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@ -181,6 +181,8 @@ static void printSensors(Logging *log, bool fileFormat) {
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if (engineConfiguration->hasAfrSensor) {
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reportSensorF(log, fileFormat, "afr", "AFR", getAfr(PASS_ENGINE_PARAMETER_F), 2);
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}
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reportSensorF(log, fileFormat, "target", "AFR", engine->engineState.targetAFR, 2);
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#endif
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#if EFI_VEHICLE_SPEED || defined(__DOXYGEN__)
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@ -204,6 +206,9 @@ static void printSensors(Logging *log, bool fileFormat) {
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reportSensorF(log, fileFormat, "tpsacc", "ms", engine->tpsAccelEnrichment.getTpsEnrichment(PASS_ENGINE_PARAMETER_F), 2);
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reportSensorF(log, fileFormat, "advance", "deg", engine->engineState.timingAdvance, 2);
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reportSensorF(log, fileFormat, "duty", "%", getInjectorDutyCycle(rpm PASS_ENGINE_PARAMETER), 2);
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reportSensorF(log, fileFormat, "tCharge", "K", engine->engineState.tChargeK, 2);
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}
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if (engineConfiguration->hasCltSensor) {
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@ -188,7 +188,7 @@ void EngineState::periodicFastCallback(DECLARE_ENGINE_PARAMETER_F) {
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* *0.01 because of https://sourceforge.net/p/rusefi/tickets/153/
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*/
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currentVE = baroCorrection * veMap.getValue(rpm, map) * 0.01;
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targerAFR = afrMap.getValue(rpm, map);
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targetAFR = afrMap.getValue(rpm, map);
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} else {
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baseTableFuel = getBaseTableFuel(engineConfiguration, rpm, engineLoad);
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}
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@ -162,7 +162,7 @@ public:
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// speed density
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float tChargeK;
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float currentVE;
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float targerAFR;
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float targetAFR;
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/**
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* pre-calculated value from simple fuel lookup
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@ -78,7 +78,7 @@ EXTERN_ENGINE;
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/**
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* @return per cylinder injection time, in Milliseconds
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*/
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float getSpeedDensityFuel(int rpm DECLARE_ENGINE_PARAMETER_S) {
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floatms_t getSpeedDensityFuel(int rpm DECLARE_ENGINE_PARAMETER_S) {
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//int rpm = engine->rpmCalculator->rpm();
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/**
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@ -91,7 +91,7 @@ float getSpeedDensityFuel(int rpm DECLARE_ENGINE_PARAMETER_S) {
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engine->engineState.airMass = getAirMass(engineConfiguration, ENGINE(engineState.currentVE), adjustedMap, tChargeK);
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return sdMath(engineConfiguration, engine->engineState.airMass, ENGINE(engineState.targerAFR)) * 1000;
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return sdMath(engineConfiguration, engine->engineState.airMass, ENGINE(engineState.targetAFR)) * 1000;
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}
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static const baro_corr_table_t default_baro_corr = {
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@ -20,6 +20,6 @@ float sdMath(engine_configuration_s *engineConfiguration, float airMass, float A
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void setDefaultVETable(DECLARE_ENGINE_PARAMETER_F);
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void initSpeedDensity(DECLARE_ENGINE_PARAMETER_F);
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float getSpeedDensityFuel(int rpm DECLARE_ENGINE_PARAMETER_S);
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floatms_t getSpeedDensityFuel(int rpm DECLARE_ENGINE_PARAMETER_S);
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#endif /* SPEED_DENSITY_H_ */
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@ -298,5 +298,5 @@ int getRusEfiVersion(void) {
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return 123; // this is here to make the compiler happy about the unused array
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if (UNUSED_CCM_SIZE[0] * 0 != 0)
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return 3211; // this is here to make the compiler happy about the unused array
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return 20160601;
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return 20160609;
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}
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