fuel_math.cpp File Reference

Detailed Description

Fuel amount calculation logic.

Date

May 27, 2013

Author

Andrey Belomutskiy, (c) 2012-2020

This file is part of rusEfi - see http://rusefi.com

rusEfi is free software; you can redistribute it and/or modify it under the terms of the GNU General Public License as published by the Free Software Foundation; either version 3 of the License, or (at your option) any later version.

rusEfi is distributed in the hope that it will be useful, but WITHOUT ANY WARRANTY; without even the implied warranty of MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU General Public License for more details.

You should have received a copy of the GNU General Public License along with this program. If not, see http://www.gnu.org/licenses/.

Definition in file fuel_math.cpp.

Functions
float	getCrankingFuel3 (float baseFuel, uint32_t revolutionCounterSinceStart)
float	getRunningFuel (float baseFuel)
AirmassModelBase *	getAirmassModel (engine_load_mode_e mode)
float	getMaxAirflowAtMap (float map)
static float	getBaseFuelMass (float rpm)
angle_t	getInjectionOffset (float rpm, float load)
int	getNumberOfInjections (injection_mode_e mode)
float	getInjectionModeDurationMultiplier ()
percent_t	getInjectorDutyCycle (float rpm)
percent_t	getInjectorDutyCycleStage2 (float rpm)
float	getCycleFuelMass (bool isCranking, float baseFuelMass)
float	getInjectionMass (float rpm)
void	initFuelMap ()
	Initialize fuel map data structure.
float	getCltFuelCorrection ()
	Engine warm-up fuel correction.
float	getIatFuelCorrection ()
float	getPostCrankingFuelCorrection ()
float	getBaroCorrection ()
percent_t	getFuelALSCorrection (float rpm)
float	getCrankingFuel (float baseFuel)
float	getStandardAirCharge ()
PUBLIC_API_WEAK_SOMETHING_WEIRD float	getCylinderFuelTrim (size_t cylinderNumber, float rpm, float fuelLoad)
float	getStage2InjectionFraction (float rpm, float load)

Variables
ve_Map3D_t	veMap
static mapEstimate_Map3D_t	mapEstimationTable {"mape"}
static SpeedDensityAirmass	sdAirmass (veMap, mapEstimationTable)
static MafAirmass	mafAirmass (veMap)
static AlphaNAirmass	alphaNAirmass (veMap)
static Hysteresis	stage2Hysteresis

Function Documentation

getAirmassModel()

AirmassModelBase * getAirmassModel

(

engine_load_mode_e

mode

)

Definition at line 152 of file fuel_math.cpp.

                                                           {
    switch (mode) {
        case LM_SPEED_DENSITY: return &sdAirmass;
        case LM_REAL_MAF: return &mafAirmass;
        case LM_ALPHA_N: return &alphaNAirmass;
#if EFI_LUA
        case LM_LUA: return &(getLuaAirmassModel());
#endif
#if EFI_UNIT_TEST
        case LM_MOCK: return engine->mockAirmassModel;
#endif
        default:
            firmwareError(ObdCode::CUSTOM_ERR_ASSERT, "Invalid airmass mode %d", engineConfiguration->fuelAlgorithm);
            return nullptr;
    }
}

Referenced by getBaseFuelMass(), and lua_getAirmass().

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getBaroCorrection()

float getBaroCorrection

(

)

Definition at line 401 of file fuel_math.cpp.

                          {
    if (Sensor::hasSensor(SensorType::BarometricPressure)) {
        // Default to 1atm if failed
        float pressure = Sensor::get(SensorType::BarometricPressure).value_or(STD_ATMOSPHERE);
 
        float correction = interpolate3d(
            config->baroCorrTable,
            config->baroCorrPressureBins, pressure,
            config->baroCorrRpmBins, Sensor::getOrZero(SensorType::Rpm)
        );
 
        if (std::isnan(correction) || correction < 0.01) {
            warning(ObdCode::OBD_Barometric_Press_Circ_Range_Perf, "Invalid baro correction %f", correction);
            return 1;
        }
 
        return correction;
    } else {
        return 1;
    }
}

Referenced by EngineState::periodicFastCallback().

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getBaseFuelMass()

static float getBaseFuelMass ( float  rpm )

static

Definition at line 176 of file fuel_math.cpp.

