only:int rpm -> float rpm
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@ -70,7 +70,7 @@ bool LaunchControlBase::isInsideTpsCondition() const {
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return engineConfiguration->launchTpsThreshold < tps.Value;
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return engineConfiguration->launchTpsThreshold < tps.Value;
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}
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}
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LaunchCondition LaunchControlBase::calculateRPMLaunchCondition(const int rpm) {
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LaunchCondition LaunchControlBase::calculateRPMLaunchCondition(const float rpm) {
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const int launchRpm = engineConfiguration->launchRpm;
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const int launchRpm = engineConfiguration->launchRpm;
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const int preLaunchRpm = launchRpm - engineConfiguration->launchRpmWindow;
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const int preLaunchRpm = launchRpm - engineConfiguration->launchRpmWindow;
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if (rpm < preLaunchRpm) {
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if (rpm < preLaunchRpm) {
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@ -82,7 +82,7 @@ LaunchCondition LaunchControlBase::calculateRPMLaunchCondition(const int rpm) {
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}
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}
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}
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}
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LaunchCondition LaunchControlBase::calculateLaunchCondition(const int rpm) {
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LaunchCondition LaunchControlBase::calculateLaunchCondition(const float rpm) {
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const LaunchCondition currentRpmLaunchCondition = calculateRPMLaunchCondition(rpm);
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const LaunchCondition currentRpmLaunchCondition = calculateRPMLaunchCondition(rpm);
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activateSwitchCondition = isInsideSwitchCondition();
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activateSwitchCondition = isInsideSwitchCondition();
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rpmLaunchCondition = (currentRpmLaunchCondition == LaunchCondition::Launch);
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rpmLaunchCondition = (currentRpmLaunchCondition == LaunchCondition::Launch);
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@ -112,7 +112,7 @@ void LaunchControlBase::update() {
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return;
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return;
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}
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}
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const int rpm = Sensor::getOrZero(SensorType::Rpm);
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const float rpm = Sensor::getOrZero(SensorType::Rpm);
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const LaunchCondition launchCondition = calculateLaunchCondition(rpm);
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const LaunchCondition launchCondition = calculateLaunchCondition(rpm);
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isLaunchCondition = (launchCondition == LaunchCondition::Launch);
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isLaunchCondition = (launchCondition == LaunchCondition::Launch);
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isPreLaunchCondition = (launchCondition == LaunchCondition::PreLaunch);
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isPreLaunchCondition = (launchCondition == LaunchCondition::PreLaunch);
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@ -27,8 +27,8 @@ public:
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bool isInsideSpeedCondition() const;
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bool isInsideSpeedCondition() const;
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bool isInsideTpsCondition() const;
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bool isInsideTpsCondition() const;
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bool isInsideSwitchCondition();
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bool isInsideSwitchCondition();
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LaunchCondition calculateRPMLaunchCondition(int rpm);
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LaunchCondition calculateRPMLaunchCondition(float rpm);
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LaunchCondition calculateLaunchCondition(int rpm);
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LaunchCondition calculateLaunchCondition(float rpm);
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bool isLaunchSparkRpmRetardCondition() const;
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bool isLaunchSparkRpmRetardCondition() const;
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bool isLaunchFuelRpmRetardCondition() const;
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bool isLaunchFuelRpmRetardCondition() const;
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@ -74,7 +74,7 @@ angle_t HpfpLobe::findNextLobe() {
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}
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}
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// As a percent of the full pump stroke
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// As a percent of the full pump stroke
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float HpfpQuantity::calcFuelPercent(int rpm) {
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float HpfpQuantity::calcFuelPercent(float rpm) {
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float fuel_requested_cc_per_cycle =
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float fuel_requested_cc_per_cycle =
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engine->engineState.injectionMass[0] * (1.f / fuelDensity) * engineConfiguration->cylindersCount;
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engine->engineState.injectionMass[0] * (1.f / fuelDensity) * engineConfiguration->cylindersCount;
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float fuel_requested_cc_per_lobe = fuel_requested_cc_per_cycle / engineConfiguration->hpfpCamLobes;
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float fuel_requested_cc_per_lobe = fuel_requested_cc_per_cycle / engineConfiguration->hpfpCamLobes;
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@ -95,7 +95,7 @@ static float getLoad() {
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}
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}
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}
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}
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float HpfpQuantity::calcPI(int rpm, float calc_fuel_percent) {
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float HpfpQuantity::calcPI(float rpm, float calc_fuel_percent) {
