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C++ fuel_Map3D_t类代码示例

原作者: [db:作者] 来自: [db:来源] 收藏 邀请

本文整理汇总了C++中fuel_Map3D_t的典型用法代码示例。如果您正苦于以下问题:C++ fuel_Map3D_t类的具体用法?C++ fuel_Map3D_t怎么用?C++ fuel_Map3D_t使用的例子?那么恭喜您, 这里精选的类代码示例或许可以为您提供帮助。



在下文中一共展示了fuel_Map3D_t类的9个代码示例,这些例子默认根据受欢迎程度排序。您可以为喜欢或者感觉有用的代码点赞,您的评价将有助于我们的系统推荐出更棒的C++代码示例。

示例1: chRegSetThreadName

	chRegSetThreadName("lcd");
	while (true) {
		if (engineConfiguration->bc.useLcdScreen) {
#if EFI_HD44780_LCD
			updateHD44780lcd(engine);
#endif
		}
		chThdSleepMilliseconds(engineConfiguration->bc.lcdThreadPeriod);
	}
}

#if EFI_TUNER_STUDIO || defined(__DOXYGEN__)

extern WallFuel wallFuel;

extern fuel_Map3D_t veMap;

void updateTunerStudioState(TunerStudioOutputChannels *tsOutputChannels DECLARE_ENGINE_PARAMETER_S) {
#if EFI_SHAFT_POSITION_INPUT || defined(__DOXYGEN__)
	int rpm = getRpmE(engine);
#else
	int rpm = 0;
#endif

	float tps = getTPS(PASS_ENGINE_PARAMETER_F);
	float coolant = getCoolantTemperature(PASS_ENGINE_PARAMETER_F);
	float intake = getIntakeAirTemperature(PASS_ENGINE_PARAMETER_F);

	float engineLoad = getEngineLoadT(PASS_ENGINE_PARAMETER_F);
	float baseFuelMs = getBaseFuel(rpm PASS_ENGINE_PARAMETER);
开发者ID:owenanthonyj,项目名称:rusefi,代码行数:30,代码来源:status_loop.cpp


示例2: periodicFastCallback

void EngineState::periodicFastCallback(DECLARE_ENGINE_PARAMETER_F) {
	int rpm = ENGINE(rpmCalculator.rpmValue);

	sparkDwell = getSparkDwell(rpm PASS_ENGINE_PARAMETER);
	dwellAngle = sparkDwell / getOneDegreeTimeMs(rpm);

	iatFuelCorrection = getIatCorrection(iat PASS_ENGINE_PARAMETER);
	cltFuelCorrection = getCltCorrection(clt PASS_ENGINE_PARAMETER);

	engineNoiseHipLevel = interpolate2d(rpm, engineConfiguration->knockNoiseRpmBins,
					engineConfiguration->knockNoise, ENGINE_NOISE_CURVE_SIZE);

	baroCorrection = getBaroCorrection(PASS_ENGINE_PARAMETER_F);

	injectionOffset = getinjectionOffset(rpm PASS_ENGINE_PARAMETER);
	float engineLoad = getEngineLoadT(PASS_ENGINE_PARAMETER_F);
	timingAdvance = getAdvance(rpm, engineLoad PASS_ENGINE_PARAMETER);

	if (engineConfiguration->algorithm == LM_SPEED_DENSITY) {
		float coolantC = ENGINE(engineState.clt);
		float intakeC = ENGINE(engineState.iat);
		float tps = getTPS(PASS_ENGINE_PARAMETER_F);
		tChargeK = convertCelsiusToKelvin(getTCharge(rpm, tps, coolantC, intakeC));
		float map = getMap();

		/**
		 * *0.01 because of https://sourceforge.net/p/rusefi/tickets/153/
		 */
		currentVE = baroCorrection * veMap.getValue(map, rpm) * 0.01;
		targerAFR = afrMap.getValue(map, rpm);
	} else {
		baseTableFuel = getBaseTableFuel(engineConfiguration, rpm, engineLoad);
	}

}
开发者ID:ioerror88,项目名称:rusefi,代码行数:35,代码来源:engine.cpp


示例3: setDefaultVETable

void setDefaultVETable(DECLARE_ENGINE_PARAMETER_F) {
	setRpmTableBin(config->veRpmBins, FUEL_RPM_COUNT);
	veMap.setAll(80);