                                        {
    ScopePerf perf(PE::GetBaseFuel);
 
    // airmass modes - get airmass first, then convert to fuel
    auto model = getAirmassModel(engineConfiguration->fuelAlgorithm);
    efiAssert(ObdCode::CUSTOM_ERR_ASSERT, model != nullptr, "Invalid airmass mode", 0.0f);
 
    auto airmass = model->getAirmass(rpm, true);
 
    // Plop some state for others to read
    float normalizedCylinderFilling = 100 * airmass.CylinderAirmass / getStandardAirCharge();
    engine->fuelComputer.sdAirMassInOneCylinder = airmass.CylinderAirmass;
    engine->fuelComputer.normalizedCylinderFilling = normalizedCylinderFilling;
    engine->engineState.fuelingLoad = airmass.EngineLoadPercent;
    engine->engineState.ignitionLoad = engine->fuelComputer.getLoadOverride(airmass.EngineLoadPercent, engineConfiguration->ignOverrideMode);
 
    auto gramPerCycle = airmass.CylinderAirmass * engineConfiguration->cylindersCount;
    auto gramPerMs = rpm == 0 ? 0 : gramPerCycle / getEngineCycleDuration(rpm);
 
    // convert g/s -> kg/h
    engine->engineState.airflowEstimate = gramPerMs * 3600000 /* milliseconds per hour */ / 1000 /* grams per kg */;
 
    float baseFuelMass = engine->fuelComputer.getCycleFuel(airmass.CylinderAirmass, rpm, airmass.EngineLoadPercent);
 
    engine->engineState.baseFuel = baseFuelMass;
 
    if (std::isnan(baseFuelMass)) {
        // todo: we should not have this here but https://github.com/rusefi/rusefi/issues/1690
        return 0;
    }
 
    return baseFuelMass;
}

Referenced by getInjectionMass().

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getCltFuelCorrection()

float getCltFuelCorrection

(

)

Engine warm-up fuel correction.

Definition at line 358 of file fuel_math.cpp.

                             {
    const auto clt = Sensor::get(SensorType::Clt);
 
    if (!clt)
        return 1; // this error should be already reported somewhere else, let's just handle it
 
    return interpolate2d(clt.Value, config->cltFuelCorrBins, config->cltFuelCorr);
}

Referenced by EngineState::periodicFastCallback().

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getCrankingFuel()

float getCrankingFuel

(

float

baseFuel

)

Returns

Duration of fuel injection while craning

Definition at line 444 of file fuel_math.cpp.

                                      {
    return getCrankingFuel3(baseFuel, engine->rpmCalculator.getRevolutionCounterSinceStart());
}

Referenced by getCycleFuelMass().

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getCrankingFuel3()

float getCrankingFuel3	(	float	baseFuel,
		uint32_t	revolutionCounterSinceStart
	)

Cranking fuel is different depending on engine coolant temperature If the sensor is failed, use 20 deg C

Definition at line 42 of file fuel_math.cpp.

                                                                             {
 
    float baseCrankingFuel;
    if (engineConfiguration->useRunningMathForCranking) {
        baseCrankingFuel = baseFuel;
    } else {
        // Cranking fuel changes over time
        baseCrankingFuel = interpolate3d(
              config->crankingCycleBaseFuel,
              config->crankingCycleFuelCltBins, Sensor::getOrZero(SensorType::Clt),
              config->crankingCycleBins, revolutionCounterSinceStart
          ) * 0.001f; // parameter is in milligrams, convert to grams
    }
 
    engine->engineState.crankingFuel.baseFuel = baseCrankingFuel * 1000; // convert to mg
 
    /**
     * Cranking fuel is different depending on engine coolant temperature
     * If the sensor is failed, use 20 deg C
     */
    auto clt = Sensor::get(SensorType::Clt).value_or(20);
    auto e0Mult = interpolate2d(clt, config->crankingFuelBins, config->crankingFuelCoef);
 
    bool alreadyWarned = false;
    if (e0Mult <= 0.1f) {
        warning(ObdCode::CUSTOM_ERR_ZERO_E0_MULT, "zero e0 multiplier");
        alreadyWarned = true;
    }
 
    if (engineConfiguration->flexCranking && Sensor::hasSensor(SensorType::FuelEthanolPercent)) {
        auto e85Mult = interpolate2d(clt, config->crankingFuelBins, config->crankingFuelCoefE100);
 
        if (e85Mult <= 0.1f) {
            warning(ObdCode::CUSTOM_ERR_ZERO_E85_MULT, "zero e85 multiplier");
            alreadyWarned = true;
        }
 
