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@ -772,5 +772,5 @@ int getRusEfiVersion(void) {
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if (initBootloader() != 0)
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return 123;
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#endif /* EFI_BOOTLOADER_INCLUDE_CODE */
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return 20190130;
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return 20190131;
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}
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@ -35,5 +35,7 @@
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#endif /* EFI_UNIT_TEST */
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#define get_operationMode CONFIG_ACCESS_FOR_CONFIG_HEADER_ONLY(operationMode)
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#define get_specs_displacement CONFIG_ACCESS_FOR_CONFIG_HEADER_ONLY(specs.displacement)
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#define get_injector_flow CONFIG_ACCESS_FOR_CONFIG_HEADER_ONLY(injector.flow)
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#endif /* CONTROLLERS_MATH_CONFIG_ENGINE_SPECS_H_ */
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@ -14,6 +14,7 @@
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#include "engine.h"
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#include "engine_math.h"
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#include "maf2map.h"
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#include "config_engine_specs.h"
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#define rpmMin 500
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#define rpmMax 8000
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@ -82,27 +83,25 @@ float getTCharge(int rpm, float tps, float coolantTemp, float airTemp DECLARE_EN
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/**
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* @return air mass in grams
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*/
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static float getCycleAirMass(float volumetricEfficiency, float MAP, float tempK DECLARE_ENGINE_PARAMETER_SUFFIX) {
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// todo: pre-calculate cylinder displacement to save one division
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float cylinderDisplacement = CONFIG(specs.displacement);
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return (cylinderDisplacement * volumetricEfficiency * MAP) / (GAS_R * tempK);
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static float getCycleAirMass(float volumetricEfficiency, float MAP, float tempK DECLARE_GLOBAL_SUFFIX) {
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return (get_specs_displacement * volumetricEfficiency * MAP) / (GAS_R * tempK);
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}
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float getCylinderAirMass(float volumetricEfficiency, float MAP, float tempK DECLARE_ENGINE_PARAMETER_SUFFIX) {
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return getCycleAirMass(volumetricEfficiency, MAP, tempK PASS_ENGINE_PARAMETER_SUFFIX)
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/ CONFIG(specs.cylindersCount);
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float getCylinderAirMass(float volumetricEfficiency, float MAP, float tempK DECLARE_GLOBAL_SUFFIX) {
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return getCycleAirMass(volumetricEfficiency, MAP, tempK PASS_GLOBAL_SUFFIX)
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/ get_specs_displacement;
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}
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/**
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* @return per cylinder injection time, in seconds
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*/
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float sdMath(float airMass, float AFR DECLARE_ENGINE_PARAMETER_SUFFIX) {
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float sdMath(float airMass, float AFR DECLARE_GLOBAL_SUFFIX) {
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/**
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* todo: pre-calculate gramm/second injector flow to save one multiplication
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* open question if that's needed since that's just a multiplication
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*/
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float injectorFlowRate = cc_minute_to_gramm_second(CONFIG(injector.flow));
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float injectorFlowRate = cc_minute_to_gramm_second(get_injector_flow);
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/**
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* injection_pulse_duration = fuel_mass / injector_flow
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* fuel_mass = air_mass / target_afr
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@ -117,7 +116,7 @@ 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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floatms_t getSpeedDensityFuel(float map DECLARE_ENGINE_PARAMETER_SUFFIX) {
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floatms_t getSpeedDensityFuel(float map DECLARE_GLOBAL_SUFFIX) {
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/**
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* most of the values are pre-calculated for performance reasons
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*/
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@ -128,10 +127,10 @@ floatms_t getSpeedDensityFuel(float map DECLARE_ENGINE_PARAMETER_SUFFIX) {
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}
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efiAssert(CUSTOM_ERR_ASSERT, !cisnan(map), "NaN map", 0);
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float adjustedMap = map + engine->engineLoadAccelEnrichment.getEngineLoadEnrichment(PASS_ENGINE_PARAMETER_SIGNATURE);
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float adjustedMap = map + engine->engineLoadAccelEnrichment.getEngineLoadEnrichment(PASS_GLOBAL_SIGNATURE);
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efiAssert(CUSTOM_ERR_ASSERT, !cisnan(adjustedMap), "NaN adjustedMap", 0);
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float airMass = getCylinderAirMass(ENGINE(engineState.currentVE), adjustedMap, tChargeK PASS_ENGINE_PARAMETER_SUFFIX);
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float airMass = getCylinderAirMass(ENGINE(engineState.currentVE), adjustedMap, tChargeK PASS_GLOBAL_SUFFIX);
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if (cisnan(airMass)) {
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warning(CUSTOM_ERR_6685, "NaN airMass");
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return 0;
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@ -142,7 +141,7 @@ floatms_t getSpeedDensityFuel(float map DECLARE_ENGINE_PARAMETER_SUFFIX) {
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#endif /*EFI_PRINTF_FUEL_DETAILS */
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engine->engineState.airMass = airMass;
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return sdMath(airMass, ENGINE(engineState.targetAFR) PASS_ENGINE_PARAMETER_SUFFIX) * 1000;
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return sdMath(airMass, ENGINE(engineState.targetAFR) PASS_GLOBAL_SUFFIX) * 1000;
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}
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static const baro_corr_table_t default_baro_corr = {
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