, 0
wallFuelCorrection = scalar, S16, 74, "mg", 0.01, 0 revolutionCounterSinceStart = scalar, U16, 74, "", 1, 0
revolutionCounterSinceStart = scalar, U16, 76, "", 1, 0 deltaTps = scalar, S16, 76, "ratio", 0.01, 0
deltaTps = scalar, S16, 78, "ratio", 0.01, 0 canReadCounter = scalar, U16, 78, "", 1, 0
canReadCounter = scalar, U16, 80, "", 1, 0 tpsAccelFuel = scalar, S16, 80, "ms", 0.0033333333333333335, 0
tpsAccelFuel = scalar, S16, 82, "ms", 0.0033333333333333335, 0 ignitionAdvance = scalar, S16, 82, "deg", 0.02, 0
ignitionAdvance = scalar, S16, 84, "deg", 0.02, 0 sparkDwellValue = scalar, U16, 84, "ms", 0.0033333333333333335, 0
sparkDwellValue = scalar, U16, 86, "ms", 0.0033333333333333335, 0 coilDutyCycle = scalar, U16, 86, "%", 0.01, 0
coilDutyCycle = scalar, U16, 88, "%", 0.01, 0 idleAirValvePosition = scalar, U16, 88, "%", 0.01, 0
idleAirValvePosition = scalar, U16, 90, "%", 0.01, 0 etbTarget = scalar, S16, 90, "%", 0.01, 0
etbTarget = scalar, S16, 92, "%", 0.01, 0 etb1DutyCycle = scalar, S16, 92, "%", 0.01, 0
etb1DutyCycle = scalar, S16, 94, "%", 0.01, 0 etb1Error = scalar, S16, 94, "%", 0.01, 0
etb1Error = scalar, S16, 96, "%", 0.01, 0 fuelTankLevel = scalar, S16, 96, "%", 0.01, 0
fuelTankLevel = scalar, S16, 98, "%", 0.01, 0 totalFuelConsumption = scalar, U16, 98, "grams", 1, 0
totalFuelConsumption = scalar, U16, 100, "grams", 1, 0 fuelFlowRate = scalar, U16, 100, "gram/s", 0.005, 0
fuelFlowRate = scalar, U16, 102, "gram/s", 0.005, 0 veTableYAxis = scalar, U16, 102, "%", 0.01, 0
veTableYAxis = scalar, U16, 104, "%", 0.01, 0 afrTableYAxis = scalar, U16, 104, "%", 0.01, 0
afrTableYAxis = scalar, U16, 106, "%", 0.01, 0
knockLevel = scalar, F32, 108, "Volts", 1, 0 knockLevel = scalar, F32, 108, "Volts", 1, 0
seconds = scalar, U32, 112, "sec", 1, 0 seconds = scalar, U32, 112, "sec", 1, 0
engineMode = scalar, U32, 116, "em", 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 = iatCorrection, "fuel: IAT correction", float, "%.3f"
entry = cltCorrection, "fuel: CLT correction", float, "%.3f" entry = cltCorrection, "fuel: CLT correction", float, "%.3f"
entry = baroCorrection, "fuel: Barometric pressure 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 = wallFuelAmount, "fuel: wall amount", float, "%.3f"
entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f" entry = wallFuelCorrection, "fuel: wall correction", float, "%.3f"
entry = revolutionCounterSinceStart, "revolutionCounterSinceStart", int, "%d" 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_DIFF, "mapVvt_MAP_AT_DIFF", float, "%.3f"
entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d" entry = mapVvt_MAP_AT_CYCLE_COUNT, "mapVvt_MAP_AT_CYCLE_COUNT", int, "%d"
entry = mapVvt_map_peak, "mapVvt_map_peak", 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 = totalRevolutionCounter, "Crank revolution counter", int, "%d"
entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f" entry = vvtSyncGapRatio, "vvtSyncGapRatio", float, "%.3f"
entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f" entry = vvtCurrentPosition, "vvtCurrentPosition", float, "%.3f"

42
java_console/models/src/main/java/com/rusefi/config/generated/TsOutputs.java
View File

@ -1,6 +1,6 @@
package com.rusefi.config.generated; 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 // by class com.rusefi.output.FileJavaFieldsConsumer
import com.rusefi.config.*; 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 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 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 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", 70, FieldType.INT16).setScale(0.01);