        // If failed flex sensor, default to 50% E
        auto flex = Sensor::get(SensorType::FuelEthanolPercent).value_or(50);
 
        engine->engineState.crankingFuel.coolantTemperatureCoefficient =
            interpolateClamped(
                0, e0Mult,
                85, e85Mult,
                flex
            );
    } else {
        engine->engineState.crankingFuel.coolantTemperatureCoefficient = e0Mult;
    }
 
    auto tps = Sensor::get(SensorType::DriverThrottleIntent);
    engine->engineState.crankingFuel.tpsCoefficient =
        tps.Valid
        ? interpolate2d(tps.Value, config->crankingTpsBins, config->crankingTpsCoef)
        : 1; // in case of failed TPS, don't correct.
 
    floatms_t crankingFuel = baseCrankingFuel
            * engine->engineState.crankingFuel.coolantTemperatureCoefficient
            * engine->engineState.crankingFuel.tpsCoefficient;
 
    engine->engineState.crankingFuel.fuel = crankingFuel * 1000;
 
    // don't re-warn for zero fuel when we already warned for a more specific problem
    if (!alreadyWarned && crankingFuel <= 0) {
        warning(ObdCode::CUSTOM_ERR_ZERO_CRANKING_FUEL, "Cranking fuel value %f", crankingFuel);
    }
    return crankingFuel;
}

Referenced by getCrankingFuel().

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getCycleFuelMass()

float getCycleFuelMass	(	bool	isCranking,
		float	baseFuelMass
	)

Definition at line 293 of file fuel_math.cpp.

                                                            {
    if (isCranking) {
        return getCrankingFuel(baseFuelMass);
    } else {
        return getRunningFuel(baseFuelMass);
    }
}

Referenced by getInjectionMass().

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getCylinderFuelTrim()

PUBLIC_API_WEAK_SOMETHING_WEIRD float getCylinderFuelTrim	(	size_t	cylinderNumber,
		float	rpm,
		float	fuelLoad
	)

Definition at line 463 of file fuel_math.cpp.

                                                                            {
    auto trimPercent = interpolate3d(
        config->fuelTrims[cylinderNumber].table,
        config->fuelTrimLoadBins, fuelLoad,
        config->fuelTrimRpmBins, rpm
    );
 
    // Convert from percent +- to multiplier
    // 5% -> 1.05
    // possible optimization: remove division by moving this scaling to TS level
    return (100 + trimPercent) / 100;
}

Referenced by EngineState::periodicFastCallback().

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getFuelALSCorrection()

percent_t getFuelALSCorrection

(

float

rpm

)

Definition at line 423 of file fuel_math.cpp.

                                          {
#if EFI_ANTILAG_SYSTEM
        if (engine->antilagController.isAntilagCondition) {
            float throttleIntent = Sensor::getOrZero(SensorType::DriverThrottleIntent);
            auto AlsFuelAdd = interpolate3d(
            config->ALSFuelAdjustment,
            config->alsFuelAdjustmentLoadBins, throttleIntent,
            config->alsFuelAdjustmentrpmBins, rpm
        );
        return AlsFuelAdd;
    } else
#endif /* EFI_ANTILAG_SYSTEM */
    {
        return 0;
    }
}

Referenced by AntilagSystemBase::update().

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getIatFuelCorrection()

float getIatFuelCorrection

(

)

Definition at line 367 of file fuel_math.cpp.

                             {
    const auto iat = Sensor::get(SensorType::Iat);
 
    if (!iat)
        return 1; // this error should be already reported somewhere else, let's just handle it
 
    return interpolate2d(iat.Value, config->iatFuelCorrBins, config->iatFuelCorr);
}

Referenced by EngineState::periodicFastCallback().

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getInjectionMass()

float getInjectionMass

(

float

rpm

)

Returns

Mass of each individual fuel injection, in grams in case of single point injection mode the amount of fuel into all cylinders, otherwise the amount for one cylinder

Definition at line 305 of file fuel_math.cpp.