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float load = getLoad();
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float load = getLoad();
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float possibleValue = m_pressureTarget_kPa - (engineConfiguration->hpfpTargetDecay *
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float possibleValue = m_pressureTarget_kPa - (engineConfiguration->hpfpTargetDecay *
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@ -136,7 +136,7 @@ float HpfpQuantity::calcPI(int rpm, float calc_fuel_percent) {
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return p_control_percent + i_control_percent;
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return p_control_percent + i_control_percent;
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}
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}
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angle_t HpfpQuantity::pumpAngleFuel(int rpm, HpfpController *model) {
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angle_t HpfpQuantity::pumpAngleFuel(float rpm, HpfpController *model) {
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// Math based on fuel requested
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// Math based on fuel requested
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model->fuel_requested_percent = calcFuelPercent(rpm);
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model->fuel_requested_percent = calcFuelPercent(rpm);
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@ -155,7 +155,7 @@ angle_t HpfpQuantity::pumpAngleFuel(int rpm, HpfpController *model) {
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void HpfpController::onFastCallback() {
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void HpfpController::onFastCallback() {
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// Pressure current/target calculation
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// Pressure current/target calculation
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int rpm = Sensor::getOrZero(SensorType::Rpm);
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float rpm = Sensor::getOrZero(SensorType::Rpm);
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isHpfpInactive = rpm < rpm_spinning_cutoff ||
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isHpfpInactive = rpm < rpm_spinning_cutoff ||
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!isGdiEngine() ||
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!isGdiEngine() ||
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@ -44,7 +44,7 @@ public:
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/**
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/**
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* Calculate where the pump should become active, in degrees before pump lobe TDC
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* Calculate where the pump should become active, in degrees before pump lobe TDC
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*/
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*/
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angle_t pumpAngleFuel(int rpm, HpfpController *model);
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angle_t pumpAngleFuel(float rpm, HpfpController *model);
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/**
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/**
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* Calculate the percent of the pump stroke needed to replace the fuel injected. Also
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* Calculate the percent of the pump stroke needed to replace the fuel injected. Also
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@ -56,7 +56,7 @@ public:
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* Return value is nominally 0-100, but may be outside that range (including negative) if
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* Return value is nominally 0-100, but may be outside that range (including negative) if
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* model parameters are not accurate.
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* model parameters are not accurate.
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*/
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*/
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float calcFuelPercent(int rpm);
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float calcFuelPercent(float rpm);
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/**
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/**
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* Calculates the PI controller contribution as a percent. This amount should be added to
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* Calculates the PI controller contribution as a percent. This amount should be added to
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@ -68,7 +68,7 @@ public:
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* Return value is nominally 0-100, but may be outside that range (including negative) if
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* Return value is nominally 0-100, but may be outside that range (including negative) if
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* model parameters are not accurate. The sum of this and calc_fuel_percent will be 0-100.
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* model parameters are not accurate. The sum of this and calc_fuel_percent will be 0-100.
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*/
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*/
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float calcPI(int rpm, float calc_fuel_percent);
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float calcPI(float rpm, float calc_fuel_percent);
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/**
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/**
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* Reset internal state due to a stopped engine.
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* Reset internal state due to a stopped engine.
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@ -350,7 +350,7 @@ static void onTdcCallback(void *) {
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}
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}
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#endif /* EFI_UNIT_TEST */
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#endif /* EFI_UNIT_TEST */
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int rpm = Sensor::getOrZero(SensorType::Rpm);
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float rpm = Sensor::getOrZero(SensorType::Rpm);
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addEngineSnifferTdcEvent(rpm);
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addEngineSnifferTdcEvent(rpm);
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#if EFI_TOOTH_LOGGER
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#if EFI_TOOTH_LOGGER
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LogTriggerTopDeadCenter(getTimeNowNt());
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LogTriggerTopDeadCenter(getTimeNowNt());
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