//	setRpmTableBin(engineConfiguration->ve2RpmBins, FUEL_RPM_COUNT);
//	setTableBin2(engineConfiguration->ve2LoadBins, FUEL_LOAD_COUNT, 10, 300, 1);
//	ve2Map.setAll(0.81);

	setRpmTableBin(config->afrRpmBins, FUEL_RPM_COUNT);
	afrMap.setAll(14.7);

	setRpmTableBin(engineConfiguration->baroCorrRpmBins, BARO_CORR_SIZE);
	setTableBin2(engineConfiguration->baroCorrPressureBins, BARO_CORR_SIZE, 75, 105, 1);
	memcpy(engineConfiguration->baroCorrTable, default_baro_corr, sizeof(default_baro_corr));
}
开发者ID:jon-weisz,项目名称:rusefi,代码行数:15,代码来源:speed_density.cpp


示例4: initSpeedDensity

void initSpeedDensity(DECLARE_ENGINE_PARAMETER_SIGNATURE) {
	veMap.init(config->veTable, config->veLoadBins, config->veRpmBins);
//	ve2Map.init(engineConfiguration->ve2Table, engineConfiguration->ve2LoadBins, engineConfiguration->ve2RpmBins);
	afrMap.init(config->afrTable, config->afrLoadBins, config->afrRpmBins);
	baroCorrMap.init(engineConfiguration->baroCorrTable, engineConfiguration->baroCorrPressureBins, engineConfiguration->baroCorrRpmBins);
	initMaf2Map();
}
开发者ID:rusefi,项目名称:rusefi,代码行数:7,代码来源:speed_density.cpp


示例5: getBaseTableFuel

/**
 * @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);
}
开发者ID:owenanthonyj,项目名称:rusefi,代码行数:10,代码来源:fuel_math.cpp


示例6: getRealMafFuel

/**
 * @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;
}
开发者ID:owenanthonyj,项目名称:rusefi,代码行数:22,代码来源:fuel_math.cpp


示例7: getinjectionOffset

float getinjectionOffset(int rpm DECLARE_ENGINE_PARAMETER_S) {
	float engineLoad = getEngineLoadT(PASS_ENGINE_PARAMETER_F);
	return fuelPhaseMap.getValue(engineLoad, rpm);
}
开发者ID:owenanthonyj,项目名称:rusefi,代码行数:4,代码来源:fuel_math.cpp


示例8: prepareFuelMap

/**
 * @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);
}
开发者ID:owenanthonyj,项目名称:rusefi,代码行数:9,代码来源:fuel_math.cpp


示例9: periodicFastCallback

void EngineState::periodicFastCallback(DECLARE_ENGINE_PARAMETER_SIGNATURE) {
	efitick_t nowNt = getTimeNowNt();
	if (ENGINE(rpmCalculator).isCranking(PASS_ENGINE_PARAMETER_SIGNATURE)) {
		crankingTime = nowNt;
		timeSinceCranking = 0.0f;
	} else {
		timeSinceCranking = nowNt - crankingTime;
	}
	updateAuxValves(PASS_ENGINE_PARAMETER_SIGNATURE);

	int rpm = ENGINE(rpmCalculator).getRpm(PASS_ENGINE_PARAMETER_SIGNATURE);
	sparkDwell = getSparkDwell(rpm PASS_ENGINE_PARAMETER_SUFFIX);
	dwellAngle = sparkDwell / getOneDegreeTimeMs(rpm);
	if (hasAfrSensor(PASS_ENGINE_PARAMETER_SIGNATURE)) {
		engine->sensors.currentAfr = getAfr(PASS_ENGINE_PARAMETER_SIGNATURE);
	}