                                  {
    ScopePerf perf(PE::GetInjectionDuration);
 
    // Always update base fuel - some cranking modes use it
    float baseFuelMass = getBaseFuelMass(rpm);
 
    bool isCranking = engine->rpmCalculator.isCranking();
    float cycleFuelMass = getCycleFuelMass(isCranking, baseFuelMass);
    efiAssert(ObdCode::CUSTOM_ERR_ASSERT, !std::isnan(cycleFuelMass), "NaN cycleFuelMass", 0);
 
    if (engine->module<DfcoController>()->cutFuel()) {
        // If decel fuel cut, zero out fuel
        cycleFuelMass = 0;
    }
 
    float durationMultiplier = getInjectionModeDurationMultiplier();
    float injectionFuelMass = cycleFuelMass * durationMultiplier;
 
    // Prepare injector flow rate & deadtime
    engine->module<InjectorModelPrimary>()->prepare();
 
    if (engineConfiguration->enableStagedInjection) {
        engine->module<InjectorModelSecondary>()->prepare();
    }
 
    float tpsAccelEnrich = engine->module<TpsAccelEnrichment>()->getTpsEnrichment();
    efiAssert(ObdCode::CUSTOM_ERR_ASSERT, !std::isnan(tpsAccelEnrich), "NaN tpsAccelEnrich", 0);
    engine->engineState.tpsAccelEnrich = tpsAccelEnrich;
 
    float tpsAccelPerInjection = durationMultiplier * tpsAccelEnrich;
 
  if (engineConfiguration->tpsTpsPercentMode) {
    return injectionFuelMass * (1 + tpsAccelPerInjection);
  } else {
      // For legacy reasons, the TPS accel table is in units of milliseconds, so we have to convert BACK to mass
      float tpsFuelMass = engine->module<InjectorModelPrimary>()->getFuelMassForDuration(tpsAccelPerInjection);
      return injectionFuelMass + tpsFuelMass;
    }
}

Referenced by EngineState::periodicFastCallback().

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getInjectionModeDurationMultiplier()

float getInjectionModeDurationMultiplier

(

)

Definition at line 256 of file fuel_math.cpp.

                                           {
    injection_mode_e mode = getCurrentInjectionMode();
 
    switch (mode) {
    case IM_SIMULTANEOUS: {
        auto cylCount = engineConfiguration->cylindersCount;
 
        if (cylCount == 0) {
            // we can end up here during configuration reset
            return 0;
        }
 
        return 1.0f / cylCount;
    }
    case IM_SEQUENTIAL:
    case IM_SINGLE_POINT:
        return 1;
    case IM_BATCH:
        return 0.5f;
    default:
        firmwareError(ObdCode::CUSTOM_ERR_INVALID_INJECTION_MODE, "Unexpected injection_mode_e %d", mode);
        return 0;
    }
}

Referenced by getInjectionMass().

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getInjectionOffset()

angle_t getInjectionOffset	(	float	rpm,
		float	load
	)

Definition at line 210 of file fuel_math.cpp.

                                                  {
    if (std::isnan(rpm)) {
        return 0; // error already reported
    }
 
    if (std::isnan(load)) {
        return 0; // error already reported
    }
 
    angle_t value = interpolate3d(
        config->injectionPhase,
        config->injPhaseLoadBins, load,
        config->injPhaseRpmBins, rpm
    );
 
    if (std::isnan(value)) {
        // we could be here while resetting configuration for example
        // huh? what? when do we have RPM while resetting configuration? is that CI edge case? shall we fix CI?
        warning(ObdCode::CUSTOM_ERR_6569, "phase map not ready");
        return 0;
    }
 
    angle_t result = value;
    wrapAngle(result, "inj offset#2", ObdCode::CUSTOM_ERR_6553);
    return result;
}

Referenced by EngineState::periodicFastCallback().

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getInjectorDutyCycle()

percent_t getInjectorDutyCycle

(

float

rpm

)

Definition at line 281 of file fuel_math.cpp.