public static final Field WALLFUELAMOUNT = Field.create("WALLFUELAMOUNT", 72, FieldType.INT16).setScale(0.01); public static final Field WALLFUELCORRECTION = Field.create("WALLFUELCORRECTION", 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", 74, FieldType.INT16).setScale(1.0);
public static final Field REVOLUTIONCOUNTERSINCESTART = Field.create("REVOLUTIONCOUNTERSINCESTART", 76, FieldType.INT16).setScale(1.0); public static final Field DELTATPS = Field.create("DELTATPS", 76, FieldType.INT16).setScale(0.01);
public static final Field DELTATPS = Field.create("DELTATPS", 78, FieldType.INT16).setScale(0.01); public static final Field CANREADCOUNTER = Field.create("CANREADCOUNTER", 78, FieldType.INT16).setScale(1.0);
public static final Field CANREADCOUNTER = Field.create("CANREADCOUNTER", 80, FieldType.INT16).setScale(1.0); public static final Field TPSACCELFUEL = Field.create("TPSACCELFUEL", 80, FieldType.INT16).setScale(0.0033333333333333335);
public static final Field TPSACCELFUEL = Field.create("TPSACCELFUEL", 82, FieldType.INT16).setScale(0.0033333333333333335); public static final Field IGNITIONADVANCE = Field.create("IGNITIONADVANCE", 82, FieldType.INT16).setScale(0.02);
public static final Field IGNITIONADVANCE = Field.create("IGNITIONADVANCE", 84, FieldType.INT16).setScale(0.02); public static final Field SPARKDWELLVALUE = Field.create("SPARKDWELLVALUE", 84, FieldType.INT16).setScale(0.0033333333333333335);
public static final Field SPARKDWELLVALUE = Field.create("SPARKDWELLVALUE", 86, FieldType.INT16).setScale(0.0033333333333333335); public static final Field COILDUTYCYCLE = Field.create("COILDUTYCYCLE", 86, FieldType.INT16).setScale(0.01);
public static final Field COILDUTYCYCLE = Field.create("COILDUTYCYCLE", 88, FieldType.INT16).setScale(0.01); public static final Field IDLEAIRVALVEPOSITION = Field.create("IDLEAIRVALVEPOSITION", 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", 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", 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", 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", 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", 98, FieldType.INT16).setScale(1.0);
public static final Field TOTALFUELCONSUMPTION = Field.create("TOTALFUELCONSUMPTION", 100, FieldType.INT16).setScale(1.0); public static final Field FUELFLOWRATE = Field.create("FUELFLOWRATE", 100, FieldType.INT16).setScale(0.005);
public static final Field FUELFLOWRATE = Field.create("FUELFLOWRATE", 102, FieldType.INT16).setScale(0.005); public static final Field VETABLEYAXIS = Field.create("VETABLEYAXIS", 102, FieldType.INT16).setScale(0.01);
public static final Field VETABLEYAXIS = Field.create("VETABLEYAXIS", 104, FieldType.INT16).setScale(0.01); public static final Field AFRTABLEYAXIS = Field.create("AFRTABLEYAXIS", 104, FieldType.INT16).setScale(0.01);
public static final Field AFRTABLEYAXIS = Field.create("AFRTABLEYAXIS", 106, 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 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 SECONDS = Field.create("SECONDS", 112, FieldType.INT).setScale(1.0);
public static final Field ENGINEMODE = Field.create("ENGINEMODE", 116, 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, IATCORRECTION,
CLTCORRECTION, CLTCORRECTION,
BAROCORRECTION, BAROCORRECTION,
CURRENTENGINEPHASE,
WALLFUELAMOUNT, WALLFUELAMOUNT,
WALLFUELCORRECTION, WALLFUELCORRECTION,
REVOLUTIONCOUNTERSINCESTART, REVOLUTIONCOUNTERSINCESTART,
@ -998,6 +997,7 @@ public class TsOutputs {
FUELFLOWRATE, FUELFLOWRATE,
VETABLEYAXIS, VETABLEYAXIS,
AFRTABLEYAXIS, AFRTABLEYAXIS,
ALIGNMENTFILL_AT_106,
KNOCKLEVEL, KNOCKLEVEL,
SECONDS, SECONDS,
ENGINEMODE, ENGINEMODE,