This commit is contained in:
rusefi 2019-02-01 21:24:07 -05:00
parent 3e953d5131
commit a9d39f760d
3 changed files with 15 additions and 14 deletions

View File

@ -772,5 +772,5 @@ int getRusEfiVersion(void) {
if (initBootloader() != 0)
return 123;
#endif /* EFI_BOOTLOADER_INCLUDE_CODE */
return 20190130;
return 20190131;
}

View File

@ -35,5 +35,7 @@
#endif /* EFI_UNIT_TEST */
#define get_operationMode CONFIG_ACCESS_FOR_CONFIG_HEADER_ONLY(operationMode)
#define get_specs_displacement CONFIG_ACCESS_FOR_CONFIG_HEADER_ONLY(specs.displacement)
#define get_injector_flow CONFIG_ACCESS_FOR_CONFIG_HEADER_ONLY(injector.flow)
#endif /* CONTROLLERS_MATH_CONFIG_ENGINE_SPECS_H_ */

View File

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