                                          {
    floatms_t totalInjectiorAmountPerCycle = engine->engineState.injectionDuration * getNumberOfInjections(engineConfiguration->injectionMode);
    floatms_t engineCycleDuration = getEngineCycleDuration(rpm);
    return 100 * totalInjectiorAmountPerCycle / engineCycleDuration;
}

Referenced by canDashboardHaltech(), EngineState::periodicFastCallback(), populateFrame(), LimpManager::updateState(), and updateTunerStudioState().

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getInjectorDutyCycleStage2()

percent_t getInjectorDutyCycleStage2

(

float

rpm

)

Definition at line 287 of file fuel_math.cpp.

                                                {
    floatms_t totalInjectiorAmountPerCycle = engine->engineState.injectionDurationStage2 * getNumberOfInjections(engineConfiguration->injectionMode);
    floatms_t engineCycleDuration = getEngineCycleDuration(rpm);
    return 100 * totalInjectiorAmountPerCycle / engineCycleDuration;
}

Referenced by updateTunerStudioState().

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getMaxAirflowAtMap()

float getMaxAirflowAtMap

(

float

map

)

Definition at line 169 of file fuel_math.cpp.

                                    {
    return sdAirmass.getAirflow(Sensor::getOrZero(SensorType::Rpm), map, false);
}

Referenced by ThrottleModel::maxEngineFlow().

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getNumberOfInjections()

int getNumberOfInjections

(

injection_mode_e

mode

)

Number of injections using each injector per engine cycle

See also

getNumberOfSparks

Definition at line 241 of file fuel_math.cpp.

                                                 {
    switch (mode) {
    case IM_SIMULTANEOUS:
    case IM_SINGLE_POINT:
        return engineConfiguration->cylindersCount;
    case IM_BATCH:
        return 2;
    case IM_SEQUENTIAL:
        return 1;
    default:
        firmwareError(ObdCode::CUSTOM_ERR_INVALID_INJECTION_MODE, "Unexpected injection_mode_e %d", mode);
        return 1;
    }
}

Referenced by getInjectorDutyCycle(), getInjectorDutyCycleStage2(), and InjectionEvent::onTriggerTooth().

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getPostCrankingFuelCorrection()

float getPostCrankingFuelCorrection

(

)

Definition at line 376 of file fuel_math.cpp.

                                      {
    const auto revolutionCounter = engine->rpmCalculator.getRevolutionCounterSinceStart();
    // if the engine run time is past the last bin, disable ASE in case the table is filled with values more than 1.0, helps with compatibility
    if (revolutionCounter > config->postCrankingDurationBins[efi::size(config->postCrankingDurationBins) - 1])
        return 1;
 
    // TODO:
    //const auto clt = Sensor::get(SensorType::Clt);
    //if (!clt)
    //  return 1; // this error should be already reported somewhere else, let's just handle it
 
    // post-cranking fuel enrichment.
    float postCrankingFactor = interpolate3d(
        config->postCrankingFactor,
        config->postCrankingCLTBins, Sensor::getOrZero(SensorType::Clt),
        config->postCrankingDurationBins, revolutionCounter
    );
 
    // for compatibility reasons, apply only if the factor is greater than unity (only allow adding fuel)
    if (postCrankingFactor < 1.0f)
        postCrankingFactor = 1.0f;
 
    return postCrankingFactor;
}

Referenced by EngineState::periodicFastCallback().

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getRunningFuel()

float getRunningFuel

(

float

baseFuel

)

Returns

baseFuel with CLT and IAT corrections

Definition at line 111 of file fuel_math.cpp.

                                     {
    ScopePerf perf(PE::GetRunningFuel);
 
    float iatCorrection = engine->fuelComputer.running.intakeTemperatureCoefficient;
    float cltCorrection = engine->fuelComputer.running.coolantTemperatureCoefficient;
    float postCrankingFuelCorrection = engine->fuelComputer.running.postCrankingFuelCorrection;
    float baroCorrection = engine->engineState.baroCorrection;
 
    efiAssert(ObdCode::CUSTOM_ERR_ASSERT, !std::isnan(iatCorrection), "NaN iatCorrection", 0);
    efiAssert(ObdCode::CUSTOM_ERR_ASSERT, !std::isnan(cltCorrection), "NaN cltCorrection", 0);
    efiAssert(ObdCode::CUSTOM_ERR_ASSERT, !std::isnan(postCrankingFuelCorrection), "NaN postCrankingFuelCorrection", 0);
 
    float correction = baroCorrection * iatCorrection * cltCorrection * postCrankingFuelCorrection;
 
