rusefi/firmware/controllers/algo/fuel_math.cpp

/**
 * @file	fuel_math.cpp
 * @brief	Fuel amount calculation logic
 *
 * While engine running, fuel amount is an interpolated value from the fuel map by getRpm() and getEngineLoad()
 * On top of the value from the fuel map we also apply
 * <BR>1) getInjectorLag() correction to account for fuel injector lag
 * <BR>2) getCltCorrection() for warm-up
 * <BR>3) getIatCorrection() to account for cold weather
 *
 * getCrankingFuel() depents only on getCoolantTemperature()
 *
 *
 * @date May 27, 2013
 * @author Andrey Belomutskiy, (c) 2012-2015
 *
 * 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/>.
 *
 */

#include "main.h"
#include "fuel_math.h"
#include "interpolation.h"
#include "engine_configuration.h"
#include "allsensors.h"
#include "engine_math.h"
#include "rpm_calculator.h"
#include "speed_density.h"

EXTERN_ENGINE
;

static fuel_Map3D_t fuelMap;
static fuel_Map3D_t fuelPhaseMap;
extern fuel_Map3D_t ve2Map;
extern fuel_Map3D_t afrMap;
extern baroCorr_Map3D_t baroCorrMap;

/**
 * @return total duration of fuel injection per engine cycle, in milliseconds
 */
float getRealMafFuel(float airSpeed, int rpm DECLARE_ENGINE_PARAMETER_S) {
	if (rpm == 0)
		return 0;
	// duration of engine cycle, in hours
	float engineCycleDurationHr = 1.0 / 60 / rpm;

	float airMassKg = airSpeed * engineCycleDurationHr;

	/**
	 * todo: pre-calculate gramm/second injector flow to save one multiplication
	 * open question if that's needed since that's just a multiplication
	 */
	float injectorFlowRate = cc_minute_to_gramm_second(engineConfiguration->injector.flow);

	float afr = afrMap.getValue(airSpeed, rpm);
	float fuelMassGramm = airMassKg / afr * 1000;

	return 1000 * fuelMassGramm / injectorFlowRate;
}

floatms_t getBaseFuel(int rpm DECLARE_ENGINE_PARAMETER_S) {
	floatms_t tpsAccelEnrich = ENGINE(tpsAccelEnrichment.getTpsEnrichment(PASS_ENGINE_PARAMETER_F));

	if (CONFIG(algorithm) == LM_SPEED_DENSITY) {
		return tpsAccelEnrich + getSpeedDensityFuel(rpm PASS_ENGINE_PARAMETER);
	} else if (engineConfiguration->algorithm == LM_REAL_MAF) {
		float maf = getRealMaf(PASS_ENGINE_PARAMETER_F) + engine->mapAccelEnrichment.getMapEnrichment(PASS_ENGINE_PARAMETER_F);
		return tpsAccelEnrich + getRealMafFuel(maf, rpm PASS_ENGINE_PARAMETER);
	} else {
		return tpsAccelEnrich + engine->engineState.baseTableFuel;
	}
}

float getinjectionOffset(int rpm DECLARE_ENGINE_PARAMETER_S) {
	float engineLoad = getEngineLoadT(PASS_ENGINE_PARAMETER_F);
	return fuelPhaseMap.getValue(engineLoad, rpm);
}

/**
 * Number of injections into each cylinder per engine cycle
 */
static int getNumberOfInjections(injection_mode_e mode DECLARE_ENGINE_PARAMETER_S) {
	switch (mode) {
	case IM_SIMULTANEOUS:
		return engineConfiguration->specs.cylindersCount;
	case IM_SEQUENTIAL:
		return 1;
	case IM_BATCH:
		return engineConfiguration->specs.cylindersCount / 2;
	default:
		firmwareError("Unexpected getFuelMultiplier %d", mode);
		return 1;
	}
}

percent_t getInjectorDutyCycle(int rpm DECLARE_ENGINE_PARAMETER_S) {
	floatms_t totalPerCycle = getFuelMs(rpm PASS_ENGINE_PARAMETER) * getNumberOfInjections(engineConfiguration->injectionMode PASS_ENGINE_PARAMETER);
	floatms_t engineCycleTime = getCrankshaftRevolutionTimeMs(rpm) * (engineConfiguration->operationMode == TWO_STROKE ? 1 : 2);
	return 100 * totalPerCycle / engineCycleTime;
}