	// todo: move this into slow callback, no reason for IAT corr to be here
	iatFuelCorrection = getIatFuelCorrection(engine->sensors.iat PASS_ENGINE_PARAMETER_SUFFIX);
	// todo: move this into slow callback, no reason for CLT corr to be here
	if (boardConfiguration->useWarmupPidAfr && engine->sensors.clt < engineConfiguration->warmupAfrThreshold) {
		if (rpm < 200) {
			cltFuelCorrection = 1;
			warmupAfrPid.reset();
		} else {
			cltFuelCorrection = warmupAfrPid.getValue(warmupTargetAfr, engine->sensors.currentAfr, 1);
		}
#if ! EFI_UNIT_TEST || defined(__DOXYGEN__)
		if (engineConfiguration->debugMode == DBG_WARMUP_ENRICH) {
			tsOutputChannels.debugFloatField1 = warmupTargetAfr;
			warmupAfrPid.postState(&tsOutputChannels);
		}
#endif

	} else {
		cltFuelCorrection = getCltFuelCorrection(PASS_ENGINE_PARAMETER_SIGNATURE);
	}

	// update fuel consumption states
	fuelConsumption.update(nowNt PASS_ENGINE_PARAMETER_SUFFIX);

	// Fuel cut-off isn't just 0 or 1, it can be tapered
	fuelCutoffCorrection = getFuelCutOffCorrection(nowNt, rpm PASS_ENGINE_PARAMETER_SUFFIX);
	
	// post-cranking fuel enrichment.
	// for compatibility reasons, apply only if the factor is greater than zero (0.01 margin used)
	if (engineConfiguration->postCrankingFactor > 0.01f) {
		// convert to microsecs and then to seconds
		float timeSinceCrankingInSecs = NT2US(timeSinceCranking) / 1000000.0f;
		// use interpolation for correction taper
		postCrankingFuelCorrection = interpolateClamped(0.0f, engineConfiguration->postCrankingFactor, 
			engineConfiguration->postCrankingDurationSec, 1.0f, timeSinceCrankingInSecs);
	} else {
		postCrankingFuelCorrection = 1.0f;
	}

	cltTimingCorrection = getCltTimingCorrection(PASS_ENGINE_PARAMETER_SIGNATURE);

	engineNoiseHipLevel = interpolate2d("knock", rpm, engineConfiguration->knockNoiseRpmBins,
					engineConfiguration->knockNoise, ENGINE_NOISE_CURVE_SIZE);

	baroCorrection = getBaroCorrection(PASS_ENGINE_PARAMETER_SIGNATURE);

	injectionOffset = getinjectionOffset(rpm PASS_ENGINE_PARAMETER_SUFFIX);
	float engineLoad = getEngineLoadT(PASS_ENGINE_PARAMETER_SIGNATURE);
	timingAdvance = getAdvance(rpm, engineLoad PASS_ENGINE_PARAMETER_SUFFIX);

	if (engineConfiguration->fuelAlgorithm == LM_SPEED_DENSITY) {
		float coolantC = ENGINE(sensors.clt);
		float intakeC = ENGINE(sensors.iat);
		float tps = getTPS(PASS_ENGINE_PARAMETER_SIGNATURE);
		tChargeK = convertCelsiusToKelvin(getTCharge(rpm, tps, coolantC, intakeC PASS_ENGINE_PARAMETER_SUFFIX));
		float map = getMap();

		/**
		 * *0.01 because of https://sourceforge.net/p/rusefi/tickets/153/
		 */
		float rawVe = veMap.getValue(rpm, map);
		// get VE from the separate table for Idle
		if (CONFIG(useSeparateVeForIdle)) {
			float idleVe = interpolate2d("idleVe", rpm, config->idleVeBins, config->idleVe, IDLE_VE_CURVE_SIZE);
			// interpolate between idle table and normal (running) table using TPS threshold
			rawVe = interpolateClamped(0.0f, idleVe, boardConfiguration->idlePidDeactivationTpsThreshold, rawVe, tps);
		}
		currentVE = baroCorrection * rawVe * 0.01;
		targetAFR = afrMap.getValue(rpm, map);
	} else {
		baseTableFuel = getBaseTableFuel(rpm, engineLoad);
	}
}
开发者ID:yongfeicao,项目名称:rusefi,代码行数:90,代码来源:engine.cpp



注:本文中的fuel_Map3D_t类示例由纯净天空整理自Github/MSDocs等源码及文档管理平台,相关代码片段筛选自各路编程大神贡献的开源项目,源码版权归原作者所有,传播和使用请参考对应项目的License;未经允许,请勿转载。


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