#if EFI_ANTILAG_SYSTEM
    correction *= (1 + engine->antilagController.fuelALSCorrection / 100);
#endif /* EFI_ANTILAG_SYSTEM */
 
#if EFI_LAUNCH_CONTROL
    correction *= engine->launchController.getFuelCoefficient();
    correction *= engine->module<NitrousController>().unmock().getFuelCoefficient();
#endif
 
    correction *= getLimpManager()->getLimitingFuelCorrection();
 
    float runningFuel = baseFuel * correction;
 
    efiAssert(ObdCode::CUSTOM_ERR_ASSERT, !std::isnan(runningFuel), "NaN runningFuel", 0);
 
    // Publish output state
    engine->fuelComputer.running.baseFuel = baseFuel * 1000;
    engine->fuelComputer.totalFuelCorrection = correction;
    engine->fuelComputer.running.fuel = runningFuel * 1000;
 
    return runningFuel;
}

Referenced by getCycleFuelMass().

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getStage2InjectionFraction()

float getStage2InjectionFraction	(	float	rpm,
		float	load
	)

Definition at line 478 of file fuel_math.cpp.

                                                        {
    if (!engineConfiguration->enableStagedInjection) {
        return 0;
    }
 
    float frac = 0.01f * interpolate3d(
        config->injectorStagingTable,
        config->injectorStagingLoadBins, load,
        config->injectorStagingRpmBins, rpm
    );
 
    // don't allow very small fraction, with some hysteresis
    if (!stage2Hysteresis.test(frac, 0.1, 0.03)) {
        return 0;
    }
 
    // Clamp to 90%
    if (frac > 0.9) {
        frac = 0.9;
    }
 
    return frac;
}

Referenced by EngineState::periodicFastCallback().

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getStandardAirCharge()

float getStandardAirCharge

(

)

Standard cylinder air charge - 100% VE at standard temperature, grams per cylinder

Should we bother caching 'getStandardAirCharge' result or can we afford to run the math every time we calculate fuel?

Definition at line 453 of file fuel_math.cpp.

                             {
    float totalDisplacement = engineConfiguration->displacement;
    float cylDisplacement = totalDisplacement / engineConfiguration->cylindersCount;
 
    // Calculation of 100% VE air mass in g/cyl - 1 cylinder filling at 1.204/L
    // 101.325kpa, 20C
    return idealGasLaw(cylDisplacement, STD_ATMOSPHERE, C_K_OFFSET + STD_IAT);
}

Referenced by MafAirmass::getAirmassImpl(), and getBaseFuelMass().

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initFuelMap()

void initFuelMap

(

)

Initialize fuel map data structure.

Note

this method has nothing to do with fuel map VALUES - it's job is to prepare the fuel map data structure for 3d interpolation

Definition at line 351 of file fuel_math.cpp.

                   {
    mapEstimationTable.initTable(config->mapEstimateTable, config->mapEstimateRpmBins, config->mapEstimateTpsBins);
}

Referenced by initDataStructures().

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Variable Documentation

alphaNAirmass

AlphaNAirmass alphaNAirmass(veMap) ( veMap  )

static

Referenced by getAirmassModel().

mafAirmass

MafAirmass mafAirmass(veMap) ( veMap  )

static

Referenced by getAirmassModel().

mapEstimationTable

mapEstimate_Map3D_t mapEstimationTable {"mape"}

static

Definition at line 38 of file fuel_math.cpp.

{"mape"};

Referenced by initFuelMap().

sdAirmass

SpeedDensityAirmass sdAirmass(veMap, mapEstimationTable) ( veMap  , mapEstimationTable    )

static

Referenced by getAirmassModel(), and getMaxAirflowAtMap().

stage2Hysteresis

Hysteresis stage2Hysteresis

static

Definition at line 476 of file fuel_math.cpp.

Referenced by getStage2InjectionFraction().

veMap

ve_Map3D_t veMap

extern

Definition at line 19 of file speed_density.cpp.

{"ve"};

Referenced by initSpeedDensity().

Go to the source code of this file.