/**
 * @returns	Length of each individual fuel injection, in milliseconds
 */
floatms_t getFuelMs(int rpm DECLARE_ENGINE_PARAMETER_S) {
	float theoreticalInjectionLength;
	if (isCrankingR(rpm)) {
		theoreticalInjectionLength = getCrankingFuel(PASS_ENGINE_PARAMETER_F)
				/ getNumberOfInjections(engineConfiguration->crankingInjectionMode PASS_ENGINE_PARAMETER);
	} else {
		float baseFuel = getBaseFuel(rpm PASS_ENGINE_PARAMETER);
		float fuelPerCycle = getRunningFuel(baseFuel, rpm PASS_ENGINE_PARAMETER);
		theoreticalInjectionLength = fuelPerCycle
				/ getNumberOfInjections(engineConfiguration->injectionMode PASS_ENGINE_PARAMETER);
	}
	return theoreticalInjectionLength + ENGINE(injectorLagMs);
}

floatms_t getRunningFuel(floatms_t baseFuel, int rpm DECLARE_ENGINE_PARAMETER_S) {
	float iatCorrection = ENGINE(engineState.iatFuelCorrection);
	float cltCorrection = ENGINE(engineState.cltFuelCorrection);

	engine->totalFuelCorrection = cltCorrection * iatCorrection;

	return baseFuel * engine->totalFuelCorrection;
}

/**
 * @brief	Injector lag correction
 * @param	vBatt	Battery voltage.
 * @return	Time in ms for injection opening time based on current battery voltage
 */
floatms_t getInjectorLag(float vBatt DECLARE_ENGINE_PARAMETER_S) {
	if (cisnan(vBatt)) {
		warning(OBD_System_Voltage_Malfunction, "vBatt=%f", vBatt);
		return engineConfiguration->injector.lag;
	}
	float vBattCorrection = interpolate2d(vBatt, engineConfiguration->injector.battLagCorrBins,
			engineConfiguration->injector.battLagCorr, VBAT_INJECTOR_CURVE_SIZE);
	return engineConfiguration->injector.lag + vBattCorrection;
}

/**
 * @brief	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
 */
void prepareFuelMap(DECLARE_ENGINE_PARAMETER_F) {
	fuelMap.init(config->fuelTable, config->fuelLoadBins, config->fuelRpmBins);
	fuelPhaseMap.init(config->injectionPhase, config->injPhaseLoadBins, config->injPhaseRpmBins);
}

/**
 * @brief Engine warm-up fuel correction.
 */
float getCltCorrection(float clt DECLARE_ENGINE_PARAMETER_S) {
	if (cisnan(clt))
		return 1; // this error should be already reported somewhere else, let's just handle it
	return interpolate2d(clt, config->cltFuelCorrBins, config->cltFuelCorr, CLT_CURVE_SIZE);
}

float getIatCorrection(float iat DECLARE_ENGINE_PARAMETER_S) {
	if (cisnan(iat))
		return 1; // this error should be already reported somewhere else, let's just handle it
	return interpolate2d(iat, config->iatFuelCorrBins, config->iatFuelCorr, IAT_CURVE_SIZE);
}

/**
 * @return Fuel injection duration injection as specified in the fuel map, in milliseconds
 */
floatms_t getBaseTableFuel(engine_configuration_s *engineConfiguration, int rpm, float engineLoad) {
	if (cisnan(engineLoad)) {
		warning(OBD_PCM_Processor_Fault, "NaN engine load");
		return NAN;
	}
	return fuelMap.getValue(engineLoad, rpm);
}

float getBaroCorrection(DECLARE_ENGINE_PARAMETER_F) {
	if (hasBaroSensor(PASS_ENGINE_PARAMETER_F)) {
		return baroCorrMap.getValue(getBaroPressure(PASS_ENGINE_PARAMETER_F), getRpm());
	} else {
		return 1;
	}
}

#if EFI_ENGINE_CONTROL || defined(__DOXYGEN__)
/**
 * @return Duration of fuel injection while craning
 */
floatms_t getCrankingFuel(DECLARE_ENGINE_PARAMETER_F) {
	return getCrankingFuel3(getCoolantTemperature(PASS_ENGINE_PARAMETER_F),
			engine->rpmCalculator.getRevolutionCounterSinceStart() PASS_ENGINE_PARAMETER);
}
#endif

floatms_t getCrankingFuel3(float coolantTemperature,
		uint32_t revolutionCounterSinceStart DECLARE_ENGINE_PARAMETER_S) {
	// these magic constants are in Celsius
	float baseCrankingFuel = engineConfiguration->cranking.baseFuel;
	if (cisnan(coolantTemperature))
		return baseCrankingFuel;
	float durationCoef = interpolate2d(revolutionCounterSinceStart, config->crankingCycleBins,
			config->crankingCycleCoef, CRANKING_CURVE_SIZE);

	float coolantTempCoef = interpolate2d(coolantTemperature, config->crankingFuelBins,
			config->crankingFuelCoef, CRANKING_CURVE_SIZE);

	float tpsCoef = interpolate2d(getTPS(PASS_ENGINE_PARAMETER_F), engineConfiguration->crankingTpsBins,
			engineConfiguration->crankingTpsCoef, CRANKING_CURVE_SIZE);

	return baseCrankingFuel * durationCoef * coolantTempCoef * tpsCoef;
}